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Process management architecture braking system to brake equipped with electromechanical actuators, and architecture for application aircraft.

机译:用于配备机电致动器的制动过程管理体系结构制动系统,以及应用飞机的体系结构。

摘要

Process management architecture braking system equipped brake electromechanical actuators (EMA), of which certain actuators are connected to a battery assembly (Batt) of the airplane and other actuators aircraft are not connected to the battery assembly (Bat) of the aircraft, wherein the method comprises the step of operating at least one actuator unbound to the battery assembly (Batt) to give exert an equal effort unit holding force tending to maintain the fixed point of the aircraft It is determined independently of a braking request of the pilot.
机译:配备有过程管理架构制动系统的制动机电致动器(EMA),其中某些致动器连接到飞机的电池组件(Batt),飞机上的其他致动器未连接到飞机的电池组件(Bat),其中该方法包括以下步骤:操作至少一个未与电池组件(Batt)绑定的致动器,以施加趋于保持飞机固定点的相等作用力的单元保持力。该确定与飞行员的制动请求无关。

著录项

  • 公开/公告号ES2298700T3

    专利类型

  • 公开/公告日2008-05-16

    原文格式PDF

  • 申请/专利权人 MESSIER-BUGATTI;

    申请/专利号ES20040292732T

  • 发明设计人 DELLAC STEPHANE;SIBRE JEROME;GIROD PIERRE;

    申请日2004-11-18

  • 分类号B60T8;B60T8/17;B60T8/32;B60T13/74;

  • 国家 ES

  • 入库时间 2022-08-21 20:04:14

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