利索-全球专利检索

  1. 登录
  2. 注册

搜索结果

168 条记录 (耗时 0.028 秒)

    Notch-reduced composite joint
    2.
    发明授权
    Notch-reduced composite joint 有权
    凹口复合接头

    公开(公告)号：US09366223B2

    公开(公告)日：2016-06-14

    申请号：US13808603

    申请日：2011-07-08

    申请人： Lars Nielsen

    发明人： Lars Nielsen

    IPC分类号： F03D1/06

    CPC分类号： F03D1/06 ,  F03D1/0675 ,  F05B2280/6003 ,  F05C2253/04 ,  Y02E10/721

    摘要： A wind turbine blade comprising a profiled hollow contour, at least one reinforcing beam (15) placed between two shell body parts (13, 14), the beam comprising a first beam flange (16a) and an opposing second beam flange (16b), a beam body (17) connected to the first beam flange (16a) by a first transition area (32a) and connected to the second beam flange (16b) by a second transition area (32b). The beam body comprises a beam core (22). The beam core (22) comprises a first outer core surface (24a) and an opposite second outer core surface (24b). The beam body further comprises a web (50) arranged on the outer core surfaces. The flanges (16a, 16b) and the web (50) are made from a fiber-reinforced polymer. The transition areas (32a, 32b) comprise notch-reducing mean formed of rounded corners of the beam core (22).

    摘要翻译： 一种风轮机叶片，其包括异形中空轮廓，至少一个放置在两个壳体部分（13,14）之间的加强梁（15），所述梁包括第一梁凸缘（16a）和相对的第二梁凸缘（16b） 梁主体（17），其通过第一过渡区域（32a）连接到第一梁凸缘（16a）并且通过第二过渡区域（32b）连接到第二梁凸缘（16b）。 梁主体包括梁芯（22）。 梁芯（22）包括第一外芯表面（24a）和相对的第二外芯表面（24b）。 梁主体还包括布置在外芯表面上的腹板（50）。 凸缘（16a，16b）和腹板（50）由纤维增强聚合物制成。 过渡区域（32a，32b）包括由梁芯（22）的圆角形成的切口减小装置。

    Wind turbine blade with base part having non-positive camber
    3.
    发明授权
    Wind turbine blade with base part having non-positive camber 有权
    风力涡轮机叶片，基部具有非正外倾角

    公开(公告)号：US09057359B2

    公开(公告)日：2015-06-16

    申请号：US13320923

    申请日：2010-05-18

    申请人： Peter Fuglsang ,  Stefano Bove ,  Lars Fuglsang

    发明人： Peter Fuglsang ,  Stefano Bove ,  Lars Fuglsang

    IPC分类号： F03D1/06

    CPC分类号： F03D1/0641 ,  F03D1/0675 ,  F05B2240/301 ,  F05B2240/32 ,  Y02E10/721

    摘要： A blade, for a rotor of a wind turbine has a profiled contour in a radial direction is divided into a root region with a substantially circular or elliptical profile closest to the hub and an airfoil region with a lift generating profile furthest away from the hub. A transition region between the root region and the airfoil region has a profile gradually changing in the radial direction from the circular or elliptical profile of the root region to the lift generating profile of the airfoil region, and the airfoil region comprises at least a first longitudinal segment extending at least 20% of a longitudinal extent of the airfoil region. The first longitudinal segment has a first base part with a cross-sectional profile such that, when impacted by an incident airflow at an angle of attack of 0 degrees has a lift coefficient, which is 0 or less.

    摘要翻译： 用于风力涡轮机的转子的叶片具有沿径向方向的轮廓轮廓，被划分成具有最靠近轮毂的大致圆形或椭圆形轮廓的根部区域以及具有离轮毂最远的升力产生轮廓的翼型区域。 根部区域和翼型区域之间的过渡区域具有在径向方向上从根部区域的圆形或椭圆形轮廓到翼型区域的升力产生轮廓的轮廓，并且翼型区域包括至少第一纵向 段延伸至翼型区域的纵向范围的至少20％。 第一纵向段具有第一基部，其具有横截面轮廓，使得当以0度的入射角受到入射气流的冲击时，升力系数为0或更小。

    Method of manufacturing an elongated composite structure
    4.
    发明授权
    Method of manufacturing an elongated composite structure 有权
    制造细长复合结构的方法

