Calculating the interior permanent-magnet motor
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Installation InstructionsWhy mix a magnetic pickup with a microphone? Because, the magnetic pickup senses the guitar string’s vibrations and the microphone accurately reproduces the complex and rich character of the acoustic tone. Congratulations on purchasing the most natural-sounding, three dimensional, acoustic guitar soundhole pickup. Ever!We strongly suggest that you read through this manual to ensure that you install it properly in your guitar and that you understand its features. This way, you’ll get the best results from your pickup system.The Mag Mic utilizes Seymour Duncan’s patented, hum-canceling Stack ® design to eliminate 60-cycle hum. This is especially useful for venues with older wiring, fluorescent lights, or computer monitors. There are two easily accessed controlsmounted on the side of the pickup: a master volume, and a microphone blend control to bring in just the right amount of the mic’s signal into the mix.Adjustable pole pieces allow you to use the Mag Mic with different playing styles, differing preferences in string output, and different gauges of strings and to achieve optimum string balance. The Mag Mic uses a pair of adjustable pole piece for each guitar string. This allows the Mag Mic to work with a wide variety of string spacings. Also, it captures a broad range of acoustic, harmonic vibrations, which translates to enhanced tone with smoother attack.You’ll notice that you can’t easily see the pole pieces for the “B” and “high-E” strings. This is normal. They are set low in the factory because they’re pre-compensated for what are normally the loudest strings, using a magnetic pickup.The Mag Mic uses a standard nine-volt battery for over 450 hours of continuous operation. Or, for total portability, you (or a qualified tech) can attach the included “N” size battery clips directly to the pickup for a completely self-contained unit. The low noise, Class A, discrete circuitry delivers extremely quiet operation.The Mag Mic’s installation can be temporary or permanent depending on how the cable is used. For permanent installation, the female output jack can be converted to an end-pin type jack by removing the finishing sleeve. For temporary installation, the cable can simply be attached to the exterior of the guitar at end-pin using the strain relief loop provided. The 1/4" female jack is then attached to any common guitar cable.Installation (Using 9 Volt Battery)Installing the Mag Mic is quick and easy. It’s best accomplished with the strings removed. The 9-Volt Battery holder is easily attached to the inside of the guitar at the neck block.Non-Permanent Installation(should take approximately 20 minutes)Tools you will need: #2 Phillips screwdriver String winder (optional)Small lint-free cloth Rubbing alcohol1) Remove the strings.2) Begin by cleaning the neck block (inside the guitar) to ensure that it’s free from sawdust, oils or any debris – this can be done with a cloth moistened with rubbingalcohol. Be careful not to get any alcohol on the finish on the outside of your guitar.3) After the alcohol is dry, apply one half of the Velcro® to the neck block where you wish to affix the battery holder.4) On the pickup unit itself, make sure that the clamps are open wide enough to accept the soundboard (refer to Fig.1).Figure 15) Insert both the battery holder (with the battery in the clip) and the pickup into the soundhole.6) Stick the battery holder to the Velcro installed in step 3.7) Slide the pickup into place on the neck-side of the soundhole.8) Tighten the screws to clamp the pickup securely in place.(Warning: over-tightening can compress the foam padding and mar your guitar top).9) Allow the cable to exit from the soundhole and use the strain relief attachment loop to secure the cable and female jack to the end pin on your guitar (refer to Fig.2).Figure 210) Reinstall your strings, plug any standard 1/4" guitarcable or patch cord into the female jack and you’re good to go!Permanent InstallationThis consists of basically two steps:1) Drilling the hole for the end pin jack (this step is best done by a qualifiedrepairperson or luthier, for whom it is a common procedure. Common sense dictates that any time you take a drill to your instrument, if you’re not 100% sure of your abilities, you’ll let someone more qualified handle this step).2) Installing the end pin jack, pickup and battery.Tools you will need: Variable Speed Hand Drill1/4", 13/32", 7/16" and 15/32" Twist Drill bits1/2" Tapered Reamer Low Tack Masking TapePrecision Saw (X-Acto saw, small coping saw, fine tooth hacksaw, etc.)Center punch1) Remove the strings.2) If possible, remove the end pin, do not use excessive force. On some guitars it will be necessary to remove a screw first. There are even a few guitars in which the end pin itself is threaded in and will need to be unscrewed. If you are successful, proceed directly to Step 6. If the end pin can not be easily removed, proceed with step 3.3) Apply low tack masking tape to the surface of the guitar around the area of the end pin. This will help protect the finish.4) Use the precision saw to remove the end pin about 1/16" above the body. If the end pin is fastened with a screw, remove the screw first.5) Centerpunch the end pin stub and drill a 1/4" pilot hole through the end pin and endblock.6) Use the reamer to ream out the hole. Continue working until the outside of the hole reaches 1/2" diameter.7) Drill the inner, tapered portion of the hole to the final diameter in progressively larger steps using the 13/32", 7/16" and 15/32" drill bits. Be careful to keep the drill perpendicular to the body and use slow, even pressure. Do not remove the drills from the hole until the rotation has fully stopped.Continued on reverse side...ControlsMaster Volume – as the name implies, this controls the volume of both the magnetic and microphone. The magnetic pickup is always on. Important note: The master volume control is the dial closest to the low e-string, and the Mic volume control is located closest to the high e-string. People often confuse these two controls because of the circuit board labels on the bottom of the pickup which read 'output' and 'mic'. Although these labels are located directly beneath the controls, the labels do not correspond to the controls. If you confuse the two controls, it will appear as though the mic is working, and the magnetic pickup is not.Microphone Volume – this allows you to regulate any amount of microphonesignal from 0% to 100% depending on your tonal needs and feedback considerations. Blending is accomplished on-board and the output signal contains a mix of thepickup and microphone. This eliminates the needs for any off-board blender systems.1) Lay the pickup upside down on a flat surface. Locate the two pairs of solder padsthat the battery clips will be mounted to.2) Press the mounting tabs on the bottom of the battery clips into the appropriate holesin the PCB that serves as the bottom cover. Be sure that the dimpled tabs that contactthe battery are both oriented toward the outside edges of the pickup (refer to Fig.4).Figure 43) Tin the solder iron tip and lay it on the inside bottom of one of the clips.Heat the clip at one end until you are able to smoothly flow solder in between the clipand the solder pad. Move the soldering iron to the other end of the clip and solderagain. Repeat the process for the second clip.4) Check your solder job, all joints should look smooth and shiny (not lumpy andgray). These solder joints are all that is mechanically holding the battery clips in place.5) It is optional to cut the 9-volt battery holder off – your choice.6) Installation of the pickup into the guitar is the same as either of the two previouslydescribed methods, depending on whether you desire a permanent or non-permanentinstallation of the end-pin jack.When to Change to BatteryWith hard plucking of notes, you will notice distortion on the attack of the note.When this occurs, your battery is starting to get low. At this point, you’ll get at least 20hours of use before it dies completely (four with the “N” battery). However, you shouldchange the battery at this point in order to preserve the great tone of the pickup.keep in mind that the “N” battery clips are secured to the PCB by the solder jointonly. Not to overly stress this point, but please take care when changing thebattery.Seymour Duncan Acoustic5427 Hollister AvenueSanta Barbara, CA 93111-2345Phone: 805-964-9610 Fax: 805-964-9749Hand built in Santa Barbara, California. Velcro is a registered trademark of Velcro Industries B.SpecificationsMagnetic pickupDC Resistance – 3.8k OhmsResonant Frequency – 16kHzGauss Strength – 780 max (adjustable)Microphone capsulePattern – Omni-directionalSensitivity - -35dBFrequency range – 20 to 20kHzS/N ratio - >62dBCurrent consumption – 0.5mAOnboard electronics2 Channels, summed at the outputSupply Voltage – 9VdcCurrent consumption – 1.1mA (preamp + mic capsule)Battery Life – 450+ hoursMaximum signal swing – 1.5V @ onset of clip w/9V power supplyThd – 0.02% @ onset of clippingNoise:·Pickup channel – -102dBV with 5k ohm source impedance·Mic channel – -96dBV with mic capsule attachedInstalling the end pin jack, pickup and batteryTools you will need:1/2" Open End Wrench3/32" Allen Wrench#2 Phillips screwdriverString winder (optional)Small lint-free clothRubbing alcohol1) Remove the strap button, small dress hex nut, and small dress washer from thefemale jack; and then remove the black plastic sleeve.2) From the inside (cable side) of the guitar, keep the large hex nut, large dress washerand star washer on the interior side of the jack and slide it through the end pin hole.The jack should protrude from the outside surface between 5/16" and 11/32". If it isnot within this range, it must be removed and the position of the large hex nut adjustedaccordingly.3) Install the small dress washer and the smaller hex nut. Hold the jack in place withthe allen wrench and use the 1/2" open end wrench to tighten the nut.4) Screw on the strap button and hand tighten.5) Clean the neck block to ensure that it’s free from sawdust, oils or any debris –this can be done with a cloth moistened with rubbing alcohol (be careful not to get anyalcohol on the finish of your guitar).6) After the alcohol is dry, apply one half of the Velcro® to the neck block where youwish to affix the battery holder.7) Insert both the battery holder (with the battery in the clip) and the pickup into thesoundhole.8) Stick the battery holder to the Velcro installed in step 2.9) On the pickup unit itself, make sure that the clamps are open wide enough to acceptthe soundboard.10) Slide the pickup into place on the neck-side of the soundhole.11) Tighten the screws to clap securely (warning: over-tightening can compress the foampadding and mar your guitar top).12) Reinstall strings and plug in a standard 1/4" guitar cable to the end pin jack andyou’re done.13) Make great music!Installation (Using “N” Battery)By installing the “N” battery clips, the Mag Mic becomes a single, integrated unit forthe ultimate in portability. However, this entails some compromises. Battery life isseverely limited: you’ll get 50 hours with an “N” battery as opposed to 450 with astandard 9 volt. Also, when inserting an “N” battery, you must ensure that it’spolarized correctly. The positive end of the battery must be oriented toward the “plus”symbol next to the microphone on the underside of the pickup (refer to Fig.4).Installing the “N” battery clips is a tricky process and requires high-level solderingabilities and a good quality iron with the correct tip. It is essential that the work bedone properly. Even when done perfectly, the clip will still not stand much abuse.It is advisable that care be used when installing and changing batteries. If you’re notentirely confident that you posses these abilities, please have this procedure done bya qualified electronics technician. Here are the steps:Installation of ClipsTools you will need:50 watt, pencil type soldering iron with medium, spade type tipRosin core solder PN# 501050-105 Rev BA C O U S T I C。
Configuration ofUPS Universal Shippingfor Magento 2.xContents●UPS Account●Addresses●Package Boxes●Shipping Methods●Configuration●Checkout●Customer AccountUPS Account1.If you don’t have UPS Account Credentials get them byhttps://2.Follow to Admin Main Menu -> Extmag -> Settings -> ShipperAccounts.3.Click on the “Add New Shipper Account” button.4.Input your credentials of UPS to fields and click on the “Save”button.Addresses1.Follow to Admin Main Menu -> Extmag -> Settings -> Addresses.2.Click on the “Add New Address” button.3.Input your Address to fields and click on the “Save” button.Package BoxesOptionally, you can create packaging boxes.1.Follow to Admin Main Menu -> Extmag -> Settings -> PackageBoxes.2.Click on the “Add New Box” button.3.Input your Box parameters to fields and click the “Save” button.Shipping MethodsCreate one or more shipping methods as needed. These methods will show in the checkout.1.Follow to Admin Main Menu -> Extmag -> Shipping Methods ->Shipping Methods.2.Click on the “Add New Shipping Method” button.3.Input shipping method data to fields and click the “Save” button.Configuration1.Follow to Admin Main Menu -> Extmag -> Settings -> UPSConfiguration.2.First, click the “General” tab on the left and fill in the necessaryfields.3.Moving from tab to tab, fill in the necessary fields.Description options of the extension configuration General Tab●General○Account■Select your carrier account by default or create an account followingthe link “Add Shipper Account” and then select it here○Shipper Address■Select your shipper address by default or create an address following the link “Add Address” and then select it here■This is the main address of your UPS account connecting with theShipper Number.○Ship From Address■Select your shipper address by default or create an address following the link “Add Address” and then select it here■It is your warehouse or store address○Destination Type■this item has two options●Auto: the carrier will automatically detect the type of recipientaddress.●Residential: the option is a flag to indicate if the receiver is aresidential location○Shipping Description■The Description of Goods for the shipment. Applies to internationaland domestic shipments. Provide a detailed description of items beingshipped for documents and non-documents■Examples: "annual reports" and "9 mm steel screws"■Required if all of the listed conditions are true: ShipFrom and ShipTocountries or territories are not the same; The packaging type is notUPS Letter; The ShipFrom and or ShipTo countries or territories arenot in the European Union or the ShipFrom and ShipTo countries orterritories are both in the European Union and the shipments servicetype is not UPS Standard.Packaging Tab●Packaging○Type■We recommend choosing by default “Customer Supplied Package” or choosing from the list at your discretion.○Additional Handling■The Additional Handling charge is an extra fee for shipmentsthat require special handling while being transported by UPS.■The Additional Handling charge depends on the packaging anddimensions. The following general guidelines apply. Though,UPS also reserves the right to assess the Additional HandlingCharge for any package that, in UPS's sole discretion, requiresspecial handling.●Weight○Attribute of Product Weight■If your products have a weight, indicate the product attribute for theweight. By default, this is the attribute with the code "weight"○Average Product Weight■If some of your products do not indicate the weight, please indicatethe average weight of the product. This is required for packagingproducts in boxes.○Pack Weight■If packing in boxes will not be used, indicate the empty package'sweight.●Dimensions○Attribute of Product Width (Length, Height)■Specify from which product attribute to get width (length, height) data ○Average Product Width (Length, Height)■Please indicate the average width (length, height) for products without dimensions. This will help you pack food into boxes.○Applicable Boxes■Specify which boxes to use for this carrier, store, or destination.■You can create missing boxes by the link "Add Package Box" underthe selection field.○Exclude Product Categories■Products from the categories selected here do not count towards boxpackaging; each product has been packaged separately.○Attribute of Product Pre-packed■The attribute must be Yes\No type. If Yes, the product will be aseparate package.●Volumetric Weight○Enabled■Enable/Disable using volumetric weight.○Attribute of Product Volumetric Weight○Type■If you are specifying volumetric weight in kilograms or pounds in theproduct, then select the "Weight" option. If you specify volumetric weightas a product of dimensions, then specify "Length x Width x Height".○Dividing factor for the metric system (kg, cm)■If you are specifying volumetric weight in kilograms or pounds in aproduct, then enter 1. If you are reporting volumetric weight as a productof dimensions, then indicate what your courier advises. Usually, it is 5000.○Dividing factor for the imperial system (lb, inch)■If you are specifying volumetric weight in kilograms or pounds in aproduct, then enter 1. If you are reporting volumetric weight as a productof dimensions, then indicate what your courier advises. As a rule, this is139.○Max Package Volume Weight for the metric system (kg, cm)○Max Package Volume Weight for the imperial system (lb, inch)Returns Tab●Returns○Creating Return Label With Shipping Label■ A return label is created together with a direct label simultaneously.You can print it and put it in the parcel.○Service■UPS Print Return Label (PRL)●Print a return label to include in an outbound shipment, orprovide a label to your customer at a later date■UPS Electronic Return Label (ERL)●Have UPS e-mail a return label to your customer●Customer○Allow Print■Allow the buyer to print the return label from their account○Allow Create■Allow the buyer to create a return label from their account. References Tab●References○Reference No. 1 Type■ A shipment reference is an identifier you define by completing the"reference" fields during the shipping process. This reference could bea purchase order (PO) number, a customer number, a company name,a Bill of Lading number, or a phrase that identifies that shipment --such as "10 crates" or "gift for Mom." Shipment references can be anycombination of letters and numbers up to 35 characters.○Reference No. 1■The data of the reference○Bar code for Reference No. 1 on shipping labels■The Code 128 bar code is used for reference bar codes.■Reference No. 1 can be selected to print as a bar code on theshipping label. The option applies to all packages in the shipment. Payments Tab●Payments○Currency■Specify the currency of your account on the carrier's website○Shipment Payer■Specify who will pay for the shipping. The payer can be the sender or athird party.○Duty And Tax Payer■Indicate who will pay the duties and taxes.○Declared Value Type■When calculating the total cost of a parcel, only the price of products orthe price of products, discounts, and fees can be taken into account.○Insurance■Specify the amount of insurance in the request○Negotiated rates■Apply specially negotiated prices.■To do this, you need to have a contract with the carrier○COD■Rely on UPS to collect payment for your shipment at the time ofdelivery■UPS will attempt to collect the amount shown on the C.O.D. tagor package label and then send the payment to you. Thepackage will be returned if UPS cannot collect the payment afterthree attempts.■The payment method must be appropriate.Notification Tab●Notification○Services■ A UPS notification service can send you and your customer e-mailsabout important events in the progress of your shipment.■For forward and return international shipments as well as for domestic shipments (for US and PR). It will be using three selected servicesonly.○Language■notification language●Emails○Email for Errors■Specify the email to which notifications of delivery errors will be sent Printing Tab●Printing○Type■Specify the type of label to print. It can be PDF or thermal type.