The invention relates to a distributed trailing edge flap control system. The distributed trailing edge flap control system comprises a plurality of flaps; the flap and slat control handle is used for a pilot to manually input an expected flap position instruction; the flap and slat electronic control device is used for controlling the position of a flap in a distributed manner according to brake control logic or starting a flap brake device when a flap fault is detected; the flap rotation actuation driving device is used for driving a corresponding flap to a specified position according to an instruction from the flap and slat electronic control device; the flap brake device is used for locking a corresponding flap according to a locking instruction from the flap and slat electronic control device; the flap position sensor is used for feeding back detected flap position data to the flap and slat electronic control device; and the transmission line system component is used for transmitting the torque of the flap rotation actuation driving device to the flap rotation actuation driving device.

    本申请涉及一种分布式后缘襟翼控制系统,包括:多块襟翼;供飞行员手动输入期望的襟翼位置指令的襟缝翼控制手柄;襟缝翼电子控制装置,用于根据刹车控制逻辑来分布式控制襟翼的位置或在探测到襟翼故障时,启动襟翼刹车装置;襟翼旋转作动驱动装置,用于根据来自襟缝翼电子控制装置的指令驱动相应襟翼至指定位置;襟翼刹车装置,用于根据来自襟缝翼电子控制装置的锁止指令,锁止对应的襟翼;襟翼位置传感器用于将检测到的襟翼的位置数据反馈给襟缝翼电子控制装置;传动线系部件,用于将襟翼旋转作动驱动装置的扭矩传递到襟翼旋转作动驱动装置。


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    Titel :

    Distributed trailing edge flap control system


    Weitere Titelangaben:

    一种分布式后缘襟翼控制系统


    Beteiligte:
    XU QING (Autor:in) / LIU YANSHENG (Autor:in) / CAO JUNZHANG (Autor:in)

    Erscheinungsdatum :

    26.01.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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