A support structure (10) to mount landing gear (90) to a wing spar (104) of an aircraft. The support structure includes a trunnion assembly (18) having a first trunnion (20) and a second trunnion (30) that are connected together with the first trunnion positioned on a first side of the wing spar and a second trunnion positioned on an opposing second side of the wing spar. The trunnion assembly is configured to support a first section of the landing gear.


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    Title :

    SUPPORT STRUCTURE FOR AN AIRCRAFT LANDING GEAR


    Additional title:

    TRAGSTRUKTUR FÜR EIN FLUGZEUGFAHRWERK
    STRUCTURE DE SUPPORT POUR UN TRAIN D'ATTERRISSAGE D'AÉRONEF


    Contributors:

    Publication date :

    2022-09-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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