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1. 发明申请

WO2014174401A1 HOVERCRAFT WITH MULTIPLE, INDEPENDENTLY-OPERABLE LIFT CHAMBERS. 审中-公开
标题翻译：具有多个独立操作的升降台。
公开(公告)号：WO2014174401A1
公开(公告)日：2014-10-30
申请号：PCT/IB2014/060626
申请日：2014-04-10
申请人： GREGORY, John , WAGAMAN, Woodrow
发明人： GREGORY, John , WAGAMAN, Woodrow
IPC分类号： B60V1/06
CPC分类号： B60V1/043 , B60V1/11 , B60V1/18 , B60V1/22
摘要： The invention is a hovercraft with multiple lift chambers which are operable independently of each other. Independently-operable pivot arm assemblies connect each lift chamber to the hovercraft main body, and his gives the hovercraft the ability to travel over uneven surfaces, traverse obstacles that would block conventional hovercrafts, and climb or descend even severe inclines. The hovercraft also includes side thrusters which allow it to maintain its vertical position on an incline while traveling laterally across the incline.
摘要翻译：本发明是具有多个提升室的气垫船，它们彼此独立地可操作。独立可操作的枢转臂组件将每个提升室连接到气垫船主体，并且他给予气垫船在不平坦的表面上行进的能力，穿过阻挡常规气垫船的障碍物，甚至爬升或下降甚至严重的倾斜。气垫船还包括侧推进器，允许其在横向横过斜坡的同时保持其在倾斜处的垂直位置。

2. 发明申请

WO1998022337A1 HYDRAULIC SYSTEM FOR MANOEUVRING BOATS, SHIPS AND CRAFTS IN GENERAL 审中-公开
标题翻译：液压系统，用于整修船舶，船舶和作业
公开(公告)号：WO1998022337A1
公开(公告)日：1998-05-28
申请号：PCT/IT1997000279
申请日：1997-11-14
申请人： DE RISI, Felice
IPC分类号： B63H25/46
CPC分类号： B60V1/11 , B63H25/46
摘要： A hydraulic system for the control of boats, ships and crafts in general that comprises nozzles (1, 2) opposed at the end of the stem, having a Venturi tube throttling (8) or an internal diameter reduction by means of flanges (10), so as to be able to determine, following to the outlet of the fluid under pressure, the movement by reaction of the front part of the boat (N) and therefore to perform immediate leftward or rightward curvings according to the nozzle used, and/or corresponding nozzles (3, 4), placed nearby the stern and with similar backward function, while the operating for hydraulic reaction of both nozzles placed on the same side determines the parallel movement of the whole craft, for coming alongside to quays or for performing other manoeuvres.
摘要翻译：一种用于控制船舶，船舶和工艺品的液压系统，其通常包括在杆的端部相对的喷嘴（1,2），其具有文丘里管节流（8）或借助于法兰（10）的内径减小，，以便能够确定在压力下的流体的出口处，通过船（N）的前部的反作用而运动，因此根据所使用的喷嘴执行立即的向左或向右的弯曲，和/ 或相应的喷嘴（3,4），放置在船尾附近并具有相似的后退功能，同时位于同一侧的两个喷嘴的液压反应操作决定了整个飞行器的平行运动，以便与码头或执行其他动作。

3. 发明申请

WO1994018045A1 HOVERCRAFT 审中-公开
标题翻译：表面效飞行器
公开(公告)号：WO1994018045A1
公开(公告)日：1994-08-18
申请号：PCT/EP1994000336
申请日：1994-02-07
申请人： WITT & SOHN GMBH & CO. , WITT, Hans , WITT, Henrik , WITT, Karsten, C.
发明人： WITT & SOHN GMBH & CO.
IPC分类号： B60V01/14
CPC分类号： F04D27/0207 , B60V1/11 , F04D27/004
摘要： A hovercraft, in particular water-borne hovercraft, has several lifting fans for generating an air cushion. Each fan (2) has a drive, a motor (5) and a pressure and/or position regulating circuit with corresponding sensors (7, 10) and regulators (6) for acting on the air cushion. A process is disclosed for regulating several lifting fans in a hovercraft whose drive has a regulator and a motor operated at a determined speed of rotation in order to generate an air cushion having a predetermined pressure or height. The motor has a corresponding power output and the performance of the lifting fan follows a determined characteristic curve.

