A flap and slat system can still reliably and efficiently detect the wing surface state of an airplane under the condition that a position sensor breaks down. The flap and slat system at least comprises two flap and slat electronic control devices, and one or two position sensors and four inclination sensors, which are arranged on flaps on each side of a left wing and a right wing of the airplanerespectively, namely, two or four position sensors and eight inclination sensors are arranged in total; and the two flap and slat electronic control devices communicate with each other through a CAN bus, and the position sensors are used for detecting the asymmetry of the wing surfaces of the left side wing and the right side wing, and when any one or more of the two or four position sensors breakdown, the inclination sensors are used for replacing the position sensors to detect the asymmetry of the wing surfaces of the left side wing and the right side wing.

    一种襟缝翼系统,能在位置传感器发生故障的情况下,依然可靠并且高效地对飞机的翼面状态进行检测。所述襟缝翼系统至少包括两个襟缝翼电子控制装置以及在飞机的左右侧机翼的每一侧的襟翼上分别设置的一个或两个位置传感器和四个倾斜传感器,即共计两个或四个位置传感器和八个倾斜传感器,两台襟缝翼电子控制装置之间通过CAN总线进行通信,利用所述位置传感器对左右侧机翼的翼面非对称进行检测,其中,在两个或四个所述位置传感器中的任一个或多个发生故障时,利用所述倾斜传感器接替所述位置传感器,对左右侧机翼的翼面非对称进行检测。


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    Title :

    Flap and slat system


    Additional title:

    襟缝翼系统


    Contributors:
    WANG WEIDA (author) / WANG XIAOYI (author) / LIU JINTAO (author) / YANG ZHIDAN (author) / XU DONGGUANG (author)

    Publication date :

    2020-07-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64C AEROPLANES , Flugzeuge



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