The invention belongs to the field of aviation flap driving control, and relates to a flap distributed driving system. The system is a distributed driving configuration in which power driving devicesare arranged on a transmission line system between the left inner and outer flaps and right inner and outer flaps; according to the configuration, a transmission line system for connecting left and right driving systems is canceled, and the number of the driving devices is reduced, and therefore, the number of parts of a high-lift system is decreased, and the configuration of the high-lift systemis simplified; the range of deflection angles between the inner flaps and the outer flaps is expanded through the distributed driving configuration; and only one power driving device is located at each airfoil; the transmission line system of each inner flap and the corresponding outer flap is not disconnected, so that the consistency of the movement of the inner flap and the outer flap of a single-side airfoil is ensured.

    本发明属于航空襟翼驱动控制领域,具体涉及一种襟翼分布式驱动系统。该系统为在左右内外襟翼之间的传输线系上各布置一个动力驱动装置的分布式驱动构型,该构型由于取消了连接左右驱动系统的传输线系和将驱动装置的数量减少,因此减少了高升力系统的部件数量,简化了高升力系统的构型。同时分布式驱动构型扩大了内外襟翼之间偏转角度的范围;每侧翼面的动力驱动装置减少到一个,同时本发明由于未将内外襟翼传输线系断开,因此确保了单侧翼面内外襟翼运动的一致性。


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    Titel :

    Flap distributed driving system


    Weitere Titelangaben:

    一种襟翼分布式驱动系统


    Beteiligte:
    KANG NING (Autor:in) / SHI YOUMIN (Autor:in)

    Erscheinungsdatum :

    11.08.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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