| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 61 | 可巡航救援投放机构、利用地面效应的可巡航救援飞行器 | CN202223399732.1 | 2022-12-19 | CN218751390U | 2023-03-28 | 温张喆; 周嘉伟 |
| 本实用新型涉及可巡航救援投放机构、利用地面效应的可巡航救援飞行器，包括舵机座，安装在舵机座上的动力装置、投放装置，所述动力装置为投放装置提供动力，所述投放装置包括与动力装置连接的齿轮组、与齿轮组连接的齿条、由齿条带动的杠杆和撞针、与杠杆连接的触发绳、与触发绳连接的装有救生圈的触发器、自动舱门装置。本申请解决了传统救援成本高、危险性高的问题。 | ||||||
| 62 | 一种用于风洞飞行器地面效应实验地面高度测量装置 | CN202222269683.3 | 2022-08-26 | CN218156773U | 2022-12-27 | 李向征; 张伟; 张秋实; 黄洁 |
| 本实用新型涉及一种用于风洞飞行器地面效应实验地面高度测量装置，主要应用于风洞飞行器地效试验过程中模拟地面高度测量。该装置由工业相机、激光定位器、移测装置、控制系统、供电系统和测量计算系统组成。该装置安装于风洞外部采用非接触测量方法，避免了测量装置对试验模型周边流场的影响，与传统测量手段相比该装置可以测量试验过程中由于飞行器支杆及天平弹性形变造成的高度变化，并且可以实现高度参数的实时测量，具有安装简单，快捷，测量精度高的特点。 | ||||||
| 63 | 多旋翼飞行器气动干扰及地面效应综合试验装置 | CN201820190414.9 | 2018-02-05 | CN208036658U | 2018-11-02 | 俞志明; 陈仁良 |
| 本实用新型公开了一种多旋翼飞行器气动干扰及地面效应综合试验装置，包括：主支架、升降平台、升降电机、减速器、传动转向器、升降平台升降机、旋翼系统升降机、旋翼系统X方向位移器、X方向平移杆、旋翼六分量天平、机体六分量天平；所述升降电机通过安装在主支架上的减速器和传动转向器驱动升降平台升降机，从而带动升降平台上下移动；旋翼系统X方向位移器安装在升降平台两侧；旋翼系统升降机安装在X方向平移杆上并沿Z方向可移动；旋翼/机体六分量天平分别安装在旋翼系统升降机/X方向平移杆和旋翼系统/机体之间的位置。本实用新型具有通用性强，操作简便等优点，可适用不同尺寸的多旋翼倾转飞行器的气动干扰和地面效应试验研究。(ESM)同样的发明创造已同日申请发明专利 | ||||||
| 64 | 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 | ||||||
| 65 | 피치제어식 공기쿠션차량 | KR1019870700215 | 1985-07-22 | KR1019920002408B1 | 1992-03-23 | 머렐디이.하우웰 |
| 내용 없음. | ||||||
| 66 | A GROUND EFFECT CRAFT | PCT/AU2001/000944 | 2001-08-03 | WO02012044A1 | 2002-02-14 | |
| A craft having symmetrical wing portions on either side of a central longitudinal axis, with the wing portions curving downwardly at their outer ends and having a lower surface profile which curls outwardly and downwardly, whereby an airflow pattern is able to be created underneath the craft which curls outwardly so as to lift the craft off a surface. | ||||||
| 67 | 一种地面效应旋翼飞行器及飞行模式切换控制方法 | PCT/CN2020/000187 | 2020-08-24 | WO2021109311A1 | 2021-06-10 | 苏兵兵; 王磊; 周亨; 王兆山; 付立春; 包明敏; 罗俊; 侯祥民; 吴令华; 洪铃 |
一种地面效应旋翼飞行器包括机身（1）、旋翼系统（2）、地效翼（3）、侧端板（4）、尾翼（5）、发动机（22）、传动与倾转系统（23）。其中，地效翼（3）对称设置在机身（1）两侧，侧端板（4）分别设置在地效翼（3）外侧，尾翼（5）位于机身（1）后方，旋翼系统（2）至少有2对，分别对称设置在尾翼（5）和侧端板（4）上，所述发动机（22）与传动与倾转系统（23）连接，并与旋翼系统（2）相连。该地面效应旋翼飞行器结合旋翼飞行器和地面效应飞行器优点，在具有垂直起降功能的同时，能够获得较大升阻比，使得旋翼飞行器获得较大的航程和巡航速度，有效提高旋翼飞行器的应用场景和功能作用。 |
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| 68 | Bodeneffekt-Fahrzeug | EP85107693.5 | 1985-06-21 | EP0170846B1 | 1989-09-27 | BLUM, Albert |
| 69 | GROUND EFFECT VEHICLE | PCT/AU1996000698 | 1996-11-05 | WO1997017241A1 | 1997-05-15 | SEA WING INTERNATIONAL PTY. LTD. |
| A ground effect vehicle has a fuselage (1) for operation in water. Wings (5) curve downwardly from each side of the fuselage. In plan the wings are triangular with leading edges jutting at right angles to the fuselage. In front elevation the wings are attached high on the fuselage and exhibit a compound downward curve to tips at the level of the bottom of the fuselage. The angle of attack of each wing increases gradually from the root area to a maximum along the wing and then decreases towards the wing tip. The high angle of attack at mid-wing gives high lift at low speeds but the increase in drag occasioned thereby does not become significant until air speeds over 180 knots. This makes for a fail-safe design as the wing will not fly out of ground effect irrespective of the installed horsepower. The diverging tail fins (19, 20) minimise banking on turns thus maintaining the air cushion under the outboard wing. | ||||||
| 70 | SURFACE EFFECT VESSEL HULL | EP97908014 | 1997-03-06 | EP0898543A4 | 1999-09-22 | HARLEY HOWARD D |
| A surface effect hull (10) particularly suitable for use with a catamaran vessel. The twin hulls (12) each comprise a V-shaped portion (formed by faces 38 and 40) and a recess portion (36) that receives pressurized gas therein. The V-shaped bow portion creates dynamic lift and the pressurized air portion creates an air cushion for reduction of drag. | ||||||
| 71 | GROUND EFFECT RAILWAY | PCT/EP1994002090 | 1994-06-28 | WO1995000377A1 | 1995-01-05 | GEOCONSULT G.M.B.H. |
| A ground effect railway has a track (10), at least a vehicle (12) and an air cushion (14) arranged between the track (10) and the vehicle (12). The air cushion (14) extends over substantially the whole width of the vehicle and is laterally delimited by walls (16, 18) which extend above the top surface (20) of the track (10). | ||||||
| 72 | Ground-surface-effect wing plane | EP88109540.0 | 1988-06-15 | EP0295652A3 | 1990-04-25 | Higashida, Akio Kobe Shipyard & Engine Works of; Matsuoka, Toshio Kobe Shipyard & Engine Works of; Satake, Tokuki Kobe Shipyard & Engine Works of; Yamaguchi, Nobuyuki Takasago Technical Institute; Sato, Tomohiko Takasago Technical Institute |
