发明名称 VERTICAL TAKEOFF AND LANDING FLYING VEHICLE
摘要 FIELD: heavier-than-air flying vehicles. SUBSTANCE: proposed flying vehicle includes unit for forming controllable flow of gas to takeoff, horizontal flight and landing. Case of flying vehicle is made in form of hemisphere with horizontal bottom. Located along vertical radius of hemisphere coaxially with it is tube with powerful gas or liquid fuel burner located inside it. Dampers made over outer surface of tube are movable along it projecting above spherical surface of flying vehicle. Flow of hot gas formed during combustion of fuel rises entrapping surrounding air. Artificial vortex is formed on spherical surface of flying vehicle during motion of air and pressure of gases on spherical surface becomes lower atmospheric pressure. EFFECT: simplified construction; enhanced control. 2 dwg
申请公布号 RU2219104(C1) 申请公布日期 2003.12.20
申请号 RU20020124502 申请日期 2002.09.16
申请人 发明人 TSIVINSKIJ S.V.
分类号 B64C29/00;(IPC1-7):B64C29/00 主分类号 B64C29/00
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