The invention provides a four-blade four-rotor type Mars aircraft and a folding restraining and unfolding unlocking device. The aircraft (2) is compressed in the bottom restraint device (4) by the top restraint device (1) after being folded, the bottom restraint device (4) is mounted above the Mars lander (5), and the lander mechanical arm (3) is further deployed on the Mars lander (5); the top restraining device (1) and the bottom restraining device (4) are connected with each other in the rocket launching stage to form a cubic envelope. Deployment of the Mars rotorcraft on the surface of the Mars is achieved, and then inspection and detection tasks of the Mars rotorcraft are carried out.

    本发明提供一种四桨叶四旋翼式火星飞行器及折叠约束与展开解锁装置。所述飞行器(2)折叠后被顶部约束装置(1)压紧在底部约束装置(4)内部,底部约束装置(4)安装在火星着陆器(5)上方,火星着陆器(5)上还部署着陆器机械臂(3);所述顶部约束装置(1)和底部约束装置(4)在火箭发射阶段相互连接,构成一个立方体包络。以实现火星旋翼飞行器在火星表面的部署,进而开展火星旋翼飞行器的巡视探测任务。


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    Title :

    Four-blade four-rotor type Mars aircraft and folding restraining and unfolding unlocking device


    Additional title:

    一种四桨叶四旋翼式火星飞行器及折叠约束与展开解锁装置


    Contributors:
    QUAN QIQUAN (author) / ZHU KAIJIE (author) / TANG DEWEI (author) / DONG YACHAO (author) / DENG ZONGQUAN (author)

    Publication date :

    2023-07-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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