4. 发明申请

WO1993025423A1 STATIC TRIMMER FOR A HOVERCRAFT 审中-公开
标题翻译：静态阀FOR气垫船
公开(公告)号：WO1993025423A1
公开(公告)日：1993-12-23
申请号：PCT/DE1993000527
申请日：1993-06-16
申请人： ABS AIRCRAFT AG , BLUM, Albert , STIEGLER, Hartmut
发明人： ABS AIRCRAFT AG
IPC分类号： B60V01/16
CPC分类号： B60V1/11
摘要： The invention relates to a static trimmer for a hovercraft which has at least one compressor mechanism to generate an air-cushion beneath the craft and in which the air-cushion is laterally limited by a peripheral elastic skirt consisting of a back skirt and a finger skirt. The aim of the invention is to provide a static trimmer for a hovercraft by means of which the craft can be effectively trimmed or its position can be controlled and by means of which the craft can be manoeuvred even when stationary. According to the invention the centre of buoyancy of the air-cushion is shifted in relation to the centre of gravity of the craft in that the elastic skirt (2) is divided into sections which can be shifted independently from one another and control components act with the laterally shiftable sections (6, 7, 8, 9) of the elastic skirt (2). These control components consist of cable winches (14), and two tension cables (15, 16) are provided for one laterally shiftable section (6; 7; 8; 9). The tension cables (15, 16) are guided at a distance apart over deflection rollers and engage with one segment (5) of the finger skirt (4).

5. 发明申请

WO2015087256A1 STEERING SYSTEM FOR A PROPELLER-DRIVEN VEHICLE 审中-公开
标题翻译：用于螺旋桨驱动的车辆的转向系统
公开(公告)号：WO2015087256A1
公开(公告)日：2015-06-18
申请号：PCT/IB2014/066761
申请日：2014-12-10
申请人： HOVERTECH LTD
发明人： MASTRANGELI, Marco , ODETTI, Angelo
IPC分类号： B60V1/14 , B63H7/02
CPC分类号： B60V1/043 , B60V1/11 , B60V1/14 , B63H7/02 , B63H25/48
摘要： A steering system for a vehicle, comprising at least one propulsion unit (2) comprising drive means for driving at least one propeller (21). The steering system comprises flow diverting means (3) located downstream from said propulsion unit (2). The orientation of said diverting means (3) is adjusted relative to the airflow generated by the propeller (21) by means of a control member (5), said flow diverting means (3) consisting of at least two flow diverting systems, said at least two systems being symmetric with respect to the direction of the airflow generated by the propeller. Each of the at least two flow diverting systems (3) is adapted to be independently driven by said control member (5). Said diverting system is characterized by a surface that allows backward travel when in the maximum open state, and by an axis of rotation that lies beyond the surface of the aileron.
摘要翻译：一种用于车辆的转向系统，包括至少一个推进单元（2），包括用于驱动至少一个螺旋桨（21）的驱动装置。转向系统包括位于所述推进单元（2）下游的分流装置（3）。所述转向装置（3）的方向相对于由螺旋桨（21）产生的气流通过控制构件（5）进行调节，所述分流装置（3）由至少两个分流系统组成，所述分流装置至少两个系统相对于由螺旋桨产生的气流的方向对称。所述至少两个分流系统（3）中的每一个适于由所述控制构件（5）独立地驱动。所述转向系统的特征在于当处于最大打开状态时允许向后行进的表面以及位于副翼表面之外的旋转轴。

6. 发明申请

WO2009068909A1 HOVER DODGEM 审中-公开
公开(公告)号：WO2009068909A1
公开(公告)日：2009-06-04
申请号：PCT/GB2008/051111
申请日：2008-11-25
申请人： ARDERN, Fergus Johnathan
发明人： ARDERN, Fergus Johnathan
IPC分类号： A63G25/00 , B60V1/00
CPC分类号： B60V1/043 , A63G25/00 , B60V1/11 , B60V1/18
摘要： A hover dodgem (1) comprising a hovercraft having seating (5) for at least one adult human and a battery-powered lift' and thrust fan, sufficient to lift the dodgem when carrying an adult human. Preferred dodgems have rotatable thrust air exit paths, are circular, or have thrust air exit paths angled towards the ground. Wireless control means allow remote control of the dodgems.
摘要翻译：一个悬停躲避物（1）包括一个气垫船，其具有用于至少一个成年人的座位（5）和一个足够提升携带成年人的躲避者的推力风扇。优选的避雷器具有可旋转的推力空气出口路径，是圆形的，或具有朝向地面成角度的推力空气出口路径。无线控制装置允许遥控遥控器。

