The invention provides a Mars multi-rotor aircraft fuselage box structure. The invention relates to the field of rotor type Mars aircrafts, in particular to a Mars multi-rotor aircraft fuselage and internal arrangement structure which comprises a shell, a heat insulation shell and other internal structures. The shell wraps the heat insulation shell, the solar cell panel connecting frame is installed in the center of the top of the shell, and other internal structures are installed in the heat insulation shell. The invention provides a structural scheme of an aircraft box body, which can protect electric control elements and batteries of an aircraft in a Mars environment.

    本发明提出一种火星多旋翼飞行器机身箱体结构。本发明涉及旋翼式火星飞行器领域,具体的是一种火星多旋翼飞行器机身与内部布置结构,包括外壳、隔热壳和其他内部结构。所述外壳包裹于隔热壳外部,顶部中心安装太阳能电池板连接架,其他内部结构安装于隔热壳内部。本发明提供了一种飞行器箱体的结构方案,能够在火星环境下保护飞行器电控元件及电池。


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    Titel :

    Body box structure of Mars multi-rotor aircraft


    Weitere Titelangaben:

    一种火星多旋翼飞行器机身箱体结构


    Beteiligte:
    QUAN QIQUAN (Autor:in) / WU YUANXU (Autor:in) / ZHU KAIJIE (Autor:in) / DONG YACHAO (Autor:in) / TANG DEWEI (Autor:in) / CAI HAO (Autor:in) / WU QI (Autor:in) / DENG ZONGQUAN (Autor:in)

    Erscheinungsdatum :

    2023-05-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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