公开(公告)号：US12085052B2

公开(公告)日：2024-09-10

申请号：US18239695

申请日：2023-08-29

申请人： Lone Gull Holdings, Ltd.

发明人： Brian Lee Moffat ,  Garth Alexander Sheldon-Coulson

IPC分类号： F03B13/22 ,  F03B11/02 ,  F03B13/10 ,  F03B13/18

CPC分类号： F03B13/22 ,  F03B11/02 ,  F03B13/10 ,  F03B13/183 ,  F05B2210/404 ,  F05B2230/60 ,  F05B2240/133 ,  F05B2250/70 ,  F05B2260/404 ,  F05B2260/95 ,  Y02E10/20 ,  Y02E10/30 ,  Y02P70/50

摘要： A wave energy converter utilizes a flotation module that rises and falls with the passage of waves, a submerged tube containing a constriction which multiplies the speed of the water passing therethrough, a turbine (or other hydrokinetic apparatus) positioned so as to extract energy from the accelerated flow of water within and/or through the tube, and a submerged gas- or liquid-filled chamber housing one or more energy conversion components (e.g. generators, transformers, rectifiers, inverters). By providing a chamber in proximity to the turbine, generators can be placed in closer proximity to the turbine that turns them, and the shared shaft can be shorter than if the generators were placed in the buoy adjacent to the surface.

公开(公告)号：US11661917B2

公开(公告)日：2023-05-30

申请号：US17273077

申请日：2019-08-12

申请人： O-INNOVATIONS LTD.

发明人： Nicolás Gonzalo Orellana Olguín

IPC分类号： F03D5/00 ,  F03D1/00 ,  F03D3/00

CPC分类号： F03D5/00 ,  F03D1/00 ,  F03D3/00 ,  F05B2220/706 ,  F05B2250/11 ,  F05B2250/70

摘要： It is about an omnidirectional generator apparatus, capable of translating the push of a fluid from any direction in the vertical, horizontal or diagonal plains to rotational movement on a unique axis. This rotational movement can be translated to electric energy by known means.

公开(公告)号：US20170130694A1

公开(公告)日：2017-05-11

申请号：US15318080

申请日：2015-06-15

申请人： Antonio LA GIOIA

发明人： Antonio LA GIOIA

IPC分类号： F03D1/06

CPC分类号： F03D1/0616 ,  F05B2210/16 ,  F05B2240/201 ,  F05B2250/70 ,  Y02E10/721

摘要： The present invention relates to a rotating blade body for turbines using the Magnus effect with an axis of rotation of the turbine parallel to the direction of the motor fluid, characterised in that it is defined by a first sector or end head, more distant from said axis of rotation of the turbine, and by a second sector or rod, connecting said first sector and said axis of rotation of the turbine, said second sector having an average diameter smaller than the diameter of said first sector, said first sector being inscribed within a solid of revolution whose profile is determined so as to maintain a constant value of lift in each section.

公开(公告)号：US08678770B2

公开(公告)日：2014-03-25

申请号：US12594205

申请日：2008-04-01

申请人： Peder Bay Enevoldsen ,  Søren Hjort ,  Jesper Laursen

发明人： Peder Bay Enevoldsen ,  Søren Hjort ,  Jesper Laursen

IPC分类号： F03D1/06

CPC分类号： F03D1/0633 ,  F05B2240/30 ,  F05B2250/70 ,  Y02E10/721

摘要： A wind turbine rotor blade defined by a tip point, a shoulder, a maximum chord interval which is defined as the radial interval over which the blade chord is no less that 95% of the shoulder chord and which extends over at least 15% of the entire blade length, and an outer blade interval extending from the maximum chord interval to the tip point, wherein the outer blade interval has a concave hyperbolic chord distribution from the maximum chord interval towards the tip point. Further a method for optimizing the chord distribution of a wind turbine blade layout is provided, wherein the chord distribution is optimized by optimizing the chord distribution in the maximum chord interval by maximizing the ratio of the annual energy production to the loads acting on the blade and in the outer blade interval with respect to the annual energy production alone.

