The invention provides a composite rotor aircraft. The composite rotor aircraft comprises an aircraft main body; an aircraft main body, wherein a main shaft bracket is mounted in the aircraft main body, the main shaft is mounted on the main shaft bracket through a main shaft bearing, and the upper end of the main shaft is connected with a rotor head; a rotor head, wherein a rotor assembly and a folding paddle assembly are mounted on the rotor head; a rotor assembly which is connected with the swash plate assembly through a rotor push-pull rod assembly; a folding paddle assembly which is used for driving the main shaft and the rotor assembly to rotate during take-off; a swash plate assembly which is used for controlling the flight attitude of the aircraft; a swash plate steering engine; a back propeller assembly which is used for enabling the aircraft to generate a propelling power; a direction steering engine assembly; and a control system. A driving motor does not need to be arranged at the main shaft, a tail rotor does not need to be arranged, the structure is simple and practical, stability and cruising ability are high, rising and falling are more stable, and safety is higher.
本发明提供了一种复合型旋翼飞行器,包括:飞行器主体;主轴,所述飞行器主体内安装有主轴支架,所述主轴通过主轴轴承安装在所述主轴支架上,所述主轴上端与旋翼头相连;旋翼头,所述旋翼头上安装设置有旋翼组件和折叠桨组件;旋翼组件,所述旋翼组件通过旋翼推拉杆组件和倾斜盘组件相连;折叠桨组件,所述折叠桨组件用于在起飞时带动主轴及旋翼组件旋转;倾斜盘组件,所述倾斜盘组件用于控制飞行器飞行姿态;倾斜盘舵机;背推桨组件,所述背推桨组件用于使飞行器产生推进动力;方向舵机组件;控制系统。本发明不需要在主轴处设置驱动电机,不需要设置尾桨,结构简单实用,且稳定性和续航能力强,起落更加稳定,安全性更强。
Composite rotor aircraft
一种复合型旋翼飞行器
2022-01-18
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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