The invention discloses a six-pull-curtain driving energy-adjustable rotary wing aircraft characterized by comprising rotary curtain wings, rotary shafts, second speed reducers, motors and a fuselage frame; the four rotary shafts in the front row and the rear row are symmetrically arranged on the two sides of the fuselage frame in the vertical direction, and the two horizontal rotary shafts are symmetrically arranged on the fuselage frame in the front-back direction; the six motors arranged on the fuselage frame are decelerated through the six second speed reducers arranged on the fuselage frame and then drive the six rotary shafts to rotate continuously; the six rotary curtain wings are fixedly connected to the six rotary shafts respectively, the four rotary curtain wings on the two sides are used for generating thrust, and the front rotary curtain wing and the rear rotary curtain wing are used for generating lift force; each rotary curtain wing comprises a rotary frame and a curtain wing mounted in the rotary frame; each curtain wing comprises a curtain wing frame and a soft curtain mounted on the curtain wing frame, and coil springs and driving motors are further arranged in the curtain wing frame and used for controlling the soft curtain to be unfolded and folded.
本发明公开了一种六拉帘驱动能量可调旋转翼飞行器,其特征在于包括旋转帘翼、旋转轴、第二减速器、电动机和机身框架,机身框架两侧对称的布置有前后两排四个竖直方向的旋转轴,机身框架前后对称的布置有两个水平的旋转轴,设置在机身框架上的六个电动机分别通过设置在机身框架上的六个第二减速器减速后分别带动六个旋转轴连续旋转,六个旋转帘翼分别固定连接在六个旋转轴上,两侧四个旋转帘翼用于产生推力,前后两个旋转帘翼用于产生升力,旋转帘翼包括旋转框架,以及安装在旋转框架内的帘翼,帘翼包括帘翼框架,以及安装在帘翼框架上的软质帘,帘翼框架内还设置有卷簧以及驱动电机,用于控制软质帘的展开和收缩。
Six-pull-curtain driving energy-adjustable rotary wing aircraft
六拉帘驱动能量可调旋转翼飞行器
2022-01-11
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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