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 coupled to the shock absorber, 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 from the spaced position to the engaged position.

    L'invention concerne un ensemble train d'atterrissage d'aéronef comprenant un amortisseur oléo-pneumatique (50) comportant un cylindre externe (52) et un tube coulissant (54) mobile entre une position comprimée et une position étendue, comprenant en outre un élément suspendu couplé à l'amortisseur, mobile entre une position espacée et une position en prise, et comprenant en outre un capteur de poids sur roues (62, 64, 66) conçu pour surveiller le mouvement de l'élément suspendu de la position espacée à la position en prise.


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    Title :

    AIRCRAFT LANDING GEAR ASSEMBLY


    Additional title:

    ENSEMBLE TRAIN D'ATTERRISSAGE D'AÉRONEF


    Contributors:
    BENNETT IAN (author)

    Publication date :

    2024-02-08


    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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