To provide a support structure to attach landing gear to a wing spar of an aircraft.SOLUTION: The support structure includes a trunnion assembly having a first trunnion and a second trunnion that are connected together with the first trunnion positioned on a first side of the wing spar and the second trunnion positioned on an opposite second side of the wing spar. The trunnion assembly is configured to support a first section of the landing gear.SELECTED DRAWING: Figure 1

    【課題】着陸装置を航空機の翼桁に取り付けるための支持構造を提供すること。【解決手段】支持構造は、第1のトラニオンと第2のトラニオンとを有し、第1のトラニオンは翼桁の第1の側に配置され、第2のトラニオンは翼桁の対向する第2の側に配置されて一緒に接続されるトラニオンアセンブリを含む。トラニオンアセンブリは、着陸装置の第1の部分を支持するように構成されている。【選択図】図1


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    Title :

    SUPPORT STRUCTURE FOR AIRCRAFT LANDING GEAR


    Additional title:

    航空機着陸装置のための支持構造


    Contributors:

    Publication date :

    2022-10-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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