安盟动态口令认证系统产品说明书

ET200智能卡读写器-动态令牌OTP身份认证加密锁USBET200 智能卡读写器ET200 智能卡读写器采用USB 接口，支持遵循T=0 和T=1 协议，符合ISO7816-1/2/3 标准的所有智能卡，它通过USB 线与计算机相连，由单个双色指示灯显示工作状态，重量仅60 克，外型小巧，不占用有限的桌面空间。

ET200 智能卡读写器适用于电子支付系统、身份认证等需要对智能卡信息读写工作的领域，支持ISO7816-1/2/3 标准，提供微软PC/SC 标准驱动，是身份认证、电子商务、家庭银行、信息安全、访问和身份控制以及其它安全应用的理想解决方案。

USB1.1接口符合PC/SC 标准可以读写所有符合ISO 7816-1/2/3的T=0和T=1协议的智能卡读写智能卡支持9，600~250，000bps的PPS（协议和参数选择）支持ISO7816的A类（5V）智能卡具有短路保护功能通过RoHS认证取得生产许可证符合的标准：ISO-7816 Class A (5V),PC/SC, EN 60950/IEC 60950,Microsoft WHQL XP、Vista, EMV 2000 Level 1,CE,FCC 使用微软PC/SC 标准驱动，为PC应用软件开发提供接口示例ET301智能卡读写器ET301读写器是一款应用于PC环境或相关智能环境的高速接触式智能卡读写器。

符合标准CCID 规范，支持USB2.0全速设备（兼容1.1接口）。

可以读写所有符合ISO 7816-1/2/3的A类、B类、C类智能卡。

支持对ISO 7816-3标准尺寸的IC卡，具有很高的系统集成稳定性。

ET301作为智能卡系统集成必备的前端处理设备，极大地提高了应用系统安全性，产品适用于具有IC卡操作和高安全需求的金融、社保、电信、电子支付、网络安全、电子商务、身份认证、电子证务等接触式CPU卡应用系统。

支持USB2.0全速设备接口（兼容1.1/2.0/3.0接口）符合标准CCID规范读写所有符合ISO7816-1/2/3的T=0和T=1协议的A类、B类、C类智能卡对接触卡支持全参数PPS协议，和ICC的数据传输波特率可达344K（此波特率是在IC 卡频率为4M时的结果）具有短路保护功能符合ISO7816、IEC/EN60950、EMV 2000 Level规范接触卡供电控制：1.8V/3V/5V 单独控制，LDO 确保1.8V/3V 供电的稳定性智能卡接口速度（如果智能卡支持）：T=0、T=1均支持10.753k ~ 344K（此波特率是在IC卡频率为4M时的结果）（D=32/F=372）操作系统：Windows 2000 SP4/XP SP2 SP3/Server2003/Vista/7/8包括32位和64位以及各种补丁版本、Windows CE 、Linux2.6以上ET502智能卡读写器ET502 NFC高速智能卡读写器是符合标准CCID协议的高速双界面智能卡读写器产品。

目录第1章产品介绍 ......................................................................... 1-11.1产品简介 ..........................................................................................1-11.1.1产品概述................................................................................................. 1-11.1.2产品特点................................................................................................. 1-11.2物理特性 ..........................................................................................1-21.3产品外观 ..........................................................................................1-21.3.1产品前面板............................................................................................. 1-21.3.2产品后面板............................................................................................. 1-21.3.3 LED指示灯说明....................................................................................... 1-31.3.4前面板接口说明...................................................................................... 1-4 第2章设备安装 ......................................................................... 2-12.1安装须知 ..........................................................................................2-12.1.1安装环境要求......................................................................................... 2-12.1.2安装操作提示......................................................................................... 2-32.1.3安全警告................................................................................................. 2-42.2安装准备 ..........................................................................................2-42.2.1核对装箱单............................................................................................. 2-42.2.2安装工具及材料...................................................................................... 2-42.3设备安装 ..........................................................................................2-52.3.1安装ER400-LAB...................................................................................... 2-52.3.2ER400-LAB设备接地............................................................................... 2-52.3.3 Console线缆连接................................................................................. 2-62.3.4 SFP收发器安装....................................................................................... 2-72.3.5电缆光纤连接......................................................................................... 2-72.3.6电源线连接............................................................................................. 2-8第1 章产品介绍1.1产品简介1.1.1产品概述ER400-LAB 是神州数码网络推出的二层千兆加千兆上行安全认证管理系统。

