The invention discloses a flexible supporting device for an aircraft engine and a using method. According to the method, a flat parallel attitude adjusting structure is formed through a vertical three-direction attitude adjusting assembly and a horizontal three-direction attitude adjusting assembly, an aircraft engine can be driven to accurately move in the X, Y and Z directions and accurately rotate in the X, Y and Z directions in a narrow space, and accurate adjustment of the spatial position and attitude of the aircraft engine is achieved; pressure between the engine mounting section and a mounting seat of an engine mounting cabin is controlled by controlling deformation of a connecting spring of the horizontal three-way posture adjusting assembly and the vertical three-way posture adjusting assembly, and low-stress and high-precision supporting mounting of the aircraft engine is achieved.

    一种飞机发动机柔性托装装置及使用方法。该方法通过竖直三向调姿组件和水平三向调姿组件形成扁平化并联调姿结构,可在狭小空间内带动飞机发动机沿X、Y、Z向精确移动及绕X、Y、Z向精确转动,实现飞机发动机空间位置、姿态的精确调整;通过控制水平三向调姿组件与竖直三向调姿组件连接弹簧的变形量,进而控制发动机安装节与发动机安装舱的安装座之间压力,实现飞机发动机的低应力、高精度托装安装。


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    Title :

    Flexible supporting device for aircraft engine and using method


    Additional title:

    一种飞机发动机柔性托装装置及使用方法


    Contributors:
    ZHANG WEI (author) / LUO QUN (author) / YAN XIQIANG (author) / LI TINGQI (author) / WANG QIXIANG (author)

    Publication date :

    2024-10-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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