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
141	MULTIPLE-MODE WING-IN GROUND EFFECT VEHICLE	PCT/US1997002691	1997-02-24	WO1997030886A1	1997-08-28
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).
142	Ground effect machine with controls therefor	US10940361	1961-05-11	US3127949A	1964-04-07	HARTER WALTER T

143	Combination aquatic-ground effect vehicle	US35390364	1964-03-23	US3205847A	1965-09-14	SMITH WILLIAM M

144	Lift augmented ground effect platform	US236646	1994-05-02	US5803199A	1998-09-08	William C. Walter
The lift augmented ground effect platform of the present invention is characterized by two pair of annular concentric air curtain nozzles and supercharge nozzles which direct respective jet streams downward and inward beneath the downwardly facing lifting surface of the platform. The concentric arrangement of the nozzles provides an inner or central supercharged air cushion surrounded by an inner central air curtain and an outer or peripheral air cushion surrounded by a peripheral air curtain. The lift augmented ground effect platform of the present invention provides an increased or "large" augmentation of the forces acting to raise or lift 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 curvature of the platform's peripheral surface, it creates a pressure differential which provides an additional force supporting the lifting of the platform. The airflow stream and the jet stream are provided by a propeller or rotating fan device mounted exterior of the platform. The exterior mounting provides two benefits: first, the propeller or fan stall due to the jet stream source is eliminated and second, smooth transition into free air (out of ground effect) is permitted where necessary to navigate rivers, canyons, and other types of physical barriers which may disrupt ground effect operation.
145	Hydrofoil stabilization of a ground effect machine	US679160	1960-02-04	US3117545A	1964-01-14	WARNER DOUGLAS K

146	Leading edge augmentor wing-in-ground effect vehicle	US413182	1982-08-30	US4442986A	1984-04-17	David G. Rousseau
A Wing-in-Ground (WIG) effect vehicle for traveling over water utilizing efflux from propulsors to create a static pressure increase under the wings. The propulsors are carried inside the fuselage or in other safe locations away from sea spray and debris. The efflux is carried by conduit running the full span of the wing leading edge and is directed under the wing. The efflux also entrains ambient air by Coanda effect to increase the resultant lift.
147	Trim-correcting facility for ground effect machines	US3797399D	1972-03-09	US3797399A	1974-03-19	BERTIN J; CROIX MARIE
An air cushion suspension system for a ground effect machine comprising in combination a movable disc bearing cushioncontaining means and balanced by the cushion pressure acting on one side of the disc and by an opposing pressure acting on the opposite side of the disc, the opposing pressure existing in a deformable suspension chamber in which a tubular air chamber is disposed, the tubular air chamber being adapted to be inflated to a pressure above the opposing pressure and to bear against the disc to provide extra stiffness in the suspension. The flexible wall of the tubular air chamber is, in the balanced state and with the machine operating normally, clear either of the disc of the suspension chamber wall opposite the disc, so that the extra stiffness is introduced into the suspension only with effect from a particular amount of deformation of the disc suspension chamber, the tubular air chamber forming a kind of resilient abutment.
148	Lift augmented ground effect platform	US15042	1998-01-28	US6082478A	2000-07-04	William C. Walter; Marshel Thomas Johnson
The lift augmented ground effect platform of the present invention is characterized by two pair of annular concentric air curtain nozzles and supercharge nozzles which direct respective jet streams downward and inward beneath the downwardly facing lifting surface of the platform. The concentric arrangement of the nozzles provides an inner or central supercharged air cushion surrounded by an inner central air curtain and an outer or peripheral air cushion surrounded by a peripheral air curtain. The present invention provides an increased or "large" augmentation of the forces acting to raise or lift 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 curvature of the platform's peripheral surface, it creates a negative pressure differential which provides an additional lifting force contributing to support of the platform. The airflow stream and the jet stream are provided by, for example, propeller(s) or rotating fan device(s) mounted exterior or interior of the platform. The exterior mounting or specialized interior mounting provides two benefits: first, the propeller or fan stall due to the jet stream source is eliminated and second, smooth transition into free air (out of ground effect) is permitted where necessary to navigate rivers, canyons, and other types of physical barriers which may disrupt ground effect operation. An unpowered variation of the platform may be adapted for releasable attachment to a separate powered vehicle to serve as a performance enhancing lift augmentation platform.
149	Confining system for ground-effect machine	US3647018D	1969-12-29	US3647018A	1972-03-07	CROIX-MARIE FRANCIS MARIE JEAN; GRIGNON ROBERT GEORGES
An arrangement for sustaining and/or guiding a load such as a machine or vehicle over a bearing surface by means of air cushions confined in a chamber formed inside an annular troughshaped inflatable wall between said bearing surface and a movable partition forming with the load and an annular deformable wall a chamber of a variable volume. The input of a compressed fluid into the latter feeds through ports in the partition the cushionconfining chamber so that the latter is sustained at a small self-adjusting distance over the bearing surface.
150	Pitch and roll control for ground effect machines	US50862965	1965-10-21	US3306389A	1967-02-28	TINAJERO ANIBAL A

