The invention relates to an aircraft gravity center shifting traction device. The traction device comprises a sun gear and the planetary gears meshing with each other, the number of teeth of the sun gear of the planetary gear teeth are equal, the sun gear is fixedly connected to the inner end of the shaft, within the outer wall of the shaft by device of a first bearing shaft axial rotation shaft sleeve is mounted, the ends of the sleeve shaft mounting a drive source; radial outer wall of the sleeve shaft connecting arm, the ends of the radial arm connected to the shaft, the shaft and sleeve shaft arranged in parallel, a second end of the shaft by device of bearing axis and the planetary gears; the upper surface of the planet gear solid company eccentric body, when the shortest distance between the center of gravity and the center axis of the eccentric shaft sleeve body between the traction device of gravity is located in the center axis of the shaft sleeve. The invention shift the focus of traction drive vehicle travels, the propulsion efficiency is greatly improved, and free from outside influence when traveling at high speed in outer space; the invention can be installed in a variety of casing, a wide range of applications.


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    Titel :

    Aircraft gravity center shifting traction device


    Beteiligte:
    XIA SHANSHENG (Autor:in)

    Erscheinungsdatum :

    29.04.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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