The invention belongs to the technical field of water unmanned aerial vehicles, and relates to an SVTOL electric propulsion tilt rotor water unmanned aerial vehicle and a flight strategy thereof. Comprising a fuselage, wings, empennages, motor propellers and buoys, and the lower part of the fuselage adopts a stepped ship bottom design. The motor propellers comprise wing tiltable propellers, wing non-tiltable propellers and empennage tiltable propellers, and the wing tiltable propellers are arranged in front of the left wing and the right wing respectively; a wing non-tilting propeller is arranged behind each of the left and right wings; the left side and the right side of the empennage are each provided with an empennage tiltable propeller, the empennage tiltable propellers of the empennage play a role in balancing, supplementing and assisting torque, and the buoys are arranged on the two sides of the wings respectively. The unmanned aerial vehicle can carry out water skiing short-distance take-off and landing, water vertical take-off and landing, land/ship skating short-distance take-off and landing and land/ship vertical take-off and landing in multiple take-off and landing modes, the favorable take-off and landing modes can be matched according to environments and tasks, and the requirements of different environments and different tasks are met.
本发明属于属于水上无人机技术领域,一种SVTOL电推进倾转旋翼水上无人机及其飞行策略。包括机身、机翼、尾翼、电机螺旋桨、浮筒;机身下部采用断阶式船底设计。所述电机螺旋桨包括机翼可倾转螺旋桨、机翼不可倾转螺旋桨、尾翼可倾转螺旋桨,左右所述机翼前方各布置一个机翼可倾转螺旋桨;左右所述机翼后方个布置一个机翼不可倾转螺旋桨;所述尾翼上左右各布置一个尾翼可倾转螺旋桨,所述尾翼的尾翼可倾转螺旋桨起到力矩的配平补充辅助作用,所述浮筒分别置于机翼两侧。该无人机能够水上滑水短距起降,水上垂直起降,陆上/舰上滑跑短距起降,陆上/舰上垂直起降,多种起降方式,可以根据环境和任务搭配有利起降方式,满足不同环境不同任务的需求。
SVTOL electric propulsion tilt rotor water unmanned aerial vehicle and flight strategy thereof
一种SVTOL电推进倾转旋翼水上无人机及其飞行策略
07.04.2023
Patent
Elektronische Ressource
Chinesisch
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