The invention discloses a combined type guidance self-destruction patrolling flight fixed wing unmanned aerial vehicle, which comprises a launch canister and an unmanned aerial vehicle body, an ejection mechanism is arranged in the launch canister, the launch canister is used for ejecting the unmanned aerial vehicle body, an adjusting mechanism is arranged at the bottom of the launch canister, and the adjusting mechanism is used for adjusting the angle of the launch canister. The unmanned aerial vehicle comprises an unmanned aerial vehicle body, folding wing mechanisms are arranged on the two side walls of the unmanned aerial vehicle body and used for providing lift force for the unmanned aerial vehicle body, and each ejection mechanism comprises a high-pressure gas cylinder, a plurality of positioning grooves and an ejection plate. By arranging the folding wing mechanism, the multiple folding wings on the two sides of the unmanned aerial vehicle body can be folded together, so that the space occupied by the unmanned aerial vehicle body can be reduced, the unmanned aerial vehicle body can be conveniently stored or conveyed, meanwhile, after the unmanned aerial vehicle body is catapulted, the folding wings can be automatically unfolded and locked, and the unmanned aerial vehicle is convenient to use. And normal flight of the unmanned aerial vehicle is not influenced.
本发明公开了一种复合式制导自毁式巡飞固定翼无人机,包括发射筒和无人机本体,所述发射筒内部设有弹射机构,所述发射筒用于对无人机本体进行弹射,所述发射筒底部设有调节机构,所述调节机构用于对发射筒的角度进行调节,所述无人机本体两侧壁设有折叠翼机构,所述折叠翼机构用于为无人机本体提供升力,所述弹射机构包括高压气瓶、定位槽和弹射板,所述定位槽数量设为多个。本发明通过设置折叠翼机构可以使无人机本体两侧的多个折叠翼折叠在一起,从而可以减少无人机本体所占据的空间,进而可以方便对无人机本体进行存放或输送,同时在对无人机本体进行弹射后折叠翼可以自动展开并锁定,进而不会影响无人机的正常飞行。
Composite guidance self-destruction patrolling fixed-wing unmanned aerial vehicle
一种复合式制导自毁式巡飞固定翼无人机
2023-03-21
Patent
Electronic Resource
Chinese
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