The invention discloses a Mars four-rotor aircraft and a slideway type inverted releasing and deploying device, and relates to an aircraft and a releasing and deploying device. The invention aims to solve the problem that a proper Mars four-rotor aircraft structure and a proper folding, unfolding and deploying scheme do not exist at present. The Mars aircraft comprises a lander, a bottom turnover component, an outer enveloping component, a multi-degree-of-freedom mechanical arm and a Mars aircraft, the bottom turnover component and the multi-degree-of-freedom mechanical arm are installed on the upper surface of the lander side by side, the bottom of the outer enveloping component is installed on the bottom turnover component, and the Mars aircraft is arranged in the outer enveloping component in an inverted mode. The invention belongs to the technical field of aerospace crafts.

    一种火星四旋翼飞行器及滑道式倒立释放与部署装置,它涉及一种飞行器及释放与部署装置。本发明为了解决目前没有合适的火星四旋翼飞行器结构、折展及部署方案的问题。本发明包括着陆器、底部翻转部件、外包络部件、多自由度机械臂和火星飞行器;底部翻转部件和多自由度机械臂并排安装在着陆器的上表面,外包络部件的底部安装在底部翻转部件上,火星飞行器倒立设置在外包络部件内。本发明属于航天飞行器技术领域。


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    Titel :

    Mars four-rotor aircraft and slideway type inverted releasing and deploying device


    Weitere Titelangaben:

    一种火星四旋翼飞行器及滑道式倒立释放与部署装置


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

    Erscheinungsdatum :

    2023-06-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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