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1. 发明申请

WO1993024366A1 FLYING VEHICLE 审中-公开
标题翻译：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
申请人： 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
发明人： NAUCHNO-PROIZVODSTVENNAYA KOOPERATIVNAYA FIRMA ...
IPC分类号： B64C39/00
CPC分类号： B64C39/10 , B60V1/22 , B64B2201/00 , B64C39/00 , Y02T50/12
摘要： 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.
摘要翻译：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。

2. 发明申请

WO1993019963A1 GROUND EFFECT VEHICLE 审中-公开
标题翻译：翼地效应机
公开(公告)号：WO1993019963A1
公开(公告)日：1993-10-14
申请号：PCT/DE1993000312
申请日：1993-03-29
申请人： BLUM, Klaus
IPC分类号： B60V01/22
CPC分类号： B60V1/22
摘要： The invention concerns a ground effect vehicle capable of floating on water, the vehicle having at least one wing assembly comprising a pair of wings located one on each side of the fuselage. A thrust-generator (4) may be located forward of each pair of wings. Each wing (2) has a trailing-edge flap (7) for lift and lateral control fitted so that it can pivot plus, located under the wings (2) and associated with the thrust-generators (4), airflow channels which are oriented in a given direction or whose orientation can be adjusted. The aim of the invention is to protect the thrust-generators from water spray. The invention is characterized in that the wings (2) are mounted on top of the fuselage (1), and fitted aft of each wing (2) is an additional wing (8) located below the level of the wing (2).

3. 发明申请

WO2005039976A1 A FLYING-FISH AIRBOAT 审中-公开
公开(公告)号：WO2005039976A1
公开(公告)日：2005-05-06
申请号：PCT/CN2004/001211
申请日：2004-10-25
IPC分类号： B64C35/00
CPC分类号： B63B1/322 , B60V1/08 , B60V1/22 , B60V3/06 , Y02T70/12
摘要： The invention provides a flying-fish airboat comprising of a hull, airfoils disposed on boch sides of the hull, a rudder which is formed on the rear end of the hull and has a shape of prolate cylinder, and one or more screw propellers formed under the rudder; wherein the hull is above water surface when the airboat is flying. The advantages of present invention lie in: compared with the prior art, the propeller power is under the water and the hull is in the air, so it can reduce the drag and energy consumption, increase the running speed, reduce the noise, and alleviate the surge phenomena behind the hull. The structure of flying-fish airboat is simple and the airboat has broad range of application. It can be not only a novel hydro-transport facility, but also a sport equipment which can be used in a sport match.

4. 发明申请

WO1998041442A1 MULTIHEAD AIR CUSHIONED MARINE VEHICLE 审中-公开
标题翻译：多海航空海上车辆
公开(公告)号：WO1998041442A1
公开(公告)日：1998-09-24
申请号：PCT/US1997004780
申请日：1997-03-14
申请人： BURG, Donald, E.
IPC分类号： B63B01/12
CPC分类号： B60V1/22
摘要： A multi-hulled gas cushion supported marine vehicle (40) that is capable of transition to airborne surface effect operation is presented. The marine vehicle (40) has optional elongated knife shaped bows (71) that slice into waves, very fine entry and low angle of divergence supporting gas cushions (47), water rejecting steps (68) that extend high onto the sidehulls (60), and retractable water stabilizers (41) to insure optimum performance in heavy seas. The retractable water stabilizers (41) are in the form of inverted-T hydrofoils and/or small boat shaped members. It also has special, normally inverted-V shaped, gas cushion and wetdeck aft seals (80, 81) to insure minimum effect of wave impacts in those areas. The gas pressurization system normally includes powered blowers (43) where a flap-like sealing device (75) can be installed to seal gas leakage. Connecting ducts (67) between gas cushions can include venturis that restrict pressure pulses in one gas cushion from traveling to another gas cushion. Retractable or fixed sidewings (90) are optional and may include outrigger hulls (92).
摘要翻译：提出了一种能够过渡到空中表面效应操作的多壳气垫支撑船用车辆（40）。船舶（40）具有可选的细长的刀形弓（71），其切成波浪，非常细的入口和支撑气垫（47）的低发散角度，高度延伸到侧翼（60）上的排水步骤（68）和可伸缩水稳定器（41），以确保在大海上的最佳性能。可伸缩水稳定器（41）是倒T型水翼和/或小船形构件的形式。它还具有特殊的，通常为倒V形的气垫和湿趾尾密封（80,81），以确保这些区域的波浪影响的最小影响。气体加压系统通常包括动力鼓风机（43），其中可安装翼状密封装置（75）以密封气体泄漏。气垫之间的连接管道（67）可以包括限制一个气垫中的压力脉冲行进到另一个气垫的通风口。伸缩或固定侧翼（90）是可选的，并且可以包括外伸支架（92）。