○Mass Print■With bulk printing, you can only print unprinted labels or all.○Thermal Settings■Height■Specify the height of the thermal label you needPickups Tab●Pickup○Earliest Pickup Time■Indicate the opening time of your store or warehouse. The time whenyou are ready to deliver the parcels to the courier.○Latest Pickup Time■Specify the closing time for your store or warehouse.○Payment Method■The carrier does not charge a pickup fee in some countries andterritories. For other countries, you need to specify the paymentmethod "Pay by shipper account"○Special Instructions■These are special instructions for the driver.○Shipping Labels Available■This element should be set to “Yes” to indicate that the user haspre-printed shipping labels for all the packages, otherwise, this will betreated as false.■Default “Yes”●Schedule○Schedule settings for which pickups will be created. You can also create pickups manually if the schedule is disabled.Tracking Tab●Tracking Schedule○If enabled, requests for delivery information will be sent according to the schedule for each created shipment. If an error is received or the delivery wassuccessfully delivered, then a request will no longer be made for this trackingnumber.Access Point Tab●Access PointA UPS Access Point™ location is a participating retail outlet, such as a grocery storeor petrol station that serves as a convenient and efficient UPS parcel delivery andretrieval location. You can also drop off labeled and prepaid UPS Returns® parcels at any UPS Access Point location.○Type■Hold for Pickup at UPS Access Point●At no additional charge, UPS can hold your package up to fivedays●For use by approved shippers to identify a UPS Access Pointlocation as an alternate delivery option during shipmentpreparation●UPS will deliver your package to the UPS Customer Centeryou choose and then call the recipient when the package isready. Packages are usually available by 8:30 a.m. on thescheduled day of delivery.■UPS Access Point Delivery●Ship parcels directly to a UPS Access Point location forcollection by the receiver.○Account■Specify the sender's account on the carrier's websiteFreight Tab●General○Service■The code for the UPS Service associated with the shipment.○Handling Unit■The code associated with handling unit type.○Packaging Type■The code for the UPS packaging type associated with the shipment.○Class○NMFC Commodity Code■National Motor Freight Classification Commodity code. The first 6digits represent the Prime Code and the remaining 2 digits representthe Sub Prime Code.●References○Reference No. 1 Type○Bar code for Reference No. 1 on shipping labels○Reference No. 2 TypeInternational Invoice Tab●International Invoice○Paperless■UPS Paperless™ Invoice is an industry first that promotessustainability and eliminates the need for paper commercial invoicesby integrating order and shipment processing, and transmittingcommercial invoice data to enable clearance by customs officesacross the globe. You can easily manage your paperless shipping lanepreferences on a per-shipment basis, or by shipping lane, to gain evenmore flexibility.■UPS Paperless Invoice works seamlessly with all current UPSshipping systems. There is no need for additional software. Anycompany, regardless of size or industry segment, can use UPSPaperless Invoice free of charge.○Terms of Shipment■Indicates the rights to the seller from the buyer.■Valid values:CFR: Cost and FreightCIF: Cost Insurance and FreightCIP: Carriage and Insurance PaidCPT: Carriage Paid ToDAF: Delivered at FrontierDDP: Delivery Duty PaidDDU: Delivery Duty UnpaidDEQ: Delivered Ex QuayDES: Delivered Ex ShipEXW: Ex WorksFAS: Free Alongside ShipFCA: Free CarrierFOB: Free On Board○Reason for Export■ A reason to export the current international shipment■Valid values: SALE, GIFT, SAMPLE, RETURN, REPAIR,INTERCOMPANYDATA, Any other reason○Invoice Number■Commercial Invoice number assigned by the exporter■Can use macro paste: #order_id#, #shipment_id#, #invoice_id#○Comments■Max length 150. Can use macro paste: #customer_name#,#order_id#, #shipment_id#, #invoice_id#, #store_id#, #store_code#,#store_name#○Declaration Statement■This is the legal explanation, used by Customs, for the delivering ofthis shipment. It must be identical to the set of declarations actuallyused by Customs. Examples of declarations that might be entered inthis field are: I hereby certify that the goods covered by this shipmentqualify as originating goods for purposes of preferential tariff treatmentunder the NAFTA. I hereby certify that the information on this invoiceis true and correct and the contents and value of this shipment is asstated above. EEA statement: The exporter of the products coveredby this document declares that except where otherwise clearlyindicated these products are of EEA preferential origin■Max length 550○Sold To Address■The Sold To party’s country code must be the same as the Ship Toparty’s country code with the exception of Canada and satellitecountries●Product Attributes○Description■Product attribute containing the short name of the product ○Country of Manufacture■Product attribute containing the country of origin○Unit of Measurement■Select the term that best describes the way your product is measured.For example, barrels, bales, tons, etc.○Harmonized (Commodity) Code■Product attribute containing Harmonized (Commodity) Code■Determining the correct rate of duty when shipping internationally is a frequent challenge for small to medium-sized businesses. You want tomake sure your shipment faces minimal disruption when it comes tocustoms clearance. At the same time, you don't want to pay more thanrequired for shipping your product across borders■The Harmonized System (HS) code is integral to this process.Organized into 97 chapters, HS codes comprise a global index usedto describe every good being imported or exported. And while the HSindex may seem complicated at first, becoming familiar with itsworkings will help you avoid the likelihood of disruptions or delays inyour product journey○ScheduleB Code■Product attribute containing the ScheduleB Code of the product■A Schedule B number is a 10-digit number used in the United States to classify physical goods for export to another country. The ScheduleB is based on the international Harmonized System (HS) of 6-digitcommodity classification codes. There is a Schedule B number forevery physical product, from paperclips to airplanes●Taxpayer Identification○VAT/Tax/EORI ID■The Tax ID number (EIN/VAT)○Consignee VAT/Tax/EORI ID■The customer in another country is responsible for paying VAT andduties but for certain products and values, the merchant can collectVAT in the checkout (as normal) and the merchant then takes over theresponsibility for reporting this VAT to this country authorities. So themerchant is, from one aspect, considered as both the exporter andimporter here.Automatic Tab●Automatic Label Creation○Enabled■Turn on or off automatic creation of shipping labels■Make sure your Magento cron job is running○Create Invoice■Create invoice after creating label(s)○Create Shipment■Create shipment after creating label(s)○Allowed Order Statuses■Specify the order statuses for which you want to create shipping labels ○Allowed Shipping Methods■Specify the shipping methods for which you want to create shippinglabels○Service■Specify the shipping methods by which the delivery will be carried out ○Service for International Destination■Specify the shipping methods that will be used for internationaldeliveryMass Actions Tab●Mass Label Creation○Create Invoice■Create invoice after creating label(s)○Create Shipment■Create shipment after creating label(s)○Allowed Order Statuses■Specify the order statuses for which you want to create shipping labels ○Allowed Shipping Methods■Specify the shipping methods for which you want to create shippinglabels○Service■Specify the shipping methods by which the delivery will be carried out ○Service for International Destination■Specify the shipping methods that will be used for internationaldeliveryManual Actions Tab●Manual Label Creation○Create Invoice■Create invoice after creating label(s)○Create Shipment■Create shipment after creating label(s)Other Options Tab●Options○Saturday Pickup■UPS is the only carrier that will pick up all services on Saturday, soshipments can reach their destinations one day sooner. With ascheduled Saturday pickup, you can also opt-in to receive Saturdaydeliveries at no additional cost.○Saturday Delivery■Saturday Delivery from UPS allows you to stretch your business week even further. Like your busy schedules, our services don't stop for theweekend. And with the expansion of our weekend services, SaturdayDelivery is now more convenient than ever. With Saturday delivery*from UPS, you can receive your orders up to two days faster thanbefore, and at no extra cost.○Carbon Neutral■UPS ships millions of packages each day. We know that ourcustomers are as concerned as we are about the impact shipping hason the environment. That's why we offer a carbon neutral shippingoption. Your business can reduce its carbon footprint whiledemonstrating your commitment to sustainability.○Delivery Confirmation for Shipment Level■Verify that your shipment was delivered with your choice of signatureor adult signature options○Delivery Confirmation for Package Level■Verify that your shipment was delivered with your choice of signatureor adult signature options■Only for destination US50 to US50,PR or Canada to Canada or Puerto Rico to US50,PR○Order Status After Created Shipping Label■Change order status after creating shipping label○Movement Reference Number (MRN)■Must contain alphanumeric characters only. Must be a length of 18characters. The 3rd and 4th Characters must be the Shipper countryISO Code.■The MRN number is the customs registration number that enables the customs authority to identify and process your export packages in theAtlas customs system. It is the main reference for customsdeclaration and the most important link with your export goods●Dangerous Goods○Product Categories with Dangerous Goods■Select product categories containing only dangerous goods. You cancreate a category for dangerous goods only and disable its display onthe site.CheckoutOn the checkout page, your customers can see and select the shipping methods you have created in the module.You can see the link for creating returns and the RMA items list in the customer account.。
Diagnosing problems using LogsThis page aims to show you how to diagnose the top 5 most common problemsaffecting Copter in particular but to some extent Plane and Rover as well.Contents [hide]∙ 1 Log Types (Dataflash vs tlogs)∙ 2 Mechanical Failures∙ 3 Vibrations∙ 4 Compass interference∙ 5 GPS glitches∙ 6 Power Problems (BrownOuts, etc)∙7 Unexpected ERRORS including FailsafesLog Types (Dataflash vs tlogs)There are two ways to record your flight data. With some exceptions, the two methods record very similar data but in different ways:∙Dataflash logs use the Pixhawk (or APM2.x) onboard dataflash memory, which you can download after the flight. On Plane and Rover dataflash logs are createdsoon after start-up. On Copter they are created after you first arm the copter.∙Telemetry logs(also known as “tlogs”) are recorded by the Mission Planner (or other ground station) when you connect ArduPilot to your computer viaa telemetry link.If you are not yet familiar with the basics of these log files, first review theintroductory pages to understand where these logs are stored and how you candownload and view the information held within them.Mechanical FailuresCommon mechanical failures include a motor or ESC failure (including ESC sync failures), the propeller slipping or coming off, etc. These appear in the log as asudden divergence in the desired roll and pitch vs the vehicles actual roll andpitch. This discrepancy is most clearly visible in the dataflash logs by graphing theATT message’s Roll-In vs Roll and Pitch-In vs Pitch and to a lesser extent in the NavYaw vs Yaw.In the example above the vehicle’s actual roll (“Roll”) closely follows the desired roll (“Roll-In”) for the first part of the log but then suddenly diverges.The flight controller wanted the roll to remain level (0 roll) but it was unable to likely meaning a mechanical failure. This is very different from a software failure in which the flight controller freaked out and for some strange reason suddenly wanted the copterup-side-down because in such cases the desired roll would be also be crazy and actual roll would follow.Extra notes:∙tlogs are generally more difficult to use in this case because although we have nav_roll and nav_pitch which hold the desired roll and pitch, they are only updated when in RTL, Loiter or Auto flight modes.∙in AC3.1 (and higher) Roll-In and Pitch-In only hold the desired roll and pitch while in stabilize mode. When in an autopilot mode you must look at the NTUN messages’s DRol and DPit columnsVibrationsHigh vibrations cause the Copter’s accelerometer based altitude a nd horizontal position estimates to drift far off from reality which leads to problems with alt hold (normally rocketing into the sky) or Loiter (drifting).Vibrations are best viewed by graphing thedataflash’s IMU message’s AccX, AccY and AccZ values. The AccX and AccY values (primarily used for horizontal position control) should be between -3 and +3 m/s/s and the AccZ should be between -15 and -5 m/s/s. The accelerometer values will change momentarily as the copter moves up and down which is why it is better to pull the data from a portion of the flight where the copter was mostly stationary but even with a copter that is moving you can still see the vibration levels by comparing the difference between the top and bottom of the “grass”.an occasional blade of grass going over the lines is ok but if it’s sustained then it’s likely a real vibration problem.The below graph shows acceptable vibration levels.Tlog’s RAW_IMU xacc, yacc and zacc can also be used but their update is much slower (generally less than 10hz) than the dataflash log (50hz) so it becomes moredifficult to see whether the changes in accelerometer values are due to the copter moving or are just vibrations.If using tlogs the scale is in milli-Gs so the acceptable range for xacc and yacc is -300 ~ +300, and for zacc is -500 ~ -1500. Note that in the image below the values appear out of that range which perhaps indicates a vibration problem although this user did not complain of AltHold or Loiter problems so it is more likely that these variations were because the copter was not in a stable hover and the update rate was low.Compass interferenceInterference from the power distribution board, motors, battery, esc and other electrical devices near the APM or PX4 can throw off the compass heading which can lead to circling (aka “toilet bowling”) or even the copter flying off in completely the wrong direction. Graphing the tlog’s mag_field (found under “CUSTOM”) and throttle (found under VFR_HUD) values are the easiest way to quickly see the amount of interference.In the graph’s below shows an acceptable amount of magnetic interference.You can see the mag_field fluctuates when the throttle is raised but only moves around by about 10% ~ 20%. Below 30% inteference is acceptable. Between 30% ~ 60% is in the grey zone where it might be ok (some users are ok, some are not) and really bad magnetic interference will show up as jumps of over 60% when the throttle is raised.Extra Notes:∙The length of the mag_field can be anywhere from 120 ~ 550 depending upon where in the world the vehicle is but it is normally around 330.∙The magnetic interference as a percentage of the total mag field is also displayed at the end of the compassmot set-up procedure.∙Dataflash log’s COMPASS message hold the compass’s raw x, y and z axis values (called MagX, MagY, MagZ) which are equivalent to the tlog’s RAW_IMU xmag, ymag and zmag fields. It’s possible to calculate the mag-field length by firstloading the dataflash log file into excel, filtering by the COMPASS message and then calculating the mag-field using the formula mag_field = sqrt(MagX^2,MagY^2, MagZ^2). Note that the COMPASS message is not enabled by defaultin the dataflash logs because it runs at 50hz and does affect CPU performance a bit.∙Another general thing to check re the compass is the offsets which should bet between -150 ~ 150. These are found in the tlog’s SENSOR_OFFSET group as mag_ofs_x, mag_ofs_y, mag_ofs_z and in the datafl ash’s COMPASS message as OfsX, OfsY, OfsZ. They can also be seen in the parametersas COMPASS_OFS_X, COMPASS_OFS_Y, COMPASS_OFS_Z.∙The image above it shows a short spike at the beginning of the graph but this can be ignored because it’s before the throttle is raised so it’s probably just as the user plugged in some other electrical device.GPS glitchesWhen in autopilot modes (Loiter, RTL, AUTO) position errors from the GPS can cause Copter to think that it’s suddenly in the wrong position and lead to aggressive flying to correct the perceived error. These “glitches” show up in both the tlogs and dataflash logs as an decrease in the number of satellites visible and an increase inthe hdop.If using tlogs graph the the you can do this by graphing the GPS_RAW_IT group’s “eph” and “satellites_visible” values.An hdop value of 1.5 (displayed as 150) or lower is very good. Over 2.0 (i.e. 200) indicates a bad position value. The number of satellites falling below 9 is also bad. A significant change in these two values often accompanies a GPS position change.In the Dataflash logs’s GPS message you will find the “HDop” and “NSats” columns. Note the hdop values are in the correct units in the dataflash (i.e. not 100x too big like in the tlogs).AC 3.1 includes GPS Glitch detection which attempts to ignore glitches by sanity checking the positions.Power Problems (BrownOuts, etc)The introduction of the 3dr power module has made it much easier for people to provide a reliable power supply to their APM/PX4. This has led to a massive reduction in the number of brown-outs reported but they do still occur. They can normally be reconised by the logs suddenly ending while the copter is still in the air (i.e. barometer or inerital navigation altitude is still well above zero).Try graphing the:∙Dataflash log’s CTUN message’s Baro Alt∙Dataflash log’s GPS message’s RelAlt (the combined accelerometer + barometer altitude estimate)∙Tlog’s VFR_HUD alt (the combined accelerometer + barometer altitude estimate)∙Tlog’s GLOBAL_POSITION relative_altChanges in the board voltage can also be a sign of a power problem. Variations of 0.10 to 0.15 volts are normal. Beyond that could be a sign that other devices sharing the power source with the APM are causing ripples in the power supply that could lead to a brown-out or other weird behaviour. The board voltage can be graphed using:∙Dataflash CURRENT message’s VCC∙Tlog HWSTATUS’s VccIn the image directly below shows the board voltage sinking by 0.15V when the throttle is raised. This is generally not a good thing but because it’s only 0.15V it’s probably ok. The 2nd graph below (a dataflash graph from a different user’s log) shows a more random variation in voltage but also up to 0.15V which is typical.Unexpected ERRORS including FailsafesWhen unexpected behaviour from the flight controller occurs (especially when the user complains that the copter no longer responded to their input) it is often caused by one of the failsafes being triggered. There are 5 failsafes that can be activated: Throttle Failsafe, GPS Failsafe, GCS Failsafe (ground station failsafe), Battery Failsafe and the Fence.The easiest way to find these is to look in the dataflash logs and filter the 1st column by “ERR”.The Subsys (aka Sub-system) gives the area that generated the error and the ECode (aka Error Code) tells you what the error was specifically. The very limited number of subsystems and error codes can be found at the bottom of the Copter defines.h file. Sub Systems / Error Codes1: Main (never used)2: RadioECode 1: “Late Frame” which means the APM’s onboard ppm encoder did not provide an update for at least 2 secondsECode 0: error resolved which means the ppm encoder started providing data again3: CompassECode 1: the compass failed to initialise (likely a hardware issue)ECode 2: failure while trying to read a single value from the compass (probably a hardware issue)ECode 0: above errors resolved4: Optical flowEcode 1: failed to initialise (likely a hardware issue)5: Throttle failsafeECode 1: throttle dropped below FS_THR_VALUE meaning likely loss of contact between RX/TXECode 0: above error resolve meaning RX/TX contact likely restored6: Battery failsafeECode 1: battery voltage dropped below LOW_VOLT or total battery capacity used exceeded BATT_CAPACITY7: GPS failsafeECode 1: GPS lock lost for at least 5 secondsECode 0: GPS lock restored8: GCS (Ground station) failsafeECode 1: updates from ground station joystick lost for at least 5 secondsECode 0: updates from ground station restored9: FenceECode 1: altitude fence breachedECode 2: circular fence breachedECode 3: both altitude and circular fences breachedECode 0: vehicle is back within the fences10: Flight ModeECode 0 ~ 10: the vehicle was unable to enter the desired flight mode(0=Stabilize, 1=Acro, 2=AltHold, 3=Auto, 4=Guided, 5=Loiter, 6=RTL, 7=Circle, 8=Position, 9=Land, 10=OF_Loiter)11: GPSECode 2: GPS GlitchECode 0: GPS Glitch cleared12: Crash CheckECode 1: Crash detected13: FlipECode 2: Flip abandoned (because of 2 second timeout)14: AutoTuneECode 2: Bad Gains (failed to determine proper gains)15: ParachuteECode 2: Too low to deploy parachute16: EKF/InertialNav Check ECode 2: Bad Variance ECode 0: Bad Variance cleared 17: EKF/InertialNav Failsafe ECode 2: EKF Failsafe triggered 18: Baro glitchECode 2: Baro glitchECode 0: Baro glitch cleared。
