The invention belongs to the technical field of aviation aircrafts, and discloses a rotary wing structure and an assembly method.The rotary wing structure comprises a rotary main shaft, a servo motor, a transmission part, a main shaft support, wings and a flight control part, the rotary main shaft is installed on the main shaft support, and the main shaft support is installed on a machine body structure; the wing part is mounted on a rotating main shaft outside the aircraft body through a wing interface, and the servo motor controls the rotating main shaft to rotate through the transmission part so as to drive the wing part to rotate; the control performance of the aircraft is further improved by adding a propeller system, an elevator and a rudder on the wings, so that the aircraft has a helicopter flight mode and a fixed wing flight mode, and the conversion between the vertical take-off and landing state and the fixed wing flight state of the aircraft is facilitated.
本发明属于航空飞行器技术领域,公开了一种旋转机翼结构及装配方法,旋转机翼结构包括旋转主轴、伺服电机、传动部分、主轴支架、机翼、飞行控制部分,旋转主轴安装在主轴支架上,主轴支架安装在机体结构上,机翼部分通过机翼接口安装在机体外的旋转主轴上,伺服电机通过传动部分控制旋转主轴旋转,从而带动机翼部分旋转;在机翼上通过增加推进器系统、升降舵、方向舵进一步改善飞机的操控性能,使其具备直升机飞行模式与固定翼飞行模式,有利于飞机的垂直起降与固定翼飞行状态的转换。
Rotary wing structure and assembly method
一种旋转机翼结构及装配方法
2024-10-15
Patent
Electronic Resource
Chinese