Unmanned aerial vehicle, has airframe that is made with wing with ailerons that fold forward, vertical stabilizer, lifts, electric impeller engine with bifurcated air intake in upper part and tapering nozzle-shaped outlet device
	ISAEV G R; SHIPULIN M V; SHAIDULLIN T V; GOROBCHUK A R
	2023-11-20
专利权人	RUSSIAN FEDERATION MIN DEFENCE MILITARY (RUDE-C)
申请日期	2023-11-20
专利号	RU231317-U1
成果简介	NOVELTY - The vehicle has a modular airframe (1) that is made using an integrated circuit. The airframe is made with a forward folding wing (2) with ailerons that fold forward, a vertical stabilizer, lifts (4), an electric impeller engine with a bifurcated air intake in an upper part and a tapering nozzle-shaped outlet device (5) that are attached to the airframe. The attached parts of the vehicle are connected using grooves, hinged fasteners and secured with screws. The vehicle includes an internal combustion engine located in a rear part of a fuselage. A propulsion system is located in the rear part of the fuselage, where an operator unfolds the wing into a flight position. USE - Heavier-than-air aircraft unmanned aerial vehicle. ADVANTAGE - The vehicle ensures increasing maintainability in field conditions. DESCRIPTION OF DRAWING(S) - The drawing shows an exploded perspective view of an unmanned aerial vehicle. 1Modular airframe 2Forward folding wing 3Rudder 4Lifts 5Tapering nozzle-shaped outlet device
IPC 分类号	B64U-020/50
国家	俄罗斯
专业领域	信息技术
语种	英语
成果类型	专利
文献类型	科技成果
条目标识符	http://119.78.100.226:8889/handle/3KE4DYBR/19238
专题	中国科学院新疆生态与地理研究所
作者单位	RUSSIAN FEDERATION MIN DEFENCE MILITARY (RUDE-C)
推荐引用方式 GB/T 7714	ISAEV G R,SHIPULIN M V,SHAIDULLIN T V,et al. Unmanned aerial vehicle, has airframe that is made with wing with ailerons that fold forward, vertical stabilizer, lifts, electric impeller engine with bifurcated air intake in upper part and tapering nozzle-shaped outlet device. RU231317-U1[P]. 2023.

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