闪存日志目录[显示]日志类型(闪存VS 数传日志)有两种方法可以记录你飞行时的数据。
尽管两种记录方法十分类似,但也有些区别:∙闪存日志(本页的主题)飞行完成后,可以从APM或PX4的板载闪存上下载。
飞机和地面车辆,只要一开机就会自动创建闪存日志。
四轴上则是解锁后才创建闪存日志。
∙数传日志(也称为―tlogs‖)用3DR或XBee数传模块连接APM到电脑上,会被Mission Planner(或其他地面站)记录下来。
你可以在这里找到详细信息。
设置你想要记录的数据LOG_BITMASK参数控制闪存内记录什么类型的数据。
如果你想指定某个消息类型附加到默认的方法上,在Mission Planner标准参数列表页面,可以在Log Bitmask的下拉列表设置。
使用终端控制会更加方便(命令行界面),如下所示:∙进入Mission Planner的终端界面∙单击―连接APM‖或―连接PX‖∙键入logs∙启用或禁用某个消息类型,在enable或disable后输入信息的类型即可。
如:enable IMU用于Arducopter的所有可能的闪存信息:ATT:roll,pitch和yaw(启用ATTITUDE_FAST记录频率是50Hz,启用ATTITUDE_MED记录频率是10HZ)。
ATUN:自动调参概览(从开头记录每一次―晃动‖测试)ATDE:自动调参详情(以100HZ记录飞行器的晃动情况)CAMERA(相机):快门按下后,记录当时的GPS时间、roll、pitch、yaw、纬度、精度、高度。
CMD(命令):从地面站接收命令,或者作为执行任务之一。
COMPASS(罗盘):罗盘原始数据和compassmot补偿值。
CURRENT(电流):以10HZ的频率,记录电流和主板电压信息。
CUTN:油门和高度信息,包括油门输入大小、超声波测得的高度(sonar alt)、气压测得的高度(baro alt),以10HZ频率记录。
The hardening soil model: Formulation and verificationT. SchanzLaboratory of Soil Mechanics, Bauhaus-University Weimar, GermanyP.A. VermeerInstitute of Geotechnical Engineering, University Stuttgart, GermanyP.G. BonnierP LAXIS B.V., NetherlandsKeywords: constitutive modeling, HS-model, calibration, verificationABSTRACT: A new constitutive model is introduced which is formulated in the framework of classical theory of plasticity. In the model the total strains are calculated using a stress-dependent stiffness, different for both virgin loading and un-/reloading. The plastic strains are calculated by introducing a multi-surface yield criterion. Hardening is assumed to be isotropic depending on both the plastic shear and volumetric strain. For the frictional hardening a non-associated and for the cap hardening an associated flow rule is assumed.First the model is written in its rate form. Therefor the essential equations for the stiffness mod-ules, the yield-, failure- and plastic potential surfaces are given.In the next part some remarks are given on the models incremental implementation in the P LAXIS computer code. The parameters used in the model are summarized, their physical interpre-tation and determination are explained in detail.The model is calibrated for a loose sand for which a lot of experimental data is available. With the so calibrated model undrained shear tests and pressuremeter tests are back-calculated.The paper ends with some remarks on the limitations of the model and an outlook on further de-velopments.1INTRODUCTIONDue to the considerable expense of soil testing, good quality input data for stress-strain relation-ships tend to be very limited. In many cases of daily geotechnical engineering one has good data on strength parameters but little or no data on stiffness parameters. In such a situation, it is no help to employ complex stress-strain models for calculating geotechnical boundary value problems. In-stead of using Hooke's single-stiffness model with linear elasticity in combination with an ideal plasticity according to Mohr-Coulomb a new constitutive formulation using a double-stiffness model for elasticity in combination with isotropic strain hardening is presented.Summarizing the existing double-stiffness models the most dominant type of model is the Cam-Clay model (Hashiguchi 1985, Hashiguchi 1993). To describe the non-linear stress-strain behav-iour of soils, beside the Cam-Clay model the pseudo-elastic (hypo-elastic) type of model has been developed. There an Hookean relationship is assumed between increments of stress and strain and non-linearity is achieved by means of varying Young's modulus. By far the best known model of this category ist the Duncan-Chang model, also known as the hyperbolic model (Duncan & Chang 1970). This model captures soil behaviour in a very tractable manner on the basis of only two stiff-ness parameters and is very much appreciated among consulting geotechnical engineers. The major inconsistency of this type of model which is the reason why it is not accepted by scientists is that, in contrast to the elasto-plastic type of model, a purely hypo-elastic model cannot consistently dis-tinguish between loading and unloading. In addition, the model is not suitable for collapse load computations in the fully plastic range.12These restrictions will be overcome by formulating a model in an elasto-plastic framework in this paper. Doing so the Hardening-Soil model, however, supersedes the Duncan-Chang model by far. Firstly by using the theory of plasticity rather than the theory of elasticity. Secondly by includ-ing soil dilatancy and thirdly by introducing a yield cap.In contrast to an elastic perfectly-plastic model, the yield surface of the Hardening Soil model is not fixed in principal stress space, but it can expand due to plastic straining. Distinction is made between two main types of hardening, namely shear hardening and compression hardening. Shear hardening is used to model irreversible strains due to primary deviatoric loading. Compression hardening is used to model irreversible plastic strains due to primary compression in oedometer loading and isotropic loading.For the sake of convenience, restriction is made in the following sections to triaxial loading conditions with 2σ′ = 3σ′ and 1σ′ being the effective major compressive stress.2 CONSTITUTIVE EQUATIONS FOR STANDARD DRAINED TRIAXIAL TESTA basic idea for the formulation of the Hardening-Soil model is the hyperbolic relationship be-tween the vertical strain ε1, and the deviatoric stress, q , in primary triaxial loading. When subjected to primary deviatoric loading, soil shows a decreasing stiffness and simultaneously irreversible plastic strains develop. In the special case of a drained triaxial test, the observed relationship be-tween the axial strain and the deviatoric stress can be well approximated by a hyperbola (Kondner& Zelasko 1963). Standard drained triaxial tests tend to yield curves that can be described by:The ultimate deviatoric stress, q f , and the quantity q a in Eq. 1 are defined as:The above relationship for q f is derived from the Mohr-Coulomb failure criterion, which involves the strength parameters c and ϕp . As soon as q = q f , the failure criterion is satisfied and perfectly plastic yielding occurs. The ratio between q f and q a is given by the failure ratio R f , which should obviously be smaller than 1. R f = 0.9 often is a suitable default setting. This hyperbolic relationship is plotted in Fig. 1.2.1 Stiffness for primary loadingThe stress strain behaviour for primary loading is highly nonlinear. The parameter E 50 is the con-fining stress dependent stiffness modulus for primary loading. E 50is used instead of the initial modulus E i for small strain which, as a tangent modulus, is more difficult to determine experimen-tally. It is given by the equation:ref E 50is a reference stiffness modulus corresponding to the reference stress ref p . The actual stiff-ness depends on the minor principal stress, 3σ′, which is the effective confining pressure in a tri-axial test. The amount of stress dependency is given by the power m . In order to simulate a loga-rithmic stress dependency, as observed for soft clays, the power should be taken equal to 1.0. As a3Figure 1. Hyperbolic stress-strain relation in primary loading for a standard drained triaxial test.secant modulus ref E 50 is determined from a triaxial stress-strain-curve for a mobilization of 50% ofthe maximum shear strength q f .2.2 Stiffness for un-/reloadingFor unloading and reloading stress paths, another stress-dependent stiffness modulus is used:where ref urE is the reference Young's modulus for unloading and reloading, corresponding to the reference pressure σ ref . Doing so the un-/reloading path is modeled as purely (non-linear) elastic.The elastic components of strain εe are calculated according to a Hookean type of elastic relation using Eqs. 4 + 5 and a constant value for the un-/reloading Poisson's ratio υur .For drained triaxial test stress paths with σ2 = σ3 = constant, the elastic Young's modulus E ur re-mains constant and the elastic strains are given by the equations:Here it should be realised that restriction is made to strains that develop during deviatoric loading,whilst the strains that develop during the very first stage of the test are not considered. For the first stage of isotropic compression (with consolidation), the Hardening-Soil model predicts fully elastic volume changes according to Hooke's law, but these strains are not included in Eq. 6.2.3 Yield surface, failure condition, hardening lawFor the triaxial case the two yield functions f 12 and f 13 are defined according to Eqs. 7 and 8. Here4Figure 2. Successive yield loci for various values of the hardening parameter γ p and failure surface.the measure of the plastic shear strain γ p according to Eq. 9 is used as the relevant parameter forthe frictional hardening:with the definitionIn reality, plastic volumetric strains p υε will never be precisely equal to zero, but for hard soils plastic volume changes tend to be small when compared with the axial strain, so that the approxi-mation in Eq. 9 will generally be accurate.For a given constant value of the hardening parameter, γ p , the yield condition f 12 = f 13 = 0 can be visualised in p'-q-plane by means of a yield locus. When plotting such yield loci, one has to use Eqs. 7 and 8 as well as Eqs. 3 and 4 for E 50 and E ur respectively. Because of the latter expressions,the shape of the yield loci depends on the exponent m . For m = 1.0 straight lines are obtained, but slightly curved yield loci correspond to lower values of the exponent. Fig. 2 shows the shape of successive yield loci for m = 0.5, being typical for hard soils. For increasing loading the failure sur-faces approach the linear failure condition according to Eq. 2.2.4 Flow rule, plastic potential functionsHaving presented a relationship for the plastic shear strain, γ p , attention is now focused on the plastic volumetric strain p υε. As for all plasticity models, the Hardening-Soil model involves a re-lationship between rates of plastic strain, i.e. a relationship between p υε and p γ . This flow rule hasthe linear form:5Clearly, further detail is needed by specifying the mobilized dilatancy angle m ψ. For the presentmodel, the expression:is adopted, where cv ϕ is the critical state friction angle, being a material constant independent ofdensity (Schanz & Vermeer 1996), and m ϕ is the mobilized friction angle:The above equations correspond to the well-known stress-dilatancy theory (Rowe 1962, Rowe 1971), as explained by (Schanz & Vermeer 1996). The essential property of the stress-dilatancy theory is that the material contracts for small stress ratios m ϕ < cv ϕ, whilst dilatancy occurs for high stress ratios m ϕ < cv ϕ. At failure, when the mobilized friction angle equals the failure angle,p ϕ, it is found from Eq. 11 that:Hence, the critical state angle can be computed from the failure angles p ϕand p ψ. The above defi-nition of the flow rule is equivalent to the definition of definition of the plastic potential functionsg 12 and g 13 according to:Using theKoiter-rule (Koiter 1960) for yielding depending on two yield surfaces (Multi-surface plasticity ) one finds:Calculating the different plastic strain rates by this equation, Eq. 10 directly follows.3 TIME INTEGRATIONThe model as described above has been implemented in the finite element code P LAXIS (Vermeer& Brinkgreve 1998). To do so, the model equations have to be written in incremental form. Due to this incremental formulation several assumptions and modifications have to be made, which will be explained in this section.During the global iteration process, the displacement increment follows from subsequent solu-tion of the global system of equations:where K is the global stiffness matrix in which we use the elastic Hooke's matrix D , f ext is a global load vector following from the external loads and f int is the global reaction vector following from the stresses. The stress at the end of an increment σ 1 can be calculated (for a given strain increment ∆ε) as:6whereσ0 , stress at the start of the increment,∆σ , resulting stress increment,4D , Hooke's elasticity matrix, based on the unloading-reloading stiffness,∆ε , strain increment (= B ∆u ),γ p , measure of the plastic shear strain, used as hardening parameter,∆Λ , increment of the non-negative multiplier,g , plastic potential function.The multiplier Λ has to be determined from the condition that the function f (σ1, γ p ) = 0 has to be zero for the new stress and deformation state.As during the increment of strain the stresses change, the stress dependant variables, like the elasticity matrix and the plastic potential function g , also change. The change in the stiffness during the increment is not very important as in many cases the deformations are dominated by plasticity.This is also the reason why a Hooke's matrix is used. We use the stiffness matrix 4D based on the stresses at the beginning of the step (Euler explicit ). In cases where the stress increment follows from elasticity alone, such as in unloading or reloading, we iterate on the average stiffness during the increment.The plastic potential function g also depends on the stresses and the mobilized dilation angle m ψ. The dilation angle for these derivatives is taken at the beginning of the step. The implementa-tion uses an implicit scheme for the derivatives of the plastic potential function g . The derivatives are taken at a predictor stress σtr , following from elasticity and the plastic deformation in the previ-ous iteration:The calculation of the stress increment can be performed in principal stress space. Therefore ini-tially the principal stresses and principal directions have to be calculated from the Cartesian stresses, based on the elastic prediction. To indicate this we use the subscripts 1, 2 and 3 and have 321σσσ≥≥ where compression is assumed to be positive.Principal plastic strain increments are now calculated and finally the Cartesian stresses have to be back-calculated from the resulting principal constitutive stresses. The calculation of the consti-tutive stresses can be written as:From this the deviatoric stress q (σ1 – σ3) and the asymptotic deviatoric stress q a can be expressed in the elastic prediction stresses and the multiplier ∆Λ:7whereFor these stresses the functionshould be zero. As the increment of the plastic shear strain ∆γ p also depends linearly on the multi-plier ∆Λ, the above formulae result in a (complicated) quadratic equation for the multiplier ∆Λwhich can be solved easily. Using the resulting value of ∆Λ, one can calculate (incremental)stresses and the (increment of the) plastic shear strain.In the above formulation it is assumed that there is a single yield function. In case of triaxial compression or triaxial extension states of stress there are two yield functions and two plastic po-tential functions. Following (Koiter 1960) one can write:where the subscripts indicate the principal stresses used for the yield and potential functions. At most two of the multipliers are positive. In case of triaxial compression we have σ2 = σ3, Λ23 = 0and we use two consistency conditions instead of one as above. The increment of the plastic shear strain has to be expressed in the multipliers. This again results in a quadratic equation in one of the multipliers.When the stresses are calculated one still has to check if the stress state violates the yield crite-rion q ≤ q f . When this happens the stresses have to be returned to the Mohr-Coulomb yield surface.4 ON THE CAP YIELD SURFACEShear yield surfaces as indicated in Fig. 2 do not explain the plastic volume strain that is measured in isotropic compression. A second type of yield surface must therefore be introduced to close the elastic region in the direction of the p-axis. Without such a cap type yield surface it would not be possible to formulate a model with independent input of both E 50 and E oed . The triaxial modulus largely controls the shear yield surface and the oedometer modulus controls the cap yield surface.In fact, ref E 50largely controls the magnitude of the plastic strains that are associated with the shear yield surface. Similarly, ref oedE is used to control the magnitude of plastic strains that originate from the yield cap. In this section the yield cap will be described in full detail. To this end we consider the definition of the cap yield surface (a = c cot ϕ):8where M is an auxiliary model parameter that relates to NC K 0 as will be discussed later. Further more we have p = (σ1 + σ2+ σ3) andwithq is a special stress measure for deviatoric stresses. In the special case of triaxial compression it yields q = (σ1 – σ3) and for triaxial extension reduces to q = α (σ1 –σ3). For yielding on the cap surface we use an associated flow rule with the definition of the plastic potential g c :The magnitude of the yield cap is determined by the isotropic pre-consolidation stress p c . For the case of isotropic compression the evolution ofp c can be related to the plastic volumetric strain rate p v ε:Here H is the hardening modulus according to Eq. 32, which expresses the relation between theelastic swelling modulus K s and the elasto-plastic compression modulus K c for isotropic compres-sion:From this definition follows a stress dependency of H . For the case of isotropic compression we haveq = 0 and therefor c p p=. For this reason we find Eq. 33 directly from Eq. 31:The plastic multiplier c Λ referring to the cap is determined according to Eq. 35 using the addi-tional consistency condition:Using Eqs. 33 and 35 we find the hardening law relating p c to the volumetric cap strain c v ε:9Figure 3. Representation of total yield contour of the Hardening-Soil model in principal stress space for co-hesionless soil.The volumetric cap strain is the plastic volumetric strain in isotropic compression. In addition to the well known constants m and σref there is another model constant H . Both H and M are cap pa-rameters, but they are not used as direct input parameters. Instead, we have relationships of theform NC K 0=NC K 0(..., M, H ) and ref oed E = ref oed E (..., M, H ), such that NC K 0and ref oed E can be used as in-put parameters that determine the magnitude of M and H respectively. The shape of the yield cap is an ellipse in p – q ~-plane. This ellipse has length p c + a on the p -axis and M (p c+ a ) on the q ~-axis.Hence, p c determines its magnitude and M its aspect ratio. High values of M lead to steep caps un-derneath the Mohr-Coulomb line, whereas small M -values define caps that are much more pointed around the p -axis.For understanding the yield surfaces in full detail, one should consider Fig. 3 which depicts yield surfaces in principal stress