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公开(公告)号：US20130309081A1
公开(公告)日：2013-11-21
申请号：US13897075
申请日：2013-05-17
发明人： Søren Hjort
IPC分类号： F03D1/04
CPC分类号： F03D1/04 , F05B2210/16 , F05B2240/122 , F05B2240/124 , F05B2240/133 , Y02E10/726
摘要： The present disclosure relates to a fluid turbine including a rotor and one or more ringed airfoil segments in fluid communication with a wake of the rotor. Each of the ringed airfoil segments includes a leading edge positioned co-planar with or downstream of the rotor plane as measured along the central axis. The ringed airfoil segments may include associated mixing elements. The fluid turbine may include a second ringed airfoil downstream of the one or more ringed airfoil segments.
摘要翻译： 本公开涉及一种流体涡轮机，其包括转子和与转子的尾流流体连通的一个或多个环形翼型段。 每个环形翼型段包括沿着中心轴测量的与转子平面共面或平行定位的前缘。 环形翼型段可以包括相关联的混合元件。 流体涡轮可以包括在一个或多个环形翼型段的下游的第二环形翼型件。
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公开(公告)号：US20140030059A1
公开(公告)日：2014-01-30
申请号：US14041895
申请日：2013-09-30
发明人： Walter M. Presz, JR. , Michael J. Werle , Søren Hjort , Rune Rubak , Bo Lovmand , Søren Dalsgaard
IPC分类号： F01D11/22
CPC分类号： F03D1/0675 , F01D11/22 , F03D1/04 , F03D7/02 , F03D7/028 , F03D9/25 , F05B2240/12 , F05B2240/122 , F05B2240/124 , F05B2250/41 , Y02E10/723
摘要： One or more variable pitch airfoils in fluid communication with a rotor of a fluid turbine can control the amount of energy directed to the rotor, and further control the amount of energy generated by the turbine. Varying the pitch of the airfoils may provide a means of controlling the power output of a fluid turbine without the need to control the pitch of the rotor blades, and may further provide a means of mitigating the effects of wind shear on the rotor. Variable pitch airfoils may also include a means of controlling the active power, reactive power and SCADA, of a group of fluid turbines.
摘要翻译： 与流体涡轮机的转子流体连通的一个或多个可变桨距翼型件可以控制指向转子的能量的量，并进一步控制涡轮机产生的能量的量。 改变翼型件的间距可以提供控制流体涡轮机的功率输出的手段，而不需要控制转子叶片的桨距，并且还可以提供减轻风切变对转子的影响的手段。 可变桨距翼型件还可以包括控制一组流体涡轮机的有功功率，无功功率和SCADA的装置。
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公开(公告)号：US20130266439A1
公开(公告)日：2013-10-10
申请号：US13860173
申请日：2013-04-10
发明人： Rune Rubak , Carsten H. Westergaard , Søren Hjort
IPC分类号： F01D1/04
CPC分类号： F01D1/04 , F03D1/04 , F05B2240/122 , F05B2240/123 , F05B2240/1231 , F05B2240/124 , F05B2240/133 , F05B2250/182 , Y02E10/72
摘要： The present disclosure relates to fluid turbines having a turbine shroud assembly formed with mixing elements (e.g., both inwardly and outwardly curving elements) having airfoil cross sections. These airfoils form ringed airfoil shapes that provide a means of controlling the flow of fluid over the rotor assembly or over portions of the rotor assembly. The fluid dynamic performance of the ringed airfoils directly affects the performance of the turbine rotor assembly. The mass and surface area of the shrouds result in load forces on support structures. By delaying or eliminating the separation of the boundary layer over the ringed airfoils, boundary layer energizing members (e.g., vortex generators, flow control ports) on the ringed airfoils increase the power output of the fluid turbine system and allow for relatively shorter chord-length airfoil cross sections and therefore reduced mass and surface area of the shroud assemblies.
