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1.发明授权Wind turbine with tower support system and associated method of construction 有权具有塔架支撑系统的风力发电机和相关的施工方法公开(公告)号：US08245458B2
公开(公告)日：2012-08-21
申请号：US13109519
申请日：2011-05-17
CPC分类号： E04H12/347 , F03D13/10 , F03D13/20 , F03D80/70 , F05B2240/913 , Y02E10/728
摘要： A wind turbine has a nacelle mounted atop a tower, with a support system configured around a base portion of the tower. The support system includes a plurality of support fins spaced radially around the base portion. Each of the support fins has a continuous header member secured to the tower and a continuous face member extending radially outward and downward from the header member towards ground. The support fins include a web extending between the header member and face member. The support fins extend from the tower with a length and at an acute extension angle relative to a longitudinal axis of the tower so as to provide vertical and lateral support around the circumference of the tower.
摘要翻译： 风力涡轮机具有安装在塔顶上的机舱，其中配置有围绕塔的基部的支撑系统。 支撑系统包括围绕基部径向地间隔开的多个支撑翅片。 每个支撑翅片具有固定到塔架的连续头部构件和从头部构件向地面径向向外和向下延伸的连续面构件。 支撑翅片包括在头部构件和面部构件之间延伸的腹板。 支撑翼片相对于塔的纵向轴线从塔架延伸一段长度并且具有一个锐角，以便围绕塔架的圆周提供垂直和侧向支撑。
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2.发明申请WIND TURBINE WITH TOWER SUPPORT SYSTEM AND ASSOCIATED METHOD OF CONSTRUCTION 有权具有塔支撑系统的风力涡轮机和相关的施工方法公开(公告)号：US20120023859A1
公开(公告)日：2012-02-02
申请号：US13109519
申请日：2011-05-17
CPC分类号： E04H12/347 , F03D13/10 , F03D13/20 , F03D80/70 , F05B2240/913 , Y02E10/728
摘要： A wind turbine has a nacelle mounted atop a tower, with a support system configured around a base portion of the tower. The support system includes a plurality of support fins spaced radially around the base portion. Each of the support fins has a continuous header member secured to the tower and a continuous face member extending radially outward and downward from the header member towards ground. The support fins include a web extending between the header member and face member. The support fins extend from the tower with a length and at an acute extension angle relative to a longitudinal axis of the tower so as to provide vertical and lateral support around the circumference of the tower.
摘要翻译： 风力涡轮机具有安装在塔顶上的机舱，其中配置有围绕塔的基部的支撑系统。 支撑系统包括围绕基部径向地间隔开的多个支撑翅片。 每个支撑翅片具有固定到塔架的连续头部构件和从头部构件向地面径向向外和向下延伸的连续面构件。 支撑翅片包括在头部构件和面部构件之间延伸的腹板。 支撑翅片相对于塔的纵向轴线从塔架延伸一段长度和一个锐角，以便围绕塔架的圆周提供垂直和侧向支撑。
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公开(公告)号：US20110283507A1
公开(公告)日：2011-11-24
申请号：US12979741
申请日：2010-12-28
CPC分类号： E04H12/34 , E04H12/10 , E04H12/345 , F03D13/10 , F05B2240/9121 , Y02E10/728 , Y10T29/49826 , Y10T29/49895 , Y10T29/53974
摘要： An assembly system for use in assembling a lattice tower section is provided. The system comprises a platform, a first mounting assembly coupled to the platform, and, a second mounting assembly coupled to the platform, the first and second mounting assemblies are configured to secure opposite ends of a plurality of leg members used in assembling the lattice tower section such that each of the plurality of leg members is suspended a distance from the platform, at least one of the first and second mounting assemblies is configured to selectively rotate a leg member of the plurality of leg members suspended therefrom.
摘要翻译： 提供了用于组装格子塔段的组装系统。 该系统包括平台，联接到平台的第一安装组件和联接到平台的第二安装组件，第一和第二安装组件构造成固定用于组装格子塔的多个腿部构件的相对端 使得所述多个腿部构件中的每一个与所述平台悬挂一段距离，所述第一和第二安装组件中的至少一个构造成选择性地旋转从其悬挂的所述多个腿部构件的腿部构件。
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公开(公告)号：US08171614B2
公开(公告)日：2012-05-08
申请号：US12979741
申请日：2010-12-28
CPC分类号： E04H12/34 , E04H12/10 , E04H12/345 , F03D13/10 , F05B2240/9121 , Y02E10/728 , Y10T29/49826 , Y10T29/49895 , Y10T29/53974
摘要： An assembly system for use in assembling a lattice tower section is provided. The system comprises a platform, a first mounting assembly coupled to the platform, and, a second mounting assembly coupled to the platform, the first and second mounting assemblies are configured to secure opposite ends of a plurality of leg members used in assembling the lattice tower section such that each of the plurality of leg members is suspended a distance from the platform, at least one of the first and second mounting assemblies is configured to selectively rotate a leg member of the plurality of leg members suspended therefrom.