151	Propellant energized ground effect machine	US9327661	1961-03-03	US3078940A	1963-02-26	ROLLE SYLVAN D

152	막대형 나사봉을 이용한 위그선의 지면효과 증강 및조절장치	KR1020070112374	2007-11-05	KR100921936B1	2009-10-15	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
153	地面效應翼機之高度控制裝置	TW079107190	1990-08-28	TW163189B	1991-07-11	大迫富重
一種地面效應翼機之高度控制裝置，係利用機體以及機翼與水面間所產生之地面效應，而與水面之間僅離開微小空間以超低高度航行於水面上之地面效應翼機(10)之高度控制裝置；其特徵在：航行中保持其與水面之接觸狀態，對當該地面效應翼機(10)之操縱系統(18)提供有關該水面與機體間距離之資訊之感測器(20)；以及，以機械性方式連接該感測器(20)與地面效應翼機(10)之連接機構(12)所構成，依前述感測器(20)傳來之有關水面與機體間之距離資訊，控制前述操縱系統(18)控制昇降舵而使其動作，由此保持地面效應翼機(10)與水面間距離一定，而使地面效應翼機(10)航行者。
154	Air cushion trunk for ground effect machines	US3727716D	1971-04-05	US3727716A	1973-04-17	JENKINS D
An air cushion trunk sealing system for ground effect machines is provided to prevent air leakage from the trunk during periods of operation and parking when the primary power of the machine or craft is turned off. This system is composed of an inner tube type liner (which may be, and preferably is, constructed of multiple cells) which is collapsed, doubled and attached to the underside of the craft and within the trunk. Before the trunk air is turned off, air of higher pressure than trunk pressure is routed into the collapsed inner tube to inflate it. As this inner tube inflates, it replaces the trunk air while the trunk air flow is still providing craft support. When the inner tube is fully inflated, the air to the trunk is fully diverted overboard and the inner tube now supports the craft. The inner tube valve is closed to contain the air and the trunk air may be turned off.
155	Fluid ground effect vehicle transportation system	US3648620D	1969-12-24	US3648620A	1972-03-14	BERTIN JEAN HENRI; NABOUR MARCEL PIERRE LE; GIRAUD FRANCOIS LOUIS
A pressure fluid supply facility for the cushions of a ground effect machine or vehicle, the facility comprising at least one fluid generator connected to the inducing nozzles of static pumps whose flow resulting from the mixing of the inducing flow with the induced fluid energizes the lift cushions and guide cushions of the machine, wherein each cushion is associated with at least one static pump disposed very near the cushion so as to reduce the pressure losses in the resulting flow by reduction of duct length.
156	Combined vtol aircraft and ground effects machine	US45055565	1965-04-23	US3291242A	1966-12-13	TINAJERO ANIBAL A

157	Skirt facility for a ground-effect machine	US3680657D	1969-12-30	US3680657A	1972-08-01	MARCHETTI CHARLES JOSEPH; FAURE MARC HENRI JEAN
An elementary cell adapted to be assembled together with other similar cells to form a compartmented-skirt facility for a ground-effect machine, the cell being formed by an outer wall element and inner wall element bounding together a substantially crescent-shaped space, such cell being adapted to be mounted and demounted individually on the structure of a ground-effect machine.
158	Combination rotary wing and ground effect machine	US28923063	1963-06-20	US3175785A	1965-03-30	DE TERE JOHN A; WERNICKE RODNEY K

159	GROUND EFFECT BASED SURFACE SENSING IN AUTOMATED AERIAL VEHICLES	PCT/US2015/037286	2015-06-23	WO2015200392A1	2015-12-30	NAVOT, Amir; BECKMAN, Brian C.; BUCHMUELLER, Daniel; KIMCHI, Gur; HENSEL, Fabian; GREEN, Scott A.; PORTER, Brian William; RAULT, Severan Sylvain Jean-Michel
This disclosure describes a system and method for operating an automated aerial vehicle wherein influences of a ground effect may be utilized for sensing the ground or other surfaces. In various implementations, an operating parameter of the automated aerial vehicle may be monitored to determine when a ground effect is influencing the parameter, which correspondingly indicates a proximity to a surface (e.g., the ground). In various implementations, the ground effect based sensing techniques may be utilized for determining a proximity to the ground, as a backup for a primary sensor system, for determining if a landing location is uneven, etc.
160	위그선의 착수 보조 장치	KR2020140000439	2014-01-20	KR2020150002927U	2015-07-29	이준모
본고안은위그선의착수보조장치에관한것이다. 본고안은, 위그선의동체의하부에형성되는착수보조장치에있어서, 곡선타입랙과맞물려형성되며, 구동장치로부터전달받은회전력을상기곡선타입랙으로전달하여, 상기위그선의착수시상기곡선타입랙의하부끝단영역에수평방향으로형성된플레이트에의한마찰력이제공되도록하는피니언; 및상기곡선타입랙 및상기플레이트외에상기곡선타입랙과상기플레이트사이를연결하기위해직선형의보강단을더 포함하여구성되는플래퍼; 를포함한다. 이에의해착수보조장치에의한동작에따라동체의착수가용이하도록하는효과를제공한다. 보다구체적으로, 위그선의착수거리와착수시간을단축시키며착수충격도경감시켜위그선의운항효율을개선할수 있는효과를제공한다.

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