    公开(公告)号：US09050786B2

    公开(公告)日：2015-06-09

    申请号：US13813581

    申请日：2011-07-20

    申请人： Martin Fredskild ,  Bjarne Krab Mortensen ,  Martin Dahl

    发明人： Martin Fredskild ,  Bjarne Krab Mortensen ,  Martin Dahl

    IPC分类号： B29C70/36 ,  B32B37/14 ,  B29C70/48 ,  B29D99/00 ,  B29L31/08

    CPC分类号： B32B37/14 ,  B29C70/48 ,  B29D99/0028 ,  B29K2101/10 ,  B29L2031/085 ,  Y02P70/523

    摘要： A method of manufacturing an elongated composite structure having two separate longitudinal composite structure sections, where said method comprises the following steps: providing a rigid mold part 13 having a first forming surface 14 with a contour defining an outer surface of the elongated composite structure, arranging a first fiber lay-up 15 in a first longitudinal section 16 of the first mold part 13, arranging a first flexible foil 18 over a first crosswise edge area 17 of the first fiber lay-up 15, arranging a second fiber lay-up 20 in a second longitudinal section 21 of the mold part 13 so as to overlap the crosswise edge area 17 of the first lay-up 15 and thereby the first flexible foil 18 in an overlap area 22 forming an interface between the fiber lay-ups 15,20, providing polymer to the fiber lay-ups 15,20 and allowing the polymer to cure.

    摘要翻译： 一种制造具有两个单独的纵向复合结构部分的细长复合结构的方法，其中所述方法包括以下步骤：提供具有第一成形表面14的刚性模具部分13，其具有限定细长复合结构的外表面的轮廓， 在第一模具部件13的第一纵向部分16中的第一纤维层叠体15，将第一柔性箔片18布置在第一纤维层叠体15的第一横向边缘区域17上，布置第二纤维层叠体20 在模具部件13的第二纵向部分21中，与第一叠层15的横向边缘区域17重叠，从而在形成纤维叠层15,15之间的界面的重叠区域22中形成第一柔性箔片18。 20，向纤维叠层15,20提供聚合物并使聚合物固化。

    Modular mould system for manufacturing a shell part
    5.
    发明授权
    Modular mould system for manufacturing a shell part 有权
    用于制造壳体部件的模块化模具系统

    公开(公告)号：US08951034B2

    公开(公告)日：2015-02-10

    申请号：US13503141

    申请日：2010-10-18

    申请人： Per Kjaer Christiansen ,  Finn Johansen

    发明人： Per Kjaer Christiansen ,  Finn Johansen

    IPC分类号： B29C33/30 ,  B64C27/46 ,  B29C33/38 ,  B29C33/00 ,  B29L31/08

    CPC分类号： B29C33/306 ,  B29C33/005 ,  B29C33/302 ,  B29C33/305 ,  B29C33/3842 ,  B29L2031/082 ,  B29L2031/085 ,  Y02P70/523

    摘要： A modular mold system for manufacturing a shell part of an oblong composite structure having a longitudinal direction from a fiber reinforced matrix material. The modular mould system includes a number of mold sections, which are adapted to being assembled to an assembled mold part. The number of mold sections includes a first mold section having a first molding surface with a contour that defines a surface of a first longitudinal part of the shell part and a first end section; and a second mold section having a second molding surface with a contour that defines a surface of a second longitudinal part of the shell part and a second end section; which, when the modular mold system is assembled to the assembled mold, the second end section of the second mold section abuts the first end section of the first mold section.

    摘要翻译： 一种用于制造长方形复合结构的外壳部分的模块化模具系统，其具有来自纤维增强基体材料的纵向方向。 模块化模具系统包括多个模具部分，其适于组装成组装的模具部件。 模具部分的数量包括第一模具部分，该第一模具部分具有限定壳体部分的第一纵向部分的表面的轮廓的第一模制表面和第一端部部分; 以及第二模具部分，其具有限定所述壳部分的第二纵向部分的表面和第二端部部分的轮廓的第二模制表面; 当模块化模具系统组装到组装的模具时，第二模具部分的第二端部部分邻接第一模具部分的第一端部部分。

