The invention discloses a tandem tiltable rotor aircraft which comprises a rack, wings, driving mechanisms and a control mechanism. The rack comprises a longitudinal supporting rod, and the two ends of the longitudinal supporting rod are connected with the driving mechanisms. The wings are detachably mounted on the longitudinal supporting rods; the driving mechanisms comprise two rotor wing assemblies and a tilting device, the rotor wing assemblies are connected with the tilting device through connecting pieces, and the tilting device drives the rotor wing assemblies to tilt transversely or longitudinally. The control mechanism is connected with the driving mechanism and controls the driving mechanism to move. The two ends of the rack are connected with the two rotor wing assemblies correspondingly, the rotor wing assemblies are pushed by the tilting device to tilt transversely or longitudinally, and therefore flexible flight of the aircraft is achieved.
本公开公开的一种纵列式可倾转旋翼飞行器,包括:机架、机翼、驱动机构和操控机构;所述机架包含纵向支撑杆,纵向支撑杆的两端分别连接驱动机构;所述机翼可拆卸的安装于所述纵向支撑杆上;所述驱动机构,包括两个旋翼组件和倾转装置,旋翼组件通过连接件与倾转装置连接,所述倾转装置带动所述旋翼组件发生横向或纵向倾转;所述操控机构与所述驱动机构连接,控制驱动机构运动。在机架的两端分别连接两组旋翼组件,旋翼组件通过倾转装置推动发生横向或纵向倾转,从而实现飞行器的灵活飞行。
Tandem tiltable rotor aircraft
一种纵列式可倾转旋翼飞行器
2020-11-06
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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