The invention relates to a parallel shaft type Mars aircraft based on electromagnetic direct-drive attitude adjustment, and belongs to the technical field of spaceflight Mars aircrafts. The problems that a traditional parallel-axis aircraft needs to adopt a duct structure or utilize an additional driver to tilt a rotor to adjust the attitude of the aircraft, the structure is complex, and the power loss is large are solved. Comprising rotors, supporting arms and landing legs, landing legs and a vehicle body, the supporting arms and the landing legs are arranged on the front side and the rear side of the vehicle body, the rotors are arranged at the ends of the supporting arms and the landing legs, and the landing legs are arranged on the left side and the right side of the vehicle body. The parallel shaft type Mars aircraft is reasonable in design, the plane vector direction of the propeller tips can be changed through the electromagnetic direct-drive attitude adjusting device, the aircraft is controlled to achieve hovering, translation, rolling and yawing movement, the longitudinal envelope size of the aircraft is small, the aircraft can be used for detecting narrow terrains, the structure is ingenious, and power loss is low.

    本发明涉及一种基于电磁直驱调姿的平行轴式火星飞行器,属于航天火星飞行器技术领域。本发明解决传统平行轴式飞行器需要采用涵道结构或者利用额外的驱动器使转子倾斜以调节飞行器姿态,其结构复杂,功率损耗大的问题。包括旋翼、支臂及着陆腿、着陆腿和机体,机体的前后两侧设置有支臂及着陆腿,支臂及着陆腿的端部设置有旋翼,机体的左右两侧设置有着陆腿。本发明设计合理,平行轴式火星飞行器能够通过电磁直驱调姿装置改变桨尖平面矢量方向,操纵飞行器实现悬停、平动、横滚及偏航运动,并且飞行器的纵向包络尺寸小,能够用于探测狭窄地形,结构巧妙,功率损耗低。


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    Titel :

    Parallel shaft type Mars aircraft based on electromagnetic direct-drive attitude adjustment


    Weitere Titelangaben:

    一种基于电磁直驱调姿的平行轴式火星飞行器


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

    Erscheinungsdatum :

    2023-09-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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