space. Both the shear locus and the yield cap have the hexagonal shape of the classical Mohr-Coulomb failure criterion. In fact, the shear yield locus can expand up to the ultimate Mohr-Coulomb failure surface. The cap yield surface expands as a function of the pre-consolidation stress p c .5 PARAMETERS OF THE HARDENING-SOIL MODELSome parameters of the present hardening model coincide with those of the classical non-hardening Mohr-Coulomb model. These are the failure parameters ϕp ,, c and ψp . Additionally we use the ba-sic parameters for the soil stiffness:ref E 50, secant stiffness in standard drained triaxial test,ref oedE , tangent stiffness for primary oedometer loading and m , power for stress-level dependency of stiffness.This set of parameters is completed by the following advanced parameters:ref urE , unloading/ reloading stiffness,10v ur , Poisson's ratio for unloading-reloading,p ref , reference stress for stiffnesses,NC K 0, K 0-value for normal consolidation andR f , failure ratio q f / q a .Experimental data on m , E 50 and E oed for granular soils is given in (Schanz & Vermeer 1998).5.1 Basic parameters for stiffnessThe advantage of the Hardening-Soil model over the Mohr-Coulomb model is not only the use of a hyperbolic stress-strain curve instead of a bi-linear curve, but also the control of stress level de-pendency. For real soils the different modules of stiffness depends on the stress level. With theHardening-Soil model a stiffness modulus ref E 50is defined for a reference minor principal stress of σ3 = σref . As some readers are familiar with the input of shear modules rather than the above stiff-ness modules, shear modules will now be discussed. Within Hooke's theory of elasticity conversion between E and G goes by the equation E = 2 (1 + v ) G . As E ur is a real elastic stiffness, one may thus write E ur = 2 (1 + v ur ) G ur , where G ur is an elastic shear modulus. In contrast to E ur , the secant modulus E 50 is not used within a concept of elasticity. As a consequence, there is no simple conver-sion from E 50 to G 50. In contrast to elasticity based models, the elasto-plastic Hardening-Soil model does not involve a fixed relationship between the (drained) triaxial stiffness E 50 and the oedometer stiffness E oed . Instead, these stiffnesses must be given independently. To define the oedometer stiff-ness we usewhere E oed is a tangent stiffness modulus for primary loading. Hence, ref oed E is a tangent stiffness ata vertical stress of σ1 = σref .5.2 Advanced parametersRealistic values of v ur are about 0.2. In contrast to the Mohr-Coulomb model, NC K 0 is not simply a function of Poisson's ratio, but a proper input parameter. As a default setting one can use the highly realistic correlation NC K 0= 1 – sin ϕp . However, one has the possibility to select different values.All possible different input values for NC K 0 cannot be accommodated for. Depending on other pa-rameters, such as E 50, E oed , E ur and v ur , there happens to be a lower bound on NC K 0. The reason for this situation will be explained in the next section.5.3 Dilatancy cut-offAfter extensive shearing, dilating materials arrive in a state of critical density where dilatancy has come to an end. This phenomenon of soil behaviour is included in the Hardening-Soil model by means of a dilatancy cut-off . In order to specify this behaviour, the initial void ratio, e 0, and the maximum void ratio, e cv , of the material are entered. As soon as the volume change results in a state of maximum void, the mobilized dilatancy angle, ψm , is automatically set back to zero, as in-dicated in Eq. 38 and Fig. 4:11Figure 4. Resulting strain curve for a standard drained triaxial test including dilatancy cut-off.The void ratio is related to the volumetric strain, εv by the relationship:where an increment of εv is negative for dilatancy. The initial void ratio, e 0, is the in-situ void ratio of the soil body. The maximum void ratio, e cv , is the void ratio of the material in a state of critical void (critical state).6 CALIBRATION OF THE MODELIn a first step the Hardening-Soil model was calibrated for a sand by back-calculating both triaxial compression and oedometer tests. Parameters for the loosely packed Hostun-sand (e 0 = 0.89), a well known granular soil in geotechnical research, are given in Tab. 1. Figs. 5 and 6 show the satis-fying comparison between the experimental (three different tests) and the numerical result. For the oedometer tests the numerical results consider the unloading loop at the maximum vertical load only.7 VERIFICATION OF THE MODEL7.1 Undrained behaviour of loose Hostun-sandIn order to verify the model in a first step two different triaxial compression tests on loose Hostun-sand under undrained conditions (Djedid 1986) were simulated using the identical parameter from the former calibration. The results of this comparison are displayed in Figs. 7 and 8.In Fig. 7 we can see that for two different confining pressures of σc = 300 and 600 kPa the stress paths in p-q-space coincide very well. For deviatoric loads of q ≈ 300 kPa excess porewater pres-sures tend to be overestimated by the calculations.Additionally in Fig. 8 the stress-strain-behaviour is compared in more detail. This diagram con-tains two different sets of curves. The first set (•, ♠) relates to the axial strain ε1 at the horizontal12Figure 5. Comparison between the numerical (•) and experimental results for the oedometer tests.Figure 6. Comparison between the numerical (•) and experimental results for the drained triaxial tests (σ3 = 300 kPa) on loose Hostun-sand.and the effective stress ratio 31/σσ′′ on the vertical (left) axis. The second set (o , a ) refers to the normalised excess pore water pressure ∆u /σc on the right vertical axis. Experimental results forboth confining stresses are marked by symbols, numerical results by straight and dotted lines.Analysing the amount of effective shear strength it can be seen that the maximum calculated stress ratio falls inside the range of values from the experiments. The variation of effective friction from both tests is from 33.8 to 35.4 degrees compared to an input value of 34 degrees. Axial stiff-ness for a range of vertical strain of ε1 < 0.05 seems to be slightly over-predicted by the model. Dif-ferences become more pronounced for the comparison of excess pore water pressure generation.Here the calculated maximum amount of ∆u is higher then the measured values. The rate of de-crease in ∆u for larger vertical strain falls in the range of the experimental data.Table 1. Parameters of loose Hostun-sand.v urm ϕp ψp ref ref s E E 50/ref ref ur E E 50/ref E 500.200.6534° 0° 0.8 3.0 20 MPa13Figure 7. Undrained behaviour of loose Hostun-sand: p-q-plane.Figure 8. Undrained behaviour of loose Hostun-sand: stress-strain relations.7.2 Pressuremeter test GrenobleThe second example to verify the Hardening-Soil model is a back-calculation of a pressuremeter test on loose Hostun-sand. This test is part of an experimental study using the calibration chamber at the IMG in Grenoble (Branque 1997). This experimental testing facility is shown in Fig. 9.The cylindrical calibration chamber has a height of 150 cm and a diameter of 120 cm. In the test considered in the following a vertical surcharge of 500 kPa is applied at the top of the soil mass by a membrane. Because of the radial deformation constraint the state of stress can be interpreted in this phase as under oedometer conditions. Inside the chamber a pressuremeter sonde of a radius r 0 of 2.75 cm and a length of 16 cm is placed. For the test considered in the following example there was loose Hostun-sand (D r ≈ 0.5) of a density according to the material parameters as shown in Tab. 1 placed around the pressuremeter by pluviation. After the installation of the device and the filling of the chamber the pressure is increased and the resulting volume change is registered.14Figure 9. Pressuremeter Grenoble .This experimental setup was modeled within a FE-simulation as shown in Fig. 10. On the left hand side the axis-symmetric mesh and its boundary conditions is displayed. The dimensions are those of the complete calibration chamber. In the left bottom corner of the geometry the mesh is finer because there the pressuremeter is modeled.In the first calculation phase the vertical surcharge load A is applied. At the same time the hori-zontal load B is increased the way practically no deformations occur at the free deformation bound-ary in the left bottom corner. In the second phase the load group A is kept constant and the load group B is increased according to the loading history in the experiment. The (horizontal) deforma-tions are analysed over the total height of the free boundary. In order to (partly) get rid of the de-formation constrains at the top of this boundary, marked point A in the detail on the right hand side of Fig. 10 two interfaces were placed crossing each other in point A . Fig. 11 shows the comparison of the experimental and numerical results for the test with a vertical surcharge of 500 kPa.On the vertical axis the pressure (relating to load group B ) is given and on the horizontal axis the volumetric deformation of the pressuremeter. Because the calculation was run taking into ac-count large deformations (updated mesh analysis ) the pressure p in the pressuremeter has to be cal-culated from load multiplier ΣLoad B according to Eq. 40, taking into account the mean radial de-formation ∆r of the free boundary:The agreement between the experimental and the numerical data is very good, both for the initial part of phase 2 and for larger deformations of up to 30%.。
机械英语考试试题及答案一、选择题(每题2分,共20分)1. The term "mechanical engineering" refers to:A. The study of machinesB. The design and manufacture of mechanical systemsC. The operation of machineryD. The maintenance of mechanical equipment答案:B2. What is the function of a bearing in a mechanical system?A. To reduce frictionB. To increase efficiencyC. To provide powerD. To transmit motion答案:A3. The process of converting thermal energy into mechanical energy is known as:A. ElectrificationB. CombustionC. ThermodynamicsD. Hydrodynamics答案:C4. In mechanical design, the principle of "KISS" stands for:A. Keep It Simple, StupidB. Keep It Short and SimpleC. Keep It Simple and SafeD. Keep It Simple, Smart答案:A5. A gear train is used to:A. Change the direction of motionB. Increase the speed of rotationC. Decrease the speed of rotationD. All of the above答案:D6. What does CAD stand for in mechanical engineering?A. Computer-Aided DesignB. Computer-Aided DraftingC. Computer-Aided DevelopmentD. Computer-Aided Diagnostics答案:A7. The SI unit for force is:A. NewtonB. JouleC. PascalD. Watt答案:A8. What is the purpose of a flywheel in a mechanical system?A. To store energyB. To increase speedC. To reduce noiseD. To dissipate heat答案:A9. The term "hydraulics" is associated with the study of:A. Fluid dynamicsB. Solid mechanicsC. Structural analysisD. Thermal engineering答案:A10. The process of cutting a material to a specific shape is known as:A. MachiningB. CastingC. ForgingD. Extrusion答案:A二、填空题(每空1分,共10分)11. The formula for calculating the moment of a force is \( F \times d \), where \( F \) is the force and \( d \) is the_______.答案:distance from the pivot12. A _______ is a device that converts linear motion into rotational motion.答案:crank13. In a four-stroke internal combustion engine, the four strokes are intake, compression, _______, and exhaust.答案:power14. The _______ of a material is its ability to resist deformation under load.答案:stiffness15. The term "overhaul" in mechanical maintenance refers to a thorough inspection and _______ of a machine or its parts.答案:repair16. The _______ of a machine is the study of how forces act on and within a body.答案: statics17. A _______ is a type of machine that uses a screw to convert rotational motion into linear motion.答案:screw jack18. The _______ of a system is the point around which the system rotates.答案:pivot19. The _______ of a lever is the ratio of the effort arm to the load arm.答案:mechanical advantage20. The _______ is a type of bearing that allows for rotation with minimal friction.答案:ball bearing三、简答题(每题5分,共30分)21. Explain the difference between static and dynamic equilibrium in mechanical systems.答案:Static equilibrium refers to a state where the net force and net moment acting on a body are zero, resulting in no acceleration. Dynamic equilibrium occurs when the net force is zero, but the body is in motion with constant velocity.22. What is the purpose of a clutch in a vehicle?答案:A clutch is used to engage and disengage the power transmission from the engine to the transmission system, allowing the vehicle to start, stop, and change gears smoothly.23. Describe the function of a governor in an engine.答案:A governor is a device that automatically controls the speed of an engine by regulating the fuel supply or the valve settings, ensuring the engine operates within safespeed limits.24. What are the three primary types of joints in structural engineering?答案:The three primary types of joints are pinned joints, fixed joints, and sliding joints, each serving different purposes in connecting and supporting structural elements.25. Explain the。
现代驱动与控制基于表贴式永磁电机定子拓扑的内嵌永磁伺服电机的设计王东南京埃斯顿自动化股份有限公司(211106)Design on the Interior Permanent Magnet Servo Motor Based on Stator Topologyof the Surface-mounted Permanent Magnet MotorWANG DongNanjing ESTUN Automation Co.,Ltd.摘要:在永磁伺服电机产品开发过程中,发现内嵌 电机不宜直接采用原有表贴电机的定子侧结构,而应重 新进行整体优化设计。
逐一分析了表贴电机的定子齿宽、槽深、槽口宽和转子磁钢边缘削减厚度对电磁转矩和转 矩脉动影响。
有限元计算表明,通过调整定子结构参数、增大定子内径和转子外径、重新分配电机电磁负荷和采用MTPA (最大转距电流比)控制策略,伺服电机轴向 长度缩短了8.6%,体积显著减小,功率密度显著提高。
关键词:表贴电机内嵌伺服电机优化设计转矩特性中图分类号:T M351文献标识码:ADOI 编码:10.3969/j.issn.l006-2807.2020.06.005Abstract: It is found that the interior permanent magnet motor is not able to directly adapt the stator side structure of original surface-mounted permanent magnet motor, but its overall and optimized design has to be restarted in the development process of permanent magnet servo motor products. Influence on electromagnetic torque and torque ripple by the stator tooth width, slot depth, slot width and reduction of the rotor magnet edge thickness is analyzed item by item. By means that the electromagnetic load of the motor is re-distributed by regulating the stator structural parameters, increasing stator inner diameter and rotor outer diameter, as well as adapting MTPA (Maximum Torque Per Ampere) control strategy onto the motor, the FEA calculation result shows the motor axial length is shortened 8.6%, making motor volume less and power density larger significantly.Keywords: surface-mounted permanent magnet motor interior permanent magnet servo motor optimized design torque characteristic永磁电机具有结构设计灵活、功率密度和功 率因数较高的优点,已被广泛应用于伺服行业[1]。
ORIGINAL :UNITED NATIONS of July 20, 1995E/ECE/324 )Rev.1/Add.94/Amend.4/Corr.1E/ECE/TRANS/505 )February 21, 2005STATUS OF UNITED NATIONS REGULATIONECE 95UNIFORM PROVISIONS CONCERNING THE APPROVAL OF:VEHICLES WITH REGARD TO THE PROTECTION OF THEOCCUPANTS IN THE EVENT OF A LATERAL COLLISIONIncorporating:00 series of amendments Date of Entry into Force: 06.07.95 Corr. 2 to 00 series of amendments Date of Entry into Force: 10.03.95 01 series of amendments Date of Entry into Force: 12.08.98 Supplement 1 to the 01 series of amendments Date of Entry into Force: 14.11.99 Corr. 1 to the 01 series of amendments Date of Entry into Force: 08.11.00 Corr. 3 to the 00 series of amendments Date of Entry into Force: 26.06.02 02 series of amendments Date of Entry into Force: 16.07.03 Supplement 1 to the 02 series of amendments Date of Entry into Force: 12.08.04ORIGINAL :UNITED NATIONS of July 20, 1995 E/ECE/324)E/ECE/TRANS/505 )Rev.1/Add.94/Amend.4/Corr.1February 21, 2005TITLE:Lateral Collision ProtectionISSUE:3 Regulation No. 95Mar/2005PAGE: IUNITED NATIONS AGREEMENTCONCERNING THE ADOPTION OF UNIFORM TECHNICAL PRESCRIPTIONS FOR WHEELED VEHICLES, EQUIPMENT AND PARTS WHICH CAN BE FITTED AND/OR BE USED ON WHEELED VEHICLES AND THE CONDITIONS FOR RECIPROCAL RECOGNITION OFAPPROVALS GRANTED ON THE BASIS OF THESE PRESCRIPTIONS(*)(Revision 2, including the amendments which entered into force on October 16, 1995)Addendum 94: Regulation No. 95Amendment 4 ErratumUNIFORM PROVISIONS CONCERNING THE APPROVAL OF VEHICLES WITH REGARD TO THEPROTECTION OF THE OCCUPANTS IN THE EVENT OF A LATERAL COLLISION(*)Former title of the Agreement:Agreement Concerning the Adoption of Uniform Conditions of Approval and Reciprocal Recognition of Approval for Motor Vehicle Equipment and Parts, done at Geneva on March 20, 1958.ORIGINAL :UNITED NATIONS of July 20, 1995REGULATION NO. 95UNIFORM PROVISIONS CONCERNING THE APPROVAL OF VEHICLES WITH REGARD TO THE PROTECTION OF THE OCCUPANTS IN THE EVENT OF A LATERAL COLLISIONCONTENTSREGULATION1. Scope2. Definitions3. Application for approval4. Approval5. Specifications and tests6. Modification of the vehicle type7. Conformity of production8. Penalties for non-conformity of production9. Production definitely discontinued10. Transitional provisions11. Names and addresses of technical services responsible for conducting approval tests, and ofadministrative departmentsANNEXESAnnex 1 - Communication concerning the approval or extension or refusal or withdrawal of approval or production definitely discontinued of a vehicle type with regard to protection of occupants inthe event of a lateral collision, pursuant to Regulation No. 95Annex 2 - Arrangements of the approval markAnnex 3 -Procedure for determining the "H" Point and the actual torso angle for seating positions in motor vehiclesAppendix 1 -Description of the three dimensional "H" Point machine (3-D H machine)Appendix 2 -Three dimensional reference systemAppendix 3 -Reference data concerning seating positionsAnnex 4 -Collision test procedureAppendix 1 -Determination of performance dataAppendix 2 -The procedure for calculating the viscous criterion for EUROSID 1 TITLE:Lateral Collision Protection ISSUE:1 Regulation No. 95Oct/2003PAGE: IIORIGINAL :UNITED NATIONS of July 20, 1995REGULATION NO. 95Annex 5 -Mobile deformable barrier characteristicsAppendix 1 - Force-deflection curves for static testsAppendix 2 - Force-deflection curves for dynamic testsAnnex 6 -Technical description of the side impact dummyAnnex 7 -Installation of the side impact dummyAnnex 8 -Partial testTITLE:Lateral Collision Protection ISSUE:1 Regulation No. 95Oct/2003PAGE: IIIORIGINAL :UNITED NATIONS of July 20, 1995REGULATION NO. 951.SCOPEThis Regulation applies to the lateral collision behaviour of the structure of the passengercompartment of M1 and N1 categories of vehicles where the R Point of the lowest seat is notmore than 700 mm from ground level when the vehicle is in the condition corresponding to thereference mass defined in Paragraph 2.10. of this Regulation.2.DEFINITIONSFor the purposes of this Regulation:2.1."Approval of a vehicle" means the approval of a vehicle type with regard to the behaviour ofthe structure of the passenger compartment in a lateral collision;2.2."Vehicle type"means a category of power-driven vehicles which do not differ in suchessential respects as:2.2.1.the length, width and ground clearance of the vehicle, in so far as they have a negative effecton the performance prescribed in this Regulation;2.2.2.the structure, dimensions, lines and materials of the side walls of the passenger compartmentin so far as they have a negative effect on the performance prescribed in this Regulation;2.2.3.the lines and inside dimensions of the passenger compartment and the type of protectivesystems, in so far as they have a negative effect-on the performance prescribed in thisRegulation;2.2.4.the siting of the engine (front, rear or centre);2.2.5.the unladen mass, in so far as there is a negative effect on the performance prescribed in thisRegulation;2.2.6.the optional arrangements or interior fittings in so far as they have a negative effect on theperformance prescribed in this Regulation;2.2.7.the type of front seat(s) and position of the "R" Point in so far as they have a negative effecton the performance prescribed in this Regulation;2.3."Passenger compartment" means the space for occupant accommodation, bounded by theroof, floor, side walls, doors, outside