An improved ground-surface-effect wing plane is disclosed. The improvements reside basically in the provision of a top plate having an upwardly convex surface portion along its front edge and having a principal portion of its entire width formed in an aerofoil section shape over its entire length, a central fuselage section provided at the center of the top plate and having a crewman's seat, end plates disposed along the opposite side surfaces of the top plate over its entire length, and a blower associated with an air exhaust duct and disposed in the rear of the central fuselage section. Besides the aforementioned basic improvement, various further improvements are proposed such as the provision of spoilers in association with the top plate, a front end cover disposed under the upwardly convex surface portion so that it can adjust an area of an opening in front of the plane body, a thrust switching damper contained in the air exhaust duct, an airflow direction control damper contained in the air exhaust duct, a vertical tail having a rudder assembled therein and disposed at the rear end of the top plate, an intake duct additionally associated with the blower, floats associated with the end plates, or the like. |
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| 73 | Ground effect vehicle | EP80304245.6 | 1980-11-26 | EP0030122A1 | 1981-06-10 | Chapman, Anthony Bruce Colin; Wright, Peter Godfrey |
A wheeled vehicle has an undertray shaped to form a venturi duct with a road or like surface over which the vehicle moves, the undertray being carried in substantially fixed relationship with the wheels, so that the vehicle chassis or body can move relative to the wheels without substantial alteration of the shape of the venturi duct. The undertray can comprise the lower wall of a sheel enclosing the vehicle body or chassis. |
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| 74 | Aeroplane with ground effect wing utilizing ground effect | JP3868577 | 1977-04-05 | JPS53124897A | 1978-10-31 | KATOU SHIGERU; MUNEDA KIYOSHI |
| 75 | Ground-surface-effect wing plane | EP90113277.9 | 1990-07-11 | EP0411358B1 | 1993-09-29 | Matsuoka, Toshio, c/o Kobe Shipyard & Engine Works; Higashida, Akio, c/o Kobe Shipyard & Engine Works; Satake, Tokuki, c/o Kobe Shipyard & Engine Works |
| 76 | Bodeneffekt-Fahrzeug | EP85107693.5 | 1985-06-21 | EP0170846A1 | 1986-02-12 | BLUM, Albert |
Ein Bodeneffekt-Fahrzeug besteht aus einem zentralen, flügelartigen Tragkörper (1), auf beiden Seiten des Tragkörpers angeordneten Schwimmern (5) und/oder Fahrwerken, einem vor dem Tragkörper angeordneten Schuberzeuger (11), einem Leitwerk (14, 16) sowie einer oben auf dem Tragkörper angeordneten Kabine (17) für mindestens eine Person und gegebenenfalls für Nutzlasten. Um die Bodeneffektwirkung zu verstärken und den Bodeneffekt auch bereits bei geringen Geschwindigkeiten wirksam werden zu lassen, ist dem Tragkörper (1) eine weit nach vorn gezogene Bugspitze (6) vorgeschaltet, die einen unter den Tragkörper gerichteten Luftströmungskanal (7) bildet, wobei der Schuberzeuger (11) unter dem vorderen Bereich der Bugspitze (6) in oder unmittelbar vor dem Luftströmungskanal (7) angeordnet ist. |
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| 77 | 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. | ||||||
| 78 | 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 | ||||||
| 79 | Ground effect ship | US390787 | 1999-09-07 | US6164401A | 2000-12-26 | Robert Henry Vollmerhausen |
| The apparatus is a ground effect ship utilizing a wing-hull to support a passenger cabin piggyback style. Each one of the wing-hull segment includes a pontoon member that, in turn, includes a turbine unit of dual use, either compressing water or air, so as to eject a quantity of water or air for generating a coefficient of drag for slowing one part of the apparatus down for maneuving. In a like manner the apparatus includes a plurality of wingvalve elements that draw ambinet air upwardly and conduit that air into a primary airstream so that a coefficient of turbulence induced drag reduces the lift on one wing-hull segment of the apparatus with the result that the apparatus biases a pontoon on the water while elevating another pontoon into the air, substantially parallel with the water's surface. This mode of operation is sailing-flight. | ||||||
| 80 | Ground effect machine | US4564760 | 1960-07-27 | US3101125A | 1963-08-20 | DE RIDDER ERNST J |
