A shock strut assembly (30, 32, 34) for a landing gear may comprise a strut cylinder (102), a strut piston (104) configured to telescope relative to the strut cylinder (102), and a locking system. The locking system may be configured to restrict rotation of the strut piston (104) relative to the strut cylinder (102) in response to compression of the shock strut assembly (30, 32, 34).


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    Title :

    SHOCK STRUT ASSEMBLIES FOR LANDING GEAR


    Additional title:

    FEDERBEINANORDNUNG FÜR EIN FAHRWERK
    ENSEMBLES JAMBES À AMORTISSEUR POUR TRAINS D'ATTERRISSAGE


    Contributors:

    Publication date :

    2022-08-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16F SPRINGS , Federn / B64C AEROPLANES , Flugzeuge



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