The invention relates to a four-drive energy adjustable continuous winged variable dip angle direct-acting aircraft. Four vertical slideways are symmetrically mounted and fixed on the periphery of the fuselage frame, the four connecting pieces are respectively connected to the four slideways in a sliding manner, the four belt wings are respectively connected to the four connecting pieces and can rotate relatively, and each belt wing comprises a belt wing frame and a soft belt mounted on the belt wing frame; a belt wheel, a tensioning wheel and a driving motor are further arranged in the winged frame and used for switching between the working state and the reset state of the winged frame, the transmission mechanism is connected to the four connecting pieces, and the motor arranged on the fuselage frame drives the transmission mechanism to move after being decelerated through a second speed reducer so that the four connecting pieces can synchronously slide up and down. The four stepping motors arranged on the four connecting pieces correspondingly drive the four belt wings to rotate after being decelerated through the four third speed reducers.
本发明涉及四驱动能量可调连续带翼可变倾角直动式飞行器。机身框架四周对称的安装固定有四个竖直方向的滑道,四个连接件分别滑动连接在四个滑道上,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,传动机构连接在四个连接件上,设置在机身框架上的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滑动,分别设置在四个连接件上的四个步进电机通过四个第三减速器减速后分别带动四个带翼转动。
Four-drive energy adjustable continuous winged variable dip angle direct-acting aircraft
四驱动能量可调连续带翼可变倾角直动式飞行器
2022-02-18
Patent
Elektronische Ressource
Chinesisch
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