A method for actuating a landing gear arrangement may include supplying a first pressure to an actuator, applying, by the actuator, a moment on a latch to rotate the latch in a first rotational direction, disengaging a first roller pin, engaging a stopper on a link, rotating the link in the first rotational direction about a pivot, the link coupled between a trailing arm and a shock strut, rotating the shock strut about a second end of the shock strut, rotating the trailing arm about a first end, and engaging a second roller pin.


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    Title :

    Retractable landing gear


    Contributors:

    Publication date :

    2019-03-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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