101. GROUND-EFFECT CRAFT AND METHOD FOR THE CRUISING FLIGHT THEREOF

申请号: PCT/RU2003/000247

申请日: 2003-05-30

公开（公告）号: WO2004009418A1

公开（公告）日: 2004-01-29

发明人:

The invention relates to flying vehicles. A centre wing is provided with aerodynamic profiles on the longitudinal sections thereof. A cigar-shaped fuselage is arranged on the central wing. A crew cabin and a cargo-passenger cabin are arranged inside the fuselage. Hollow hermetical longitudinal beams are mounted on the periphery of the central wing on the sides thereof. Inflatable shock-absorbing balloons are arranged under said longitudinal beams. Two keels provided with rudders are mounted on the ends of the longitudinal beams. A horizontal tail is arranged on the keels and comprises a diving rudder which is disposed on a section between the keels and ailerons which are disposed on the sections of the longitudinal beams. The thrust propeller for horizontal thrust is accommodated inside an external annular cowl. The engine for the thrust propeller is arranged inside the tail cone of the fuselage. A set of tale-off and landing devices comprises a means for producing a static air cushion. The cruising flight of the inventive ground-effect craft is carried out by the propeller thrust and a lifting force produced by the interaction of the central wing and a ram air and by the ground-effect of a ground or water surface. The height over ground or water surface must be equal to 0.1-0.5 of the mean chord of the central wing or to 0.2-0.9 of the span thereof when the angle of attack of the central wing is equal to 5-6 DEG , the horizontal propeller thrust ranges from 0.25 to 0.33 of the flying weight of the craft and the speed is equal to 200-280 km/h.

102. WING IN GROUND EFFECT VEHICLE WITH ENDPLATES

申请号: EP01931204.0

申请日: 2001-05-17

公开（公告）号: EP1286873B1

公开（公告）日: 2004-11-17

发明人: ALLEN, Ken, R.

A Wing In Ground Effect Vehicle has a pair of supercavitating endplates ( 17 ) which extend below the fuselage ( 2 ) such that they can be immersed in water during flight thereover. The endplates have a nose ( 28 ) defining a leading edge ( 20 ) and adapted to generate a supercavity. The endplates ( 17 ) typically pivot about a pivot axis P to provide a stabilising weathercock-type effect.

103. PITCH CONTROLLED GROUND EFFECT VEHICLE

申请号: EP85905013.0

申请日: 1985-07-22

公开（公告）号: EP0230412B1

公开（公告）日: 1992-12-09

发明人: HOWELL, Murrell D.; HOWELL, Mary E.

A vehicle utilizing a pair of counter rotating lift fans (36) driven by an air cooled internal combustion engine (34) provide compressed air into a plenum under a shell (26) moving the vehicle away from the surface upon which it is resting with the gas escape velocity evenly distributed around a peripheral skirt (28). A separate forward thrust fan (68) driven directly by a rotating pedestal mounted engine (56) provide the forward propulsion. An aileron (72) is rotatably mounted directly behind the thrust fan (68) and provides controlled response to the pitch direction of the vehicle by changing the angle of the air flow discharge. The vehicle contains a pair of movable keels (82) for operation on the water and side wings (86) to extend the effective surface of the craft.

104. Ground effect airplane

申请号: US10055411

申请日: 2001-10-29

公开（公告）号: US20030080243A1

公开（公告）日: 2003-05-01

发明人: Zachary C. Hoisignton; Blaine K. Rawdon

An extremely large aircraft which is suitable for overseas cargo transport and which includes a fuselage defining a central storage cavity, a wing assembly defining a pair of wing storage cavities, an altitude control system, and a plurality of independently steerable landing gear units. The central storage cavity has a length, height and width of at least 100 feet, at least 16 feet and at least 24 feet, respectively. The wing assembly has a wingspan of at least 300 feet and is configured with a moderate aspect ratio to permit both ground-effect and high altitude operation. The altitude control system controls the aircraft in ground effect such that the aircraft is maintained at about a predetermined altitude. The landing gear units are coupled to the fuselage and are arranged in at least two discrete columns and at least ten discrete rows. The central storage cavity and the wing storage cavities are configured to receive cargo including intermodal re-usable cargo containers.

