A torque link assembly (128) may comprise an upper torque link (130), a lower torque link (132), and a torque link pin (134). The upper torque link (130) may define an upper hydraulic fluid channel (200). The lower torque link (132) may define a lower hydraulic fluid channel (202). The torque link pin (134) may fluidly couple the upper hydraulic fluid channel (200) to the lower hydraulic fluid channel (202).


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    Title :

    LANDING GEAR WITH HYDRAULIC FLUID CHANNELS


    Additional title:

    FAHRWERK MIT HYDRAULIKFLÜSSIGKEITSKANÄLEN
    TRAIN D'ATTERRISSAGE AVEC CANAUX DE FLUIDE HYDRAULIQUE


    Contributors:

    Publication date :

    2022-11-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16L PIPES , Rohre



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