A support structure for an aircraft landing gear is used for mounting the landing gear to a support structure of a spar of an aircraft. 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 spar and the second trunnion positioned on an opposite second side of the spar. The trunnion assembly is configured to support a first section of the landing gear.

    一种用于飞机起落架的支撑结构,用于将起落架安装到飞机的翼梁的支撑结构。所述支撑结构包括耳轴组件,所述耳轴组件具有第一耳轴和第二耳轴,所述第一耳轴和所述第二耳轴连接在一起,其中所述第一耳轴定位在所述翼梁的第一侧上,所述第二耳轴定位在所述翼梁的相对的第二侧上。所述耳轴组件被配置为支撑所述起落架的第一区段。


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    Title :

    Support structure for aircraft landing gear


    Additional title:

    用于飞机起落架的支撑结构


    Contributors:

    Publication date :

    2022-09-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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