glazing and front bulkhead and the plane of the rearcompartment bulkhead or the plane of the rear-seat back support;2.4."R Point" or "seating reference point" means the reference point specified by the vehiclemanufacturer which:2.4.1.has co-ordinates determined in relation to the vehicle structure;2.4.2.corresponds to the theoretical position of the point of torso/thighs rotation (H Point) for thelowest and most rearward normal driving position or position of use given by the vehiclemanufacturer for each seating position specified by him;TITLE:Lateral Collision Protection ISSUE:1 Regulation No. 95Oct/2003PAGE: 1ORIGINAL :UNITED NATIONS of July 20, 19952.5."H Point" is as established by Annex 3 to this Regulation;2.6."Capacity of the fuel tanks" means the fuel-tank capacity as specified by the manufacturerof the vehicle;2.7."Transverse plane" means a vertical plane perpendicular to the median longitudinal verticalplane of the vehicle;2.8."Protective system" means devices intended to restrain and/or protect the occupants;2.9."Type of protective system" means a category of protective devices which do not differ insuch essential respects as their:technologygeometryconstituent materials;2.10."Reference mass" means the unladen mass of the vehicle increased by a mass of 100 kg(that is the mass of the side impact dummy and its instrumentation);2.11."Unladen mass" means the mass of the vehicle in running order without driver, passengersor load, but with the fuel tank filled to 90% of its capacity and the usual set of tools and sparewheel on board, where applicable;2.12."Mobile deformable barrier" means the apparatus with which the test vehicle is impacted. Itconsists of a trolley and an impactor;2.13."Impactor" means a crushable section mounted on the front of mobile deformable barrier;2.14."Trolley"means a wheeled frame free to travel along its longitudinal axis at the point ofimpact. Its front supports the impactor.3.APPLICATION FOR APPROVAL3.1.The application for approval of a vehicle type with regard to the protection of the occupants inthe event of a lateral collision shall be submitted by the vehicle manufacturer or by his dulyaccredited representative.3.2.It shall be accompanied by the undermentioned documents in triplicate and the followingparticulars:3.2.1. a detailed description of the vehicle type with respect to its structure, dimensions, lines andconstituent materials;3.2.2.photographs and/or diagrams and drawings of the vehicle showing the vehicle type in front,side and rear elevation and design details of the lateral part of the structure;3.2.3.particulars of the vehicle's mass as defined by Paragraph 2.11. of this Regulation;3.2.4.the lines and inside dimensions of the passenger compartment;3.2.5. a description of the relevant side interior fittings and protective systems installed in thevehicle.TITLE:Lateral Collision Protection ISSUE:1 Regulation No. 95Oct/2003PAGE: 2ORIGINAL :UNITED NATIONS of July 20, 1995 TITLE:Lateral Collision ProtectionISSUE:1 Regulation No. 95Oct/2003PAGE: 33.3.The applicant for approval shall be entitled to present any data and results of tests carried out which make it possible to establish that compliance with the requirements can be achieved on prototype vehicles with a sufficient degree of accuracy.3.4. A vehicle which is representative of the type to be approved shall be submitted to the technical service responsible for conducting the approval tests.3.4.1.A vehicle not comprising all the components proper to the type may be accepted for tests provided that it can be shown that the absence of the components omitted has no detrimental effect on the performance prescribed in the requirements of this Regulation.3.4.2. It shall be the responsibility of the applicant for approval to show that the application of Paragraph 3.4.1 is in compliance with the requirements of this Regulation. 4.APPROVAL4.1. If the vehicle type submitted for approval pursuant to this Regulation meets the requirements of Paragraph 5 below, approval of that vehicle type shall be granted.4.2.In case of doubt, account shall be taken, when verifying the conformity of the vehicle to the requirements of this Regulation, of any data or test results provided by the manufacturer which can be taken into consideration in validating the approval test carried out by the technical service.4.3.An approval number shall be assigned to each type approved. Its first two digits (at present 01 corresponding to the 01 series of amendments) shall indicate the series of amendments incorporating the most recent major technical amendments made to the Regulation at the time of issue of the approval. The same Contracting Party may not assign the same approval number to another vehicle type.4.4.Notice of approval or of extension or of refusal of approval of a vehicle type pursuant to this Regulation shall be communicated by the Parties to the Agreement applying this Regulation by means of a form conforming to the model in Annex l to this Regulation and photographs and/or diagrams and drawings supplied by the applicant for approval, in a format not exceeding A4 (210 x 297) mm or folded to that format and on an appropriate scale.4.5.There shall be affixed to every vehicle conforming to a vehicle type approved under this Regulation, conspicuously and in a readily accessible place specified on the approval form, an international approval mark consisting of:4.5.1.a circle surrounding the Letter "E" followed by the distinguishing number of the country whichhas granted approval;(1)(1)1 for Germany,2 for France,3 for Italy,4 for the Netherlands,5 for Sweden,6 for Belgium,7 for Hungary,8 for the Czech Republic,9 for Spain, 10 for Yugoslavia, 11 for the United Kingdom, 12 for Austria, 13 for Luxembourg, 14 for Switzerland, 15 (vacant), 16 for Norway, 17 for Finland, 18 for Denmark, 19 for Romania, 20 for Poland, 21 for Portugal, 22 for the Russian Federation, 23 for Greece, 24 for Ireland, 25 for Croatia, 26 for Slovenia, 27 for Slovakia, 28 for Belarus, 29 for Estonia, 30 (vacant), 31 for Bosnia and Herzegovina, 32 for Latvia, 33 (vacant), 34 for Bulgaria, 35-36 (vacant), 37 for Turkey, 38-39 (vacant), 40 for The former Yugoslav Republic of Macedonia, 41 (vacant), 42 for the European Community (Approvals are granted by its Member States using their respective ECE symbol), 43 for Japan, 44 (vacant), 45 fort Australia and 46 for Ukraine. Subsequent numbers shall be assigned to other countries in the chronological order in which they ratify the Agreement Concerning the Adoption of Uniform Technical Prescriptions for Wheeled Vehicles, Equipment and Parts which can be Fitted and/or be Used on Wheeled Vehicles and the Conditions of for Reciprocal Recognition of Approvals Granted on the Basis of these Prescriptions for Motor Vehicle Equipment and Parts, or in which they accede to that Agreement, and the numbers thus assigned shall be communicated by the Secretary-General of the United Nations to the Contracting Parties to the Agreement.ORIGINAL :UNITED NATIONS of July 20, 1995 TITLE:Lateral Collision ProtectionISSUE:1 Regulation No. 95Oct/2003PAGE: 44.5.2. the number of this Regulation, followed by the Letter "R", a dash and the approval number, to the right of the circle prescribed in Paragraph 4.5.1.4.6.If the vehicle conforms to a vehicle type approved, under one or more other Regulations Annexed to the Agreement, in the country which has granted approval under this Regulation, the symbol prescribed in Paragraph 4.5.1. need not be repeated; in this case the Regulation and approval numbers and the additional symbols of all the Regulations under which approval has been granted in the country which has granted approval under this Regulation shall be placed in vertical columns to the right of the symbol prescribed in Paragraph 4.5.1. 4.7. The approval mark shall be clearly legible and shall be indelible.4.8. The approval mark shall be placed close to or on the vehicle data plate affixed by the manufacturer.4.9. Annex 2 to this Regulation gives examples of approval marks.5.SPECIFICATIONS AND TESTS5.1. The vehicle shall undergo a test in accordance with Annex 4 to this Regulation.5.1.1.The test will be carried out on the driver's side unless asymmetric side structures, if any, are so different as to affect the performance in a side impact. In that case either of the alternatives in Paragraph 5.1.1.1. or 5.1.1.2. may be used by agreement between the manufacturer and test authority.5.1.1.1.The manufacturer will provide the authority responsible for approval with information regarding the compatibility of performances in comparison with the driver's side when the test is being carried out on that side.5.1.1.2. The approval authority, if concerned as to the construction of the vehicle, will decide to have the test performed on the side opposite the driver, this being considered the least favourable. 5.1.2.The Technical Service, after consultation with the manufacturer, may require the test to be carried out with the seat in a position other than the one indicated in Paragraph 5.5.1. ofAnnex 4. This position shall be indicated in the test report.(1)5.1.3.The result of this test shall be considered satisfactory if the conditions set out in Paragraphs 5.2. and 5.3. below are satisfied.(1)Until September 30, 2000, for the purposes of the test requirements, the range of normal longitudinal adjustments shall be limited such that the H-point lies within the length of the door aperture.ORIGINAL :UNITED NATIONS of July 20, 19955.2.Performance criteria5.2.1.The performance criteria, as determined for the collision test in accordance with the Appendixto Annex 4 to this Regulation shall meet the following conditions:5.2.1.1. the head performance criterion (HPC) shall be less than or equal to 1,000; when there is nohead contact, then the HPC shall not be measured or calculated but recorded as "No HeadContact."5.2.1.2. the thorax performance criteria shall be:(a) Rib Deflection Criterion (RDC) less than or equal to 42 mm;(b) Soft Tissue Criterion (VC) less or equal to 1.0 m/sec.For a transitional period of two years after the date specified in Paragraph 10.2. of thisRegulation the V * C value is not a pass/fail criterion for the approval testing, but this valuehas to be recorded in the test report and to be collected by the approval authorities. After thistransitional period, the VC value of 1.0 m/sec shall apply as a pass/fail criterion unless theContracting Parties applying this Regulation decide otherwise.5.2.1.3. the pelvis performance criterion shall be:Pubic Symphysis Peak Force (PSPF) less than or equal to 6 kN.5.2.1.4. the abdomen performance criterion shall be:Abdominal Peak Force (APF) less than or equal to 2.5 kN internal force (equivalent to externalforce of 4.5 kN).5.3.Particular Requirements5.3.1.No door shall open during the test.5.3.2.After the impact, it shall be possible without the use of tools to:5.3.2.1 open a sufficient number of doors provided for normal entry and exit of passengers, and ifnecessary tilt the seat-backs or seats to allow evacuation of all occupants;5 3.2.2. release the dummy from the protective system;5.3.2.3. remove the dummy from the vehicle;5.3.3.no interior device or component shall become detached in such a way as noticeably toincrease the risk of injury from sharp projections or jagged edges;5.3.4.ruptures, resulting from permanent deformation are acceptable, provided these do notincrease the risk of injury;5.3.5.if there is continuous leakage of liquid from the fuel-feed installation after the collision, the rateof leakage shall not exceed 30 g/min; if the liquid from the fuel-feed system mixes with liquidsfrom the other systems and the various liquids cannot easily be separated and identified, allthe liquids collected shall be taken into account in evaluating the continuous leakage. TITLE:Lateral Collision Protection ISSUE:1 Regulation No. 95Oct/2003PAGE: 5ORIGINAL :UNITED NATIONS of July 20, 19956.MODIFICATION OF THE VEHICLE TYPE6.1.Any modification affecting the structure, the number and type of seats, the interior trim orfittings, or the position of the vehicle controls or of mechanical parts which might affect theenergy-absorption capacity of the side of the vehicle, shall be brought to the notice of theadministrative department granting approval. The department may then either:6.1.1.consider that the modifications made are unlikely to have an appreciable adverse effect andthat in any case the vehicle still complies with the requirements, or6.1.2.require a further test report from the technical service responsible for conducting the tests;6.1.2.1. Any modification of the vehicle affecting the general form of the structure of the vehicle or anyvariation in the reference mass greater than 8% which in the judgement of the authority wouldhave a marked influence on the results of the test shall require a repetition of the test asdescribed in Annex 4.6.1.2.2. If the technical service, after consultation with the vehicle manufacturer, considers thatmodifications to a vehicle type are insufficient to warrant a complete retest then a partial testmay be used. This would be the case if the reference mass is not more than 8% differentfrom the original vehicle or the number of front seats is unchanged. Variations of seat type orinterior fittings need not automatically entail a full retest. An example of the approach to thisproblem is given in Annex 8.6.2.Confirmation or refusal of approval, specifying the alteration, shall be communicated by theprocedure specified in Paragraph 4.4. above to the Parties to the Agreement which apply thisRegulation.6.3.The competent authority issuing an extension of approval shall assign a series number toeach communication form drawn up for such an extension.7.CONFORMITY OF PRODUCTIONThe conformity of production procedures shall comply with those set out in the Agreement,Appendix 2 (E/ECE/324-E/ECE/TRANS/505/Rev.2), with the following requirements:7.1.Every vehicle approved under this Regulation shall be so manufactured as to conform to thetype approved by meeting the requirements set out in Paragraph 5 above.7.2.The holder of the approval shall ensure that for each type of vehicle at least the testsconcerning the taking of measurements are carried out.7.3.The authority which has granted type approval may at any time verify the conformity controlmethods applied in each production facility. The normal frequency of these verifications shallbe once every two years.TITLE:Lateral Collision Protection ISSUE:1 Regulation No. 95Oct/2003PAGE: 6ORIGINAL :UNITED NATIONS of July 20, 19958.PENALTIES FOR NON-CONFORMITY OF PRODUCTION8.1.The approval granted in respect of a vehicle type, pursuant to this Regulation, may bewithdrawn if the requirement laid down in Paragraph 7.1. above is not complied with, or if thevehicle or vehicles selected have failed to pass the checks prescribed in Paragraph 7.2.above.8.2.If a Contracting Party to the Agreement applying this Regulation withdraws an approval it haspreviously granted, it shall forthwith so notify the other Contracting Parties applying thisRegulation by means of a communication form conforming to the model in Annex 1 to thisRegulation.9.PRODUCTION DEFINITELY DISCONTINUEDIf the holder of the approval completely ceases to manufacturer a type of vehicle approved inaccordance with this Regulation, he shall so inform the authority which granted theapproval. Upon receiving the relevant communication that authority shall inform thereof theother Parties to the 1958 Agreement applying this Regulation by means of a communicationform conforming to the model in Annex 1 to this Regulation.10. TRANSITIONAL PROVISIONS10.1.As from the official date of entry into force of Supplement 1 to the 02 series of amendments,no Contracting Party applying this Regulation shall refuse to grant ECE approval under thisRegulation as amended by Supplement 1 to the 02 series of amendments.10.2.As from 12 months after the entry into force of the 02 series of amendments ContractingParties applying this Regulation shall grant ECE approvals only to those types of vehicleswhich comply with the requirements of this Regulation as amended by the 02 series ofamendments.10.3.As from 60 months after the entry into service of the 02 series of amendments ContractingParties applying this Regulation may refuse first national registration (first entry into service) ofvehicles which do not meet the requirements of this Regulation as amended by the 02 seriesof amendments.10.4.As from 36 months after the entry into force of Supplement 1 to the 02 series of amendmentsContracting Parties applying this Regulation shall grant ECE approvals only to those types ofvehicles which comply with the requirements of this Regulation, as amended by Supplement 1to the 02 series of amendments.10.5.As from 84 months after the entry into force of Supplement 1 to the 02 series of amendmentsContracting Parties applying this Regulation may refuse first national registration (first entryinto service) of vehicles which do not meet the requirements of this Regulation as amendedby Supplement 1 to the 02 series of amendments.S AND ADDRESSES OF TECHNICAL SERVICES RESPONSIBLE FORCONDUCTING APPROVAL TESTS, AND OF ADMINISTRATIVE DEPARTMENTSThe Contracting Parties to the Agreement applying this Regulation shall communicate to theUnited Nations secretariat the names and addresses of the technical services responsible forconducting approval tests, and of the administrative departments which grant approval and towhich forms certifying approval or extension, or refusal or withdrawal of approval, issued inother countries, are to be sent.TITLE:Lateral Collision Protection ISSUE:2 Regulation No. 95Oct/2004PAGE: 7ORIGINAL :UNITED NATIONS of July 20, 1995TITLE:Lateral Collision Protection ISSUE:2Regulation No. 95 Oct/2004PAGE: 8ANNEX 1(maximum format: A4 (210 x 297 mm))COMMUNICATIONissued by: Name of administration: (1) ............................................................................................................................................................concerning: (2) APPROVAL GRANTEDAPPROVAL EXTENDEDAPPROVAL REFUSEDAPPROVAL WITHDRAWNPRODUCTION DEFINITELY DISCONTINUEDof a vehicle type with regard to protection of occupants in the event of a lateral collision pursuant to Regulation No. 95Approval No. .....Extension No............. l.Trade name or mark of the power-driven vehicle ................................................................................ 2.Vehicle type ......................................................................................................................................... 3.Manufacturer's name and address ...................................................................................................... 4.If applicable name and address of manufacturer's representative ..................................................... 5.Vehicle submitted for approval on ....................................................................................................... 6.Side impact dummy utilized ES-1/ES-2. (2)7.Technical service responsible for conducting approval tests .............................................................. 8.Date of test report ................................................................................................................................ 9.Number of test report .......................................................................................................................... 10. Approval granted/refused/extended/withdrawn. (2) (1)Distinguishing number of the country which has granted/extended/refused/withdrawn approval (see approval provisions in the Regulation).(2)Strike out what does not apply.ORIGINAL :UNITED NATIONS of July 20, 199511. Position of approval mark on the vehicle.............................................................................................12. Place.....................................................................................................................................................13. Date......................................................................................................................................................14. Signature..............................................................................................................................................15. The list of documents deposited with the Administrative Service which has granted approval isAnnexed to this communication and may be obtained on request.TITLE:Lateral Collision Protection ISSUE:2 Regulation No. 95Oct/2004PAGE: 9ÝÑËÒÌÎÇ :E.C.E.© InterRegs Ltd 2004ÑÎ×Ù×ÒßÔ :UNITED NATIONS of July 20, 1995Ì×ÌÔÛæLateral Collision Protection ×ÍÍËÛæ1Regulation No. 95 Oct/2003ÐßÙÛæ 10ANNEX 2ARRANGEMENTS OF THE APPROVAL MARKMODEL AøÍ»» п®¿¹®¿°¸ ìòëò ±º ¬¸·-λ¹«´¿¬·±²÷ ̸» ¿¾±ª» ¿°°®±ª¿´ ³¿®µ ¿ºº·¨»¼ ¬± ¿ ª»¸·½´» -¸±©- ¬¸¿¬ ¬¸» ª»¸·½´» ¬§°» ½±²½»®²»¼ ¸¿-ô ©·¬¸ ®»¹¿®¼ ¬± ¬¸» °®±¬»½¬·±² ±º ¬¸» ±½½«°¿²¬- ·² ¬¸» »ª»²¬ ±º ¿ ´¿¬»®¿´ ½±´´·-·±²ô ¾»»² ¿°°®±ª»¼ ·² ¬¸» Ò»¬¸»®´¿²¼- øÛì÷ °«®-«¿²¬ ¬± λ¹«´¿¬·±² Ò±ò çëò ̸» ¿°°®±ª¿´ ²«³¾»® ·²¼·½¿¬»- ¬¸¿¬ ¬¸» ¿°°®±ª¿´ ©¿- ¹®¿²¬»¼ ·² ¿½½±®¼¿²½» ©·¬¸ ¬¸» ®»¯«·®»³»²¬- ±º λ¹«´¿¬·±² Ò±ò çë ¿- ¿³»²¼»¼ ¾§ ¬¸» ðï -»®·»- ±º ¿³»²¼³»²¬-òMODEL BøÍ»» п®¿¹®¿°¸ ìòêò ±º ¬¸·-λ¹«´¿¬·±²÷̸» ¿¾±ª» ¿°°®±ª¿´ ³¿®µ ¿ºº·¨»¼ ¬± ¿ ª»¸·½´» -¸±©- ¬¸¿¬ ¬¸» ª»¸·½´» ¬§°» ½±²½»®²»¼ ¸¿- ¾»»² ¿°°®±ª»¼ ·² ¬¸» Ò»¬¸»®´¿²¼- øÛì÷ °«®-«¿²¬ ¬± λ¹«´¿¬·±²- Ò±-ò çë ¿²¼ îì (1)ø×² ¬¸» ½¿-» ±º ¬¸» ´¿¬¬»® λ¹«´¿¬·±²ô ¬¸» ¿¼¼·¬·±²¿´ -§³¾±´ ©¸·½¸ º±´´±©- ¬¸» λ¹«´¿¬·±² ²«³¾»® ·²¼·½¿¬»- ¬¸¿¬ ¬¸» ½±®®»½¬»¼ ¿¾-±®°¬·±² ½±ó»ºº·½·»²¬ ·- ïòíð ³óï÷ò ̸» º·®-¬ ¬©± ¿°°®±ª¿´ ²«³¾»®- ·²¼·½¿¬» ¬¸¿¬ ¿¬ ¬¸» ¼¿¬» ©¸»² ¬¸» ®»-°»½¬·ª» ¿°°®±ª¿´- ©»®» ¹®¿²¬»¼ô λ¹«´¿¬·±² çë ·²½±®°±®¿¬»¼ ¬¸» ðï -»®·»- ±º ¿³»²¼³»²¬- ¿²¼ λ¹«´¿¬·±² Ò±ò îì ·²½±®°±®¿¬»¼ ¬¸» ðí -»®·»- ±º ¿³»²¼³»²¬-ò øï÷̸» ´¿¬¬»® ²«³¾»® ·- ¹·ª»² ±²´§ ¿- ¿² »¨¿³°´»ò。
