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; and a mechanical fixing (30, 52) arranged to mechanically couple the ground fitting to the second end region of the sliding tube, wherein the sliding tube comprises a tubular body portion formed from a ceramic coated fibre composite tube.


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    Titel :

    AIRCRAFT LANDING GEAR SHOCK ABSORBER ASSEMBLY


    Weitere Titelangaben:

    ENSEMBLE AMORTISSEUR POUR TRAIN D`ATTERRISSAGE D`AERONEF


    Beteiligte:

    Erscheinungsdatum :

    18.06.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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