5. 发明申请

WO1993011986A1 AIR-CUSHION FLYING VEHICLE 审中-公开
标题翻译：空中飞行车
公开(公告)号：WO1993011986A1
公开(公告)日：1993-06-24
申请号：PCT/RU1992000238
申请日：1992-12-11
申请人： KIZILOV, Viktor Nikolaevich
IPC分类号： B60V03/08
CPC分类号： B60V1/22
摘要： A flying vehicle comprises a forcibly collapsible air cushion (2) located along the periphery of the lower part of the body (1) whose lower nose part is shaped as a hydroplaning surface (3) limited by a planing step (4) behind which is located the nose part of the air-cushion flexible skirt (2) behind the stern part of which is located a hydroplaning support (7) mounted with the possibility of its deviation.
摘要翻译：飞行器包括沿着主体（1）的下部的周边设置的强制可折叠的气垫（2），其下部鼻部形成为由刨削步骤（4）限制的滑水表面（3）位于其船尾部分后面的气垫柔性裙部（2）的鼻部部分，其安装有可能偏移的滑水支撑件（7）。

6. 发明申请

WO2014174401A1 HOVERCRAFT WITH MULTIPLE, INDEPENDENTLY-OPERABLE LIFT CHAMBERS. 审中-公开
标题翻译：具有多个独立操作的升降台。
公开(公告)号：WO2014174401A1
公开(公告)日：2014-10-30
申请号：PCT/IB2014/060626
申请日：2014-04-10
申请人： GREGORY, John , WAGAMAN, Woodrow
发明人： GREGORY, John , WAGAMAN, Woodrow
IPC分类号： B60V1/06
CPC分类号： B60V1/043 , B60V1/11 , B60V1/18 , B60V1/22
摘要： The invention is a hovercraft with multiple lift chambers which are operable independently of each other. Independently-operable pivot arm assemblies connect each lift chamber to the hovercraft main body, and his gives the hovercraft the ability to travel over uneven surfaces, traverse obstacles that would block conventional hovercrafts, and climb or descend even severe inclines. The hovercraft also includes side thrusters which allow it to maintain its vertical position on an incline while traveling laterally across the incline.
摘要翻译：本发明是具有多个提升室的气垫船，它们彼此独立地可操作。独立可操作的枢转臂组件将每个提升室连接到气垫船主体，并且他给予气垫船在不平坦的表面上行进的能力，穿过阻挡常规气垫船的障碍物，甚至爬升或下降甚至严重的倾斜。气垫船还包括侧推进器，允许其在横向横过斜坡的同时保持其在倾斜处的垂直位置。

