FLYING VEHICLE.
    2.
    发明公开
    FLYING VEHICLE. 失效
    FLUGOBJEKT。

    公开(公告)号:EP0596131A4

    公开(公告)日:1994-10-19

    申请号:EP93905682

    申请日:1993-01-21

    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,即涉及适于乘坐气垫并在任何类别的机场上起飞和降落的飞行器。 本发明的目的在于设计一种飞行器,该飞行器能够在低水平和高水平飞行中以空气动力学高效飞行,以及在所有飞行器的稳定和运动控制条件下从未准备好的机场和从水中起飞和着陆 飞行状态。 该目标是由于以下事实而实现的,即在包括机翼形式的机身,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 离开后缘以及稳定和飞行控制系统的流动位置,起飞和着陆气垫装置包括推进槽喷嘴(12)和侧ske鳍(17),在它们之间安装可旋转襟翼(21, 22,23)控制车辆的飞行并且调节压力中心在底部的位置。 机身具有圆柱形部分的形式,其侧面与球形整流罩结合。

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