摘要翻译： 由尖端，肩部，最大弦间隔限定的风力涡轮机转子叶片，其最大弦间隔被定义为叶片弦不小于肩弦的95％并且延伸至至少15％ 整个刀片长度和从最大弦间隔延伸到尖端点的外刀片间隔，其中外刀片间隔具有从最大弦间隔朝向尖端点的凹双曲线和弦分布。 还提供了一种用于优化风力涡轮机叶片布置的弦分布的方法，其中通过使年能量产生与作用在叶片上的载荷的比例最大化来优化最大弦间隔中的弦分布来优化弦分布;以及 在相对于年度能源生产的外叶间隔中。

公开(公告)号：US20130259696A1

公开(公告)日：2013-10-03

申请号：US13712834

申请日：2012-12-12

申请人： The Regents of the University of California

发明人： Vladimir Krivcov ,  Vladimir Krivospitski ,  Vasili Maksimov ,  Richard Halstead ,  Jurij Vasiljevich Grahov

IPC分类号： F01D5/14 ,  F03D3/02

CPC分类号： F01D5/141 ,  F03D3/005 ,  F03D3/061 ,  F03D9/11 ,  F03D9/25 ,  F05B2240/214 ,  F05B2240/301 ,  F05B2240/40 ,  F05B2250/70 ,  F05B2280/6003 ,  F05B2280/6012 ,  F05C2253/14 ,  Y02E10/74

摘要： A vertical axis wind turbine airfoil is described. The wind turbine airfoil can include a leading edge, a trailing edge, an upper curved surface, a lower curved surface, and a centerline running between the upper surface and the lower surface and from the leading edge to the trailing edge. The airfoil can be configured so that the distance between the centerline and the upper surface is the same as the distance between the centerline and the lower surface at all points along the length of the airfoil. A plurality of such airfoils can be included in a vertical axis wind turbine. These airfoils can be vertically disposed and can rotate about a vertical axis.

摘要翻译： 描述了垂直轴风力涡轮机翼型。 风力涡轮机翼型件可以包括前缘，后缘，上曲面，下弯曲表面和在上表面和下表面之间以及从前缘到后缘行进的中心线。 翼型件可以被构造成使得中心线和上表面之间的距离与沿着翼型长度的所有点处的中心线和下表面之间的距离相同。 多个这样的翼型件可以包括在垂直轴风力涡轮机中。 这些翼型件可以垂直设置并且可以围绕垂直轴线旋转。

公开(公告)号：US20120288372A1

公开(公告)日：2012-11-15

申请号：US13558179

申请日：2012-07-25

申请人： Fabio P. Bertolotti

发明人： Fabio P. Bertolotti

IPC分类号： F03D1/06 ,  F03D11/00

CPC分类号： F03D7/02 ,  F05B2240/2022 ,  F05B2250/70 ,  F05B2260/76 ,  F05B2260/96 ,  F05B2270/506 ,  F05B2270/604 ,  Y02E10/721 ,  Y02E10/723

摘要： A wind turbine system includes a shaft, a rotor for driving the shaft, and a first fluidic teeter control assembly. The rotor includes a first blade engaged to the shaft by a hub, and has a degree of freedom to pivot relative to the shaft. A first teeter angle is defined between an instantaneous position of the first blade and a time-averaged plane of rotation of the first blade. The first fluidic teeter control assembly is engaged between the rotor and the shaft for providing a first dynamic teeter restraining force as a function of the first teeter angle and a fluidic resistance. The first dynamic restraining force is relatively low when the first teeter angle is within a first teeter operation range, and the first dynamic restraining force is higher when the first teeter angle is outside that range.

