The invention relates to a synchronous swing type variable-dip-angle driving energy-adjustable four-continuous-wing aircraft. The aircraft comprises belt wings, swing shafts, connecting pieces, first speed reducers, stepping motors, a transmission mechanism, a second speed reducer, a motor, a fuselage frame, a third speed reducer and driving motors; the four swing shafts in the horizontal direction are symmetrically and fixedly mounted on the periphery of the fuselage frame, and the four connecting pieces are connected to the four swing shafts correspondingly and rotate relatively; the four belt wings are connected to the four connecting pieces respectively and can rotate relatively; each belt wing comprises a belt wing frame and a soft belt mounted on the belt wing frame; belt wheels, tensioning wheels and driving motors are further arranged in each belt wing frame and used for switching between the working state and the reset state of the belt wings; the transmission mechanism is connected to the two connecting pieces; the motor drives the transmission mechanism to move after being decelerated by the second speed reducer, so that the four connecting pieces synchronously swing up and down, and the four stepping motors respectively drive the four belt wings to rotate after being decelerated by the two first speed reducers.
本发明涉及同步摆动式变倾角驱动能量可调四连续带翼飞行器。包括带翼、摆动轴、连接件、第一减速器、步进电机、传动机构、第二减速器、电动机、机身框架、第三减速器以及驱动电机,机身框架四周对称的安装固定有四个水平方向的摆动轴,四个连接件分别连接在四个摆动轴上且相对转动,四个带翼分别连接在四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,电动机通过第二减速器减速后带动传动机构运动使四个连接件同步上下摆动,四个步进电机通过两个第一减速器减速后分别带动四个带翼转动。
Synchronous swing type variable-dip-angle driving energy-adjustable four-continuous-wing aircraft
同步摆动式变倾角驱动能量可调四连续带翼飞行器
2022-01-11
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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