The invention relates to the field of aircrafts, in particular to an adjustable aircraft which comprises an aircraft body, at least four multi-direction adjusting mechanisms are arranged on the peripheral side of the aircraft body, the fixed ends of the multi-direction adjusting mechanisms are fixedly connected with the aircraft body, and the movable ends of the multi-direction adjusting mechanisms are fixedly connected with one ends of connecting arms. A propeller assembly is installed at the other end of the connecting arm, a controller is installed on the aircraft body, and the controller is electrically connected with the propeller assembly and the multi-direction adjusting mechanism. The propeller is adaptively adjusted at multiple angles, so that the aircraft can be operated and adjusted more flexibly.
本发明设计飞行器领域,具体的涉及一种可调节飞行器,包括飞行器主体,所述飞行器主体周侧设有至少四个多向调节机构,所述多向调节机构的固定端与所述飞行器主体固定连接,所述多向调节机构的活动端固定连接有连接臂的一端,所述连接臂的另一端安装有螺旋桨总成,所述飞行器主体上安装有控制器,所述控制器与所述螺旋桨总成、多向调节机构电连接。本发明通过使螺旋桨在多个角度上进行适应性的调整,以使得飞行器可以更加灵活的进行操作调整。
Adjustable aircraft
一种可调节飞行器
2025-05-06
Patent
Electronic Resource
Chinese
IPC: | B64U |