The invention discloses a low-altitude manned aircraft, and relates to the technical field of manned aircrafts, the low-altitude manned aircraft comprises a cavity, the lower surface of the cavity is fixedly connected with a fixing plate, the upper surface of the cavity is provided with a flight mechanism, the flight mechanism comprises a fixing frame and a fixing box, the fixing box is fixedly connected to the outer surface of the cavity, and the fixing plate is fixedly connected to the fixing frame. The fixing frame is fixedly connected to the upper surface of the fixing box, and the flying mechanism is arranged, so that the cavity can complete take-off work under control, and the effect of flying in different directions in the air under control is achieved; an air circulation mechanism penetrates through the upper surface of the cavity, the air circulation mechanism is used for purifying air in the cavity, the air circulation mechanism comprises an exhaust pipe, the exhaust pipe penetrates through the upper surface of the cavity, and a first supporting rod is fixedly connected to the top end of the exhaust pipe; the end of the first supporting rod is fixedly connected with a stepping motor, and the effect that the aircraft can be flexibly changed to stop on the water surface and the ground is achieved.
本发明公开了一种低空载人飞行器,本发明涉及载人飞行器技术领域,包括腔室,所述腔室的下表面固定连接有固定板,所述腔室的上表面设置有飞行机构,所述飞行机构包括固定架和固定箱,所述固定箱固定连接在腔室的外表面,所述固定架固定连接在固定箱的上表面,通过设置飞行机构,可以在控制下,使腔室能够完成起飞工作,并控制下在空中完成不同方向飞行的效果;所述腔室的上表面贯穿有空气流通机构,该空气流通机构用于对腔室中的空气进行净化,所述空气流通机构包括排气管,所述排气管贯穿腔室的上表面,所述排气管的顶端固定连接有第一支撑杆,所述第一支撑杆的端部固定连接有步进电机,达到使飞行器能够灵活改变停止于水面和地面的效果。
Low-altitude manned aircraft
一种低空载人飞行器
2025-03-11
Patent
Electronic Resource
Chinese
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