The four-rotor flight mechanism comprises a machine body fixing plate and four spiral wings arranged on the two sides of the machine body fixing plate, and two sliding supporting plates used for fixing the two spiral wings at the corresponding ends are arranged on the machine body fixing plate; the machine body fixing plate is further provided with a driving mechanism used for driving the two sliding supporting plates to move in the face-to-face direction or the back-to-back direction. Bat wing frames are arranged on the positions, located on the same side of the machine body fixing plate, of the two sliding supporting plates respectively, bat wings are arranged between the oppositely-arranged bat wing frames, and when the two sliding supporting plates move in the face-to-face direction or the back-to-back direction, the bat wings are correspondingly folded or unfolded. By combining the advantages of the fixed wings and the four rotors, the unmanned aerial vehicle can vertically take off, land and hover, and can fly in a gliding mode.
本发明公开了一种结合可折叠蝠翼的四旋翼飞行机构,包括机体固定板和设置于机体固定板两侧的四个螺旋翼,所述机体固定板上设置有两个用于固定对应端两个螺旋翼的滑动支撑板,机体固定板上还设置有用于驱动两所述滑动支撑板相向/背向移动的驱动机构;两滑动支撑板上位于机体固定板同侧分别设置有蝠翼边框,相对设置的蝠翼边框之间设置有蝠翼,两滑动支撑板相向/背向移动时,所述蝠翼对应折叠/展开。本发明通过结合固定翼与四旋翼的优势,可垂直起降悬停,并可以通过滑翔的方式飞行。
Four-rotor flight mechanism combined with foldable bat wing
一种结合可折叠蝠翼的四旋翼飞行机构
2022-10-25
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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