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    FLYING VEHICLE
    2.
    发明申请
    FLYING VEHICLE 审中-公开
    飞行车辆

    公开(公告)号：WO1993024366A1

    公开(公告)日：1993-12-09

    申请号：PCT/RU1993000019

    申请日：1993-01-21

    Applicant: NAUCHNO-PROIZVODSTVENNAYA KOOPERATIVNAYA FIRMA ... ,  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

    Inventor： NAUCHNO-PROIZVODSTVENNAYA KOOPERATIVNAYA FIRMA ...

    IPC: B64C39/00

    CPC classification number: B64C39/10 ,  B60V1/22 ,  B64B2201/00 ,  B64C39/00 ,  Y02T50/12

    Abstract: 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 aerodynamically 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.

    Abstract translation: 本发明涉及航空，即适用于乘坐气垫的飞行车辆，以及在任何类别的机场起飞和降落。 本发明的目标是设计一种能够在低和高水平飞行中进行空中动力学有效飞行的飞行器，以及在所有的稳定和运动控制条件下从未准备的机场和水中起飞和着陆 飞行政权 目的是实现这样的事实，即在包括机身形式的机身，动力装置，起飞和着陆气垫装置，边界层控制的气动系统，控制装置 离开后缘的流动位置以及稳定和飞行控制系统，起飞和着陆气垫装置包括推进式狭缝喷嘴（12）和侧部塞子（17），在其间安装有可旋转的翼片（21， 控制车辆的飞行并调节压力中心在底部的位置。 机身具有圆柱形段的形式，其侧面与球形整流罩共轭。

    FLYING VEHICLE
    3.
    发明公开
    FLYING VEHICLE 失效
    FLUGOBJEKT。

    公开(公告)号：EP0596131A1

    公开(公告)日：1994-05-11

    申请号：EP93905682.6

    申请日：1993-01-21

    Applicant: NAUCHNO-PROIZVODSTVENNAYA KOOPERATIVNAYA FIRMA "EKIP"

    Inventor： 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

    IPC: B64C39/00 ,  B64C29/00 ,  B60V3/08

    CPC classification number: B64C39/10 ,  B60V1/22 ,  B64B2201/00 ,  B64C39/00 ,  Y02T50/12

    Abstract: 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.

    Abstract translation: 本发明涉及航空，即适用于乘坐气垫的飞行车辆，以及在任何类别的机场上起飞和降落。 本发明的目的是设计一种能够在低和高水平飞行中进行航空飞行高效飞行的飞行器，以及在所有的稳定和运动控制的条件下从未准备的机场和水中起飞和着陆 飞行政权 目标是实现这样的事实，即在飞行载体中包括机身形式的机身，动力装置，起飞和着陆气垫装置，边界层控制的气动系统，控制装置 离开后缘的流动位置以及稳定和飞行控制系统，起飞和着陆气垫装置包括推进式狭缝喷嘴（12）和侧部销钉（17），在其间安装有可旋转的折翼（21， 控制车辆的飞行并且调节压力中心在底部的位置。 机身具有圆柱形段的形式，其侧面与球形整流罩共轭。

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