| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 1 | 用于空气动力学的型面元件的发射和回收装置，以及空气动力学的型面元件 | CN200680055610.5 | 2006-08-15 | CN101511671A | 2009-08-19 | 斯特凡·弗拉格; 斯特凡·布拉贝克 |
| 本发明涉及一种用于借助牵引力产生能量的空气动力学的型面元件，尤其是用于驱动水上交通工具。所述空气动力学的型面元件包括：沿横向方向和纵向方向延伸的柔性的上层；柔性的下层，所述下层平行于上层延伸并且借助多个沿型面元件的深度方向延伸的腹板与上层连接；在上层和下层之间的充气的内腔；至少一个布置在上层和下层的两个相互平行放置的前缘之间的用于内腔通风的通风口；多条牵拉绳，所述牵拉绳的第一端固定在型面元件上的间隔的位置上并且其第二端与牵拉索连接用于连接型面元件和水上交通工具；以及多条缩帆绳，所述缩帆绳的第一端固定在层和/或腹板上。所述缩帆绳构成为使得通过上层和下层的缩帆或放帆来减小或增大型面元件的尺寸。所述空气动力学的型面元件通过沿型面元件的纵向方向延伸的用于稳定空气动力学的型面的杆元件改进，其中杆元件固定在上层和/或下层上和/或腹板上，并且在杆元件上至少一条缩帆绳从自第一端上的固定点开始沿上层或下层的型面元件的横向方向延伸的缩帆绳段转向到沿纵向方向延伸的缩帆绳段。 | ||||||
| 2 | 用于结构应用的可充气提花织物 | CN201680017986.0 | 2016-03-25 | CN107429444A | 2017-12-01 | N·A·坎德瑞安-贝尔; T·G·贝尔 |
| 本发明的实施例包括具有成形的、封闭的可充气袋的编织的多层织物，其中，所述充气织物承载张力、压缩、扭转和/或弯曲载荷。还描述并要求保护包含这种可充气元件或翼梁的复合结构。 | ||||||
| 3 | 用于空气动力学的型面元件的发射和回收装置及型面元件 | CN200680055610.5 | 2006-08-15 | CN101511671B | 2013-01-02 | 斯特凡·弗拉格; 斯特凡·布拉贝克 |
| 本发明涉及一种用于借助牵引力产生能量的空气动力学的型面元件，尤其是用于驱动水上交通工具。所述空气动力学的型面元件包括：沿横向方向和纵向方向延伸的柔性的上层；柔性的下层，所述下层平行于上层延伸并且借助多个沿型面元件的深度方向延伸的腹板与上层连接；在上层和下层之间的充气的内腔；至少一个布置在上层和下层的两个相互平行放置的前缘之间的用于内腔通风的通风口；多条牵拉绳，所述牵拉绳的第一端固定在型面元件上的间隔的位置上并且其第二端与牵拉索连接用于连接型面元件和水上交通工具；以及多条缩帆绳，所述缩帆绳的第一端固定在层和/或腹板上。所述缩帆绳构成为使得通过上层和下层的缩帆或放帆来减小或增大型面元件的尺寸。所述空气动力学的型面元件通过沿型面元件的纵向方向延伸的用于稳定空气动力学的型面的杆元件改进，其中杆元件固定在上层和/或下层上和/或腹板上，并且在杆元件上至少一条缩帆绳从自第一端上的固定点开始沿上层或下层的型面元件的横向方向延伸的缩帆绳段转向到沿纵向方向延伸的缩帆绳段。 | ||||||
| 4 | Launching / recovery mechanism and aerodynamic profile element for the aerodynamic profile element | JP2009524080 | 2006-08-15 | JP2010500221A | 2010-01-07 | シュテファン・ヴラゲ; シュテファン・ブラベック |
| ウォータークラフトを駆動するために引っ張り力によってエネルギーを生成する空気力学的プロファイル要素は、上側可撓層、上側層と平行で複数のウェブで上側層へ接続される下側可撓層、上側及び下側層間の内部空間、上側及び下側層の前縁間の空気取入開口、及びウォータークラフトへと接続するための複数の縮帆線を備える。 縮帆線は、第１の端部がプロファイル要素上の離間した位置に固定され、第２の端部が引張ケーブルに接続されている複数の引張線へ接続され、上側及び下側層の縮帆又は伸帆でプロファイル要素のサイズを増減させる。 空気力学的プロファイルの安定のために長手方向に延び棒部材によって発展させられる。 縮帆線の少なくとも１つが棒部材において、第１の端部の固定点からプロファイル要素の横方向に延びる縮帆線部分から、長手方向に延びる縮帆線部分へ向きを変える。 | ||||||
| 5 | JPS6125598B2 - | JP9862380 | 1980-07-18 | JPS6125598B2 | 1986-06-16 | ANDORIU UIRUFURITSUDO JOONZU; REIMONDO MERII |
| 6 | Vane structure | JP9862380 | 1980-07-18 | JPS5617794A | 1981-02-19 | ANDORIU UIRUFURITSUDO JIYOONZU; REIMONDO MERII |
| 7 | METHOD FOR MONITORING KITE AIR PRESSURE WHEN KITE BOARDING | US15107645 | 2015-01-15 | US20160325831A1 | 2016-11-10 | Ross Davis Harrington; Peter G. Berrang |
| A method for monitoring air pressure in a kite when kite boarding is described. The method involves a first step of connecting an air pressure sensor to one or more bladders of the kite. The method involves a second step of positioning a visual display for the air pressure sensor where it will be visible to a user conducting a visual inspection of the kite to display a pressure reading as sensed by the pressure sensor. | ||||||
| 8 | IN-FLIGHT KITE DEFLATION AND CONTROL SYSTEMS | US14386324 | 2012-03-27 | US20150129721A1 | 2015-05-14 | Peter G. Berrang; Ross D. Harrington; Richard K. Myerscough |
| A massive de-powering system for a kite wing used in kite boarding comprises a deflation control line that connects to a valve on the kite wing's leading edge bladder. In the preferred embodiment, disengaging the tether line from the harness causes the deflation control line to tension and to open the valve, thereby deflating the bladder. Tension along the deflation control line may also act to draw in spaced portions of the wing thereby collapsing it and further reducing the power generated by the wing. | ||||||
| 9 | Traction kite with high projected leading edge | US13531819 | 2012-06-25 | US08844875B1 | 2014-09-30 | Peter Stiewe |
