An aircraft landing gear shock absorber assembly comprising: an outer cylinder (14) having a bore which extends into the outer cylinder, the bore defining an opening in the outer cylinder; a sliding tube (12) comprising a first end region slidably coupled within the bore and a second end region which projects out of opening; a ground fitting (28, 54) distinct from the sliding tube (12); and a mechanical fixing (30, 52) arranged to mechanically couple the ground fitting (28, 54) to the second end region of the sliding tube (12), wherein the sliding tube (12) comprises a tubular body portion (36) formed from a ceramic coated fibre composite tube.


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    Titel :

    AIRCRAFT LANDING GEAR SHOCK ABSORBER ASSEMBLY


    Weitere Titelangaben:

    FLUGZEUGFAHRWERKSTOSSDÄMPFERANORDNUNG
    ENSEMBLE AMORTISSEUR DE CHOCS DE TRAIN D'ATTERRISSAGE D'AVION


    Beteiligte:

    Erscheinungsdatum :

    26.01.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn



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