The invention relates to an engine mounting section accessory. Accessory for mounting an engine to an aircraft wing. The fitting includes a body having a first end and a second end. A first pocket is located at the first end, wherein the first pocket is sized to receive a front engine mount assembly. A second pocket is located at the second end, wherein the second pocket is sized to receive a strut of an aircraft wing. The body includes a first section and a second section connected together.

    本发明的名称为发动机安装节配件。将发动机安装到航空器机翼上的配件。配件包括具有第一端和第二端的主体。第一袋区位于第一端,其中第一袋区被设定尺寸以接收前发动机安装节配件。第二袋区位于第二端,其中第二袋区被设定尺寸以接收航空器机翼的支柱。主体包括连接在一起的第一区段和第二区段。


    Access

    Download


    Export, share and cite



    Title :

    Engine mounting joint accessory


    Additional title:

    发动机安装节配件


    Contributors:

    Publication date :

    2025-03-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT





    Accessory mounting for a gas turbine engine

    BEIER JÜRGEN / VENTER GIDEON DANIEL | European Patent Office | 2019

    Free access

    ACCESSORY MOUNTING FOR A GAS TURBINE ENGINE

    BEIER JÜRGEN / VENTER GIDEON DANIEL | European Patent Office | 2017

    Free access

    Accessory mounting for a gas turbine engine

    BEIER JÜRGEN / VENTER GIDEON DANIEL | European Patent Office | 2017

    Free access