| A traction kite having a variable geometry leading edge that defines a high projected central propulsive region of increased surface area along the top portion of the kite, and lateral control regions of decreased surfaces area extending on opposite sides of the propulsive region. The leading edge thus defines a concave shape when viewed from the side while in flight. Providing a variable geometry leading edge maximizes propulsive forces due to increased surface area, while enhancing control and turning performance by minimizing the surface area of the control regions, namely those generally vertically disposed regions that begin at the tips and end at the propulsive region. | ||||||
| 10 | SYSTEM FOR RELEASING OPPOSING TENSIONED LINES | US12375214 | 2007-07-30 | US20100006703A1 | 2010-01-14 | Corwin Hardham; Johannes Van Niekerk; Daniel W. Meyers; Gregory C. Ashton |
| Release systems for tensioned lines, which release under a predetermined change in tension; particularly systems for use in towing airfoils for sports and recreational activities coupling the airfoil to a rider. | ||||||
| 11 | INFLATABLE KITE WITH VENTS | US12190473 | 2008-08-12 | US20090045291A1 | 2009-02-19 | Ross Davis Harrington |
| An inflatable kite uses an inflatable tubular member as a leading edge. The wing is a membrane attached to the front of the leading edge to form a high camber for high lift. Vents in the wing fabric have flaps on them to form nozzles which, when wind is blowing over the kite, cause high pressure air under the kite to exhaust to the top surface of the kite and extend conditions of near laminar flow towards the trailing edge. This increases kite stability and improves stall characteristics. | ||||||
| 12 | Device for launching a power kite | US11098093 | 2005-04-04 | US07374129B2 | 2008-05-20 | Mark Brian Godley |
| A device is provided for the management of multiple lines attached to a bar, of the type used in power kites for kiteboarding. The device is formed of an elongate body having a shaft region, a spool region adjacent the shaft region and distal thereto, and a line retaining region distal to the spool region. The shaft region has a hollow body having a longitudinal groove running from a proximal opening to a distal end point, and a bar retaining means for retaining a bar against rotational or axial movement. The spool region has a spool shaft defined by proximal and distal containment means for retaining spooled lines wound about the spool shaft. A line retaining region has a means for separately retaining one or more lines of a plurality of lines. | ||||||
| 13 | Launch and retrieval arrangement for an aerodynamic profile element and an aerodynamic profile element | US11529902 | 2006-09-29 | US07287481B1 | 2007-10-30 | Stephan Wrage; Stephan Brabeck |
| The invention relates to an aerodynamic profile element for energy production using traction force, in particular for driving watercraft. The invention further relates to a launch and retrieval arrangement for a profile element, and a drive arrangement for a watercraft including the profile element and the launch and retrieval arrangement. | ||||||
| 14 | Tube kite | US10558347 | 2004-11-10 | US20070120016A1 | 2007-05-31 | Till Eberle; Ken Winner |
| What is disclosed is a tube kite comprising two front lines which are combined into a tug line and adapted to be releasably secured to the surfer, and comprising two back lines which are adapted to be secured to a bar, wherein a supplementary line serving as an additional front line during the flight phase is provided. | ||||||
| 15 | Inflatable wing with manifold | US10773652 | 2004-02-06 | US07140576B2 | 2006-11-28 | Tony Logosz |
| An aerodynamic wing with a leading edge inflatable strut and at least one inflatable rib strut, wherein the struts are provided with a connection air pathway that allows the leading edge strut to act as a manifold for the inflation of the connected rib struts. Preferably, the connection air pathway is provided with a valve mechanism for selectively isolating the connected rib strut from the leading edge strut. | ||||||