Rev. NCTABLE OF CONTENTS1.0INTRODUCTION (1)2.0AIRWORTHINESS REQUIREMENTS (2)3.0AAIR SYSTEM DEFINITION (3)3.1AAIR System Overview (3)3.2Seatbelt Airbag Assembly and Belt Extender (4)3.3Inflator Assembly (5)3.4Electronics Module Assembly (7)3.5Cable Interface Assembly (10)3.6System Diagnostic Tool (11)4.0AAIR V23 SYSTEM OPERATION (12)4.1Normal Operation (12)4.2Diagnostics Operation (12)FIGURESFigure 1 – AAIR V23 System Components – Two Seat Placement (3)Figure 2 – Seatbelt Airbag Features (5)Figure 3 – Inflator Assembly Features (6)Figure 4 – Inflation Igniter Connector (7)Figure 5 – EMA Assembly (8)Figure 6 – AAIR V23 System Schematic (9)Figure 7 – EMA with Cable Interface Assembly (10)Figure 8 – V23 System Diagnostic Tool (11)Rev. NC1.0 INTRODUCTIONThis report provides the system description of the AMSAFE Aviation Inflatable Restraint (AAIR®) System, Version V23, using a Three-point Seatbelt Airbag Restraint with Dual Sensor EMA. This description defines all system components, their critical features, and their operation.The AAIR V23 System is comprised of various core components. The core components are equivalent in design and manufacture for all aircraft using this generation product (referred to as AAIR System, Version V23, or AAIR V23 System) using a three-point restraint along with a dual sensor EMA. Certification data for the core components is common to all programs. These core items will be certified through dynamic testing (installation on seat test fixture) and vibration testing of the AAIR System. Refer to Paragraph 3.1 for further information on core components.Rev. NC 2.0 AIRWORTHINESSREQUIREMENTSThe AAIR System will be installed in aircraft to comply with the requirements of Special Condition 1 of the Proposed Special Conditions listed below. The applicable airworthiness requirements are:14 CFR Part 23, up to Amdt 23-55 Federal Aviation RegulationsFAA AC 23.1309 Federal Aviation Administration Advisory Circular –Equipment, Systems, and InstallationsRTCA-DO160D Environmental Conditions and Test Procedures for AirborneEquipmentRTCA-DO183 Minimum Operational Performance Standards for Emergency Locator TransmittersFAA TSO C114 FAA Technical Standard Order C114: Torso Restraint SystemsFAA Notice 23-03-01-SC, 17-Jul-03 Proposed Special ConditionsRev. NC3.0 AAIR SYSTEM DEFINITIONThe AAIR is a self-contained, modular restraint specifically designed to improve occupant protection from serious head injury during a survivable accident. The lapbelt is a three-point restraint system including the AAIR airbag attached to standard webbing, a webbing retractor, fixed anchor point, and buckle anchor point. This AAIR System is primarily located in the front two (pilot and copilot) aircraft seats, and can be used for passenger-only aircraft seating. It is completely independent with no interface to aircraft wiring.The system is divided into the components listed below. These have means to be inspected or replaced as required for continued airworthiness. This design, verification, and certification testing have considered environmental conditions as specified in document RTCA DO-160D, as well as vibration robustness to RTCA DO-183.3.1 AAIR SYSTEM OVERVIEWThe AAIR System contains the following core components corresponding to Figure 1.Seatbelt Airbag Assembly (SAA)Electronics Module Assembly (EMA) Inflator AssemblySystem Diagnostics Tool (not shown) Figure 1 – AAIR V23 System Components – Two Seat PlacementEMA and End-Release Buckle Assy Inflator Assy Diagnostic Connector Airbag Assy w/Inertia ReelRev. NC 3.2 SEATBELT AIRBAG ASSEMBLY AND BELT EXTENDERThe Seatbelt Airbag Assembly (SAA) is the basic lapbelt restraint and is certified to FAA TSO C114. The SAA consists of standard polyester webbing, the packed airbag assembly, a webbing retractor assembly, a fixed anchor point, and a buckle assembly anchor point. The AAIR SAA has the same basic configuration as conventional, three-point, non-inflatable lapbelts, but has the addition of an airbag, a gas delivery hose, and an activation circuit. The buckle is located at a fixed point and uses a push-button type release mechanism. The buckle assembly has a built-in activation system using a magnet and a reed switch. Buckling the lapbelt automatically activates the AAIR System. The lapbelt also includes stiffening device that mechanically resists buckling 180 degrees out of phase, i.e., twisting the belt. Any limitations and information necessary for safe operation of the AAIR are included in the AAIR SMM (Supplemental Maintenance Manual). Special instructions are not required for the passenger to use the device. Child seats are not allowed with pilot/copilot aircraft configurations of the AAIR V23 System. Reference Figures 2, 3, and 7 for seatbelt airbag features and end-release buckle assy features.The AAIR SAA components and their special features are listed below and referenced in Figures 2 and 3:•Standard polyester webbing with standard attachment anchors (ref. 2A).•Airbag sewn to webbing with approximately 30-liter airbag volume made of two fabric panels. The panels consist of a 315-denier nylon 6,6 substrate with an anti-flammability treatment (ref. 2B). The webbing also retracts within an Inertia Reel (ref. 2E) automatically maintaining tight fit of the seatbelt to an individual occupant’s body shape.