The invention belongs to the technical field of manned aircrafts. The invention provides a tilt rotor manned aircraft capable of vertically taking off and landing and provided with foldable wings. The tilt rotor manned aircraft can solve many problems in the aspects of safety, energy consumption, voyage, parking conditions and the like of existing middle and low altitude manned aircrafts. The aircraft adopts a structure that the upper part is provided with the rotatable folding wings and the lower part is provided with the cabin with the tilting multi-rotor wings, the aircraft takes off and lands vertically by utilizing the vertical lift force provided by the multi-rotor wings in the take-off and landing stage, and the tilting rotor wings push the aircraft forwards and fly by utilizing the lift force generated by the opened wings at the upper part in the flying process; due to the structure, the safety performance of the aircraft is greatly improved, meanwhile, the energy consumption of the rotors can be reduced, the voyage is correspondingly increased, the occupied area and the parking space of the aircraft during parking are greatly reduced due to the fact that the wings are foldable, and the effects of high safety, low energy consumption, long endurance, take-off and landing in any place and convenient parking can be achieved. The aircraft is suitable for manned flight in middle and low airspaces.
本发明属于载人飞行器技术领域。本发明提供一种可垂直起降的可折叠机翼的倾转旋翼载人飞行器,可以解决现有中低空载人飞行器安全性、能耗、航程、停放条件等方面的诸多问题。本飞行器采用上部为可转动折叠机翼而下部为座舱带可倾转多旋翼的结构,起降阶段利用多旋翼提供的竖直方向的升力垂直起降,飞行过程中倾转旋翼向前推动飞行器并利用上部张开的机翼产生的升力进行飞行,这样的结构使得飞行器的安全性能大幅提高,同时可降低旋翼的能耗相应增大航程,且由于机翼可折叠,使飞行器停放时的占地面积及停放空间大为缩小,可达到高安全性、低能耗长航时、任意场地起降和方便停放的效果。本发明所述飞行器适用于中低空域载人飞行。
Tilt rotor manned aircraft with foldable wings
一种可折叠机翼的倾转旋翼载人飞行器
2024-01-16
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
Small domestic manned aircraft with foldable and light oval wings
European Patent Office | 2024
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