摘要翻译： 风力涡轮机系统包括轴，用于驱动轴的转子和第一流体跷跷板控制组件。 转子包括通过毂接合到轴的第一叶片，并且具有相对于轴枢转的自由度。 在第一叶片的瞬时位置和第一叶片的时间平均旋转平面之间限定第一跷跷板角度。 第一流体跷跷板控制组件接合在转子和轴之间，用于提供作为第一跷跷板角度和流体阻力的函数的第一动态踩踏器限制力。 当第一跷跷板角度在第一踩踏器操作范围内时，第一动态限制力相对较低，并且当第一跷跷板角度在该范围之外时，第一动态限制力较高。

公开(公告)号：US08226349B2

公开(公告)日：2012-07-24

申请号：US12181289

申请日：2008-07-28

申请人： Marty A. Ferman

发明人： Marty A. Ferman

IPC分类号： F03D7/02

CPC分类号： F01D5/147 ,  B64C11/18 ,  B64C27/06 ,  B64C27/467 ,  F01D7/00 ,  F03D1/0625 ,  F05B2250/70 ,  F05D2250/70 ,  Y02E10/721 ,  Y02T50/673

摘要： A method of using a delta shaped blade as an aircraft propeller, helicopter or autogiro rotor, or wind turbine propeller is presented. The invention combines the delta blade system with the use of torsion bars to achieve desirable control of blade twist. The invention uses blade twist to control the air loading on the craft; hence better control of maneuvering is achieved. The invention also optionally includes adjustable blade roots such that the sweep and aspect ratio of the delta blade is controllably variable. Compared to traditional propeller blade configurations, the invention boasts improved performance and enhanced aeroelastic properties. The invention is a far more efficient system providing economic advantages, higher speeds, and more durable designs.

摘要翻译： 提出了使用三角形叶片作为飞行器螺旋桨，直升机或自动转子或风力涡轮机螺旋桨的方法。 本发明结合了三角叶片系统与扭杆的使用，以实现叶片扭转的理想控制。 本发明使用叶片扭转来控制工艺上的空气负载; 从而更好地控制机动。 本发明还可选地包括可调叶片根部，使得叶片的扫掠和纵横比可控地变化。 与传统的螺旋桨叶片结构相比，本发明具有改进的性能和增强的气动弹性性能。 本发明是提供经济优点，更高速度和更耐用的设计的更有效的系统。

公开(公告)号：US20120051916A1

公开(公告)日：2012-03-01

申请号：US13094237

申请日：2011-04-26

申请人： Bharat Bagepalli ,  Aniruddha D. Gadre ,  Nitin Narayan Bhate

发明人： Bharat Bagepalli ,  Aniruddha D. Gadre ,  Nitin Narayan Bhate

IPC分类号： F01D15/10

CPC分类号： F03D1/025 ,  F03D1/0641 ,  F03D1/065 ,  F03D1/0658 ,  F03D9/25 ,  F03D15/10 ,  F05B2220/7066 ,  F05B2240/30 ,  F05B2250/70 ,  Y02E10/721 ,  Y02E10/725

摘要： A wind turbine includes a nacelle mounted atop a tower. Power generating components are housed within the nacelle. A rotor hub is rotationally coupled to the power generating components. A plurality of blades are fixed to the rotor hub. The blades include a root section extending radially outward from the rotor hub and an aerodynamic section extending radially outward from the root section, wherein lift is generated by the blades primarily along the aerodynamic section. Aerodynamic fins extend radially outward from the rotor hub alongside the root sections of the blades and have an aerodynamic shape so as to capture wind and impart rotational torque to the hub from a central impinging wind zone that is coaxial to the rotor hub and the blade root sections.

