The invention relates to a mechanism for limiting the motion of a wing flap. The mechanism comprises a limit wheel support (1), a first bearing set (2), a circlip set (3) for holes, a working shaft (4), a second bearing set (5), a small shaft set (6), a stopper screw set (7), a flat head shaft set (8), a third bearing set (9) and a split pin set (10). Through the change of the value of a gap between upper and lower limit mechanisms at the connecting position of two sliding rails, and a web surface of one sliding rail, the situation that the space motion of the wing flap performs along a designed limit track is guaranteed, the motion of the wing flap in the other directions is simultaneously limited, and the situation that the wing flap cannot be stuck during the motion is guaranteed.


    Access

    Download


    Export, share and cite



    Title :

    Mechanism for limiting motion of wing flap


    Contributors:
    CHEN YULI (author) / XU LANBO (author) / GAO WANCHUN (author) / LIU YONGSHENG (author)

    Publication date :

    2015-04-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Flap support assembly for wing comprising flap and wing comprising flap

    YANG GUIQIANG / DONG MENG / LIU XIANGYUN | European Patent Office | 2023

    Free access

    Dynamic Wing Airloads with Higher Harmonic Flap Motion

    Gerontakos, P. | Online Contents | 2007


    Dynamic Wing Airloads with Higher Harmonic Flap Motion

    Tim Lee / P. Gerontakos | AIAA | 2007


    SYSTEM AND METHOD FOR CONTROLLING AIRCRAFT WING FLAP MOTION

    MICHAEL RAYMOND FINN / PATRICK MCCORMICK / GEORGE MOY et al. | European Patent Office | 2017

    Free access

    SYSTEM AND METHOD FOR CONTROLLING AIRCRAFT WING FLAP MOTION

    FINN MICHAEL RAYMOND / MCCORMICK PATRICK / MOY GEORGE et al. | European Patent Office | 2017

    Free access