A landing gear arrangement (30) may comprise a shock strut (32), a retraction actuator (10), and a shrink actuator (20). The retraction actuator (10) may move the shock strut (32) between a stowed position and a deployed position. The shrink actuator (20) may move between a shrink position and an unshrink position in response to the shock strut (32) moving between the stowed position and the deployed position.


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    Title :

    LANDING GEAR ARRANGEMENT WITH PASSIVE SHOCK STRUT SHRINK ACTUATOR


    Additional title:

    FAHRWERKANORDNUNG MIT PASSIVEM FEDERBEIN-SCHRUMPFSTELLGLIED
    AGENCEMENT DE TRAIN D'ATTERRISSAGE AVEC ACTIONNEUR RÉTRÉCISSABLE JAMBE À AMORTISSEUR PASSIF


    Contributors:

    Publication date :

    2020-05-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn



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