An aircraft landing gear assembly comprising an oleo-pneumatic shock absorber 50 comprising an outer cylinder 52 and sliding tube 54 movable between a compressed position and an extended position, further comprising a sprung element 71 coupled to the shock absorber 50, movable between a spaced position and an engaged position, and further comprising a weight-on-wheels sensor (62, 64, 66) arranged to monitor movement of the sprung element 71 from the spaced position to the engaged position against spring 68.


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    Title :

    Aircraft landing gear assembly


    Contributors:
    IAN BENNETT (author)

    Publication date :

    2024-12-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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