| 16 | Bridle assembly for a kite | US11254490 | 2005-10-20 | US20060097114A1 | 2006-05-11 | Patrick Goodman |
| A bridle assembly for attaching a control line to a kite has a bridle line extending between a first attachment point located at or near a first wing tip of a kite and a second attachment point located near a leading edge of the kite away from the wing tip. A pulley is positioned about the bridle line and is movable along the bridle line. The pulley has a third attachment point for a kite control line. | ||||||
| 17 | Kite safety, control, and rapid depowering apparatus | US10914364 | 2004-08-09 | US07036771B1 | 2006-05-02 | Alexander S. Pouchkarev |
| A kite safety, control, and depowering device for a kite having an airfoil with leading and trailing edges, at least two control lines attached to the airfoil and a control flying bar attached to at least two of the control lines. The device features a continuous trim and safety flying line disposed at their lower ends over a rapid depowering apparatus. The depowering apparatus includes means for capturing and rapidly releasing an expansion disposed on the trim line, such that when rapid depowering is required, a simply release mechanism may be actuated to change the angle of attack of the airfoil rapidly. | ||||||
| 18 | Safety system for a kite user that allows rotational independence of the user in relation to the flying control bar and the kite. The system also induces stable and powerless descent of the kite when safety system is activated. Easy and quick recovery prior to re-launching the kite | US10360791 | 2002-07-03 | US20040195459A1 | 2004-10-07 | Alexander Sergeevich Pouchkarev |
| This device is a safety system for a kite use that allows rotational independence of the user in relation to the flying control bar and the kite. This safety system also induces stable and powerless descent of the kite when safety system is activate. Easy and quick recovery prior to re-launching the kite is another benefiting feature to this safety system device. | ||||||
| 19 | Traction kite design | US10473114 | 2003-09-29 | US20040113019A1 | 2004-06-17 | Peter Robert Lynn |
| A traction kite in use is arch-shaped, when flying lines (1a, 1b, 2a, 2b) are connected to a flier, boat, buggy, etc. The kite's leading edge (9) when viewed in plan, with the kite laid out flat, is concave at centre section (A) and straight or convex near wing tips (5a-5b). The kite is rigidified by ram air, pneumatic tube framing on a single skin, etc. The convexity of the shoulders of leading edge (9) resists shoulder collapse due to line loading whilst the concavity of centre section (A) allows lower angles of attack. | ||||||
| 20 | Adaptable kite/airfoil | US10361957 | 2003-02-10 | US20030150957A1 | 2003-08-14 | Paul J. Thomas |
| An Adaptable kite/airfoil preferably for structured kites having effectively nullreefablenull sub-section(s) typically changing the effective width and/or length of the airfoil, thereby substantially changing the aerodynamic characteristics of the airfoil, using continuous sheet material sections not separated in flight use or in changing the kite aerodynamics. Thus, all of the sheet material, skin of the kite remain with the kite in its various configurations. Seven exemplary embodiments which achieve this approach are described including (1) roll-up section(s) (FIGS. 2A & 2B); (2) integrally contiguous, fold over, over-lapped section(s) (FIGS. 3 & 5); (3) continuous but not integrally contiguous, overlap section(s) using a telescoping arrangement (FIGS. 4A-4C);(4) varyingly compressed and/or aligned battens (FIGS. 5-6); (5) variable wing tips (FIG. 7); (6) center pull-down or up (FIGS. 8 & 9); and (7) in flight expandable/contractible center pulled up or down (FIG. 10). | ||||||
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