摘要翻译： 风力涡轮机包括安装在塔顶上的机舱。 发电部件容纳在机舱内。 转子毂旋转地联接到发电部件上。 多个叶片固定在转子轮毂上。 叶片包括从转子毂径向向外延伸的根部段和从根部部分径向向外延伸的空气动力部分，其中主要沿着空气动力学部分由叶片产生升力。 空气动力翼片从转子毂沿径向向外延伸，并且具有空气动力学形状，以便从与转子轮毂和叶片根部共轴的中心冲击风区向轮毂施加旋转扭矩 部分。

公开(公告)号：US08100661B2

公开(公告)日：2012-01-24

申请号：US12218481

申请日：2008-07-15

申请人： Peder Bay Enevoldsen ,  Søren Hjort ,  Rune Rubak

发明人： Peder Bay Enevoldsen ,  Søren Hjort ,  Rune Rubak

IPC分类号： B63H1/26 ,  B63H7/02 ,  B64C11/16 ,  B64C27/46 ,  F01D5/14 ,  F03B7/00 ,  F03D11/02 ,  F04D29/38

CPC分类号： F03D1/0633 ,  F05B2240/301 ,  F05B2250/70 ,  F05B2260/96 ,  F05B2270/20 ,  Y02E10/721

摘要： A wind turbine rotor blade is provided which includes a root end and a tip end located opposite the root end. A leading edge extends from the root end to the tip end. A trailing edge extends from the root end to the tip end. A span direction is defined by a line extending linearly from the root end to the tip end. A chord direction is perpendicular to the span direction and lies in the plane extending through the leading edge and the trailing edge. A shoulder is the point of the maximum chord-wise extension. An airfoil portion extends from the shoulder to the tip end. The airfoil portion comprises a span-wise interval begging before the tip end and extending to or close to the tip end and in which the distribution of the chord-wise extension is increased as compared to the load optimised distribution of the chord-wise extension.

摘要翻译： 提供了一种风力涡轮机转子叶片，其包括根端和位于根端相对的尖端。 前缘从根端延伸到尖端。 后缘从根端延伸到尖端。 跨度方向由从根端到尖端线性延伸的线限定。 弦方向垂直于跨度方向，并且位于延伸穿过前缘和后缘的平面中。 肩膀是最大和弦延伸点。 翼型部分从肩部延伸到尖端。 翼型部分包括在尖端之前乞求并且延伸到或接近尖端的跨度间隔，并且与弦向延伸部的载荷优化分布相比，弦向延伸部的分布增加。

公开(公告)号：US07975438B2

公开(公告)日：2011-07-12

申请号：US12523712

申请日：2008-01-17

申请人： Jordi Puigcorbé Punzano ,  Enrique Elkoroberezibar Markiegi

发明人： Jordi Puigcorbé Punzano ,  Enrique Elkoroberezibar Markiegi

IPC分类号： E02D27/42

CPC分类号： F03D13/22 ,  F03D13/10 ,  F03D13/20 ,  F05B2240/912 ,  F05B2250/232 ,  F05B2250/70 ,  F05B2260/30 ,  Y02E10/728

摘要： A joining device (8) for hybrid wind turbine towers (5) intended for the fixation of a metal portion (6) of a wind turbine tower (5) to a concrete portion (7) of said wind turbine (1) which comprises a metal body (9) having a generally tubular configuration that is suitable to be fixed to the metal portion (6) of the tower (5) which in use is adjacent to the concrete portion (7), and suitable for being at least partially embedded into said concrete portion (7), said metal body (9) being provided with a number of anchoring openings (11) adapted such that the material of the concrete portion (7) passes therethrough. A hybrid wind turbine tower (5) comprises such a joining device (8) provided between one metal portion (6) and one concrete portion (7).

摘要翻译： 一种用于将风力涡轮机塔架（5）的金属部分（6）固定到所述风力涡轮机（1）的混凝土部分（7）上的混合风力涡轮机塔架（5）的接合装置（8），其包括 金属体（9）具有大致管状的结构，其适于固定在塔（5）的金属部分（6）上，塔（5）在使用中与混凝土部分（7）相邻，并且适于至少部分地嵌入 在所述混凝土部分（7）中，所述金属体（9）设置有多个适于使混凝土部分（7）的材料穿过其中的锚定开口（11）。 混合风力涡轮机塔架（5）包括设置在一个金属部分（6）和一个混凝土部分（7）之间的这种接合装置（8）。