7. 发明申请

WO2004035382A2 AIRSTREAM CONTROL SYSTEM FOR A HOVERCRAFT 审中-公开
标题翻译： HOVERCRAFT的AIRSTREAM控制系统
公开(公告)号：WO2004035382A2
公开(公告)日：2004-04-29
申请号：PCT/US2003/032814
申请日：2003-10-16
申请人： AEROMOBILE, INC.
发明人： BERTELSEN, William, R. , GRANT, John, W.
IPC分类号： B64D
CPC分类号： B60V1/14 , B60V1/11
摘要： Three aspects are disclosed of an airstream control system for a hovercraft that includes a platform (20) and a lift gas chamber (20) beneath the platform. Firstly, the system includes an impeller (14) for receiving air at an inlet and discharging pressurized air at an outlet as an airstream. The impeller is positioned above an orifice (28) of the lift gas chamber. The impeller is supported along a first axis transverse to the airstream and about which the impeller is rotatable by a first axis frame (48, 50) that is rotatable about a pair of first axis supports (44, 46) fixed to the plateform. The impeller is further supported along a second axis transverse to the airstream and about which the impeller is rotatable by a second axis frame (58, 60) that is attached to the first axis frame and that comprises a first arm (58 or 60) supporting a first point of the impeller and extending upstream of the impeller. A first channel arrangement (68 or 70) fixed to the platform can receive the first arm (58 or 60) of the second axis frame so as to allow a higher degree of tilting of a main axis of the impeller from vertically downward than in the absence of the first channel arrangement. Secondly, the system may include an arrangement (90) to substantially seal the orifice or the lift gas chamber downstream of the impeller from upward flow of air. Thirdly, the system may include a stator (120) positioned downstream of the impeller to prevent various airflow problems when the impeller is titled at 90 degrees from vertically downward.
摘要翻译：公开了用于气垫船的气流控制系统的三个方面，所述气垫船包括平台（20）和位于平台下方的提升气体室（20）。首先，该系统包括叶轮（14），用于在入口处接收空气并作为气流在出口处排出加压空气。叶轮定位在提升气体室的孔口（28）上方。叶轮沿横向于气流的第一轴线被支撑，并且叶轮可围绕第一轴框架（48,50）旋转，该第一轴框架可围绕固定到平板模型的一对第一轴支撑件（44,46）旋转。所述叶轮进一步沿横切所述气流的第二轴线被支撑，并且所述叶轮可通过附接到所述第一轴框架且包括支撑所述叶轮的第一臂（58或60）的第二轴框架（58,60）叶轮的第一点并延伸到叶轮的上游。固定在平台上的第一通道装置（68或70）可以容纳第二轴架的第一臂（58或60），从而允许叶轮的主轴线垂直向下的倾斜程度高于没有第一个频道安排。其次，该系统可以包括用于基本密封叶轮下游的孔口或提升气体室免于向上空气流动的装置（90）。第三，该系统可以包括定位器（120），定子（120）定位在叶轮的下游，以防止当叶轮从垂直向下以90度标题时出现各种气流问题。

8. 发明申请

WO2017063205A1 一种使用单涵道风扇进行矢量推进的气垫船审中-公开
公开(公告)号：WO2017063205A1
公开(公告)日：2017-04-20
申请号：PCT/CN2015/092450
申请日：2015-10-21
申请人：佛山夸克兄弟科技有限公司
发明人：封鸿涛 , 王建生 , 康献民 , 李忠峰
IPC分类号： B60V1/14
CPC分类号： B60V1/14 , B60V1/04 , B60V1/043 , B60V1/11 , B60V1/18 , B60V3/02 , B60V3/06 , B63H7/02 , B63H11/12 , B64C27/20
摘要：一种使用单涵道风扇（2）进行矢量推进的气垫船，包括船体（1）和设置在船体上的单涵道风扇，单涵道风扇包括筒状的壳体（21）和设置于壳体内腔的桨叶组件（22），壳体朝向船体尾部的一端设置有第一出风口（211），壳体上设置有可封闭第一出风口的导流舵（212），壳体的两侧还分别设置有两个均与壳体内腔相连通的第一导风管（213），第一导风管上设置有朝向单涵道风扇外部的第二出风口（214），第二出风口与第一出风口反向设置或形成一个数值大于0的夹角。该气垫船用单涵道风扇配合第一出风口、导流舵、第二出风口和第一导风管来完成气垫船的推进、垫升、转向和后退等任务，结构简单，维修保养方便，行驶过程很稳定。

