地面效应相关的专利数据

序号	专利名	申请号	申请日	公开（公告）号	公开（公告）日	发明人
101	계단식 날개형 지면 효과 비행기	KR1019950029529	1995-09-05	KR1019970015405A	1997-04-28	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.
102	Ground Effect Vanes Arrangement	US12224549	2007-03-01	US20090084907A1	2009-04-02	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.
103	Winged ground effect machines	US29448963	1963-07-12	US3244246A	1966-04-05	WALTER WEILAND CARL

104	PITCH CONTROLLED GROUND EFFECT VEHICLE	PCT/US1985001386	1985-07-22	WO1987000492A1	1987-01-29
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.
105	КРЫЛАТАЯ РАКЕТА-ЭКРАНОЛЕТ (КРЭ)	PCT/RU2016/000557	2016-08-17	WO2017030470A1	2017-02-23	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.
106	Wing In Ground Effect Hydrofoil Vessel	US11308532	2006-04-03	US20070245943A1	2007-10-25	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.
107	LIFT AUGMENTED GROUND EFFECT PLATFORM	EP97937180.4	1997-08-08	EP0999965A1	2000-05-17	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.
108	Wing in ground effect vehicle	US831635	1977-09-08	US4151893A	1979-05-01	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.
109	Gimbal ground effect vehicles	US10735071	1971-01-18	US3827527A	1974-08-06	BERTELSEN W
Ground effect vehicles including power means for providing a flow of gas and gimbal mounted flow-directing means for selectively directing the flow of gas into a lift component and a propulsion or control component. The propulsion or control component acts directly from the flow-directing means and is directed over the top of a deck or platform. Single and multiengine versions are disclosed, and eye lid devices which cooperate with the flow-directing means to reduce loss of liftgas are described.
110	Plenum chamber ground effect machine	US7125260	1960-11-23	US3195665A	1965-07-20	BEARDSLEY MELVILLE W

111	Sumersible ground effect machine	US18214562	1962-03-23	US3127863A	1964-04-07	TINAJERO AUIBAL A

112	ЭКРАНОЛЕТ ВНЕАЭРОДРОМНОГО БАЗИРОВАНИЯ	PCT/RU2015/000099	2015-02-16	WO2015126283A1	2015-08-27	ФИЛИМОНОВ, Александр Иосифович
Изобретение относится к авиации и касается летательных аппаратов (ЛА), способных совершать полет на небольшой высоте в режиме экранолета, а также вблизи земной поверхности в режиме экраноплана и на большой высоте как обычный самолет. Экранолет внеаэродромного базирования содержит центроплан в виде пилотско-пассажирской кабины, тоннель, расположенный сзади внутри центроплана, нагнетатель воздушной подушки, размещенный в нижней части тоннеля, хвостовое оперение, закрепленное сзади центроплана на двух балках, имеющее два киля, сверху которых расположено горизонтальное оперение, взлетно-посадочное устройство в виде шасси на воздушной подушке (ШВП). ШВП содержит заднюю и переднюю поворотные заслонки и два поплавка-скега, расположенные под центропланом с его боков. При этом верхняя поверхность центроплана имеет профильный коллекторный канал. При реализации изобретения достигается повышение безопасности на взлетно-посадочных режимах, увеличение аэродинамической подъемной силы, а также снижение массы конструкции.
113	Axial flow ground effect machine	US3486577D	1965-10-21	US3486577A	1969-12-30	JACKES ARTHUR M

114	확장판 구동기어를 이용한 위그선의 지면효과 증강 및조절장치	KR1020070112373	2007-11-05	KR1020090046318A	2009-05-11	여동진; 김무롱; 이창민; 강창구
본 발명은 위그선 날개의 끝단부에 존재하는 판 형상의 구조물이 날개의 상·하 또는 상하 양방향으로 확장하여 지면효과를 증강시키는 장치로서, 위그선이 수면에서 이동하거나 이·착수하는 과정에서는 판 형상의 구조물이 접혀있되 위그선이 수면 위를 항주하는 과정에서는 판 형상의 구조물이 확장하여 지면효과를 증강시키도록 함으로써, 위그선이 수면에서 이동하거나 이·착수하는 과정에서 날개의 끝단이 수면에 잠기어 물에 의한 큰 저항을 받아 날개가 파손될 위험이나 위그선의 항주 고도를 낮추어서 양력의 증가를 얻고자 하는 경우에 위그선의 선체가 수면에 닿아서 사고가 발생할 위험을 전면적으로 차단하고 효과적으로 위그선의 지면효과를 증강시킬 수 있는 장치에 관한 것이다. 위그선, 지면효과, 양력
115	Heavy load ground effect machines	US44221065	1965-03-24	US3366195A	1968-01-30	WARNER LUCILLE E; ROBERTS ELVA W

116	Pitch controlled ground effect vehicle	US862221	1986-04-15	US4666012A	1987-05-19	Murrell D. Howell; Mary E. Howell
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.
117	Control system for ground effect machines	US58416366	1966-10-04	US3362495A	1968-01-09	LACEY RICHARD E

118	Track for ground effect machines	US3658010D	1970-11-12	US3658010A	1972-04-25	MERLE GUY CHARLES MARIE JOSEPH
A track for guided ground effect machines, the track having a machine-supporting portion and a guidance rib and including a passage arranged within the thickness of the said rib to cause the space covering the top of the said rib to be in communication through the said passage with a space defined by the machinesupporting portion of the track and which communicates with the outside atmosphere, whereby redundant lifting forces acting on the machine are substantially avoided.
119	Aerodynamic and ground effect craft	US257526	1994-06-09	US5636702A	1997-06-10	Gordon S. Kolacny
A craft for ground effect and aerodynamic flight has, in addition to the usual vertical and horizontal stabilizer(s), a primary, upper airfoil, a lower secondary airfoil and a pivotable flap. The upper surface of the primary airfoil forms the primary lifting surface for aerodynamic flight while the lower surface forms, at its anterior and, an air intake for the compressors powering the craft and, to the rear, the upper surface of a plenum for ground effect flight. The upper surface of the secondary airfoil forms the lower surface of the compressor air intake at its anterior end and a compressed air exhaust at its other end. The lower surface forms the anterior end of the plenum when the pivotable flap is in the down position. The pivotable flap is attached near the forward end of the lower surface of the secondary airfoil to block the flow of compressed gases out the front of the craft during landing and while in hovercraft mode. Preferred models have a vertical stabilizer forward of the cockpit.
120	Articulated ground effect machine system	US62386767	1967-03-17	US3401767A	1968-09-17	CHARLES BARR

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