摘要翻译： 本公开涉及具有涡轮机护罩组件的流体涡轮机，该涡轮机护罩组件形成有具有翼型截面的混合元件（例如，向内和向外的弯曲元件）。 这些翼型件形成环形翼型，其提供控制流体在转子组件上或在转子组件的部分上方的流动的手段。 环形翼型件的流体动力学性能直接影响涡轮转子组件的性能。 护罩的质量和表面积导致支撑结构上的载荷力。 通过延迟或消除环形翼型件上的边界层的分离，环形翼型上的边界层通电构件（例如，涡流发生器，流量控制端口）增加了流体涡轮机系统的功率输出并且允许相对较短的弦长 机翼横截面因此降低了护罩组件的质量和表面积。
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公开(公告)号：US20130266438A1
公开(公告)日：2013-10-10
申请号：US13857750
申请日：2013-04-05
IPC分类号： F01D1/04
CPC分类号： F03D1/0675 , F03D1/04 , F05B2240/122 , F05B2240/123 , F05B2240/133 , Y02E10/72
摘要： A ring airfoil with a voluminous leading edge region, an intermediate region, a trailing edge region including a flap. The ringed structural leading edge region combined with a rigid trailing edge region having intermediate discrete support portions extending therebetween provides sufficient rigidity to support the flap on the trailing edge region while using a membrane intermediate surface to form a portion of the intermediate region of the airfoil.
摘要翻译： 具有大量前缘区域的环形翼片，中间区域，包括翼片的后缘区域。 环形结构前缘区域与具有在其间延伸的中间离散支撑部分的刚性后缘区域结合，提供足够的刚度以在使用膜中间表面以形成翼型的中间区域的一部分的同时支撑后缘区域上的翼片。
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公开(公告)号：US20130195655A1
公开(公告)日：2013-08-01
申请号：US13627361
申请日：2012-09-26
发明人： Jonathan H. Kerner , John Romualdez , Jason Barnes
IPC分类号： F01D5/22
CPC分类号： F01D5/225 , F03B3/123 , F03B3/14 , F03B3/18 , F03B17/061 , F03D1/04 , F03D1/0675 , F03D7/0236 , F03D17/00 , F05B2240/313 , Y02E10/223 , Y02E10/28 , Y02E10/721 , Y02E10/723
摘要： Shrouded fluid turbines having features for setting, adjusting or controlling a blade tip-shroud clearance are described. Also described are methods for setting, adjusting or controlling a blade tip-shroud clearance in a shrouded fluid turbine.
摘要翻译： 描述了具有用于设置，调整或控制叶片尖端 - 护罩间隙的特征的有罩流体涡轮机。 还描述了在被覆盖的流体涡轮机中设置，调节或控制叶片尖端 - 护罩间隙的方法。
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6.发明授权公开(公告)号：US09115690B2
公开(公告)日：2015-08-25
申请号：US13902318
申请日：2013-05-24
CPC分类号： F03D7/00 , F03D1/04 , F03D7/02 , F03D7/0264 , F03D7/028 , F03D17/00 , F03D80/60 , F05B2270/1033 , F05B2270/3032 , H02J3/1885 , Y02E10/723 , Y02E10/763 , Y02E40/32
摘要： Systems and methods for maintaining the active power production of a fluid turbine and regulating the temperature of an electrical generating component by controlling the reactive power production are disclosed. A thermal parameter of the electrical generating component is monitored. If the electrical generating component exceeds a thermal parameter the reactive power production of the turbine is reduced. A fluid turbine may be de-rated to further reduce an electrical generating component's thermal parameter. A fluid turbine may shut down to further reduce an electrical generating component's thermal parameter. A fluid turbine's power production is re-started when the electrical generating component returns to an acceptable thermal parameter.
摘要翻译： 公开了通过控制无功功率产生来维持流体涡轮机的有功功率生产和调节发电部件的温度的系统和方法。 监测发电部件的热参数。 如果发电部件超过热参数，则涡轮机的无功功率减少。 流体涡轮可以被降低以进一步减少发电部件的热参数。 流体涡轮机可以关闭以进一步减少发电部件的热参数。 当发电组件返回到可接受的热参数时，流体涡轮机的功率产生被重新启动。
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公开(公告)号：US20130287543A1
公开(公告)日：2013-10-31
申请号：US13870348
申请日：2013-04-25
发明人： Robert H. Dold , Skye H. Morse
IPC分类号： F03D1/04
CPC分类号： F03D1/04 , F03D7/0204 , F03D13/20 , F05B2240/2213 , F05B2270/402 , Y02E10/723 , Y02E10/726
摘要： A shrouded fluid turbine includes a support structure, a nacelle body rotationally coupled to the support structure and configured to pivot about a pivot axis passing through the support structure, a rotor coupled to the nacelle body and having a rotor plane passing therethrough, the rotor plane being offset from the pivot axis, and an aerodynamically contoured turbine shroud surrounding the rotor and having a leading edge, a trailing edge and a plurality of mixing elements disposed therein. A center of pressure may be located downstream of the rotor plane with respect to direction of a fluid flow, and a combination of the nacelle body, the rotor, and the aerodynamically contoured turbine shroud may be configured to pivot about the pivot axis in response to a force exerted on the combination by the fluid flow such that the leading edge faces into the direction of the fluid flow.
