The invention relates to a synchronous double-direct-acting driving energy-adjustable continuous belt wing unmanned aerial vehicle. Four slideways in the vertical direction are symmetrically and fixedly installed on the periphery of the fuselage top plate, the two belt wings can slide on the slideways, meanwhile, the two belt wings are connected to the two connecting pieces respectively and can rotate relatively, each belt wing comprises a belt wing frame and a soft belt installed on the belt wing frame, and a belt wheel, a tensioning wheel and a driving motor are further arranged in the belt wing frame, and used for switching between the working state and the reset sate of the belt wings, the transmission mechanism is connected to the two connecting pieces, and a motor arranged on the bottom plate of the fuselage drives the transmission mechanism to move after being decelerated through a third speed reducer so that the two connecting pieces can synchronously slide up and down. The two stepping motors arranged on the two connecting pieces correspondingly drive the two belt wings to rotate after being decelerated through the two first speed reducers.
本发明涉及同步双直动驱动能量可调连续带翼式无人机。机身顶板四周对称的安装固定有四个竖直方向的滑道,两个带翼可在滑道上滑动,同时两个带翼分别连接在两个连接件上且可相对转动,带翼包括带翼框架,以及安装在带翼框架上的软质带,带翼框架内还设置有带轮、张紧轮以及驱动电机,用于带翼工作状态与复位状态的切换,传动机构连接在两个连接件上,设置在机身底板上的电动机通过第三减速器减速后带动传动机构运动使两个连接件同步上下滑动,分别设置在两个连接件上的两个步进电机通过两个第一减速器减速后分别带动两个带翼转动。
Synchronous double-direct-acting driving energy-adjustable continuous winged unmanned aerial vehicle
同步双直动驱动能量可调连续带翼式无人机
2022-01-07
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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