The invention discloses a rotary wing vertical take-off and landing hybrid power unmanned aerial vehicle. The unmanned aerial vehicle comprises a vehicle body, a left wing, a right wing, a left aileron, a right aileron, a left flap, a right flap, an empennage, a main propeller, a left wing motor, a left wing propeller, a left wing rotating motor, a right wing motor, a right wing propeller, a rightwing rotating motor, an empennage motor, an empennage motor rotating motor, an empennage motor rotating shaft, a motor steering converter, a vertical stabilizer, an elevator, a rudder, a turboprop engine, a turboprop engine reducing mechanism, a clutch A, a clutch B, an inverter, a power generation/electric all-in-one machine, a storage battery pack, an oil tank, a temperature sensor, a pressuresensor, a state-of-charge estimation module and a control module. When the unmanned aerial vehicle takes off and lands, take-off and landing of the unmanned aerial vehicle are achieved through the rotating wings and the empennage motor, the excellent cruise dynamic characteristics of a fixed-wing aircraft and the vertical take-off and landing capacity of a rotorcraft are combined, and the cruisingability, the power capacity, the survival capacity, the maneuverability and the like of the unmanned aerial vehicle are improved.
本发明公开了一种旋转翼垂直起降混合动力无人机,包括:机身、左机翼、右机翼、左副翼、右副翼、左襟翼、右襟翼、尾翼、主螺旋桨、左翼电动机、左翼螺旋桨、左翼旋转电机、右翼电动机、右翼螺旋桨、右翼旋转电机、尾翼电动机、尾翼电机旋转电机、尾翼电机旋转轴、电机转向变换器、垂直安定面、升降舵、方向舵、涡桨发动机、涡桨发动机减速机构、离合器A、离合器B、逆变器、发电/电动一体机、蓄电池组、油箱、温度传感器、压力传感器、荷电状态估计模块和控制模块;本发明在无人机起降时通过旋转机翼和尾翼电机实现无人机的起降,结合了固定翼飞机优秀的巡航动力特性和旋翼机的垂直起降能力,提高了无人机的续航、动力、生存、机动等能力。
Rotary wing vertical take-off and landing hybrid power unmanned aerial vehicle and control method thereof
一种旋转翼垂直起降混合动力无人机及其控制方法
2020-12-08
Patent
Electronic Resource
Chinese
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