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公开(公告)号：US09688356B2
公开(公告)日：2017-06-27
申请号：US15080509
申请日：2016-03-24
申请人： Walter Schulz
发明人： Walter Schulz
摘要： A three stage watercraft for operation in the water as a traditional boat at low speeds in stage one, for operation on the water's surface at mid-range speeds at stage two, and for traveling in ground effect at higher range speeds is disclosed. The three stage craft includes a hydro-wing 12, either at least a single hydrofoil 13 or gyration rotor 14 to aid with lift from stage one to stage two, and a pair of outboard floats or hydro-floats 16a, 16b supported by the hydro-wing 12, which are also designed to aid with lift from stage one to stage two.
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公开(公告)号：US20130068879A1
公开(公告)日：2013-03-21
申请号：US13233545
申请日：2011-09-15
申请人： Hokan Colting
发明人： Hokan Colting
摘要： A WIG (wing in ground effect) vessel includes a hull with wings attached. The WIG vessel includes means for propulsion as well as altitude and directional control. The lift of the wings in ground effect is augmented by partial aerostatic lift, achieved through interior gas holding envelopes containing a lighter-than-air gas. The wings have a high mean chord length, for example fourteen meters or more, allowing the vessel to fly in ground effect above water at an altitude where waves are of minimal concern. The vessel has a low wing loading, below 1.5 kg/m2, and the wings are of uniform thickness and have an aspect ratio of less than 1. The conical fore end of the hull forces air below the surface of the wings for ground effect. Weight transfer is used to alter the pitch of the vessel.
摘要翻译： WIG（地面效应翼）船包括一个附有翼的船体。 WIG船包括推进装置以及高度和方向控制。 地面效应的机翼升力通过部分空气静力提升增加，通过内部气体保持包含轻于空气气体的信封实现。 翼的平均弦长很高，例如十四米或以上，允许船只在波浪最不重要的高度处在水面以上地面飞行。 该船具有低于1.5kg / m 2的低翼载荷，并且翼部具有均匀的厚度并且具有小于1的纵横比。船体的锥形前端迫使在翼的表面下面的空气用于地面效应。 重量转移用于改变船只的桨距。
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3.发明申请公开(公告)号：US20110266081A1
公开(公告)日：2011-11-03
申请号：US13142884
申请日：2010-01-05
申请人： Ivan Novikov-Kopp
发明人： Ivan Novikov-Kopp
摘要： The group of inventions relates to aviation and to transport means having (static and dynamic) air discharge, in particular to self-stabilizing wing-in-ground-effect craft of types A, B and C. The following technical results are achieved: increased flight safety and maneuvering safety, increased load-bearing capacity and flight height in ground effect mode, reduced dimensions, improved take-off and landing characteristics, as well as amphibian characteristics and economic efficiency, increased functionality and a wider range of operational alignments, and greater ease of use and maintenance. This result is achieved by simultaneously applying the methods for generating a system of aerodynamic forces, the structural solutions and the piloting methods conceptually linked therewith which are proposed in the present group of inventions to “flying wing” or “composite wing” design layouts.
摘要翻译： 本发明涉及具有（静态和动态）空气排放的航空和运输手段，特别是A，B和C类型的自稳定式地面效应工艺。实现以下技术成果：增加 飞行安全和机动安全，地面效应模式下的承载能力和飞行高度的增加，尺寸减小，起飞和着陆特性的改善，以及两栖动力特性和经济效率，功能的增加和更广泛的操作对准，以及 更易于使用和维护。 这个结果是通过同时应用在本发明组中提出的“飞翼”或“复合翼”设计布局的生成空气动力系统的方法，结构解决方案和与其概念相关的驾驶方法来实现的。
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公开(公告)号：US20110056422A1
公开(公告)日：2011-03-10
申请号：US10536097
申请日：2006-03-03
摘要： The personnel water jet, or boat jets, haven't really change there design or function that much, and there very limited use. The flying water jet-flying submarine are able to fly above the rough water waves and always get a very smooth ride and the true feeling of true flight, jump in and out of the water or through the waves just like a flying fish and stay in flight for a while and also be able to go under water at any given time, with and adjustable impeller water flow tube that can rotate 360 degrees with fins, at any given time, and also giving the operator a much more creative and thrilling or spectacular ride every time, further more many more uses for personnel and professional operations, and with the impeller having continues fins or blade on the entire impeller its self, and this system will use less fuel in an average motor. Further more this is self energizing with the solar panels that are part or the body it's self with an ever lasting of fuel that will not harm the environment.
