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    Electromagnetic-driven attitude-adjusting coaxial Mars aircraft

    Electromagnetic-driven attitude-adjusting coaxial Mars aircraft

    Freier Zugriff

    The invention discloses an electromagnetic-driven attitude-adjusting coaxial Mars aircraft, and relates to the technical field of research and development of Mars aircrafts, the electromagnetic-driven attitude-adjusting coaxial Mars aircraft comprises an overall frame module, the overall frame module is sequentially provided with an upper rotor module and a lower rotor module in the vertical direction, and main shafts of the upper rotor module and the lower rotor module are coaxially arranged; the upper rotor module comprises an upper blade, the lower rotor module comprises a lower blade, and the lower blade and the upper blade are opposite in rotation direction, so that the anti-torque directions pneumatically generated when the upper blade and the lower blade rotate are opposite, and the course of the aircraft is controllable.

    本发明公开一种电磁驱动调姿共轴式火星飞行器，涉及火星飞行器研发技术领域，包括总体框架模块，所述总体框架模块上下方向依次设有上旋翼模块和下旋翼模块，上旋翼模块和下旋翼模块的主轴采用同轴布置的形式，上旋翼模块包括上桨叶，下旋翼模块包括下桨叶，下桨叶与上桨叶旋转方向相反，使上下桨叶旋转时气动产生的反扭距方向相反，保证飞行器航向可控。

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    Titel :

    Electromagnetic-driven attitude-adjusting coaxial Mars aircraft

    Weitere Titelangaben:

    一种电磁驱动调姿共轴式火星飞行器

    Beteiligte:
    QUAN QIQUAN (Autor:in) / WU QI (Autor:in) / TANG DEWEI (Autor:in) / WU YUANXU (Autor:in) / ZHU KAIJIE (Autor:in) / DENG ZONGQUAN (Autor:in)
    Erscheinungsdatum :

    2022-11-22

    Medientyp :

    Patent

    Format :

    Elektronische Ressource

    Sprache :

    Chinesisch

    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS

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