2024上学期期末考试试卷高一英语(答案在最后)第一部分听力(共两节,满分30分)第一节(共5小题;每小题1.5分,满分7.5分)听下面5段对话。
每段对话后有一个小题,从题中所给的A、B、C三个选项中选出最佳选项,并标在试卷的相应位置。
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1.【此处可播放相关音频,请去附件查看】Where is the new supermarket?A.Next to the bank.B.Near the cinema.C.Beside the theater.【答案】B【解析】【原文】W:I heard there’s a newly opened supermarket in our block.Is it near the theater?M:No.It’s opposite the bank,right next to the cinema.2.【此处可播放相关音频,请去附件查看】What does the woman decide to do?e back another time.B.Buy other flowers instead.C.Go to another shop.【答案】A【解析】【原文】W:I’d like to buy a bunch of red roses,please.M:Sorry.They just sold out.Do you want some yellow tulips,or white lilies maybe?W:Never mind.I’ll come a little earlier tomorrow.Thanks.3.【此处可播放相关音频,请去附件查看】How will the boy go to the museum?A.By foot.B.By underground.C.By bike.【答案】B【解析】【原文】M:I don’t want to walk to the museum.Have you seen my bike?W:Oh,your cousin borrowed it this morning.I forgot to tell you.M:Never mind.I’ll take the subway then.4.【此处可播放相关音频,请去附件查看】Why does the woman refuse to see another movie?A.She has to go out.B.She needs to work now.C.She wants to rest.【答案】C【解析】【原文】M:The action movie we just saw is excellent!Now let’s see another one.A romance perhaps?W:Maybe another time,Peter.I have an important meeting tomorrow morning and I really need to sleep now.5.【此处可播放相关音频,请去附件查看】When will the company bus pass by?A.At8:30.B.At8:45.C.At9:00.【答案】B【解析】【原文】W:Oh,I’m so dead.It’s already8:30now.I should have thrown that stupid alarm clock away long ago! M:Calm down,Honey.Your company bus will pass by our apartment in15minutes.You still have time.第二节(共15小题;每小题1.5分,满分22.5分)听下面5段对话或独白。
Problems of the 20th International Physics Olympiad 1(Warsaw, 1989)Waldemar GorzkowskiInstitute of Physics, Polish Academy of Sciences, Warsaw, Poland 2AbstractThe article contains problems given at the 20th International Physics Olympiad (1989) and their solutions. The 20th IPhO was the third IPhO organized in Warsaw, Poland.LogoThe emblem of the XX InternationalPhysics Olympiad contains a picture that is ahistorical record of the first hypernuclear eventobserved and interpreted in Warsaw by M.Danysz and J. Pniewski3. The collision of ahigh-energy particle with a heavy nucleus wasregistered in nuclear emulsion. Tracks of thesecondary particles emitted in the event, seen inthe picture (upper star), consist of tracks due tofast pions (“thin tracks”) and to much slowerfragments of the target nucleus (“black tracks”).The “black track” connecting the upper star (greater) with the lower star (smaller) in the figure is due to a hypernuclear fragment, in this case due to a part of the primary nucleus containing an unstable hyperon Λinstead of a nucleon. Hyperfragments (hypernuclei) are a new kind of matter in which the nuclei contain not only protons and neutrons but also some other heavy particles.In the event observed above the hyperon Λ, bound with nucleon, decays like a free particle through a week (slow) process only. This fact strongly suggested the existence of a new quantum number that could explain suppression of the decay, even in presence of nucleons. Indeed, this was one of the observations that, 30 months later, led to the concept of strangeness.1This article has been sent for publication in Physics Competitions in October 20032e-mail: gorzk@.pl3M. Danysz and J. Pniewski, Bull. Acad. Polon. Sci., 3(1) 42 (1952) and Phil. Mag., 44, 348 (1953). Later the same physicists, Danysz and Pniewski, discovered the first case of a nucleus with two hyperons (double hyperfragment).IntroductionTheoretical problems (including solutions and marking schemes) were prepared especially for the 20th IPhO by Waldemar Gorzkowski. The experimental problem (including the solution and marking scheme) was prepared especially for this Olympiad by Andrzej Kotlicki. The problems were refereed independently (and many times) by at least two persons after any change was made in the text to avoid unexpected difficulties at the competition. This work was done by:First Problem:Andrzej Szadkowski, Andrzej Szymacha, Włodzimierz UngierSecond Problem:Andrzej Szadkowski, Andrzej Szymacha, Włodzimierz Ungier, Stanisław WoronowiczThird Problem:Andrzej Rajca, Andrzej Szymacha, Włodzimierz UngierExperimental Problem:Krzysztof Korona, Anna Lipniacka, Jerzy Łusakowski, Bruno SikoraSeveral English versions of the texts of the problems were given to the English-speaking students. As far as I know it happened for the first time (at present it is typical). The original English version was accepted (as a version for the students) by the leaders of the Australian delegation only. The other English-speaking delegations translated the English originals into English used in their countries. The net result was that there were at least four English versions. Of course, physics contained in them was exactly the same, while wording and spelling were somewhat different (the difference, however, were not too great).This article is based on the materials quoted at the end of the article and on personal notes of the author.THEORETICAL PROBLEMSProblem 1Consider two liquids A and B insoluble in each other. The pressures p i (i = A orB) of their saturated vapors obey, to a good approximation, the formula:i i o i Tp p βα+=)/ln(; i = A or B,where p o denotes the normal atmospheric pressure, T – the absolute temperature of the vapor, and i α and i β (i = A or B) – certain constants depending on the liquid. (The symbol ln denotes the natural logarithm, i.e. logarithm with base e =2.7182818…)The values of the ratio p i /p 0 for the liquids A and B at the temperature 40︒C and 90︒C are given in Tab. 1.1.Table 1.1The errors of these values are negligible.A. Determine the boiling temperatures of the liquids A and B under the pressure p 0.B. The liquids A and B were poured into a vessel in which the layersshown in Fig. 1.1 were formed. The surface of the liquid B has been coveredwith a thin layer of a non-volatile liquid C, which is insoluble in the liquids A and B and vice versa, thereby preventing any free evaporation from the uppersurface of the liquid B, The ratio of molecular masses of the liquids A and B (in the gaseous phase) is:.8/==BA μμγp 0 p 0Fig. 1.1Fig. 1.2The masses of the liquids A and B were initially the same, each equal to m = 100g. The heights of the layers of the liquids in the vessel and the densities of the liquids are small enough to make the assumption that the pressure in anypoint in the vessel is practically equal to the normal atmospheric pressure p0.The system of liquids in the vessel is slowly, but continuously and uniformly, heated. It was established that the temperature t of the liquids changed with timeτ as shown schematically in the Fig. 1.2.Determine the temperatures t1 and t2 corresponding to the horizontal parts of the diagram and the masses of the liquids A and B at the time τ1. Thetemperatures should be rounded to the nearest degree (in ︒C) and the masses of the liquids should be determined to one-tenth of gram.REMARK: Assume that the vapors of the liquids, to a good approximation,(1)obey the Dalton law stating that the pressure of a mixture of gases isequal to the sum of the partial pressures of the gases forming the mixture and(2)can be treated as perfect gases up to the pressures corresponding tothe saturated vapors.SolutionPART AThe liquid boils when the pressure of its saturated vapor is equal to the external pressure. Thus, in order to find the boiling temperature of the liquid i (i - A or B), one should determine such a temperature T bi(or t bi) for which p i/p0 = 1.Hence,Thus, the boiling temperature of the liquid A is equal toT= 3748.49K/10.711 ≈349.95 K.bAIn the Celsius scale the boiling temperature of the liquid A ist(349.95 – 273.15)︒C = 76.80︒C ≈77︒C.=bAFor the liquid B, in the same way, we obtain:α-5121.64 K,≈Bβ13.735,≈BT372-89 K,≈bBt99.74°C ≈100°C.≈bBPART BAs the liquids are in thermal contact with each other, their temperatures increase in time in the same way.At the beginning of the heating, what corresponds to the left sloped part of the diagram, no evaporation can occur. The free evaporation from the uppersurface of the liquid B cannot occur - it is impossible due to the layer of the non-volatile liquid C. The evaporation from the inside of the system is considered below.Table 1.2t67︒ C (with required accuracy).Therefore, ≈1Now we calculate the pressures of the saturated vapors of the liquids A and B at t67°C, i.e. the pressures of the saturated vapors of the liquids A the temperature ≈1and B in each bubble formed on the surface separating the liquids. From the equations (1) and (2), we get:≈A p 0.7340p ,≈B p 0.2670p ,)001.1(00p p p p B A ≈=+.Marking Scheme1.physical condition for boiling 1 point2.boiling temperature of the liquid A (numerical value) 1 point 3.boiling temperature of the liquid B (numerical value) 1 point 4.analysis of the phenomena at the temperaturet 3 points15.numerical value oft11 point6.numerical value of the mass ratio of the saturated vapors in the bubble 1 pointτ 1 point 7.masses of the liquids at the time18.determination of the temperaturet 1 point2REMARK: As the sum of the logarithms is not equal to the logarithm of the sum, the formula given in the text of the problem should not be applied to the mixture of the saturated vapors in the bubbles formed on the surface separating the liquids. However, the numerical data have been chosen in such a way that even such incorrect solution of the problem gives the correct value of the temperaturet(within required1accuracy). The purpose of that was to allow the pupils to solve the part B of the problem even if they determined the temperaturet in a wrong way. Of course, one1cannot receive any points for an incorrect determination of the temperaturet even if1its numerical value is correct.Typical mistakes in the pupils' solutionsNobody has received the maximum possible number of points for this problem, although several solutions came close. Only two participants tried to analyze proportion of pressures of the vapors during the upward movement of the bubble trough the liquid B. Part of the students confused Celsius degrees with Kelvins. Many participants did not take into account the boiling on the surface separating the liquids A and B, although this effect was the essence of theproblem. Part of the students, who did notice this effect, assumed a priori that the liquid with lower boiling temperature "must" be the first to evaporate. In general, this need not be true: if γwere, for example, 1/8 instead 8, then liquid A ratherthan B would remain in the vessel. As regards the boiling temperatures,practically nobody had any essential difficulties.Problem 2Three non-collinear points P 1, P 2 and P 3, with known masses m 1, m 2 andm 3, interact with one another through their mutual gravitational forces only; they are isolated in free space and do not interact with any other bodies. Let σ denote the axis going through the center-of-mass of the three masses, and perpendicular to the triangle P 1P 2P 3. What conditions should the angular velocities ω of the system (around the axis σ) and the distances:P 1P 2 = a 12, P 2P 3 = a 23, P 1P 3 = a 13,fulfill to allow the shape and size of the triangle P 1P 2P 3 unchanged during the motion of the system, i.e. under what conditions does the system rotate around the axis σ as a rigid body?SolutionAs the system is isolated, its total energy, i.e. the sum of the kinetic and potential energies, is conserved. The total potential energy of the points P 1, P 2 and P 3 with the masses 1m , 2m and 3m in the inertial system (i.e. when there are no inertial forces) is equal to the sum of the gravitational potential energies of all the pairs of points (P 1,P 2), (P 2,P 3) and (P 1,P 3). It depends only on the distances 12a , 23a and 23a which are constant in time. Thus, the total potential energy of the system is constant. As a consequence the kinetic energy of the system is constant too. The moment of inertia of the system with respect to the axis σ depends only on the distances from the points P 1, P 2 and P 3 to the axis σ which, for fixed 12a , 23a and 23a do not depend on time. This means that the moment of inertia I is constant. Therefore, the angular velocity of the system must also be constant:=ωconst. (1)This is the first condition we had to find. The other conditions will be determined by using three methods described below. However, prior to performingGM a =32ω (9)where321m m m M ++= (10)denotes the total mass of the system.In the same way, for the points P 2 and P 3, one gets the relations:a) the point P 2:1223a a =; GM a =32ωb) the point P 3:2313a a =; GM a =32ωSummarizing, the system can rotate as a rigid body if all the distances between the masses are equal:a a a a ===132312, (11)the angular velocity ω is constant and the relation (9) holds.SECOND METHODAt the beginning we find the moment of inertia I of the system with respect to the axis σ. Using the relation (2), we can write:222)(02323313121212323222221212332211r r r r r r r r r r r r m m m m m m m m m m m m +++++=++=Of course,22i i r =r i = 1, 2, 3and,011312313=-a a hence,The method described here does not differ essentially from the first method. In fact they are slight modifications of each other. However, it is interesting to notice how application of a proper mathematical language, e.g. the vector product, simplifies the calculations.The relation (9) can be called a “generalized Kepler’s law” as, in fact, it is very similar to the Kepler’s law but with respect to the many -body system. As far as I know this generalized Kepler’s law was presented for the first time right at the 20th IPhO.Marking scheme1. the proof that =ωconst 1 point2. the conditions at the equilibrium (conditions for the forcesand their moments or extremum of the total potential energy) 3 points3. the proof of the relation a a ij = 4 points4. the proof of the relation GM a =32ω 2 pointsRemarks and typical mistakes in the pupils' solutionsNo type of error was observed as predominant in the pupils' solutions.Practically all the mistakes can be put down to the students' scant experience in calculations and general lack of skill. Several students misunderstood the text of the problem and attempted to prove that the three masses should be equal. Of course, this was impossible. Moreover, it was pointless, since the masses were given. Almost all the participants tried to solve the problem by analyzingequilibrium of forces and/or their moments. Only one student tried to solve the problem by looking for a minimum of the total potential energy (unfortunately, his solution was not fully correct). Several participants solved the problem using a convenient reference system: one mass in the origin and one mass on the x -axis. One of them received a special prize.Problem 3The problem concerns investigation of transforming the electronmicroscope with magnetic guiding of the electron beam (which is accelerated with the potential difference U = 511 kV) into a proton microscope (in which the proton beam is accelerated with the potential difference –U ). For this purpose, solve the following two problems:A. An electron after leaving a device, which accelerated it with thepotential difference U , falls into a region with an inhomogeneous field Bgenerated with a system of stationary coils L 1, L 2, … , L n . The known currents in the coils are i 1, i 2, … , i n , respectively.What should the currents i 1’, i 2’, … , i n ’ in the coils L 1, L 2, … , L n be, inorder to guide the proton (initially accelerated with the potential difference –U ) along the same trajectory (and in the same direction) as that of the electron?HINT: The problem can be solved by finding a condition under which theequation describing the trajectory is the same in both cases. It may be helpful to use the relation:p dt d p = dt d 21p 2 = dtd 21p 2.B. How many times would the resolving power of the above microscopeincrease or decrease if the electron beam were replaced with the proton beam? Assume that the resolving power of the microscope (i.e. the smallest distance between two point objects whose circular images can be just separated) depends only on the wave properties of the particles.Assume that the velocities of the electrons and protons before theiracceleration are zero, and that there is no interaction between own magneticmoment of either electrons or protons and the magnetic field. Assume also that the electromagnetic radiation emitted by the moving particles can be neglected.NOTE: Very often physicists use 1 electron-volt (1 eV), and its derivativessuch as 1 keV or 1 MeV, as a unit of energy. 