105. 全翼型地面效應船舶

申请号: TW086215671

申请日: 1997-09-12

公开（公告）号: TW409696U

公开（公告）日: 2000-10-21

发明人: 溫志湧; 陳彥明

一種全翼型具有地面效應的船舶，係利用機翼本身就是機身的概念。該機身本身左右各具有一個可上下移動的翼端阻流板，以增加飛行的高度，機身的前方有一組副翼，後方則有一組姿態控制翼(副翼與水平安定面)，機身前方下緣具有一高壓空氣噴出口以降低黏滯阻力，提供起飛所需。本載具主要的機械組成包括了：一大面積主翼，此主翼即是機身，前後各有一組對稱的姿態控制翼，左右各有一個翼端阻流板，空氣噴出裝置。

106. Ground-surface-effect wing plane

申请号: US556253

申请日: 1990-07-19

公开（公告）号: US5065833A

公开（公告）日: 1991-11-19

发明人: Toshio Matsuoka; Akio Higashida; Tokuki Satake

An improved ground-surface-effect winged craft has a main body in the shape of an airfoil, side plates extending nearly vertically at the opposite lateral sides of the main body for intercepting air flowing outwards from the underside of the main body, side plate floats provided at the side plates, a float provided at a central lower portion of the main body, an operator's seat provided on the float, vertical and horizontal tails provided at a rear portion of the main body, and a propelling device for lifting and propelling the airframe of the craft by making use of both a power augment ramwing effect with the horizontal tail and a ground-surface-effect generated between the main body and a flat surface such as a water surface or a ground surface.

107. WING IN GROUND EFFECT VEHICLE WITH ENDPLATES

申请号: PCT/AU2001/000564

申请日: 2001-05-17

公开（公告）号: WO01087682A1

公开（公告）日: 2001-11-22

发明人:

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.

108. 피치제어식 공기쿠션차량

申请号: KR1019870700215

申请日: 1985-07-22

公开（公告）号: KR1019920002408B1

公开（公告）日: 1992-03-23

发明人: 머렐디이.하우웰

내용 없음.

109. 종판을 구비한 지면효과익선

申请号: KR1020027015494

申请日: 2001-05-17

公开（公告）号: KR100730600B1

公开（公告）日: 2007-06-21

发明人: 알랜켄알

A Wing In Ground Effect Vehicle has a pair of supercavitating endplates ( 17 ) which extend below the fuselage ( 2 ) such that they can be immersed in water during flight thereover. The endplates have a nose ( 28 ) defining a leading edge ( 20 ) and adapted to generate a supercavity. The endplates ( 17 ) typically pivot about a pivot axis P to provide a stabilising weathercock-type effect.

110. 加大浮力之地面效應氣墊

申请号: TW086111374

申请日: 1997-08-08

公开（公告）号: TW349065B

公开（公告）日: 1999-01-01

发明人: 威廉C.瓦特

本發明之加大浮力之地面效應氣墊之特徵在具有二對環形之同心氣幕噴嘴及增壓噴嘴，其引導對應之噴射氣流向下及向內地進入該氣墊之面朝下之浮力面之下方，噴嘴之同心配置係提供一由一內部中央氣幕所環繞之內部或中央增壓氣墊，及一為外圍氣幕所環繞之外部或外圍氣墊。本發明之加大浮力之地面效應氣墊係藉由引導一氣流流經該氣墊之向下彎曲之外圍表面，以提供一增大之用以浮起該氣墊之力，而該力較先前之地面效應裝置所提供者大。當氣流沿著該氣墊之外圍曲面向下流動時產生一壓力梯度，該壓力梯度提供一支撐該氣墊之額外力量。該氣流及噴射氣流係來自一安裝於該氣墊外部之螺旋槳或風扇裝置，該外部安裝具有二項優點：第一，可消除起因於噴射氣流源之螺旋槳或風扇失速；第二，可平順地轉移至自由空氣(無地面效應)，此為航行於河流、峽谷及其他型式之天然障礙物所必須，其中該障礙物會破壞地面效應之運作。

