发明名称 FLYING VEHICLE
摘要 <p>The invention relates to aviation namely to flying vehicles adapted to ride on an air cushion and to effect a take-off and landing on aerodromes of any category. The goal of the invention is to design a flying vehicle capable of aerodinamically efficient flight both at low and high level flight, as well as take-off and landing from non-prepared aerodromes and from water under the conditions of stabilization and movement control of all flight regimes. The goal is achieved due to the fact that in a flying vehicle comprising a fuselage in the form of a carrying wing, a power installation, a take-off and landing air cushion device, a gasodynamic system of boundary layer control, a device for controlling the position of flow leaving the trailing edge as well as stabilization and flight control systems, the take-off and landing air cushion device consists of a propelling slot nozzle (12) and side skegs (17) between which are mounted rotatable flaps (21, 22, 23) controlling the flight of the vehicle and regulating the position of the pressure centre on the bottom. The fuselage has the form of a cylindrical segment conjugating at its sides with spherical fairings. <IMAGE></p>
申请公布号 EP0596131(B1) 申请公布日期 1997.12.29
申请号 EP19930905682 申请日期 1993.01.21
申请人 NAUCHNO-PROIZVODSTVENNAYA KOOPERATIVNAYA FIRMA "EKIP" 发明人 SAVITSKY, ANATOLY IVANOVICH;SCHUKIN, LEV NIKOLAEVICH;KARELIN, VIKTOR GEORGIEVICH;PUSHKIN, ROSTISLAV MIKHAILOVICH;MASS, ALEXANDR MIKHAILOVICH;SHIBANOV, ANATOLY PETROVICH;SCHUKIN, ILYA LVOVICH;KHUTSISCHVILI, VLADIMIR GEORGIEVICH;FISCHENKO, SERGEI VIKTOROVICH;ERMISCHIN, ALEXANDR VIKTOROVICH;SOBKO, ALEXANDR PAVLOVICH
分类号 B60V3/08;B60V1/00;B60V1/22;B64C21/00;B64C29/00;B64C39/00;B64C39/10;(IPC1-7):B64C39/00 主分类号 B60V3/08
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