•Cover with a tearable seam, which opens upon deployment. Cover is constructed of a durable material which protects the internal components from contamination and wear (ref.2B).•Gas delivery hose is tubular woven 1100-denier polyester with Kevlar-like filler and EPDM hose lining. The hose also contains a protective sleeve, which consists of a urethane-type treated, 1100-denier polyester fabric. The hose to inflation device connector is a threaded anodized aluminum fitting with a stainless steel ferrule. The gas hose construction provides resistance to wear and tear and provides safeguards preventing in-service tampering (ref.2C).•Activation circuit consists of a magnetically-activated reed switch and durable magnet mounted onto the end-release buckle assembly. The circuit conductors are strain-relieved, 20-gauge, copper-stranded cables with aerospace-specification connectors (ref. 2D). •Igniter Connector connects the activation circuit to the inflation device’s electrically activated igniter.Rev. NCFigure 2 – Seatbelt Airbag Features• Standard push-button type release mechanism (ref. 2A).• The End-Release Buckle Assembly contains magnet and a reed switch to passively closeactivation circuit. (ref. 2A and 2D).No belt extender is allowed with the AAIR V23 System.The system does not contain sharp or hard surfaces that could cause injury to occupants during normal operation, during a crash, or in secondary impacts. The following design features remove hard points or sharp edges from interfacing with the occupant:• Deployment gas ducted from behind-seat area removes inflation devices from occupantvicinity.• The airbag, belt, and protective cover do not contain any hard points or sharp edges.3.3 INFLATOR ASSEMBLYThe Inflator Assembly is mounted behind each seat position and provides the gas source to inflate the airbag upon command from the EMA. The Inflator Assembly has adhesive labels with appropriate product and shipping information. The Inflator Assembly and its electrical connection are standard automotive components produced and used in high volume with extremely high reliability and safe operation. The Inflator Assembly contains special features for safety and tamper resistance. Reference Figures 3 and 4.The Inflator Assembly components and their special features are listed below:• The inflation device is a stored gas, single-stage, blow-down type using only non-heatedinert helium gas to fill the airbag (ref. 3A).• The inflation device uses a shielded, electrically activated igniter to burst a stainless steelmembrane to release the gas to fill the airbag (ref. 3B). The igniter uses a self-shunting pin clip to automatically safe the Inflator Assembly when the igniter connector is removed. Cover with Airbag folded inside D B A Standard webbing and anchormechanism for three-point seatbelt Retractor DeviceE CRev. NC• The inflation device is a cylindrical, extruded steel, pressure vessel with welded end capsand a welded membrane. Helium gas is contained at a nominal pressure of 6,250 psig. The low carbon alloy steel vessel and all manufacturing processes are specially developed and controlled for high reliability and long-life gas storage (less than 5% gas loss over 15 years). Design values and verification testing are conducted using industry recognized statistical methods. The factors of safety for the pressure vessel are 2.7 at the maximum expected operating pressure and 3.1 at ambient temperature. The Inflator Assembly meets DOT Class 9 and UN3268 requirements for compressed, non-flammable gas devices (ref. 3A).• The inflation device and igniter have independent automatic gas release mechanisms thatare temperature activated (~ +210°C) to protect from vessel fragmentation in the event of prolonged exposure to fire (not shown).• The gas is released from the Inflator through a machined fitting assembly which isconnected to the Inflator via a threaded attachment. It is connected to the gas hose by a threaded end on the fitting (ref. 3C).Figure 3 – Inflator Assembly Features• The Inflator Assembly Igniter Connector (type FCI ABX-3) is attached to the SAA’s activationcircuit by a separate wire cable leg of the End-Release Buckle Assembly (ref. 4A).Inflation Device Body Inflator Fitting Assy and Gas Hose Connection Point A IgniterRev. NCIgniter ConnectorAFigure 4 – Inflation Igniter Connector3.4 ELECTRONICS MODULE ASSEMBLYThe Electronics Module Assembly (EMA) is a plastic box mounted to the aircraft structure on the floor. One EMA is mounted to aircraft floor for each pilot/copilot seat assembly. The EMA enclosure is designed to resist moisture and contamination and can withstand electrostatic discharge. The EMA contains crash sensors, electrical circuits, power, and connectors to service one pilot/copilot seat assembly. Reference Figures 5 and 6 for EMA and AAIR V23 System schematic, respectively.The EMA components and their special features are listed below:•The crash sensors are a spring-mass-damper type inertial switch used in high volume in automotive airbag sensor systems, but calibrated specifically for an aircraft’s operating environment. Proper deployment of the AAIR requires it to deploy at a predetermined threshold. This threshold allows enough time for proper airbag fill, but will not allow inadvertent deployment during normal operations. Below the activation threshold, the AAIR System functions as a conventional seatbelt.