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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    Titel :

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


    Erscheinungsdatum :

    04.08.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Russisch


    Klassifikation :

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