111. 계단식 날개형 지면 효과 비행기

申请号: KR1019950029529

申请日: 1995-09-05

公开（公告）号: KR1019970015405A

公开（公告）日: 1997-04-28

发明人: 이희우

본 발명은 지면효과 비행기에 관한 것으로 기존의 지면효과 비행기의 피치 불안정성을 제거하고 파도 조우시의 생존성 능력을 향상시키기 위하여 주날개를 전후방 2단으로 계단식으로 장착함으로써 전방주익은 파도로부터 충분한 격리될 수 있으며, 후방주익이 전방주익의 지면효과를 유발시킴으로써 전체적으로 비행 안전성을 높인 지면효과 비행기임. 본 발명에 의한 계단식 날개형 지면효과 비행기는 병력 신속이동 등의 군수용과, 승객 및 화물 수송을 위한 민수용으로 운용될 수 있다.

112. Ground Effect Vanes Arrangement

申请号: US12224549

申请日: 2007-03-01

公开（公告）号: US20090084907A1

公开（公告）日: 2009-04-02

发明人: Raphael Yoeli

A vehicle, particularly a VTOL air vehicle, includes a duct carried by the vehicle frame with the longitudinal axis of the duct perpendicular to the longitudinal axis of the vehicle frame; a propeller rotatably mounted within the duct about the longitudinal axis of the duct to force an ambient fluid therethrough from its inlet at the upper end of the duct through its exit at the lower end of the duct, and thereby to produce an upward lift force applied to the vehicle, and a plurality of spaced vanes mounted to and across the inlet and exit ends of the duct about axes substantially perpendicular to the longitudinal axis of the duct and selectively operational to produce a desired horizontal control force in addition to the lift force applied to the vehicle.

113. Winged ground effect machines

申请号: US29448963

申请日: 1963-07-12

公开（公告）号: US3244246A

公开（公告）日: 1966-04-05

发明人: WALTER WEILAND CARL

114. PITCH CONTROLLED GROUND EFFECT VEHICLE

申请号: PCT/US1985001386

申请日: 1985-07-22

公开（公告）号: WO1987000492A1

公开（公告）日: 1987-01-29

发明人:

A vehicle utilizing a pair of counter rotating lift fans (36) driven by an air cooled internal combustion engine (34) provide compressed air into a plenum under a shell (26) moving the vehicle away from the surface upon which it is resting with the gas escape velocity evenly distributed around a peripheral skirt (28). A separate forward thrust fan (68) driven directly by a rotating pedestal mounted engine (56) provide the forward propulsion. An aileron (72) is rotatably mounted directly behind the thrust fan (68) and provides controlled response to the pitch direction of the vehicle by changing the angle of the air flow discharge. The vehicle contains a pair of movable keels (82) for operation on the water and side wings (86) to extend the effective surface of the craft.