•Power is provided by two non-rechargeable, lithium cells with a fused thermal protection circuit. This arrangement precludes short circuits or other failures causing the batteries to release electrolyte or energy into the system in an uncontrolled manner. The system operates nominally at 7.2 VDC, and can maintain functional capability down toRev. NC approximately 7 VDC. The long-life, lithium/thionyl chloride battery system has stand-by capability of 10 years at room temperature.•The electrical connectors have 20-gauge pins and a mistake proof, keyed interface.•The “pigtail” cable consists of 20-gauge, copper-stranded insulated conductors with a woven protective wrap.The EMA assembly has a total mass of approximately .85 pounds. The housing is fabricated from ABS plastic which is lightweight, durable, and rugged. The housing is made up of a body and a lid with the lid held to the body using four machine screws. The internal components consist of a printed circuit board (PCB) onto which are attached the sensors. The battery pack (complete with capacitors and fuse) is connected to the PCB.Under an inertial load of 9g, the internal components could exert a maximum combined force of 5 lbs on the EMA housing, far below the rated capability of the housing or the fasteners including a factor of safety of 1.5. Under extremely severe circumstances, should the internalRev. NC3.5 CABLE INTERFACE ASSEMBLYThe Cable Interface Assembly consists of a connector that interfaces to the EMA pigtail connector on one side and the SAA connector on the other. A Diagnostic Tool Connector leg branches from the EMA connection leg. This diagnostics connector mates with the connector on the System Diagnostic Tool to allow functional testing of the AAIR V23 System. This cable is independent and routed separately from all other aircraft wiring (ref. Figure 7).The connectors have 20-gauge pins and a mistake proof, keyed interface. The cable is 20-gauge, copper-stranded insulated conductors with a woven protective wrap.Diagnostic ToolConnectorEMA ConnectorSAA ConnectorsFigure 7 – EMA with Cable Interface AssemblyRev. NC3.6SYSTEM DIAGNOSTIC TOOLA System Diagnostic Tool (SDT) is used to check the functional status of the AAIR. This small, portable, hand-held device has been designed for use by maintenance personnel at intervals predetermined by the AAIR System Safety Assessment, E508436. The SDT has a connector on the end of a short length of cable and a set of red/green/amber indicator lights. The connector plugs into the Diagnostic Tool Connector on the Electrical Interface Cable. The SDT provides readouts for proper and improper function for the seat position. The SDT has a built-in power supply that does not drain the AAIR battery. The SDT battery is replaceable by the user with a standard, commercially available, 9-volt battery. Figure 8 provides an illustration of the SDT.Figure 8 – V23 System Diagnostic ToolON/OFF SwitchSDT Battery LED SEAT LEDsRev. NC4.0 AAIR V23 SYSTEM OPERATIONThe AAIR V23 System requires no intervention during normal operation. The AAIR is active (able to deploy) upon buckling the seatbelt by the seat occupant and deactivated upon release of the same. The two functional states, active and inactive, both occur in the normal AAIR operational mode. The system has another non-functional, fundamental mode of operation, the diagnostic mode. This mode occurs when the SDT is connected and the system is undergoing a diagnostic test.OPERATION4.1 NORMALThe AAIR System is fully operational and considered “active” when properly installed and buckled. When buckled, the activation switch closes, completing its portion of the deployment circuit. This will allow the system to deploy upon closure of the sensor switch. When active, the AAIR is designed to protect the pilot/copilot occupants seated in the cockpit during emergency landing conditions. Proper deployment of the AAIR requires it to deploy at a predetermined deceleration level, known as the activation point. This is a point in the beginning of a crash that allows enough time for proper airbag fill. Impacts below the activation point will not cause deployment and the system functions as a conventional three-point seatbelt. Decelerations equal to or above the activation point will cause the EMA to sense the crash and initiate the firing sequence and deploy the system as previously described.The inflated airbag acts as a cushion to decelerate the head and torso of the occupant. The kinetic energy of the seat occupant is dissipated on impact with the airbag. The airbag accommodates a range of occupant sizes, and the total time period for inflation and deflation of the airbag poses no hazard to egress.The AAIR System operates within all aspects of the flight envelop environment.OPERATION4.2 DIAGNOSTICSThe system diagnostic check is conducted at pre-determined intervals. This interval must be determined such that the resulting system reliability calculated from the System Safety Assessment (reference AMSAFE document E508436) meets regulatory requirements (FAA AC 23.1309).Maintenance personnel perform the diagnostics check by using a hand-held SDT. First, the seatbelt is buckled to close the circuit and activate the system. Second, the protective cap covering the Diagnostics Tool Connector is removed. Third, the SDT is connected to the Diagnostics Tool Connector and the diagnostics check is performed. Indicators on the SDT provide system status for the seat position’s circuit.。

