The invention discloses a multi-rotor manned helicopter which comprises a manned cabin, lifting rotors, an equipment cabin and a steering rudder. The upper portion of the manned cabin is provided witha window, the bottom edge of the manned cabin is provided with sliding wheels, the rear wall of the manned cabin is provided with a cabin door, the outer walls of the two sides of the manned cabin are each provided with a side pushing rotor wing, and the rear ends of the side pushing rotor wings are provided with first power equipment for driving the side pushing rotor wings to operate. There areat least two lifting rotors, the lifting rotors are distributed on the two sides of the manned cabin side by side, and the lower end of each lifting rotor is provided with second power equipment fordriving 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 top of the manned cabin. The flight and take-off and landing device is similar to an unmanned aerial vehicle, and has the advantages of small size, flexibility, low altitude, low speed, vertical take-off and landing, economy and practicability.
本发明公开了一种多旋翼载人直升飞机,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,底部边缘设置有滑行轮,后壁设置有舱门,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,并排分布于所述载人舱的两侧,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顶部。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 helicopter
一种多旋翼载人直升飞机
2020-10-30
Patent
Electronic Resource
Chinese
Civil helicopter ground joint test manned rotor control system
European Patent Office | 2024
|Double-rotor helicopter and fixed wing combined integrated manned aircraft
European Patent Office | 2021
|