115. КРЫЛАТАЯ РАКЕТА-ЭКРАНОЛЕТ (КРЭ)

申请号: PCT/RU2016/000557

申请日: 2016-08-17

公开（公告）号: WO2017030470A1

公开（公告）日: 2017-02-23

发明人: КОЖЕВНИКОВ, Дмитрий Дмитриевич

Изобретение относится к крылатым ракетам большой дальности. Крылатая ракета - экранолет состоит из корпуса, несущих крыльев, аэродинамических элементов управления полетом, маршевого двигателя, антенны обзора, поиска цели и наведения, высотомера и боевой части. Корпус и несущие крылья выполнены в виде «летающего крыла» с большой площадью и средней длиной хорды несущей поверхности с возможностью лететь с или без использования эффекта «экрана». Корпус «летающее крыло» складывается гармошкой вдоль продольной оси симметрии ракеты с регулируемой степенью сложения. Маршевый двигатель выполнен с возможностью работы с регулировкой в диапазонах дозвуковых и сверхзвуковых скоростей и расположен внутри шарнира складывающихся сегментов корпуса. Крылатая ракета имеет более одного маршевого двигателя, которые работают в одном режиме или предназначены для разных диапазонов скоростей с частичным перекрытием диапазонов, работающие с перестройкой одновременно в перекрываемом диапазоне и по отдельности, каждый в своем диапазоне, с возможностью многократного чередования их работы. Как минимум один маршевый двигатель может отделяться от крылатой ракеты. Изобретение позволяет увеличить дальность полёта, повысить поражающую способность, компактность при хранении и транспортировке.

116. Wing In Ground Effect Hydrofoil Vessel

申请号: US11308532

申请日: 2006-04-03

公开（公告）号: US20070245943A1

公开（公告）日: 2007-10-25

发明人: Mark Rice

The present invention concerns a marine vehicle that derives its lift and control forces and moments from a combination of the following mechanisms; aerodynamic effects on a lifting surface in ground effect, hydrodynamic effects on submerged hydrofoils, planing forces on deployed winglets, and hydrostatic effects on submerged elements. The portion of the overall lift and control forces that is contributed by each mechanism varies as a function of vessel speed. The hydrofoils may be subcavitating, supercavitating, transcavitating or superventilated. The three lift and control mechanisms are individually found on existing Wing-In-Ground Effect (WIG) vehicles, hydrofoil vessels, and multi-hull vessels but have not previously been combined in the manner described. The present invention combines these three elements to achieve high lift-to-drag ratios, low fuel consumption, good maneuverability, low noise, low vessel draft, low vessel motions, and operation in higher sea states at all relative headings to the wind and waves. Applications of this craft include both civilian and military uses.

117. LIFT AUGMENTED GROUND EFFECT PLATFORM

申请号: EP97937180.4

申请日: 1997-08-08

公开（公告）号: EP0999965A1

公开（公告）日: 2000-05-17

发明人: WALTER, William, C.

A lift augmented ground effect platform characterized by two pair of annular concentric air curtain nozzles (32, 33) and supercharge nozzles (46, 64) which direct respective jet streams downward and inward beneath the platform downwardly facing lifting surface (38). The concentric arrangement of the nozzles provides a central supercharged air cushion surrounded by an inner air curtain and a peripheral air cushion surrounded by a peripheral air curtain. This arrangement provides an increased augmentation of the forces acting to raise the platform over that experienced in prior ground effect devices by directing an air flow stream over the downwardly curved peripheral surface of the platform. As the air flows downwardly along the platform's peripheral surface, it creates a pressure differential which provides an additional force supporting the platform. The airflow stream and the jet stream are provided by a propeller or rotating fan (54) mounted exterior or interior of the platform.

118. Wing in ground effect vehicle

申请号: US831635

申请日: 1977-09-08

公开（公告）号: US4151893A

公开（公告）日: 1979-05-01

发明人: Peter J. Mantle

A wing in ground effect (WIG) vehicle, the body of which is a low aspect io airfoil. Soft end plates allow for proper sealing of pressure below the wing while preventing the transmittal of wave action forces to the vehicle. Fin rudders and a dorsal fin provide turning control. Efflux from the propulsor engines can be split to flow both over and under the wing so that the vehicle will be capable of both rapid movement and hover over both land and water. Two designs are disclosed providing this vehicle with the ability to jump out of ground effect mode to avoid obstacles appearing in its flight path.