北京动向体育发展有限公司安全接入与双因素身份认证系统建议解决方案目录第一章现状分析第二章待解决的问题第三章技术方案－VPN安全接入第四章技术方案－双因素身份验证第五章整体设计规划与解决方案第六章产品选型第七章供应商选择第八章实施方案第九章产品报价第十章产品测试安全接入解决方案现状分析●所有业务应用直接开放端口暴露在公网上；●每增加一个业务系统就需要新购买一个域名和一个公网IP地址；●所有数据在传输过程中都是明文，因此容易被截获或者篡改；●对业务系统的登陆验证过于简单，容易被暴力破解；待解决的问题●所有业务系统全部隐藏到安全接入设备之后，不直接暴露在公网上；●在数据传输过程中对数据进行加密封装处理；●对业务系统的权限采用双因素身份验证，加强业务系统的身份验证强度；技术方案第一代IPSEC VPN●第一代VPN目前的应用范围主要是site-to-site端点到端点的网络环境中，部署IPSec需要对网络基础设施进行重大改造，花费的人力物力甚巨，同时IPSec VPN在解决远程安全访问时有几个比较大的缺点:安全性低●无法定位每个用户目前使用资源的情况●需要与网络设备互动控制访问资源●最终端没有安全性检查●无法清楚访问痕迹可用性差●需要当地网络环境允许使用才行维护费用高●客户端配置非常复杂●需要专人维护第二代SSL VPN第二代VPN采用的是SSL协议，与IPSec VPN相比，SSL VPN具有如下优点：●SSL瘦身客户端，支持自动安装；●不需要修改网络设备的配置信息；●支持客户端安全性检查●设备本地访问策略控制第二代VPN采用的是SSL协议，与IPSec VPN相比，SSL VPN具有如下缺点：●性能远比不上ipsec vpn●瘦身客户端导致身份验证过于简单第三代SSL VPN-Plus为了从根本上解决SSL VPN性能瓶颈，以新安捷（NeoAccel,INC）为代表的专业安全接入厂商，凭借强大的研发实力，经过刻苦的攻关，终于研制出了新一代SSL VPN构架——SSL VPN-Plus。

