The invention relates to a system and method for detecting flap jamming of an aircraft wing. There is provided a jam detection system for a flap of a wing of an aircraft, the jam detection system comprising: a linkage coupled to the flap and a support of the wing; and a sensor configured to detect a position of at least a portion of the linkage mechanism. The sensor is further configured to compare the position of the at least a portion of the linkage to a jamming threshold to determine if a jamming condition exists. The linkage may also be coupled to a carriage movably coupled to the support.

    本发明涉及用于检测飞行器机翼的襟翼卡住的系统和方法。提供了一种用于飞行器的机翼的襟翼的卡住检测系统,该卡住检测系统包括:连杆机构,该连杆机构联接至襟翼和机翼的支承件;以及传感器,该传感器被配置成检测连杆机构的至少一部分的位置。传感器还被配置成,将连杆机构的所述至少一部分的位置与卡住阈值进行比较,以确定是否存在卡住状况。连杆机构还可以联接至滑架,滑架可移动地联接至支承件。


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    Titel :

    System and method for detecting flap jamming of aircraft wing


    Weitere Titelangaben:

    用于检测飞行器机翼的襟翼卡住的系统和方法


    Beteiligte:
    BLOCK STEVEN L (Autor:in) / BOWERS BENJAMIN A (Autor:in) / TSAI KEVIN R (Autor:in)

    Erscheinungsdatum :

    2023-05-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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