1 electron-volt is the energy gained by the electron that passed the potential difference equal to 1 V.Perform the calculations assuming the following data:Rest energy of electron: E e = m e c 2 = 511 keVRest energy of proton: E p = m p c 2 = 938 MeVSolutionPART AAt the beginning one should notice that the kinetic energy of the electron accelerated with the potential difference U = 511 kV equals to its rest energy 0E . Therefore, at least in the case of the electron, the laws of the classical physics cannot be applied. It is necessary to use relativistic laws.The relativistic equation of motion of a particle with the charge e in the magnetic field B has the following form:L dtd F p =It means that the value of the particle momentum (and the value of the velocity) is constant during the motion:==γv m p 0 const; v = const.The same result can be obtained without any formulae in the following way:The Lorentz force L F is perpendicular to the velocity v (and to theis the same in both cases.where c denotes the velocity of light.It is worthwhile to notice that our protons are 'almost classical', because their kinetic energy )(e k E E = is small compared to the proton rest energy p E . Thus, one can expect that the momentum of the proton can be determined, with a good accuracy, from the classical considerations. We have:.212121'22p e e p e e p e e p e p eE E c E E c E E E c E E E E E c E p =≈+=⎪⎪⎭⎫ ⎝⎛-⎪⎪⎭⎫ ⎝⎛+=In accordance with our expectations, we have obtained the same result as above.that λis inversely proportional to the momentum of the particle. Therefore, after replacing the electron beam with the proton beam the resolving power will be changed by the factor p/p' ≈1/35. It means that our proton microscope would allow observation of the objects about 35 times smaller than the electron microscope.Marking scheme1. the relativistic equation of motion 1 point2. independence of p and v of the time 1 point3. identity of e B/p in both cases 2 points4. scaling of the fields and the currents with the same factor 1 point5. determination of the momenta (relativistically) 1 point6. the ratio of the momenta (numerically) 1 point7. proportionality of the resolving power toλ 1 point8. inverse proportionality of λto p 1 point9. scaling of the resolving power 1 pointRemarks and typical mistakes in the pupils' solutionsSome of the participants tried to solve the problem by using laws of classicalmechanics only. Of course, this approach was entirely wrong. Some studentstried to find the required condition by equating "accelerations" of particles inboth cases. They understood the "acceleration" of the particle as a ratio of theforce acting on the particle to the "relativistic" mass of the particle. Thisapproach is incorrect. First, in relativistic physics the relationship between force and acceleration is more complicated. It deals with not one "relativistic" mass, but with two "relativistic" masses: transverse and longitudinal. Secondly, identity of trajectories need not require equality of accelerations.The actual condition, i.e. the identity of e B/p in both cases, can be obtained from the following two requirements:1° in any given point of the trajectory the curvature should be the same in both cases;2° in the vicinity of any given point the plane containing a small arc of the trajectory should be oriented in space in both cases in the same way.Most of the students followed the approach described just above. Unfortunately, many forgot about the second requirement (they neglected the vector character of the quantity e B/p).EXPERIMENTAL PROBLEM 4The following equipment is provided:1. Two piezoelectric discs of thickness 10 mm with evaporated electrodes (Fig. 4.1) fixed in holders on the jaws of the calipers;Fig. 4.12. The calibrated sine wave oscillator with a photograph of the control panel, explaining the functions of the switches and regulators;3. A double channel oscilloscope with a photograph of the control panel, explaining the functions of the switches and regulators;4. Two closed plastic bags containing liquids;5. A beaker with glycerin (for wetting the discs surfaces to allow better mechanical coupling);6. Cables and a three way connector;7. A stand for support the bags with the liquids;8. Support and calipers.A piezoelectric material changes its linear dimensions under the influence of an electric field and vice-versa, the distortion of a piezoelectric material induces an electrical field. Therefore, it is possible to excite the mechanical vibrations in a piezoelectric material by applying an alternating electric field, and also to induce an alternating electric field by mechanical vibrations.A. Knowing that the velocity of longitudinal ultrasonic waves in the material of the disc is about 3104 m/s, estimate roughly the resonant frequency of the mechanical vibrations parallel to the disc axis. Assume that the disc holders do no4 The Organizing Committee planned to give another experimental problem: a problem on high T c superconductivity. Unfortunately, the samples of superconductors, prepared that time by a factory, were of very poor quality. Moreover, they were provided after a long delay. Because of that the organizers decided to use this problem, which was also prepared, but considered as a second choice.10 mm Electrodesrestrict the vibrations. (Note that other types of resonant vibrations with lower or higher frequencies may occur in the discs.)Using your estimation, determine experimentally the frequency for which the piezoelectric discs work best as a transmitter-receiver set for ultrasound in the liquid. Wetting surfaces of the discs before putting them against the bags improves penetration of the liquid in the bag by ultrasound.B.Determine the velocity of ultrasound for both liquids without opening the bags and estimate the error.C. Determine the ratio of the ultrasound velocities for both liquids and its error.Complete carefully the synopsis sheet. Your report should, apart from the synopsis sheet, contain the descriptions of:-method of resonant frequency estimation;-methods of measurements;-methods of estimating errors of the measured quantities and of final results.Remember to define all the used quantities and to explain the symbols.5In the real Synopsis Sheet the students had more space for filling.Solution (draft)6A. As the holders do not affect vibrations of the disc we may expectantinodes on the flat surfaces of the discs (Fig. 4.2; geometric proportions not conserved). One of the frequencies is expected forfv l 221==λ,where v denotes the velocity of longitudinal ultrasonic wave (its value is given in the text of the problem), f - the frequency and l - the thickness of the disc. Thus:lv f 2=.Numerically 5102⋅=f Hz = 200 kHz.6 This draft solution is based on the camera-ready text of the more detailed solution prepared by Dr. Andrzej Kotlicki and published in the proceedings [3]l = λ/2Fig. 4.2One should stress out that different modes of vibrations can be excited in the disc with height comparable to its diameter. We confine our considerations to the modes related to longitudinal waves moving along the axis of the disc as the sound waves in liquids are longitudinal. We neglect coupling between different modes and require antinodes exactly at the flat parts of the disc. We assume also that the piezoelectric effect does not affect velocity of ultrasound. For these reasons the frequency just determined should be treated as only a rough approximation. However, it indicates that one should look for the resonance in vicinity of 200 kHz.The experimental set-up is shown in Fig. 4.3. The oscillator (generator) is connected to one of the discs that works as a transmitter and to one channel of the oscilloscope. The second disc is connected to the second channel of the oscilloscope and works as a receiver. Both discs are placed against one of the bags with liquid (Fig. 4.4). The distance d can be varied.Fig. 4.3Fig. 4.4One searches for the resonance by slowly changing the frequency of theoscillator in the range 100 – 1000 kHz and watching the signal on theoscilloscope. In this way the students could find a strong resonance at frequency 220≈f kHz. Other resonance peaks could be found at about 110 kHz and 670 kHz. They should have been neglected as they are substantially weaker. (They correspond to some other modes of vibrations.) Accuracy of these measurements was 10 kHz (due to the width of the resonance and the accuracy of the scale on the generator).B. The ultrasonic waves pass through the liquid and generate anelectric signal in the receiver. Using the same set-up (Fig. 4.3 and 4.4) we can measure dependence of the phase shift between the signals at Y 1 and Y 2 vs.distance between the piezoelectric discs d at the constant frequency found in point A . This phase shift is 0/2ϕπϕ+=∆l v df , where l v denotes velocity of ultrasound in the liquid. 0ϕ denotes a constant phase shift occurring whenultrasound passes trough the bag walls (possibly zero). The graph representing dependence )(ϕ∆d should be a straight line. Its slope allows to determine l v and its error. In general, the measurements of ϕ∆ are difficult for manyreflections in the bag, which perturb the signal. One of the best ways is tomeasure d only for πϕn =∆ (n - integer) as such points can be found rather easy. Many technical details concerning measurements can be found in [3] (pp. 37 and 38).The liquids given to the students were water and glycerin. In the standardsolution the author of the problem received the following values:v water = 310)10.050.1(⋅± m/s; v glycerin = 310)10.096.1(⋅± m/s.The ratio of these values was 1531.1 ..0The ultrasonic waves are partly reflected or scattered by the walls of the bag. This effect somewhat affects measurements of the phase shift. To minimize its role one can measure the phase shift (for a given distance) or distance (at the same phase shift) several times, each time changing the shape of the bag. Asregards errors in determination of velocities it is worth to mention that the most important factor affecting them was the error in determination of the frequency.This error, however, practically does not affect the ratio of velocities.Marking SchemeFrequency estimation1.Formula 1 point2.Result (with units) 1 point3.Method of experimental determining the resonance frequency 1 point4.Result (if within 5% of standard value) 2 points5.Error 1 pointMeasurements of velocities1.Explanation of the method 2 points2.Proper number of measurements in each series 3 points3.Result for velocity in the first liquid (if within 5% of standard value) 2 points4.Error of the above 1 point5.Result for velocity in the second liquid (if within 5% of standard value) 2 points6.Error of the above 1 pointRatio of velocities1.Result (if within 3% of standard value) 2 points2.Error of the above 1 pointTypical mistakesThe results of this problem were very good (more than a half of competitors obtained more than 15 points). Nevertheless, many studentsencountered some difficulties in estimation of the frequency. Some of themassumed presence of nodes at the flat surfaces of the discs (this assumption is not adequate to the situation, but accidentally gives proper formula). In part B some students tried to find distances between nodes and antinodes for ultrasonicstanding wave in the liquid. This approach gave false results as the pattern ofstanding waves in the bag is very complicated and changes when the shape of the bag is changed.AcknowledgementI would like to thank very warmly to Prof. Jan Mostowski and Dr. Andrzej Wysmołek for reading the text of this article and for valuable critical remarks. I express special thanks to Dr. Andrzej Kotlicki for critical reviewing the experimental part of the article and for a number of very important improvements.Literature[1] Waldemar Gorzkowski and Andrzej Kotlicki, XX Międzynarodowa Olimpiada Fizyczna - cz. I, Fizyka w Szkole nr1/90, pp. 34 - 39[2] Waldemar Gorzkowski,XX Międzynarodowa Olimpiada Fizyc zna - cz. II, Fizyka w Szkole nr2/3-90, pp. 23 - 32[3] XX International Physics Olympiad - Proceedings of the XX International Physics Olympiad, Warsaw (Poland), July 16 - 24, 1989, ed. by W. Gorzkowski, World Scientific Publishing Company, Singapore 1990 [ISBN 981-02-0084-6]。
关于Maxwell参数化扫描时添加calculations报错的说明当需要考查某一物理量改变时,对其他量的影响,这时需要用到参数化扫描的功能。
以同步发电机为例,常常需要考察不同励磁电流下,空载电压的大小,以便绘制空载特性曲线。
这时,可以将励磁电流作为变量,然后扫描之,具体操作为:右键Optimetrics,选择add parametric,通过add定义励磁电流变化范围。
在calculations里面,点击左下角setup calculations,report type选择transient,parameter选择moving1,category选择winding,quantity 选择A相induced voltage,function选择none。
这时,点击add calculation,done,就会发现出现红叉叉,系统提示“calculation must be a dimension reducing ranged function,when using solution'setup1:transient'”。
之所以出现这个错误,原因就在于定义的A相induced voltage是一个函数,是随时间变化的量,而软件要求A相induced voltage也就是calculation expression必须是“single, real number”,因此在上述操作的基础上,还需点击右上角的Range function,category选择math,function选择rms,点击ok。
这时,再add calculation,done,就正确了。
以上操作的目的是,通过扫描励磁电流和A相电压有效值的关系,实现了绘制同步发电机空载特性曲线的功能。
现在,该知道错在哪里,以及如何避免出错了吧?其实,setup calculations功能完全多此一举,即使这个地方不设置,求解完成后,后处理一样可以得到表达式与扫描量的关系,不会的同学可自己试着发掘一下Maxwellhelp文件为Maxwell2D/3D的瞬态求解设置铁芯损耗一、铁损定义(coreloss definition)铁损的计算属性定义(CalculatingPropertiesforCoreLoss(BPCurve)要提取损耗特征的外特性(BP曲线),先在View/EditMaterial对话框中设置损耗类型(CoreLoss Type)是硅钢片(ElectricalSteel)还是铁氧体(PowerFerrite)。
机械设计与制造第4期Mach ine ry D e s ig n&M a n u fa c t u r e2010年4月文章编号:1001—3997(2010)04-0096-03零件失效寿命相关的储备系统Copula可靠性模型唐家银1.2何平-施继忠z宋冬利z (1西南交通大学数学系,成都610031)(2西南交通大学牵引动力国家重点实验室,成都610031) Co p ul a s relia bilit y calc ulation m o de l fo r s tandb ysystems co n si d er in g th e cor relatione xi s t e d in failure Iives of co mp on en tsTA N G Jia-yinl,2,HE PingI,SH I Ji-zhon92.SONG Dong-Ii2(1C o l l e g e of maths,Southwest J i ao t o n g University,Chengdu610031China)(2State Key L a b or a t o r y o f T r ac t i o n Power,So uthwest Jiaotong University,Chengdu610031,China)【摘要】基于Copula函数,刻画当前工作零件寿命和储备零件工作寿命之间的相关结构,给出了2 单元冷、温储备不可修系统可靠度计算模型。
利用阿基米德Co pu la函数的可加性,通过迭代和降维,解决了n个寿命异型非指数分布零件构成的储备系统可靠度建模问题。
根据极大似然估计和k呻检验思想,给出零件失效寿命相关程度参数的估计方法及相关结构的选择准则。
最后,通过算例,说明该理论方法的可行}生、有效性。
关键词:C op u la;零件失效寿命;相关性;储备系统;可靠度计算【Abstract】For t he c or re l at io n s t r u c t u r e existed讥fa ilure life ofcurrent work in g c o mp o n en t a n d l&es of st a nd b y s,w e presen t a n e w theore ti cal m et h o d for reliabilit y c al c u la t i on con sidering c or r el at i onin t w o co mpo ne nt s cold an d wa rm sta ndb y systems.By using th e technique of iteration an d d i m e n s i o n al i t yredue- t ion accor ding t o a ddi ti vit y ofArchimedea n Copulas,the mod e li n gp r ob l em ofrel i ab il it ycalculationf or the standby sys tems c o mp o s ed of n components wh os e live s ar e not exponential dist ri bu ti onw a s solved sw—cessfully.Combining with m e t ho d ofmax im um li kel iho od an d k-s t es t,es tim ati onmethod for the parameter of co rr e l at i on d egree a nd s el ec ti on c rit er io n for cor re l at io n structu re w e r egiv er k Fi na ll y,a pr a c ti c alca l c ul a ti o n demonstrates the fe as ib il it y and effect ive ne ss of the the o r y.Ke y wo rds:Copu la;F ail ure l iv es of components;Correlation;Standby systems;Reliability caI—culation中图分类号:TH l6,TB ll4.3。
a rXiv:q uant-ph/03394v216M ay23Collisional decoherence reexamined Klaus Hornberger and John E.Sipe ∗Universit¨a t Wien,Institut f¨u r Experimentalphysik,Boltzmanngasse 5,1090Wien,Austria (Dated:Apil 17,2003)Abstract We re-derive the quantum master equation for the decoherence of a massive Brownian particle due to collisions with the lighter particles from a thermal environment.Our careful treatment avoids the occurrence of squares of Dirac delta functions.It leads to a decoherence rate which is smaller by a factor of 2πcompared to previous findings.This result,which is in agreement with recent experiments,is confirmed by both a physical analysis of the problem and by a perturbative calculation in the weak coupling limit.PACS numbers:03.65.Yz,03.65.Ta,03.75.-bI.INTRODUCTIONA classic result of decoherence theory is the rapid decay in the off-diagonal matrix el-ements in the coordinate representation of the density operatorρ(R1,R2;t)of a massive Brownian particle suffering collisions with the lighter particles of a thermal bath.Early cal-culations by Joos and Zeh[1]were improved by later authors,and the result of Gallis and Fleming[2]seems to be the most widely quoted[3].Theyfind,in the limit of an infinitely massive Brownian particle,that∂ρ(R1,R2;t)m dˆn1dˆn2equation derivations undertaken in,e.g.,quantum optics.In thefirst calculation wefind(2) withε=1.In the second wefind(2)withε=1and f(qˆn2,qˆn1)replaced by f B(qˆn2,qˆn1), thefirst Born approximation to that scattering amplitude.This is precisely what would be expected,since the second calculation requires the assumption of weak interaction;it thus serves to confirm theε=1result of thefirst.Neither of these is the most elegant or general calculation one could imagine;thefirst is rather cumbersome,and the second would be neater if generalized to second quantized form[5].But thefirst has the advantage of displaying the physics of decoherence in an almost pictorial way,while allowing a calculation involving the full scattering amplitude.And the second,in its simple form,establishes a clear connection with the usual approach to decoherence through the master equation approach common in quantum optics.Totally separate in their approaches,we feel that together they are a convincing demonstration thatε=1.These two calculations are presented in sections II and IV below.In section III we return to the traditional derivation and highlight its inherent shortcomings.We show how it should be modified by using a simple physical argument,which leads to a replacement rule for the occurring square of a Dirac delta function.This treatment then also yields the resultε=1. Our concluding remarks are presented in section V.II.SCATTERING CALCULATIONTo set our notation we begin with a review of the standard approach used to calculate collisional decoherence.However,we also wish to point out the difficulties that can arise in its application,so we begin in a more detailed way than is normally done.To apply scattering theory in a careful way one has to begin with an asymptotic-in state |φm |ψ ,a normalized ket that is the direct product of a Brownian particle ket|φm and abath particle ket|ψ .The asymptotic-in ket is the result of the evolution of a product ket |φ(−∞)m |ψ(−∞) at t=−∞to t=0under the Hamiltonian that describes the free evolution of both particles,without interaction.The effect of the two-particle scattering operator S on this asymptotic-in state,S(|φm |ψ ),then produces the asymptotic-out state.When evolved from t=0to t=∞by the non-interacting Hamiltonian,the asymptotic-out stateyields the actual state at t=∞that evolves from|φ(−∞)m |ψ(−∞) at t=−∞under the influence of the full Hamiltonian.FIG.1:Sketched are the wave packets associated with|φm and|ψ at t=0.In configuration(a) the state|φm |ψ could be taken as both an asymptotic-in state and an initial state at t=0;for configuration(b)that would not be possible.In general,of course,|φm |ψ does not describe the actual ket at t=0that evolves from |φ(−∞)m |ψ(−∞) at t=−∞,because the evolution of that actual ket involves the particle interaction.But if the kets|φm and|ψ are such that the(short-range)interaction between the particles has not yet had an effect(e.g.,Fig.1a but not Fig.1b),then|φm |ψ can be taken as the actual ket at t=0as well as the asymptotic-in ket.We only consider kets|φm and|ψ of this form below.We now turn to the impending collision of a bath particle characterized by|ψ and a Brownian particle described by a reduced density operator at t=0given by a convex sum of projectors|φm φm|,ρin= m p m|φm φm|= d R1d R2|R1 ρo(R1,R2) R2|,with probabilities p m>0, p m=1.Here the|R1,2 label position eigenkets of the Brownian particle,andρo(R1,R2)= m p m R1|φm φm|R2 (3) its position representation.Thenρtotalin=ρin⊗|ψ ψ|(4) can be considered both as the full initial(at t=0)density operator,and the full asymptotic-in density operator.The full asymptotic-out density operator is thenρtotal out =Sρtotalin S†= d R1d R2S(|R1 |ψ )ρo(R1,R2)( ψ| R2|)S†.To determine terms such as S(|R |ψ )it is useful tofirst consider the effect of the S operator on direct products|P |p of eigenkets|P of the Brownian particle momentum and eigenkets |p of the bath particle momentum.Since the total momentum commutes with the Soperator the scattering transformation can be reduced to a one-particle problem,with S(|P |p )= d q|P−q |p+q m∗M P+q|S o|m∗M P ,where the matrix element here is that of the one-particle scattering operator S o corre-sponding to the two-body interaction acting in the Hilbert space of the bath particle,and m∗=mM/(m+M)is the reduced mass.In the limit that the Brownian particle is much more massive than the bath particle,M≫m,this reduces toS(|P |p )→ d q|P−q |p+q p+q|S o|por,moving to a position representation for the Brownian particle,S(|R |p )= d q|R e−i q·R/ |p+q p+q|S o|p= d q|R |p+q p+q|e−i p·R/ S o e i p·R/ |p=|R e−i p·R/ S o e i p·R/ |p ,where p is the momentum operator for the bath particle,and so for general states|ψS(|R |ψ )=|R e−i p·R/ S o e i p·R/ |ψ≡|R ψR ,whereψR =e−i p·R/ S o e i p·R/ |ψ ,and thusρtotal= d R1d R2|R1 ψR1 ρo(R1,R2) ψR2 R2|.outis not thefinal density operator at t=∞,but only the asymptotic-out density Althoughρtotaloutoperator,it evolves to thefinal density operator through the non-interacting Hamiltonian, and overlaps of the form ψR2|ψR1 will be preserved during this free evolution.So thefinal reduced density operator for the Brownian particle at t=∞isρfinal= d R1d R2|R1 ψR2|ψR1 ρo(R1,R2) R2|≡ d R1d R2|R1 ρ(R1,R2) R2|,whereρ(R 1,R 2)= ψR 2|ψR 1 ρo (R 1,R 2).(5)As is well understood,decoherence arises because the bath particle becomes entangled with the Brownian particle and the two (asymptotic-out)states ψR 2 and ψR 1 resulting from scattering interactions associated with the same bath ket |ψ and different position eigenkets|R 2 and |R 1 can have negligible overlap even for |R 2−R 1|small.The change of the Brownian particle’s reduced density operator by a single collision is ∆ρ(R 1,R 2)≡ρ(R 1,R 2)−ρo (R 1,R 2)= ψR 2|ψR 1 −1 ρo (R 1,R 2).