KeySafetyV8.0产品手册国瑞信安终端安全登录与监控审计系统产品手册Version 8.0江苏国瑞信安科技有限公司国瑞信安（北京）科技有限公司KeySafetyV8.0产品手册版权声明非常感谢您使用国瑞信安（北京）科技有限公司的安全产品，我们将竭诚为您的终端信息安全提供全面的服务。

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本手册所介绍的TM KeySafety TM产品是由国瑞信安（北京）科技有限公司自主开发的信息安全产品，其版权受中华人民共和国版权法保护。

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国瑞信安（北京）科技有限公司江苏国瑞信安科技有限公司2016年4月目录第一部分KeySafety产品总体介绍 (3)1.1系统总体介绍 (3)第二部分KeySafety单机版产品安装 (4)2.1KeySafety的应用环境 (4)2.2系统安装软硬件需求 (4)2.3安装前准备 (4)2.4KeySafety产品安装步骤 (5)2.4.1 32位Windows XP/Windows 7系统安装步骤 (5)2.4.3 Windows 7 64位系统安装步骤 (11)2.4.4 主机审计单机无Key版（支持XP32位、Win 7 32/64位）安装 (19)第三部分KeySafety单机版产品使用 (23)3.1 系统登录 (23)3.2 KeySafety用户管理中心 (24)3.2.1增加系统用户 (24)3.2.2修改系统用户 (25)3.2.3删除系统用户 (25)3.2.4查看用户信息 (25)3.3 管理平台使用 (26)3.3.1安全保密员 (26)3.3.1.1用户权限设置 (27)3.3.1.2 RierSecDisk初始化（标准版不带此功能） (29)3.3.1.3介质加载（标准版不带此功能） (30)3.3.1.4主机授权中心 (30)3.3.1.5审计管理中心 (31)3.3.1.6资源使用 (32)3.3.1.7 锁屏机制 (32)3.3.2 系统管理员 (33)3.3.3安全审计员 (35)3.4光盘刻录工具使用说明 (36)3.4.1 光盘刻录工具主界面简介 (36)3.4.2 光盘刻录工具主界面简介 (39)3.4.3刻录安全光盘 (40)3.4.4刻录镜像文件到光盘 (41)3.4.5刻录音乐光盘 (42)3.4.6刻录mp3光盘 (43)3.4.7刻录VCD光盘 (44)3.4.8刻录DVD影碟 (45)第四部分产品卸载 (46)第一部分KeySafety产品总体介绍1.1系统总体介绍KeySafetyV8.0产品是国瑞信安(北京)科技有限公司针对网络信息系统开发的内部网络信息防泄密系统，该系统从多方面入手，解决网络中信息泄密的安全性问题。

目录动环FSU门禁安装调测说明 (2)前言 (2)一、接线说明 (2)高新兴接线说明 (2)邦讯接线说明 (3)中兴力维接线说明 (5)艾默生接线说明 (6)二、调试说明 (7)平台增加非智能门禁 (10)高新兴调试说明 (11)邦讯调试说明 (13)中兴力维调试说明 (15)艾默生调试说明 (19)三、功能验证 (20)远程开门验证 (21)门磁、锁舌告警验证 (22)动环FSU门禁安装调测说明前言铁塔门禁设备正确连接调试后，可以在运维监控系统“”实现平台远程开门、门磁告警上报、锁舌告警上报。

一、接线说明高新兴接线说明第一套门锁：门磁1接上排接线端子的IN12通道和GND，锁舌1接IN21和GND，门锁供电接上排接线端子的12V和GND，门锁1DO控制分别接DO3公共，DO3常开串一根线到GND。

第二套门锁：门磁2接上排接线端子的IN13通道和GND，锁舌2接IN22和GND，门锁供电接上排接线端子的12V和GND（IN21通道前的12V），第2套门锁的DO控制分别接DO4公共，DO4常开串一根线到GND。

