The invention provides an aeroengine mounting device which comprises a left mounting device and a right mounting device. The left mounting device is composed of a mounting base, a left thrust pin and a movable clamping band. The movable clamping band is connected with the mounting base through a pin and an eye bolt. One end of the left thrust pin has a cylindrical structure and is mounted between the mounting base and the movable clamping band, and the other end is a fork ear structure which is connected with the left joint of the aeroengine. The right mounting device is different from the left mounting device in that an eccentric bushing sleeves the cylindrical structure part of a right thrust pin. The aeroengine mounting device is advantageous in that the movable clamping band is connected with the eye bolt rotatably; convenient detachment is realized; quick detachment of the aeroengine from an aeroplane is realized; and high detachment-and-assembling maintainability of the aeroengine on a body is ensured.


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    Titel :

    Aeroengine mounting device


    Beteiligte:
    YE BIN (Autor:in) / LUO JINLIANG (Autor:in) / PENG ZHIJUN (Autor:in) / TENG CHUNMING (Autor:in) / WU QIANG (Autor:in) / ZHENG TIAN (Autor:in) / LONG SIHAI (Autor:in) / LI BIN (Autor:in) / WANG JINJIAN (Autor:in) / SHEN WENJING (Autor:in)

    Erscheinungsdatum :

    27.01.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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