(6)It involves overlap terms of the form ψR 2|ψR 1 = ψ|e −i p ·R 2/ S †o e −i p ·(R 1−R 2)/ S o e i p ·R 1/ |ψ = ψ|S †2S 1|ψ =tr bath S †2S 1|ψ ψ| ,(7)where the operators S j =e −i p ·R j / S o e i p ·R j /(8)for j =1,2are translated scattering operators.We introduce corresponding T j operators according toS j =1+i T j ,(9)and using the unitarity of the S j ,which follows immediately because S o is unitary,we findS †2S 1=1+T †2T 1−12T †2T 2+i 2 T 2+T †2and so ψR 2|ψR 1 =1+ ψ|A|ψ ,(10)where A =T †2T 1−12T †2T 2+i 2T 2+T †2 .Thus the change in the Brownian particle reduced density operator is∆ρ(R1,R2)= ψ|A|ψ ρo(R1,R2)(11)The general strategy is to evaluate the matrix element ψ|A|ψ by inserting complete sets of momentum eigenstates,ψ|A|ψ = d q1d q2 ψ|q2 q2|A|q1 q1|ψ ,(12) determine q2|A|q1 ,and then perform the momentum eigenstate integrals.Writing S o= 1+i T o as well,and using the relations(8)and(9)wefindq2|A|q1 =e i(q1·R1−q2·R2)/ q2|T†o e i p·(R2−R1)/ T o|q1 (13)−1e i(q1−q2)·R2/ q2|T†o T o|q12i+δ(E2−E1)f(q2,q1),(14)2π mwhere f(q2,q1)is the scattering amplitude,we can identifyq2|T o|q1 =1f(q2,q1),2π q2where E i=q2i/(2m).Now in the traditional calculations[1,2,3]one calculates∂ρ(R1,R2)/∂t by considering the change∆ρ(R1,R2)in a time∆t due to collisions with bath particles that would pass in the neighborhood of the Brownian particle,taking the distribution of their velocities from the assumed thermal equilibrium of the bath.To calculate∆ρ(R1,R2)from one of these bath particles,a box-normalized momentum eigenstate, |q is used in place of a localized ket|ψ .Unlike the|φm |ψ states we introduced above,the|φm |q obviously cannot be considered either as asymptotic-in states or as the actual states at t=0since the |q are delocalized.Nonetheless,the traditional approach seems to simplify the calculation because, as is clear from(12),only diagonal elements q|A|q are required if the limit of an infinite boxis taken.But from the expression(13)for q2|A|q1 it is clear that,when a resolution over a complete set of momentum states|q′ is inserted between T†o and T o and the expression(15) for the matrix elements of T o is used,the diagonal elements q|A|q involve the square of Dirac delta functionsδ(q−q′).To evaluate these the“magnitude”ofδ(0)must be somehow set.This is done by relating it to an original normalization volume of the box.While not implausible,such a protocol is certainly not rigorous and is open to question.To avoid the necessity of this kind of maneuver we will employ bath states|ψ that are normalized and localized,as is required by a strict application of scattering theory.Before addressing the full calculation for a bath in thermal equilibrium we consider scattering involving a single state|ψ .A.Scattering of a single bath ketFrom the equations(12)and(13)for ψ|A|ψ in terms of q2|A|q1 it is clear that we require integrals of the formI1= d q1d q2u(q1,q2) q2|T o+T†o|q1 ,(16)I2(R)= d q1d q2u(q1,q2) q2|T†o e i p·R/ T o|q1 ,which we work out in Appendix A for an arbitrary function u(q1,q2)of the two momentum variables.Wefind that we can write these expressions exactly asI1= d q ˆq⊥d∆u(q−∆2)M1(q,∆)(17) andI2(R)= dˆn d q ˆq⊥d∆u(q−∆2)e i Q·R/ M2(q,ˆn,∆),(18) The integration over q covers all momentum space,while∆is a two dimensional momentum vector ranging over the plane perpendicular to q;ˆn is a unit vector with dˆn the associated solid angle element.Moreover,M1(q,∆)=12,q−∆2,q+∆4π2 2Q2)f(Q,q−∆FIG.2:For this as both the total asymptotic-inwithQ=ˆn 4.(21) With these formulas in hand we can address the expression for ψ|A|ψ once|ψ is specified. To do this,we take the bath particle wave function r′|ψ to be a Gaussian wave packet centered at r o in position and p o in momentum,r′|ψ =e i p o·(r′−r o)/√√2 q−∆πb2 3/2e i∆·r o/ e−∆2/(4b2)e−|q−p o|2/b2.We now assume that this wave packet is located far enough away from the regions of space where an initial density operator(3)is concentrated,and with an average momentum directed towards the Brownian particle such that the combined density operator(4)can be taken both as an initial density operator at t=0,and as the asymptotic-in density operator (see Fig.2).Then using the expressions above wefindψ|A|ψ = 1whereB(ˆn,q,∆)=e i q·(R1−R2)/ e i Q·(R2−R1)/ e−i∆·(r o−2e−i∆·(r o−R1)/ e−∆2/(4b2)M2(q,ˆn,∆)−12 e−i∆·(r o−R1)/ −e−i∆·(r o−R2)/ e−∆2/(4b2)M1(q,∆),and where we have put2.(23) The Gaussian functions will keep∆within about b of zero and q within about b of p o.We now assume that the central momentum p o is much greater in magnitude than its variance, p o≫b,and hence q≫b for all q that make a significant contribution;we also assume that the scattering amplitude varies little over the momentum range b.Then we can putM1(q,∆)≈14π2 2|f(qˆn,q)|2.Once these approximation are made the integral over∆of the three terms in B(ˆn,q,∆) can be done immediately.The integral over∆of thefirst term is not so simple because∆still appears in Q.In the exponential we have phase factors that vary asQ·(R2−R1)q2+∆2=qˆn·(R2−R1)8 q+...Thefirst correction term is of orderb2|R2−R1|(q/b)(24) Since q≫b this term will still be much smaller than unity even if the distance between the two positions of the Brownian particle is several widths of the wave packet.We assume that|R2−R1|is indeed such this quantity is much less than unity.Then we can replace the phase by its leading order expansionQ·(R2−R1) ,in the exponentials of thefirst two integrals,and the integration over∆can be done as well.These are two dimensional integrals over a plane perpendicular to q,and so they are of the form ˆq⊥d∆e−i∆·(r o−R),where we have used the fact that ab= and introducedexp − R2−(ˆq·R)2 /a2Γq(R)=A r o(q),(26)(πb2)3/2whereA r o(q)=Γq(r o−(Γq(r o−R1)+Γq(r o−R2)) dˆn|f(qˆn,q)|222πi+R.Moreover,since the integral in(26)restricts q to within a distance of about b of p o,in(27)we can replace q by p o in the scattering amplitudes and in the phase,using the assumption already made thatthey vary little over a range of b;we can also replace theΓq functions by correspondingΓpo functions.The integral in(26)can then be done,and using(11)wefind∆ρ(R1,R2)=−ρo(R1,R2)Γp(r o−oe−ℓ2/a2R)=FIG.3:A configuration where a≫R=|R1−R2|;ℓ=e−βp2/(2m)(29)ΩprovidedΩis much larger than the cube of the thermal de Broglie wave lengthλ= m.(30) The usual convex decomposition of(29)in terms of the delocalized energy eigenstates is the obvious one and,aside from the freedom in choosing orthogonal states from among adegenerate set,it is the only one in terms of orthogonal states.But a host of others can also found.A particularly convenient set of convex decompositions for our problem at hand can be obtained by usinge−βp2/(2m)= ¯β 2πm/ˆβ 3/2e−¯β(p−p)2/(2m)(31) which holds as long asˆβand¯βare both positive and11¯β+ ArrayΩ d pˆµ(p)|ψrp ψrp|,(32) whereˆµ(p)= ˆββ 3/4e−¯β(p−p)2/(4m)|r (34)=¯λ3/2e−¯β(p−p)2/(4m)|r ,are characterized by the length scale¯λ= m,(compare with (30)).One then immediately finds r ′|ψrp =2√¯λ3/2e i p ·(r ′−r )/ e −2π|r ′−r |2/¯λ2(35)so the wave packet |ψrp is centered at r and has an average momentum p .Indeed,it is of the Gaussian form used in the preceding section with minimal uncertainties,b ≡2m =k B ¯T2m =k B ˆT2m +(δp x )22.We see that in the class (32,33)of convex decompositions of ρbath a part of the thermal kinetic energy is associated with the size of the wave packets themselves,while the rest resides inthe motion of the centres of the wave packets.If we take ˆT→0then the wave packets are essentially all at rest characterized by a size ¯λ→λ,which is the thermal de Broglie wavelength.On the other hand,for ˆT≫¯T the wave packets are much larger than the thermal de Broglie wavelength,and essentially all the thermal kinetic energy is associated with the expectation value of the momenta of the wave packets;we have p 2 2mp 2ˆµ(p )d p =33k B ˆT1.Assumptions and choices1.We neglect initial correlations,taking the initial full density operator at t=0to be adirect product of a Brownian particle density operator and a density operator for the bath particles in thermal equilibrium,ρtotal(t=0)=ρo⊗ρbath.(36) 2.We assume that the density of bath particles is much less thanλ−3;then the issue ofparticle degeneracy does not matter and we may consider the density operator of the total bath to be just the product of density operators for individual particles.Thus we can calculate effects‘particle by particle’.We choose a volumeΩmuch larger than any other volume of interest.3.We use a convex decomposition ofρbath for a single bath particle of the type describedabove,with¯T≪T such thatˆT≈Tand thereforeb2≪ p2 .(37) This renders b sufficiently small so that the variation in scattering amplitudes over the momentum spread of a wave packet is negligible for essentially all of the wave packets in the convex decomposition.4.The value of¯T should also be small enough that the neglect of the variation of thescattering amplitudes in the integral(22)is justified,and that we can use the approx-imation of neglecting terms on the order of(24)above.For the latter we needb2q|R2−R1|≪1Now for typical wave packets the average momentum p,and hence q,will be of the order of mv wp=|R2−R1|= 8π λ≪1,vwpand sinceˆT≈T this reduces to¯T≪|R2−R1|5.We choose a coarse-graining time∆t sufficiently large thatv wp∆t≫a,(38)v wp∆t≫|R2−R1|.That is,a typical packet travels a distance much greater than its width and much greater than the distance between the two decohering sites during the coarse graining ing the expressions for v wp and a above,andˆT≈T,thefirst condition readsT∆t≫R(recall(23);see Fig.4).Of course,some of these will completely miss the Brownian particle,but none have had a collision with it in the past.For a given p we refer to this region of space as R(p).Returning to the wave packets,note that those with central positions r close to the R1 or R2of interest will initially be overlapping with regions of space for whichρo(R1,R2)is non-vanishing;here any talk of a collision is inappropriate,since at initiation,at t=0,the Brownian and bath particle would immediately be strongly interacting.This is an artifactΩ ψrp|A|ψrp ,where we assume that the inclusion of the problematic class of wave packets identified above will not lead to serious ing the result(26)from our scattering calculation above, we have∆ρ(R1,R2)=nρo(R1,R2) d pˆµ(p) R(p)d r d q e−|q−p|2/b2But this is not necessary.We can simply note that,by virtue of(37),ˆµ(p)will vary little over the range b that e−|q−p|2/b2peaks and falls.Hence we can replaceˆµ(p)byˆµ(q)and R(p)by R(q),and immediately do the integral over p to yield∆ρ(R1,R2)=nρo(R1,R2) d qˆµ(q) R(q)d r A r(q).Since the only r dependence is in theΓq,see(25),one can now do the r integral for each fixed q,putting d r=d r⊥dr ,where r refers to the distance in the direction−q.Since the integration over r⊥is unrestricted in the region R(q)we haveR(q)d r⊥Γq(r⊥−R⊥i)=1=R1,R2,orfor R∆t,mand so wefind∆ρ(R1,R2)ˆµ(q) dˆn e i(q−qˆn)·(R1−R2)/ −1 |f(qˆn,q)|2.mFinally,we recall thatˆT≈T and therefore putˆµ(q)≈µ(q),whereµ(q)= β,(41)4πand hence on a coarse grained time scale wefind(1,2)withε=1.III.THE TRADITIONAL APPROACH:A REMEDYWe showed in the preceding section how the problem of evaluating a squared Dirac function can be circumvented by expressing the thermal state of the bath particles in an over-complete,non-orthogonal basis of Gaussian wave packets(see Eq.(32)).However,it iscertainly reasonable to explore the possibility of using the standard diagonal representation of the thermal bath density operator,which facilitates the formal calculation considerably. After all,all the representations ofρbath are equally valid and should yield the same master equation provided the calculation is done in a correct way.It is therefore worthwhile to search for a way to deal properly with such an ill-defined object as the“square”of a delta distribution function.In this section we show how a proper evaluation of the diagonal momentum basis matrix elements can be implemented.This leads to an alternate derivation of the master equation (1,2),and allows us to highlight the origin of the problem plaguing earlier workers and to discuss further implications.However,rather than attempting a mathematically rigorous formulation,we base our presentation on a simple physical argument.Our point is that such an argument can lead to a prescription for correctly evaluating improper products of Dirac delta functions,although this differs from previous naive treatments.A.A single collisionLet us consider again the action of a single scattering event on the Brownian particle in position representationρo(R1,R2)and in the limit of a large mass.It follows from the discussion in section II that after the collision it differs merely by a factor from the initial Brownian state,ρ(R1,R2)=η(R1,R2)ρo(R1,R2)(42) which is given byη(R1,R2)=tr bath{e−i p R2/ S†o e i p(R2−R1)/ S o e i p R1/ ρbath},(43) (see Eqs.(5)and(7)).In section II only pure statesρbath=|ψ ψ|of the bath particle were considered,but the reasoning is immediately generalized to mixed states.The factorη(R1,R2)may be called the decoherence function,since it describes the ef-fective loss of coherence in the Brownian state which arises from disregarding the scattered bath particle.The normalization ofρbath impliesη(R1,R2)=1(44)lim|R1−R2|→0which means that the collision does not change the position distribution of the Brownian point particle,ρ(R,R)=ρo(R,R).On the other hand,possible quantum correlationsbetween increasingly far separated points will vanish,since a collision may be viewed as a position measurement of the Brownian particle by the bath which destroys superpositions of distant locations:lim|R1−R2|→∞η(R1,R2)=0(45) This complete loss of coherence implies that the collision took place with a probability of one.It could be realized,in particular,by taking the incoming bath particle state to be a momentum eigenket in a box centered on one of the scattering sites.In thermal equilibrium the density operator(29)of the bath particle can be written asρbath=λ3Ω p∈PΩµ(p) |p p|,(46) with the normalized momentum distribution function(40)atβ=1/(k B T).The |p are momentum eigenkets normalized with respect to the bath volumeΩ,|p =(2π )3/2(2π )3/2,(49) which satisfyp|p′ =δ(p−p′)and span the full space, d p|p p|=I.(50)Since the bath state(46)is diagonal in the momentum representation,an explicit expres-sion for the decoherence function(43)is readily obtained:η(R1,R2)→ d pµ(p) p|e−i p·R2/ S†o e i p·(R2−R1)/ S o e i p·R1/ |p= d pµ(p) 1− p|T†o T o |p +e i p·(R1−R2)/ p|T†o e i p·(R2−R1)/ T o |p= d pµ(p) 1−(2π )3Ω p∈PΩ→ d p.In the second line we introduced the operator T o=i(1−S o)and used the unitarity of S o,i(T o−T†o)=−T†o T o,as in section II and in[2,3].The last line follows after inserting a complete set of states (50)and noting the relation(47).The expression in square brackets in(51)should be well-defined andfinite.However, it involves two arbitrarily large quantities,the“quantization volume”Ω,which stems from the normalization of the bath particle,and the squared amplitude of the T o-operator with respect to(improper)momentum kets.The simple matrix element is given by the expression (15)p′|T o|p =δ(p−p′)|R1−R2|→∞.Therefore the limit(45)allows to specify the unknown function g(p)in(53).One obtainsg(p)=Ωσ(p)p2withσ(p)= dˆn f(pˆn,p) 2the total cross section for scattering at momentum p.Formally,this means that one should treat the expression involving the squaredδ-function and scattering amplitude asδ(p−p′)f(p′ˆn,p) 2→Ω∆t=−n d pµ(p)p∂tρ(R1,R2)=−F(R1−R2)ρ(R1,R2).(55) with F given by(2),again withε=1.C.InterpretationIt is clear that the derivation of the decoherence function(43)does not hold rigorously even for volume-normalized(47)momentum states,since their amplitude is uniform in spaceand they cannot be considered as asymptotic-in or asymptotic-out states.Nonetheless, the fact that one obtains the“correct”master equation by using the diagonal momentum representation(46)indicates that it can be reasonable,at least in a formal sense,to extend the applicability of(43)to volume-normalized momentum eigenstates.Then the appearance of the total cross section in the appropriate replacement rule(54) has a clear physical interpretation.The squared matrix element of the T o operator with respect to two orthogonal proper states may be viewed as the probability for a transition between the states due to a collision.The appropriate normalization of the probability necessary in the limit of improper states is then effected by the appearance of the total cross sectionσ(p)in(54),which is absent in the usual naive treatments of the squared delta function.This point of view is confirmed by the fact that the rule(54),which was derived from a simple physical argument(45),implies a conservation condition.Integrating(54)we have (2π )3=1(56)p2σ(p)and hence,using(50)and switching to volume-normalized states,p|T o T†o |p →1.(57) Inserting the identity(48)yieldsp′∈PΩ p′|T o |p 2→1.(58)This is reminiscent of the situation of a multi-junction in mesoscopic physics[8],or of the scattering offa quantum graph[9],where one defines a transition matrix T mn=|t mn|2 which connects afinite number of incoming and outgoing channels.There the t mn are the transmission amplitudes between the incoming and outgoing states and the currentconservation impliesm T mn=1with T mn=|t mn|2,in analogy to(58).The fact that the conservation relation(58)has no meaningful equivalence in the contin-uum limitΩ→∞is closely connected to the difficulty of evaluating the squared scattering amplitude in the momentum representation.It suggests that the diagonal representation ofρbath can be used in a rigorous formulation of the master equation only if the transition of going from a discrete to a continuous set of bath states is delayed until after the square of the scattering matrix element is evaluated.A calculation along this line,albeit in a perturbative framework,is presented in the following section.IV.WEAK-COUPLING CALCULATIONWe now consider an approach that is totally different from the derivation in Section II. Instead of performing a scattering calculation,we obtain a master equation for the reduced density operator from a weak coupling approximation that is very similar to the analyses of quantum optics.Again the assumption of a low density of bath particles will allow us to calculate the effect of the bath particles one particle at a time,so we begin with our Brownian particle and a single bath particle restricted to a box of normalization volumeΩ. While we will take the limitΩ→∞in the course of the calculation,we can do it in such a way that products of Dirac delta functions never appear.In the absence of any interaction between the particles the Hamiltonian readsH o=P22m,where m and M are the bath and Brownian particle masses and p and P are their momentum operators.The normalized eigenstates of H o are direct products |P |p ,where |p is given by(47)with(49),and similarlyR |P =e i P·R/ Ω.(59) The values of p and P are restricted to a discrete set,p,P∈PΩ,so that the wave functions respect periodic boundary conditions.Our full Hamiltonian is thenH=H o+V(r−R),where r and R are respectively the bath and Brownian particle position operators,and V describes the interaction.In the interaction picture the full density operator evolves according toρtotal I (t)=U(t)ρtotalI(0)U†(t),(60)。
自动化专业英语姜书艳主编张昌华徐心皓何芳编著习题参考解答Unit 1A. Basic laws of Electrical Networks[EX.1] Comprehension1. KCL:The algebraic sum of the currents entering any node is zero.KVL:The algebraic sum of the voltage around any closed path is zero.2. Node: A point at which two or more elements have a common connection is calleda node.Branches: a single path in a network composed of one simple element and the node at each end of that element.Path: If no node was encountered more than once, then the set of nodes and elements that we have passed through is defined as a path.Loop: If the node at which we started is the same as the node on which we ended, then the path is, by definition, a closed path or a loop. a path is a particular collection of branches.3. 4, 5, We can form a path but not a loop.4. v R2=32V, V x=6V[EX.2] Translation from English to Chinese1. 如果定义具有最大连接支路数的节点为参考节点,那么得到的方程相对来说比较简单。