摘要翻译： 提供了用于组装格子塔段的组装系统。 该系统包括平台，联接到平台的第一安装组件和联接到平台的第二安装组件，第一和第二安装组件构造成固定用于组装格子塔的多个腿部构件的相对端 使得所述多个腿部构件中的每一个与所述平台悬挂一段距离，所述第一和第二安装组件中的至少一个构造成选择性地旋转从其悬挂的所述多个腿部构件的腿部构件。
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5.发明授权Apparatus and method for aerodynamic performance enhancement of a wind turbine 有权风力发电机的空气动力性能增强的装置和方法公开(公告)号：US09194363B2
公开(公告)日：2015-11-24
申请号：US13537520
申请日：2012-06-29
申请人： Dmytro Floriyovych Opaits , Seyed Gholamali Saddoughi , Grover Andrew Bennett, Jr. , Matthew Patrick Boespflug , Stephen Bertram Johnson , Peggy Lynn Baehmann , Anurag Gupta
发明人： Dmytro Floriyovych Opaits , Seyed Gholamali Saddoughi , Grover Andrew Bennett, Jr. , Matthew Patrick Boespflug , Stephen Bertram Johnson , Peggy Lynn Baehmann , Anurag Gupta
CPC分类号： F03D1/04 , F03D1/0608 , F05B2240/12 , F05B2240/33 , Y02E10/721 , Y10T29/49316
摘要： A deployable aerodynamic component configured to be mounted to a wind turbine. The wind turbine includes at least one rotor blade. The deployable aerodynamic component configured to be positioned in front of an inner portion of the at least one rotor blade, and is structurally configured to cover a substantial portion of the inner portion of the at least one rotor blade in a wind direction during deployment of the deployable aerodynamic component and to allow the passage therethrough of an incoming wind when non-deployed. Further described is a wind turbine including the above-described deployable aerodynamic component and method for aerodynamic performance enhancement of an existing wind turbine, wherein the method includes mounting the above-described deployable aerodynamic component to a wind turbine.
摘要翻译： 配置为安装到风力涡轮机的可部署的空气动力学部件。 风力涡轮机包括至少一个转子叶片。 所述可部署空气动力学部件被构造成定位在所述至少一个转子叶片的内部部分的前面，并且在结构上构造成在所述至少一个转子叶片的展开期间在风向方向上覆盖所述至少一个转子叶片的内部部分的大部分 可部署的空气动力学部件，并且当未部署时允许通过其中的风。 进一步描述了一种风力涡轮机，其包括上述可部署的空气动力学部件和用于现有风力涡轮机的空气动力学性能增强的方法，其中所述方法包括将上述可部署空气动力学部件安装到风力涡轮机。
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公开(公告)号：US08550957B2
公开(公告)日：2013-10-08
申请号：US13155417
申请日：2011-06-08
申请人： Daniel Jason Erno , Fulton Jose Lopez , Darren Lee Hallman , Erik Karl Jacobson , Robert Michael Zirin , Munishwar Ahuja , Stephen Bertram Johnson
发明人： Daniel Jason Erno , Fulton Jose Lopez , Darren Lee Hallman , Erik Karl Jacobson , Robert Michael Zirin , Munishwar Ahuja , Stephen Bertram Johnson
IPC分类号： F16H57/08
CPC分类号： F16H1/2836 , F16H57/082 , F16H2057/085
摘要： A planetary gear system and a method. The planetary gear system includes a carrier body configured to receive planet gears, at least one pin received by the carrier body, and flex means positioned between the carrier body and the at least one pin. The method includes preparing the carrier, upon which a plurality of planet gears is mounted through planet pins, and providing flex means between the planet pins and the carrier, the flex means configured to enable movement of the planet pins in response to a force directed thereon.
