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    • 1. 发明申请
    • AUTOMATED TEST MANAGEMENT SYSTEM FOR ELECTRONIC CONTROL MODULE
    • 电子控制模块自动测试管理系统
    • US20140354321A1
    • 2014-12-04
    • US14459413
    • 2014-08-14
    • Caterpillar Inc.
    • Rajeev V. KumarAmanda J. WilkeAdam R. Long
    • G01R31/28G01R1/04
    • G05B19/042G01R1/0416G01R31/007G05B2219/21115G05B2219/24036
    • An automatable management system for testing one or more electronic control modules (ECMs), in one or more machines, is disclosed. The one or more ECMs are switchably connected to a testing unit (TU). The system includes at least one ECM connector, connectable to the one or more ECMs. The at least one ECM connector is one of a male connector or a female connector. Similarly, the system includes at least one TU connector connectable with the TU. Further, at least one actuator is operably connectable to at least one of the at least one ECM connector and the at least one TU connector. The actuator is configured to facilitate an electrical connection between the ECM and the testing unit in response to a relay signal generated by the testing unit.
    • 公开了一种用于在一个或多个机器中测试一个或多个电子控制模块(ECM)的自动化管理系统。 一个或多个ECM可切换地连接到测试单元(TU)。 该系统包括可连接到一个或多个ECM的至少一个ECM连接器。 至少一个ECM连接器是公连接器或母连接器之一。 类似地,该系统包括可与TU连接的至少一个TU连接器。 此外,至少一个致动器可操作地连接到至少一个ECM连接器和至少一个TU连接器中的至少一个。 致动器被配置为响应于由测试单元产生的继电器信号,促进ECM与测试单元之间的电连接。
    • 2. 发明申请
    • METHOD AND APPARATUS FOR TESTING VALVE CONTROL SYSTEM
    • 用于测试阀门控制系统的方法和装置
    • US20110208442A1
    • 2011-08-25
    • US12745251
    • 2007-11-29
    • Jürgen Lohmann
    • Jürgen Lohmann
    • G06F19/00
    • G05B19/0428F16K37/0083G05B17/00G05B19/056G05B23/0256G05B2219/24036G05B2219/24038
    • The present invention provides a method and apparatus for testing a valve control system in an aircraft fuel supply system having a plurality of control valves, wherein the control system includes a processor adapted to receive feedback signals from each of the plurality of control valves, the method comprising the steps of: connecting a test device to the control system such that the test device is connected for signal transmission to the processor; outputting a signal to the processor simulating a feedback signal from at least one of the control valves; detecting a control signal which is output by the processor to the at least one of the control valves; and identifying the detected control signal which is output by the processor to the control valve.
    • 本发明提供了一种用于测试具有多个控制阀的飞行器燃料供应系统中的阀控制系统的方法和装置,其中控制系统包括适于接收来自多个控制阀中的每一个的反馈信号的处理器,该方法 包括以下步骤:将测试设备连接到控制系统,使得测试设备被连接用于信号传输到处理器; 向所述处理器输出信号,所述处理器模拟来自所述控制阀中的至少一个的反馈信号; 检测由所述处理器输出到所述至少一个所述控制阀的控制信号; 并且将由处理器输出的检测到的控制信号识别到控制阀。
    • 3. 发明授权
    • Method and apparatus for testing valve control system
    • 阀门控制系统测试方法及装置
    • US08868354B2
    • 2014-10-21
    • US12745251
    • 2007-11-29
    • Jürgen Lohmann
    • Jürgen Lohmann
    • G01B5/00G05B23/02G05B19/042G05B17/00G05B19/05F16K37/00
    • G05B19/0428F16K37/0083G05B17/00G05B19/056G05B23/0256G05B2219/24036G05B2219/24038
    • The present invention provides a method and apparatus for testing a valve control system in an aircraft fuel supply system having a plurality of control valves, wherein the control system includes a processor adapted to receive feedback signals from each of the plurality of control valves, the method comprising the steps of: connecting a test device to the control system such that the test device is connected for signal transmission to the processor; outputting a signal to the processor simulating a feedback signal from at least one of the control valves; detecting a control signal which is output by the processor to the at least one of the control valves; and identifying the detected control signal which is output by the processor to the control valve.
    • 本发明提供了一种用于测试具有多个控制阀的飞行器燃料供应系统中的阀控制系统的方法和装置,其中控制系统包括适于接收来自多个控制阀中的每一个的反馈信号的处理器,该方法 包括以下步骤:将测试设备连接到控制系统,使得测试设备被连接用于信号传输到处理器; 向所述处理器输出信号,所述处理器模拟来自所述控制阀中的至少一个的反馈信号; 检测由所述处理器输出到所述至少一个所述控制阀的控制信号; 并且将由处理器输出的检测到的控制信号识别到控制阀。
    • 6. 发明授权
    • Electronic control unit including monitoring control circuit
    • 电子控制单元包括监控控制电路
    • US07107488B2
    • 2006-09-12
    • US10758003
    • 2004-01-16
    • Kohji HashimotoKatsuya Nakamoto
    • Kohji HashimotoKatsuya Nakamoto
    • G06F11/00
    • G05B19/0428G05B2219/24036G05B2219/24054G05B2219/24125
    • A microprocessor 20a controls an electrical load group 12 responsive to content of a non-volatile program memory 25a and operation state of an input sensor group 11. A monitoring control circuit section 30a sequentially transmits a large number of question items with an inquiry packet, and compares response content from the microprocessor 20a with correct answer information to carry out an error determination. The microprocessor 20a diagnoses an interval of receiving an inquiry packet to monitor in reverse the monitoring operation of the monitoring control circuit section 30a. Thus, in an electronic control unit having a microprocessor built-in, a monitoring control circuit is obtained that alternatively executes at regular intervals a part of control programs to carry out operation inspection during operation.
    • 微处理器20a响应于非易失性程序存储器25a的内容和输入传感器组11的操作状态来控制电负载组12.监视控制电路部分30a依次发送询问的问题项目 并且将来自微处理器20a的响应内容与正确的应答信息进行比较,以执行错误确定。 微处理器20a诊断接收查询分组的间隔,反过来监视监视控制电路部分30a的监视操作。 因此,在具有内置微处理器的电子控制单元中,获得监视控制电路,该监控控制电路交替执行控制程序的一部分,以在操作期间执行操作检查。