The invention is applicable to the technical field of aircrafts, and provides an integrated fuselage of an unmanned aerial vehicle, which comprises an aircraft main body of a butterfly-shaped structure; the aircraft body comprises a flat bottom cover plate, a plurality of protection rings are arranged on the side wall of the flat bottom cover plate, and a support is arranged in each protection ring. One end of the support is fixedly connected with the protection ring, and the other end is provided with a motor. The airplane main body is arranged to be of a butterfly-shaped structure, the airplane main body of the structure has a certain thickness, the propeller blades can be wrapped in the protection ring while buoyancy can be provided, the risk that the propeller blades hit foreign matter is reduced, and the propeller blades can be prevented from hurting people to a certain extent while the propeller blades are protected; by arranging the flat-bottom cover plate and the flat-bottom structure of the flat-bottom cover plate, the wave resistance of the aircraft can be improved, the aircraft can float more stably in water, and the aircraft can be guaranteed to float and prevented from sinking in water and being thoroughly lost.
本发明适用于飞行器技术领域,提供了一种无人机一体化机身,包括飞机主体,飞机主体呈蝶型结构;飞机主体包括平底盖板,平底盖板的侧壁上设置有多个保护圈,每一个保护圈的内部均设置有支架;支架的一端和保护圈固定连接,支架的另一端安装有电机;通过设置飞机主体呈蝶型结构,该结构的飞机主体具有一定的厚度,能够在提供浮力的同时还能将桨叶包裹在保护圈内,降低桨叶打到异物的风险,保护桨叶的同时,也能在一定程度上防止桨叶伤人;通过设置平底盖板,平底盖板这种平底结构,能够提高飞机的抗浪性,使飞机在水中漂浮更稳定,通过本发明能够保证飞机漂浮,防止飞行器沉水,彻底丢失。
Integrated fuselage of unmanned aerial vehicle
一种无人机一体化机身
2022-05-24
Patent
Electronic Resource
Chinese
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