7. 发明申请

WO01087682A1 WING IN GROUND EFFECT VEHICLE WITH ENDPLATES 审中-公开
标题翻译：地面效应车辆与终点车
公开(公告)号：WO01087682A1
公开(公告)日：2001-11-22
申请号：PCT/AU2001/000564
申请日：2001-05-17
IPC分类号： B60V3/08 , B60V1/08 , B60V1/22 , B60V1/18
CPC分类号： B60V1/22 , B60V1/08
摘要： A wing-in-ground effect vehicle has endplates (17) at the ends of wings (3). These extend below fuselage (2) and are designed for constant submergence during flight over water. The nose of each endplate (17) is designed to generate a supercavity extending the length of endplate (17) at cruising speed. To facilitate lengthening of the supercavity at lower speeds, protruding ridges may be provided downstream from each nose. At least the rear portions of endplates (17) are laterally displaceable (eg due to pivoting around a vertical axis) to avoid damage to endplates (17) by water pressure when the vehicle travels at a yaw angle. This "weathercocking" of endplates (17) aligns them with the water flow and allows them to be narrower.
摘要翻译：机翼地面效应车辆在机翼（3）的端部处具有端板（17）。这些延伸到机身（2）以下，并设计用于在水中飞行期间不断淹没。每个端板（17）的鼻部被设计成以巡航速度产生延伸端板（17）的长度的超空腔。为了便于以较低的速度延长超空腔，可以在每个鼻子的下游设置突出的脊。端板（17）的至少后部可横向移动（例如由于围绕垂直轴线枢转），以避免当车辆以偏航角行驶时，通过水压损坏端板（17）。端板（17）的这种“风标”使它们与水流一致，并允许它们变窄。

8. 发明申请

WO99033690A1 WING-IN-GROUND-EFFECT VEHICLE WITH STATIC AIR CUSHIONS FOR LOW SPEEDS AND HOVERING (WIG-ACV) 审中-公开
标题翻译：带有静态空气垫圈的低功率和低功率的WING-IN-GROUND-EFFECT车辆（WIG-ACV）
公开(公告)号：WO99033690A1
公开(公告)日：1999-07-08
申请号：PCT/RU1998/000063
申请日：1998-03-06
IPC分类号： B60F5/02 , B60V1/08 , B60V1/10 , B60V1/22 , B63B1/32 , B64C29/00
CPC分类号： B60V1/22 , B60V1/08 , B60V1/10
摘要： The invention relates to the field of transportation and concerns Wing-In-Ground-Effect vehicles (WIGs, also called Ekranoplans). Specifically, a WIG vehicle capable of starting and landing on unprepared terrain or water surfaces. This vehicle incorporates new lift-increasing features, namely a system using ducted lift fans (5) suctioning air from the wing upper surfaces and creating a multi-chamber air cushion under the fuselage (1) and wings (9) of the vehicle. Each lift fan will be powered by a turbine actuated by high-pressure combustion gases diverted from the main power units (4). The WIG's flight control system distributes power between the lift fans and the forward propulsion units (8), through valves (6) in the high-pressure gas conducts (7) leading to turbines (19) powering the lift fans or the forward propulsion units. Starting with 100 % of the power directed to the lift fans for hovering, the available power is gradually transferred to the forward propulsion units. As the speed increases, an increasing amount of lift is generated dynamically until the Wing-In-Ground effect is enough to carry the vehicle on its own and 100 % of the power is available for forward thrust. The lift fans are mounted in the fuselage-wing junctions and suspended passenger or freight modules (11) can be fastened to the wing end plates (10).
摘要翻译：本发明涉及运输领域，涉及地面效应车辆（WIG，也称为Ekranoplans）。具体来说，WIG车辆能够在无准备的地形或水面上起飞和着陆。该车辆结合了新的提升功能，即使用管道升降风扇（5）从机翼上表面吸入空气的系统，并在车辆的机身（1）和机翼（9）下方形成多室气垫。每个提升风扇将由从主动力单元（4）转向的高压燃烧气体致动的涡轮机供电。 WIG的飞行控制系统通过高压气体导管（7）中的阀（6）在升降机风扇和前进推进单元（8）之间分配动力，从而通向为提升风机或前进推进单元供电的涡轮机（19）。从100％的电力指向升降机风扇开始盘旋，可用功率逐渐转移到前进推进单元。随着速度的增加，动力产生的电梯数量增加，直到地面效应足以使车辆独立运行，并且100％的功率可用于向前推力。升降机风扇安装在机身翼连接处，悬挂的乘客或货运模块（11）可以固定在机翼端板（10）上。