摘要翻译： 被覆盖的流体涡轮机包括支撑结构，旋转地联接到支撑结构并且构造成围绕通过支撑结构的枢转轴线枢转的机舱主体，联接到机舱本体并具有通过其的转子平面的转子，转子平面 偏心于枢转轴线，以及围绕转子并具有设置在其中的前缘，后缘和多个混合元件的空气动力学轮廓的涡轮机护罩。 压力中心可以相对于流体流动的方向位于转子平面的下游，并且机舱本体，转子和空气动力学轮廓的涡轮机护罩的组合可以被配置为响应于枢转轴线枢转 通过流体流施加在组合上的力，使得前缘面向流体流动的方向。
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公开(公告)号：US20130266446A1
公开(公告)日：2013-10-10
申请号：US13860037
申请日：2013-04-10
IPC分类号： F01D5/12
CPC分类号： F01D5/12 , F03D1/04 , F05B2240/122 , F05B2240/123 , F05B2240/1231 , F05B2240/124 , F05B2240/133 , F05B2250/182 , Y02E10/72
摘要： A shrouded fluid turbine includes a ringed airfoil having a leading edge, a trailing edge, an outer surface, an inner surface, and a body extending from the leading edge to the trailing edge. The shrouded turbine further includes a rotor surrounded by the ringed airfoil. The rotor is disposed downstream of the leading edge and about a central axis of the fluid turbine. The shrouded turbine further includes an aperture extending through the body of the ringed airfoil between the outer surface and the inner surface. The aperture is configured to mix a first fluid flow adjacent to the outer surface of the ringed airfoil and a second fluid flow downstream of the rotor.
摘要翻译： 被覆盖的流体涡轮机包括具有前缘，后缘，外表面，内表面和从前缘延伸到后缘的主体的环形翼型件。 被覆盖的涡轮机还包括由环形翼片包围的转子。 转子设置在前缘的下游并且围绕流体涡轮机的中心轴线。 被覆盖的涡轮机还包括在外表面和内表面之间延伸穿过环形翼型件的主体的孔。 孔被构造成将邻近环形翼型件的外表面的第一流体流与转子下游的第二流体流混合。
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公开(公告)号：US20130101403A1
公开(公告)日：2013-04-25
申请号：US13657768
申请日：2012-10-22
IPC分类号： F03D11/00
CPC分类号： F03D1/04 , F05B2240/13 , Y02E10/72
摘要： A ring fluid foil including a modified trailing portion for a shrouded fluid turbine and shrouded fluid turbine including such ring fluid foils are described herein. The modification of the trailing portion increases flow turning by the fluid foil without, or with reduced, boundary layer separation on a suction side of the fluid foil.
摘要翻译： 本文描述了包括用于被覆流体涡轮机的改进的后部部分和包括这种环形流体箔的被覆盖的流体涡轮机的环形流体箔。 拖尾部分的修改增加了在流体箔的吸力侧上没有边界层分离或减少的流体箔片流动的流动。
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公开(公告)号：US20140169937A1
公开(公告)日：2014-06-19
申请号：US14133547
申请日：2013-12-18
发明人： Daniel Gysling , Ercan Dumlupinar
IPC分类号： F03D1/04
摘要： Example embodiments are directed to fluid turbines that include a turbine shroud, a rotor and an ejector shroud. The turbine shroud includes an inlet, an outlet, a leading edge and a trialing edge. The leading edge of the turbine shroud can be round and the trialing edge of the turbine shroud can include linear faceted segments. The rotor can be disposed within the turbine shroud and can define a rotor plane. The turbine shroud can provide a first portion of a fluid stream to the rotor plane via the inlet of the turbine shroud. The ejector shroud can provide a second portion of the fluid stream to the outlet of the turbine shroud via an open area. An example method of operating a fluid turbine is also provided.
摘要翻译： 示例性实施例涉及包括涡轮机罩，转子和喷射器护罩的流体涡轮机。 涡轮机罩包括入口，出口，前缘和修复边缘。 涡轮机护罩的前缘可以是圆形的，并且涡轮机护罩的修剪边缘可以包括线性分面段。 转子可以设置在涡轮罩内并且可以限定转子平面。 涡轮机护罩可以经由涡轮机护罩的入口将流体流的第一部分提供给转子平面。 喷射器护罩可以经由开放区域将流体流的第二部分提供给涡轮机护罩的出口。 还提供了操作流体涡轮机的示例性方法。
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