An assistance device is provided to maneuver of a cover of a nacelle of a turbojet engine. The assistance device includes a joint collinear with an existing joint or hinge for a fitting of the cover, and the joint of the device is rigidly secured to an angled part of which one end bears on the fitting of the cover and of which one point is hinged to a compression spring in order to apply assistance momentum to the fitting of the cover when the cover is raised.


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    Title :

    ВСПОМОГАТЕЛЬНОЕ УСТРОЙСТВО ДЛЯ ВЫПОЛНЕНИЯ МАНИПУЛЯЦИЙ С КАПОТОМ И ГОНДОЛА ТУРБОРЕАКТИВНОГО ДВИГАТЕЛЯ, ОСНАЩЕННАЯ ТАКИМ УСТРОЙСТВОМ


    Publication date :

    2017-08-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

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