邦讯接线说明设备左下角的“DC12V输出”为FSU的12V电源输出端，左脚为+、右脚为-，如下图：设备水印上标注的门磁1对应FSU的DI-11通道，设备水印上标注的门磁2对应FSU的DI-12通道，如下图：1设备接线定义门锁电源线：门锁的电源正、负极分别接入FSU12V输出端的正、负极；第一把锁：1、门磁：门磁的两根线，第一把门锁：低电平接入DI-9左侧的GND，高电平接入DI-11通道；2、锁舌：锁舌的两根线，第一把门锁：低电平接入DI-9左侧的GND，高电平接入DI-12通道；3、门锁控制：第一把门锁控制线接入DO-3的NC(常闭)端口，再从DO-3的com(公共)端口接入一根线到FSU12V输出端的负极；第二把锁：门磁：第二把门锁：低电平接入DI-9左侧的GND，高电平接入DI-13通道锁舌：第二把门锁：低电平接入DI-9左侧的GND，高电平接入DI-14通道；门锁控制：第二把门锁控制线接入DO-4的NC(常闭)端口，再从DO-4的com(公共)端口接入一根线到FSU12V输出端的负极。

银安二代证系统终端API使用手册(验证API)银安-二代证系统终端api使用手册(验证api)第二代证书系统终端API用户手册内蒙古银安科技开发有限公司第二代证书系统终端API用户手册1.前言............................................................................ ...............................................................22.系统要求............................................................................ ..................................................23.api列表............................................................................ ...................................................24.api详细说明............................................................................ (3)4.1端口API三4.2sam类api........................................................................... .. (5)4.2.1sdt重置SAM。

54.2.2sdt_uSAMStatus。

64.2.3sdt_uGetsamid。

64.3.4sdt uuSamidToStr。

七4.3身份证卡类api........................................................................... (7)4.3.1sdt开始指示牌。

用户指南安装使用前请仔阅读本说明书目录引言产品外观系统功能主要参数安装接线基本操作联网设置故障检修原装附件软件安装门禁软件考勤软件一、引言：感谢您使用本非接触式感应卡门禁考勤管理系统，在使用本系统之前，请您详细阅读本用户指南，并严格按照手册中的要求来操作。

此用户指南将介绍本系统主要功能及操作使用方法。

本门禁系统采用目前世界上先进的技术-非接触式感应卡技术（也称射频识别卡（RFID）技术，RFID卡具有全球卡号唯一、不易仿制的读写特性和安全性能。

RFID卡片不会产生使用磁卡时因磁头磨损、磁粉脱落、灰尘等影响所带来的麻烦，而且避免了接触式IC卡因芯片与读卡器外露而引起的沾污、接触不良和外物损伤而导致的读卡不良现象，RFID卡适应各种环境，经久耐用。

每一次感应卡读的信息，无论是否向电锁发出开锁指令，系统都自动记录下来，管理者可以通过计算机下载调阅门禁控制系统存储的信息资料，轻松查阅、打印所有的通行事件。

管理软件将根据此原始资料自动统计员工考勤情况、编制考勤报表。

本系统提供了一种智能化的出入口控制及考勤管理方式，适用于需要控制人员出入的通道、商务机构、政府机关、住宅小区等等。

二、产品外观：数字键门铃按钮电源指示灯开门指示灯通讯指示灯三、系统功能：1、存储容量达8000条通行记录，1000张用户卡及密码2、每天自由设定八个限制通行时段3、具备读卡开门、读卡加密码开门、读卡或密码开门三种方式4、内置、外接读卡器，可实时区分进入、外出人次数5、采用RS485总线联网通讯方式，布线简易实用，最多可联网16台6、主要输入/输出功能：电锁、开门按钮、报警器、门磁、门铃7、管理软件集门禁、考勤、人事于一体8、管理软件界面人性化，操作简易，使用方便9、系统图示可导入电子地图，自由设定门的名称、位置10、实时显示通过人员的姓名、相片、卡号、编号等资料11、自定义考勤规则及班次设定等12、自动统计迟到、早退、缺勤的次数及时间13、考勤结果可打印成报表或按Excel导出四、主要参数：五、安装接线：1、接口插座示意图：警告：安装接线时切记先断开电源，确认接线无误后再接通电源！！2、颜色识别接线示意图外接读卡器：系统自动识别外接读卡器读卡为进门，内置读卡器读卡为出门。