The invention discloses a multi-rotor manned aircraft. The multi-rotor manned aircraft comprises a manned cabin, lifting rotors, an equipment cabin and a steering rudder. An upper portion of the manned cabin is provided with a window, an edge of a bottom of the manned cabin is provided with an undercarriage, a side wall of the manned cabin is provided with a cabin door, the outer walls of the twosides of the manned cabin are provided with side pushing rotor wings, and the rear ends of the side pushing rotor wings are provided with first power equipment driving the side pushing rotor wings tooperate. The number of the lifting rotors is at least two, the lifting rotors are distributed on the upper portion of the manned cabin in a circumferential direction, and the lower end of each liftingrotor is provided with second power equipment for driving the corresponding lifting rotor to operate. The equipment cabin is arranged at the bottom of the manned cabin, and a power source for the first power equipment and the second power equipment to operate is arranged in the equipment cabin; and the steering rudder is arranged at the rear part of the manned cabin. Flight, take-off and landingof the manned aircraft are similar to an unmanned aerial vehicle, and the manned aircraft has advantages of a small size, flexibility, a low altitude, a low speed, vertical take-off and landing, economy and practicability.
本发明公开了一种多旋翼载人飞行器,包括载人舱、举升旋翼、设备仓以及转向舵;所述载人舱的上部具有视窗,底部边缘设置有起落架,侧壁设置有舱门,两侧外壁还分别设置有侧推旋翼,所述侧推旋翼的后端设置有驱动所述侧推旋翼运转的第一动力设备;所述举升旋翼设置有至少两个,并周向分布于所述载人舱的上部,每个所述举升旋翼的下端分别设置有驱动所述举升旋翼运转的第二动力设备;所述设备仓设置于所述载人舱的底部,其内设置有供所述第一动力设备和第二动力设备运转的动力源;所述转向舵设置于所述载人舱的后部。本发明的飞行、起降类同无人飞行器,具有小巧灵活、低空低速、垂直升降、经济实用的优势。
Multi-rotor manned aircraft
多旋翼载人飞行器
2020-10-30
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |