The invention relates to a ground deployment device and method for an aircraft, and belongs to the technical field of rotary wing type Mars aircrafts. The defects that the deployment mode of the Mars aircraft is influenced by the surrounding terrain and the adaptability is low are overcome. Comprising a top cover, a Mars aircraft, a pushing device and a lower enveloping body, the top cover is connected with the lower enveloping body, the Mars aircraft and the pushing device are arranged in an enveloping body formed by the top cover and the lower enveloping body, and the Mars aircraft is arranged on the upper portion of the pushing device. The aircraft is deployed on the landing platform to take off, the dependence on the terrain around the lander is not strong, the deployment applicability is higher, and the aircraft is not limited by the terrain.

    本发明涉及一种飞行器的地面部署装置及方法,属于旋翼式火星飞行器技术领域。针对上述火星飞行器部署方式受周围地形的影响,适应性较低的缺陷。包括顶盖、火星飞行器、推送装置和下包络体,所述顶盖与下包络体连接,顶盖与下包络体形成的包络体内设置有火星飞行器、推送装置,火星飞行器设置在推送装置上部。本发明的飞行器在着陆平台上进行部署起飞,对着陆器周围地形依赖性不强,部署的适用性更强,不受地形限制。


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    Title :

    Ground deployment device and method for Mars aircraft


    Additional title:

    一种火星飞行器的地面部署装置及方法


    Contributors:
    QUAN QIQUAN (author) / TANG BO (author) / TANG DEWEI (author) / DENG ZONGQUAN (author)

    Publication date :

    2023-09-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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