The invention relates to a retractable rotary wing type Mars manned aircraft overall device and an unfolding method thereof, and belongs to the technical field of spaceflight Mars rotary wing aircrafts. For an existing Mars aircraft overall structure, a retractable eight-shaft sixteen-rotor type Mars manned aircraft overall structure is lacked. The retractable rotor type Mars manned aircraft overall device comprises a main frame, a seat, a landing frame and rotor assemblies, the main frame is connected with the rotor assemblies arranged at equal intervals in the circumferential direction, the seat is arranged in the middle of the main frame, and the land frame is arranged on the lower portion of the seat; the rotor wing assembly comprises a forward paddle, a motor, a rotor wing supporting arm and a reverse paddle, the forward paddle and the reverse paddle are connected with the motor, and the forward paddle and the reverse paddle which are coaxially arranged are connected with the main frame through the rotor wing supporting arm. The multi-rotor type Mars manned aircraft is stable in structure, easy to operate, small in folding envelope size and capable of completing manned flight, and has important significance on the overall configuration and the like of the multi-rotor type Mars manned aircraft.
本发明涉及可收展的旋翼式火星载人飞行器总体装置及其展开方法,属于航天火星旋翼飞行器技术领域。针对已有的火星飞行器总体构型,尚缺少可收展的八轴十六旋翼式火星载人飞行器总体构型。提供可收展的旋翼式火星载人飞行器总体装置及其展开方法,包括主框架、座椅、着陆架和旋翼组件,主框架与周向等距布置的旋翼组件连接,主框架的中部设置有座椅,座椅的下部设置有着陆架;所述旋翼组件包括正向桨叶、电机、旋翼支臂和反向桨叶,正向桨叶、反向桨叶与电机连接,同轴设置的正向桨叶、反向桨叶通过旋翼支臂与主框架建立连接。本发明结构稳定、操纵简单、收拢包络尺寸小,能完成载人飞行,对多旋翼式火星载人飞行器总体构型等具有重要意义。
Foldable rotor type Mars manned aircraft overall device and unfolding method thereof
可收展的旋翼式火星载人飞行器总体装置及其展开方法
2024-06-28
Patent
Electronic Resource
Chinese
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