9. 发明申请

WO2014068115A1 PLANING HYDROFOILS FOR MARINE CRAFT 审中-公开
标题翻译：为海洋工程建设水电站
公开(公告)号：WO2014068115A1
公开(公告)日：2014-05-08
申请号：PCT/EP2013/072947
申请日：2013-11-04
申请人： DUNCAN, Ian James
发明人： DUNCAN, Ian James
IPC分类号： B63B1/18 , B63B1/24
CPC分类号： B63B1/18 , B60V1/08 , B60V1/22 , B60V3/065 , B63B1/248 , B63B9/002
摘要： A hydrofoil (20) for mounting to a high speed surface vessel arranged for planing operation at least at higher craft speeds and in which the trailing edge (202) remain substantially fully wetted at all craft speeds when operating under calm conditions.
摘要翻译：一种用于安装到高速表面容器的水翼（20），其布置成至少在较高的飞行速度下进行刨削操作，并且其中在平静的条件下操作时，后缘（202）在所有飞行速度下基本上完全润湿。

10. 发明申请

WO1997030886A1 MULTIPLE-MODE WING-IN GROUND EFFECT VEHICLE 审中-公开
标题翻译：多模式WING-IN地面效应车辆
公开(公告)号：WO1997030886A1
公开(公告)日：1997-08-28
申请号：PCT/US1997002691
申请日：1997-02-24
申请人： KLEM, Richard, H.
IPC分类号： B63B01/24
CPC分类号： B60V1/08 , B60V1/22 , B63B1/322 , Y02T70/12
摘要： A high-speed air-supported vehicle capable of multiple mode operations as both a water-contacting vehicle and an aircraft includes an aero roll-stabilizing plan form (3), a stabilizing ski/hydrofoil below a planing surface of a hull portion of the aero roll-stabilizing plan form (3) for providing stabilization and lift to the plan form (3) in at least one mode of operation, the ski/hydrofoil being mounted to a front underside of a hull portion of the aero roll-stabilizing plan form (3) and being mounted forward of a centre of gravity of the plan form (3), whereby a leading edge of the plan form is kept at a substantially constant level with respect to a surface of water during at least one mode of operation. A stabilizing ski (9) provides stabilization and lift in at least one mode of operation. A flexible ski mount (7, 8) is provided for mounting the stabilizing ski (9) to the aero roll-stabilizing plan form (3). Trim flaps (105) are provided for altering the direction of the plan form (3), and turning vanes (5a, 5b) are provided to reduce turbulence originating near the edge of the tip plates (71a, 71b).
摘要翻译：能够作为水接触车辆和飞行器进行多模式操作的高速空中支撑车辆包括航空辊稳定计划形式（3），在船体部分的刨面下方的稳定滑雪/水翼用于在至少一种操作模式下提供稳定和提升到计划形式（3）的航空滚动稳定计划表格（3），滑雪/水翼安装在航空辊稳定计划的船体部分的前下侧形式（3）并且被安装在平面形式（3）的重心的前方，由此在至少一种操作模式期间，平面形式的前缘相对于水面保持在基本恒定的水平。稳定滑雪板（9）提供至少一种操作模式的稳定和提升。提供了一种用于将稳定滑雪板（9）安装到气动滚动稳定平台（3）上的柔性滑雪板（7,8）。提供修整翼片（105）用于改变平面形式（3）的方向，并且设置转动叶片（5a，5b）以减少起始端板（71a，71b）边缘附近产生的湍流。

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