9. 发明申请

WO2004035382A3 AIRSTREAM CONTROL SYSTEM FOR A HOVERCRAFT 审中-公开
标题翻译：空中客车控制系统
公开(公告)号：WO2004035382A3
公开(公告)日：2004-07-01
申请号：PCT/US0332814
申请日：2003-10-16
申请人： AEROMOBILE INC
发明人： BERTELSEN WILLIAM R , GRANT JOHN W
IPC分类号： B60V1/11 , B60V1/14 , B60V1/02
CPC分类号： B60V1/14 , B60V1/11
摘要： Three aspects are disclosed of an airstream control system for a hovercraft that includes a platform (20) and a lift gas chamber (20) beneath the platform. Firstly, the system includes an impeller (14) for receiving air at an inlet and discharging pressurized air at an outlet as an airstream. The impeller is positioned above an orifice (28) of the lift gas chamber. The impeller is supported along a first axis transverse to the airstream and about which the impeller is rotatable by a first axis frame (48, 50) that is rotatable about a pair of first axis supports (44, 46) fixed to the plateform. The impeller is further supported along a second axis transverse to the airstream and about which the impeller is rotatable by a second axis frame (58, 60) that is attached to the first axis frame and that comprises a first arm (58 or 60) supporting a first point of the impeller and extending upstream of the impeller. A first channel arrangement (68 or 70) fixed to the platform can receive the first arm (58 or 60) of the second axis frame so as to allow a higher degree of tilting of a main axis of the impeller from vertically downward than in the absence of the first channel arrangement. Secondly, the system may include an arrangement (90) to substantially seal the orifice or the lift gas chamber downstream of the impeller from upward flow of air. Thirdly, the system may include a stator (120) positioned downstream of the impeller to prevent various airflow problems when the impeller is titled at 90 degrees from vertically downward.
摘要翻译：公开了一种用于气垫船的气流控制系统的三个方面，该系统包括平台下方的平台（20）和提升气室（20）。首先，系统包括用于在入口处接收空气并将作为空气流的出口处的加压空气排出的叶轮（14）。叶轮位于提升气室的孔口（28）上方。叶轮沿着横向于气流的第一轴线被支撑，并且叶轮可围绕该第一轴线框架（48,50）旋转，该第一轴向框架可围绕固定到平板的一对第一轴承座（44,46）转动。叶轮进一步沿横向于气流的第二轴线被支撑，并且叶轮可通过第二轴架（58,60）旋转，第二轴架（58,60）连接到第一轴框架上，并且包括第一臂（58或60）叶轮的第一点并延伸到叶轮的上游。固定到平台的第一通道装置（68或70）可以容纳第二轴架的第一臂（58或60），以便允许叶轮的主轴线垂直向下倾斜的程度比在没有第一个渠道安排。其次，该系统可以包括用于将叶轮下游的孔口或提升气体室基本上密封的空气的上部流动的装置（90）。第三，该系统可以包括定位在叶轮下游的定子（120），以便当叶轮从垂直向下倾斜90度时被标记以防止各种气流问题。

10. 发明申请

WO1993025420A1 TRIMMER FOR A HOVERCRAFT 审中-公开
标题翻译：准备就绪，等待气垫船
公开(公告)号：WO1993025420A1
公开(公告)日：1993-12-23
申请号：PCT/DE1993000526
申请日：1993-06-16
申请人： ABS AIRCRAFT AG , BLUM, Albert , STIEGLER, Hartmut
发明人： ABS AIRCRAFT AG
IPC分类号： B60V01/11
CPC分类号： B60V1/11
摘要： The invention relates to a trimmer for a hovercraft with two engines to provide forward motion, an air compressor to generate the air-cushion beneath the craft and a stabiliser arrangement at its stern. It is the aim of the invention to provide a trimmer for a hovercraft which can be made with simple means and is capable of largely compensating for a shift in the centre of gravity. According to the invention, an additional force component is generated which compensates for the shift in the centre of gravity from the centre of buoyancy caused by difference, in the load aboard the craft. To this end, the stabiliser consists of a negatively arranged V-plane (7), whose downwardly directed stabiliser surfaces (9, 10) which are also fitted with a rudder element (11, 12) run centrally through the flow outlet apertures of the engines (2, 3).

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