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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    Titel :

    TEMPERATURE COMPENSATED LANDING GEAR SHOCK STRUT


    Weitere Titelangaben:

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


    Beteiligte:
    M N HEMANTH (Autor:in) / BODKI BASAVARAJ (Autor:in)

    Erscheinungsdatum :

    22.01.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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