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METHOD FOR CONTROLLING AN ELECTRIC BRAKING SYSTEM AND AIRCRAFT ELECTRIC BRAKING SYSTEM

机译:控制电制动系统的方法和飞机电制动系统

摘要

The method of electric braking system for flying aircraftIncludes a number of applicable electromechanical actuators (53)OneBraking force on friction organ Each actuatorIncludes one or more motors equipped with one or more motorscoil The braking system also includes at least one braking module.The power () is configured to be sent to each motor coilOneThe phase current () and at least one control module () are configured toIn response to the braking command (11 times), it is sent by the modulefromThe power of the set phase current determined by the powerfrombrake rigging The method also includes the variation of current.stageIt is transmitted to each coil of the motor to cause the motor to swingthisSets the phase current of the phase current.
机译:飞行器电制动系统的方法包括许多适用的机电执行器(53)一摩擦器官上的制动力每个执行器包括配备一台或多台电机的一台或多台电机制动系统还包括至少一个制动模块。电源()配置为发送到每个电机线圈一相电流()和至少一个控制模块()配置为响应制动命令(11次),由模块发送从设定相电流的功率由功率决定从刹车索具该方法还包括电流变化。阶段它被传输到电动机的每个线圈,从而导致电动机摆动这个设置相电流的相电流。

著录项

  • 公开/公告号CA3078353A1

    专利类型

  • 公开/公告日2020-11-06

    原文格式PDF

  • 申请/专利权人 SAFRAN LANDING SYSTEMS;

    申请/专利号CA20203078353

  • 发明设计人 FREY OLIVIER;

    申请日2020-04-20

  • 分类号B64C25/44;B60T8/17;H02P27;

  • 国家 CA

  • 入库时间 2022-08-21 11:14:30

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