A landing gear assembly is provided. The landing gear assembly includes a shock strut. The shock strut includes a shock strut cylinder (204) and a shock strut piston slidably disposed within the shock strut cylinder (204). The landing gear assembly further includes a temperature control unit assembly (250) disposed within the shock strut cylinder (204). The temperature control unit assembly (250) is configured to, responsive to a temperature within the shock strut cylinder (204) falling below a predetermined temperature, circulate heated fluid into a chamber of the shock strut cylinder (204) to heat gas within the shock strut cylinder (204).


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    Title :

    TEMPERATURE COMPENSATED LANDING GEAR SHOCK STRUT


    Additional title:

    TEMPERATURKOMPENSIERTER FAHRWERKFEDERBEIN
    JAMBE DE AMORTISSEUR DE TRAIN D'ATTERRISSAGE À COMPENSATION DE TEMPÉRATURE


    Contributors:

    Publication date :

    2025-01-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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