摘要翻译： 人员喷水或喷气式飞机没有真正改变那里的设计或功能，使用非常有限。 飞翔的飞行潜艇能够在粗糙的水浪之上飞行，总是得到一个非常顺利的骑行，真正的飞行真正的感觉，跳入和流出水面，或通过波浪就像一条飞鱼，留在 飞行一段时间，也可以在任何给定的时间在水下，与可调节的叶轮水流量管可以在任何给定的时间旋转360度与鳍，并给予操作者更多的创意和惊险或壮观 每次乘坐更多的人员和专业操作的更多用途，并且叶轮在整个叶轮上自身持续的叶片或叶片，并且该系统将在平均电机中使用更少的燃料。 进一步，这是太阳能电池板的自我激励，太阳能电池板是部分或身体，它是自己的持久的燃料，不会伤害环境。
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公开(公告)号：US20100213308A1
公开(公告)日：2010-08-26
申请号：US12677917
申请日：2008-08-12
申请人： Masahiko Suzuki
发明人： Masahiko Suzuki
IPC分类号： B64C39/04
CPC分类号： B64C39/04 , B60V1/08 , B64B2201/00
摘要： Provided is a positive-pressure floating type airplane comprising an airfoil portion, left-right fuselages, a central fuselage, an elevator and a rudder disposed at the back of the airfoil portion, a thruster disposed at the back of the central fuselage, and a horizontal stabilizer disposed at the rear ends of the left-right fuselages. The individual front ends of the airfoil portion, the left-right fuselages and the central fuselage are formed into arcuate shapes in longitudinal sections. On the lower side of the airfoil portion, a recessed air capture is formed from the front end to the rear end. As a result, the positive-pressure floating type airplane is floated by the reaction from the air at the time when the air to pass the air capture through the airfoil portion is pushed by the thrust of the thruster, and is propelled forward by the component of that thrust.
摘要翻译： 本发明提供一种正压浮式飞机，其包括设置在翼型部分的后部的机翼部分，左右机身，中央机身，电梯和方向舵，设置在中央机身背面的推进器，以及 设置在左右机身后端的水平稳定器。 机翼部分，左右机身和中央机身的各个前端在纵向部分形成为弓形。 在翼型部分的下侧，从前端到后端形成凹陷的空气捕获。 结果，正压浮式飞机在通过空气捕获通过翼型部的空气被来自空气的反作用力推动推动器的推力而被推动时被部件 的推力。
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6.发明授权Multi-mission/purpose ground-effect craft derived from a common modular platform 失效多任务/目的地面工艺从通用模块化平台衍生而来公开(公告)号：US07398740B2
公开(公告)日：2008-07-15
申请号：US11043578
申请日：2005-01-26
申请人： Franz B. Boncodin
发明人： Franz B. Boncodin
摘要： A multi-mission/purpose ground-effect craft is provided which is derived from a common modular platform which includes a hull; an inner floor structure adapted to be installed over the hull; a body adapted to be attached to at least one of the top surface of the hull and the inner floor structure, such that a interior compartment is formed thereinside; a tail wing assembly adapted to be attached to the aft end of the body; a forward nose cowl adapted to be attached to at least one of the forward nose portion of the hull and the forward body portion of the body; a windshield integrated into the forward end of the body; at least one door assembly integrated into the left or right body side; at least one window assembly integrated into the left or right body side; a propulsion system integrated within the aft end of the body; and a retractable skirt attached and draped from the outer or inner perimeter of the hull.
摘要翻译： 提供了一种多任务/目的地面作战工具，其衍生自包括船体在内的通用模块化平台; 适于安装在船身上的内层结构; 适于附接到船体的顶表面和内部地板结构中的至少一个的主体，使得在其内部形成内部隔室; 适于附接到身体的后端的尾翼组件; 适于附接到船体的前鼻部和身体的前身部中的至少一个的前鼻罩， 集成到身体前端的挡风玻璃; 集成在左或右身体侧的至少一个门组件; 集成在左右身体侧的至少一个窗组件; 整合在身体后端的推进系统; 以及从船体的外部或内部周边连接并悬挂的可伸缩裙部。
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公开(公告)号：US20070272795A1
公开(公告)日：2007-11-29
申请号：US10587680
申请日：2005-01-27
申请人： Piet Ellnor
发明人： Piet Ellnor
IPC分类号： B64C5/04
摘要： An wing-in-ground-effect craft (11) having a loaded canard forewing (13) and a main forward delta configuration wing (15) attached to fore (17) and mid (19) sections of a body (21) respectively. The body (21) is formed with an integral planning hull (23) for amphibious applications, extending rearward to a tail section (25) which incorporates a ducted fan (27), and a vertical stabiliser (29). Rudder (31) is located in the exhaust of the ducted fan (27) for steering the craft (11), and serves as a stator to reduce spiral induced in the airflow exiting the duct (27). The canard forewing (13) has about 12% of the area of the main wing (15), and has inner portions (35) having a dihedral configuration disposed at a first angle of inclination from the vertical of 68° (equating to a dihedral angle of 22°), and outer portion (37) disposed at a first angle of inclination from the vertical of about 91° (equating to an anhedral angle of about 1°). The inner portions (35) have an angle of attack of 7.5%, while the outer portions (37) have an angle of attack of 4.5°. The main wing (15) has a flat to slightly anhedral configuration and an angle of attack of from 4° to 4.5°. The main wing (15) incorporates a pontoon float (39) attached on the outer end of each main wing (15). The canard forewing (13) has control surfaces in the form of elevons (41) attached behind the inner portions (35).
