The invention discloses a multi-rotor wing cargo loading aircraft which comprises a cargo loading cabin, lifting rotor wings, an equipment cabin and a steering rudder. A window is arranged on the front surface of the upper part of the cargo loading cabin, sliding wheels are arranged at the edge of the bottom, a cabin door is arranged on the outer wall, side pushing rotor wings are further arrangedon the outer walls of two sides or the top, separately, and first power equipment that drives the side pushing rotor wings to operate is arranged at the back end of each side pushing rotor wing; theat least two lifting rotor wings are distributed around or on two sides of the cargo loading cabin in parallel, and second power equipment that drives the side pushing rotor wing to operate is arranged at the lower end of each lifting rotor wing; the equipment cabin is arranged at the bottom of the cargo loading cabin, and a power source that enables the first and second power equipment to operateis arranged in the equipment cabin; and the steering rudder is arranged on the top of the cargo loading cabin. The multi-rotor wing cargo loading aircraft is similar to an unmanned aerial vehicle inflying, taking off and landing and has the advantages of being flexible to operate, low in altitude and low in speed, capable of ascending and descending vertically and economical and practical.
本发明公开了一种多旋翼载货飞行器,包括载货舱、举升旋翼、设备仓以及转向舵;所述载货舱的上部前面具有视窗,底部边缘设置有滑行轮,外壁设置有舱门,两侧外壁或顶部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,并列分布于所述载货舱的四周或两侧,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货舱的底部,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货舱的顶部。本发明的飞行、起降类同无人飞行器,具有操控灵活、低空低速、垂直升降、经济实用的优势。
Multi-rotor wing cargo loading aircraft
多旋翼载货飞行器
2020-12-29
Patent
Elektronische Ressource
Chinesisch
HYBRID-POWER SYSTEM FOR MULTI-ROTOR-WING AIRCRAFT AND MULTI-ROTOR-WING AIRCRAFT
Europäisches Patentamt | 2021
|HYBRID-POWER SYSTEM FOR MULTI-ROTOR-WING AIRCRAFT AND MULTI-ROTOR-WING AIRCRAFT
Europäisches Patentamt | 2021
|