摘要翻译： 行星齿轮系统及方法。 行星齿轮系统包括承载体，其构造成接收行星齿轮，由承载体容纳的至少一个销和位于承载体与至少一个销之间的挠性装置。 该方法包括制备载体，多个行星齿轮通过行星销安装在该载体上，并且在行星销和载体之间提供弯曲装置，弹性装置构造成能够响应于其上的力而使行星销的移动 。
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7.发明申请公开(公告)号：US20140003940A1
公开(公告)日：2014-01-02
申请号：US13537520
申请日：2012-06-29
申请人： Dmytro Floriyovych Opaits , Seyed Gholamali Saddoughi , Grover Andrew Bennett, JR. , Matthew Patrick Boespflug , Stephen Bertram Johnson , Peggy Lynn Baehmann , Anurag Gupta
发明人： Dmytro Floriyovych Opaits , Seyed Gholamali Saddoughi , Grover Andrew Bennett, JR. , Matthew Patrick Boespflug , Stephen Bertram Johnson , Peggy Lynn Baehmann , Anurag Gupta
CPC分类号： F03D1/04 , F03D1/0608 , F05B2240/12 , F05B2240/33 , Y02E10/721 , Y10T29/49316
摘要： A deployable aerodynamic component configured to be mounted to a wind turbine. The wind turbine includes at least one rotor blade. The deployable aerodynamic component configured to be positioned in front of an inner portion of the at least one rotor blade, and is structurally configured to cover a substantial portion of the inner portion of the at least one rotor blade in a wind direction during deployment of the deployable aerodynamic component and to allow the passage therethrough of an incoming wind when non-deployed. Further described is a wind turbine including the above-described deployable aerodynamic component and method for aerodynamic performance enhancement of an existing wind turbine, wherein the method includes mounting the above-described deployable aerodynamic component to a wind turbine.
摘要翻译： 配置为安装到风力涡轮机的可部署的空气动力学部件。 风力涡轮机包括至少一个转子叶片。 所述可部署空气动力学部件被构造成定位在所述至少一个转子叶片的内部部分的前面，并且在结构上构造成在所述至少一个转子叶片的展开期间在风向方向上覆盖所述至少一个转子叶片的内部部分的大部分 可部署的空气动力学部件，并且当未部署时允许通过其中的风。 进一步描述了一种风力涡轮机，其包括上述可部署的空气动力学部件和用于现有风力涡轮机的空气动力学性能增强的方法，其中所述方法包括将上述可部署空气动力学部件安装到风力涡轮机。
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公开(公告)号：US08314529B2
公开(公告)日：2012-11-20
申请号：US12288605
申请日：2008-10-22
申请人： Kiruba Sivasubramaniam , Patrick Lee Jansen , Gary Randall Barnes , Jessica Mary Brower , Stephen Bertram Johnson
发明人： Kiruba Sivasubramaniam , Patrick Lee Jansen , Gary Randall Barnes , Jessica Mary Brower , Stephen Bertram Johnson
CPC分类号： H02K3/18 , H02K7/1823 , H02K7/183 , H02K7/1838 , Y02E10/725 , Y10T29/49009
摘要： A technique for winding multi-turn, stranded wire coils using rectangular cables avoids the risk of damage associated with edge-wise bends.
摘要翻译： 使用矩形电缆卷绕多匝绞合线圈的技术避免了与边缘弯曲相关的损坏风险。
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公开(公告)号：US20100096944A1
公开(公告)日：2010-04-22
申请号：US12288605
申请日：2008-10-22
申请人： Kiruba Sivasubramaniam , Patrick Lee Jansen , Gary Randall Barnes , Jessica Mary Brower , Stephen Bertram Johnson
发明人： Kiruba Sivasubramaniam , Patrick Lee Jansen , Gary Randall Barnes , Jessica Mary Brower , Stephen Bertram Johnson
CPC分类号： H02K3/18 , H02K7/1823 , H02K7/183 , H02K7/1838 , Y02E10/725 , Y10T29/49009
摘要： A technique for winding multi-turn, stranded wire coils using rectangular cables avoids the risk of damage associated with edge-wise bends.
摘要翻译： 使用矩形电缆卷绕多匝绞合线圈的技术避免了与边缘弯曲相关的损坏风险。
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10.发明授权公开(公告)号：US08869940B2
公开(公告)日：2014-10-28
申请号：US13351471
申请日：2012-01-17
IPC分类号： F03D11/00
CPC分类号： F16N7/40 , F03D15/00 , F03D15/10 , F03D80/60 , F03D80/70 , F16N39/04 , F16N2250/08 , F16N2270/20 , Y02E10/726
摘要： A system and method are provided for supplying oil at different temperatures to different locations within a wind turbine gearbox, wherein oil is pumped from a common oil sump to the different locations via a common header. The different gear box locations are divided into at least two groups, wherein each of said groups receives inlet oil at a respective inlet oil temperature. A first temperature control device is disposed between the common header and the first group, and a second temperature control device is disposed between the common header and the second group of gearbox locations.
摘要翻译： 提供了一种用于将不同温度的油供应到风力涡轮机齿轮箱内的不同位置的系统和方法，其中油通过公共集管从普通油底壳泵送到不同位置。 不同的齿轮箱位置被分成至少两组，其中每个所述组在相应的入口油温度下接收入口油。 第一温度控制装置设置在公共集管和第一组之间，第二温度控制装置设置在公共集管和第二组变速箱位置之间。
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