摘要翻译： 一种具有装载的鸭舌头前缘（13）和主体前三角形构造翼（15）的机翼地面效应工艺（11），其分别附接到主体（21）的前部（17）和中部（19）部分。 主体（21）形成有用于水陆两用应用的整体规划船体（23），向后延伸到包括管道风扇（27）的尾部（25）和垂直稳定器（29）。 方向舵（31）位于用于转向工艺（11）的管道风扇（27）的排气中，并且用作定子以减少离开管道（27）的气流中引起的螺旋。 所述前翅（13）具有所述主翼（15）的面积的约12％，并且具有内部部分（35），所述内部部分（35）具有从垂直于68°的第一倾斜角度设置的二面体构型（相当于二面体 角度为22°）以及从垂直于约91°（相当于大约1°的面角）倾斜的第一倾斜角度的外部部分37。 内部部分（35）的入射角为7.5％，而外部部分（37）的入射角为4.5°。 主翼（15）具有平坦至略微的四面体形状，并且攻角为4°至4.5°。 主翼（15）包括附接在每个主翼（15）的外端上的浮筒浮子（39）。 鸭子前叶（13）具有安装在内部部分（35）后面的升降部（41）形式的控制表面。
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公开(公告)号：US20060009093A1
公开(公告)日：2006-01-12
申请号：US11153476
申请日：2005-06-16
申请人： David Murphy
发明人： David Murphy
IPC分类号： B63H7/00
摘要： The present invention relates to a surface effect craft comprising a supporting deck structure having two pontoons mounted thereto in catamaran like fashion. A propulsion mechanism is mounted to a rear portion of the deck structure. A lift control member is disposed under the deck structure between the two pontoons. The lift control member is pivotally movable mounted to the front portion of the deck structure. A lift adjust mechanism pivotally moves the lift control member between a first position with the rear end of the lift control member being in close proximity to the surface and a second position with the rear end of the lift control member being in close proximity to the deck structure. Employment of the lift control member enables the craft to achieve surface effect at low speed and, furthermore, allows control of the aerodynamic lift in a wide range from maximum lift to negative lift. This substantially widens the range of surface conditions and speed the craft is operable, such as uneven ground, choppy water surfaces, snow, and ice.
摘要翻译： 本发明涉及一种表面效果工艺，其包括具有以双体船方式安装的两个浮筒的支撑甲板结构。 推进机构安装在甲板结构的后部。 升降机控制构件设置在两个浮筒之间的甲板结构之下。 升降控制构件可枢转地安装在甲板结构的前部。 升降机调节机构将提升控制构件在提升控制构件的后端处于紧邻表面的第一位置和第二位置之间枢转地移动，第二位置与升降控制构件的后端紧邻甲板 结构体。 使用电梯控制构件使得工艺能够以低速实现表面效果，并且还允许在从最大升力到负升力的宽范围内控制空气动力升程。 这大大地扩大了工艺的可操作范围，例如不平坦的地面，波涛汹汹的水面，积雪和冰。
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公开(公告)号：US06845833B2
公开(公告)日：2005-01-25
申请号：US10442622
申请日：2003-05-21
申请人： Lawrence Shuniak
发明人： Lawrence Shuniak
CPC分类号： B60V1/08
摘要： The present invention concerns an all-terrain vehicle for use over a variety of terrain. The vehicle includes a main body having a cabin, a forward side, a backward side and two lateral sides; a pair of ground effect wings connected to the lateral sides of the main body, each wing having an angle of attack; a lift engine having necessary auxiliary equipment for operation thereof, wherein the lift engine is connected to the backward side of the main body and supplies a lift power to the vehicle; at least one lift fan connected to the lift engine; an engine mounted to the main body to provide energy to propel the vehicle forward; a wheel connected to the forward side of the main body, wherein the wheel is connected to the main body by a drive shaft; a control system to control the angle of attack.
摘要翻译： 本发明涉及用于各种地形的全地形车辆。 车辆包括具有车厢，前侧，后侧和两个侧边的主体; 一对地面效应翼连接到主体的侧面，每个翼具有迎角; 具有用于其操作的必要辅助设备的升降机引擎，其中所述提升发动机连接到所述主体的后侧，并向所述车辆提供升力; 至少一个升降风机连接到升降机发动机; 发动机安装到主体以提供能量以推进车辆向前; 连接到所述主体的前侧的轮，其中所述轮通过驱动轴连接到所述主体; 控制系统来控制攻角。
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公开(公告)号：US6164401A
公开(公告)日：2000-12-26
申请号：US390787
申请日：1999-09-07
摘要： 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.
摘要翻译： 该装置是利用机翼支撑乘客背负式的地面效应船。 翼壳段中的每一个包括浮筒构件，该浮筒构件又包括双重用途的涡轮机单元，压缩水或空气，以便喷射一定量的水或空气，以产生用于减速的拖拉系数 装置的一部分用于操纵。 以类似的方式，该装置包括多个翼形元件，其向上抽吸混合空气并将空气导入主空气流中，使得湍流诱发阻力的系数降低装置的一个翼壳段上的升力，结果是 装置将浮筒偏置在水上，同时将另一个浮筒升高到空气中，与水的表面基本平行。 这种运行方式是航行。
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