The invention discloses a flapping-like rotor aircraft, which is characterized in that revolution spindles of flapping rotors are arranged on the two sides of a fuselage through flapping rotor supports, meanwhile, a front rotating arm and a rear rotating arm are correspondingly and perpendicularly fixed to the head end and the tail end of each revolution spindle respectively, and autorotation spindles are rotationally connected with the front rotating arms and the rear rotating arms respectively and located on the two sides of the revolution spindles respectively; a revolution motor drives therevolution spindle to revolve for a circle through a revolution transmission gear set, the revolution spindle drives the autorotation spindle to autorotate for a half circle through an autorotation transmission device, retractable upper single wings are arranged on the two sides of the back of the fuselage respectively, the height difference between the retractable upper single wings and the flapping rotor support is greater than the sum of the heights of the front rotating arm and the rotor mechanism, and meanwhile, the controller is electrically connected with the retractable upper single wing and a jet engine to control the working states of the retractable upper single wing and the jet engine. The invention provides a flapping-like rotor aircraft which improves the ascending efficiency and the navigation speed.
本发明公开了一种类扑旋翼飞行器,扑旋翼的公转主轴通过扑旋翼支架设置在机身的两侧,同时公转主轴的首尾两端分别对应垂直固定有前转臂和后转臂,自转主轴分别与前转臂和后转臂转动连接,并分别位于在公转主轴的两侧;公转电机通过公转传动齿轮组驱动公转主轴公转一周,公转主轴通过自转传动装置驱动自转主轴自转半周,同时收缩式上单翼分别设置在机身的背部两侧,且其与扑旋翼支架之间的高度差大于前转臂和旋翼机构的高度之和,同时控制器分别与收缩式上单翼以及喷气式发动机电性连接,控制收缩式上单翼和喷气式发动机的工作状态。本发明提供了一种类扑旋翼飞行器,提高了上升的效率以及提高航行的速度。
Flapping-like rotor aircraft
一种类扑旋翼飞行器
2021-03-05
Patent
Elektronische Ressource
Chinesisch
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