    Wind turbine blade with base part having inherent non-ideal twist
    6.
    发明授权
    Wind turbine blade with base part having inherent non-ideal twist 有权
    风力涡轮机叶片，其基部具有固有的非理想扭转

    公开(公告)号：US08899922B2

    公开(公告)日：2014-12-02

    申请号：US13320977

    申请日：2010-05-18

    申请人： Peter Fuglsang ,  Stefano Bove ,  Lars Fuglsang

    发明人： Peter Fuglsang ,  Stefano Bove ,  Lars Fuglsang

    IPC分类号： F03D11/00 ,  F03D1/06

    CPC分类号： F03D1/0641 ,  F03D1/0675 ,  F05B2240/301 ,  F05B2240/32 ,  Y02E10/721

    摘要： A blade for a rotor of a wind turbine is divided into a root region closest to the hub and an airfoil region with a lift generating profile furthest away from the hub. A transition region has a profile gradually changing in the radial direction from the circular or elliptical profile of the root region to the lift generating profile of the airfoil region, and includes at least a first longitudinal segment extending along at least 20% of a longitudinal extent of the airfoil region. A base part has an inherent non-ideal twist, such as no twist, or a reduced twist compared to a target blade twist, so that an axial induction factor of the first base part at a design point deviates from a target axial induction factor. A number of flow altering devices are arranged so as to adjust the aerodynamic properties of the first longitudinal segment.

    摘要翻译： 用于风力涡轮机的转子的叶片被分成最靠近轮毂的根部区域和具有离轮毂最远的升力产生轮廓的翼型区域。 过渡区域具有在径向方向上从根部区域的圆形或椭圆形轮廓到翼型区域的升力产生轮廓的纵向变化的轮廓，并且包括至少沿纵向延伸的至少20％延伸的第一纵向段 的翼型区域。 与目标叶片扭转相比，基部具有固有的非理想扭转，例如无扭转或减小的扭转，使得设计点处的第一基部的轴向感应系数偏离目标轴向感应系数。 布置多个流动改变装置以调节第一纵向段的空气动力特性。

    Wind turbine blade with variable trailing edge
    8.
    发明授权
    Wind turbine blade with variable trailing edge 有权
    具有可变后缘的风力涡轮机叶片

    公开(公告)号：US08794919B2

    公开(公告)日：2014-08-05

    申请号：US13175414

    申请日：2011-07-01

    申请人： Peter Baek ,  Peter Grabau

    发明人： Peter Baek ,  Peter Grabau

    IPC分类号： F03B3/14

    CPC分类号： F03D1/0641 ,  F03D1/0675 ,  F03D7/0232 ,  F05B2240/31 ,  F05B2240/311 ,  F05B2270/32 ,  F05B2270/331 ,  Y02E10/721 ,  Y02E10/723

    摘要： The present invention relates to a wind turbine blade for a rotor of a wind turbine having a substantially horizontal rotor shaft. The blade may comprise a profiled contour comprising a pressure side and a suction side as well as a leading edge and a trailing edge, a chord extending between the leading edge and the trailing edge, and the profiled contour generating a lift when being impacted by an incident airflow. In a cross section of the wind turbine blade perpendicular to a lengthwise direction of the wind turbine blade, a suction side point is defined on the suction side at the trailing edge of the blade, and a pressure side point is defined on the pressure side at the trailing edge of the blade. The suction side point is movable in relation to the pressure side point, and the blade is further provided with a displacement device configured to displace the pressure side point and the suction side point so that a distance between the suction side point and the pressure side point can be varied. The present invention further relates to a wind turbine including such a wind turbine blade and to a method of operating a wind turbine including such a wind turbine blade.

    摘要翻译： 本发明涉及一种用于风力涡轮机转子的风力涡轮机叶片，其具有基本上水平的转子轴。 叶片可以包括异形轮廓，其轮廓包括压力侧和吸力侧以及前缘和后缘，在前缘和后缘之间延伸的弦，并且轮廓轮廓在受到一个 事件气流。 在垂直于风力涡轮机叶片的长度方向的风力涡轮机叶片的横截面中，在叶片的后缘处的吸力侧上限定吸入侧点，并且压力侧点被限定在压力侧 叶片的后缘。 吸入侧点可以相对于压力侧点移动，并且叶片还设置有移动装置，其构造成使压力侧点和吸入侧点移位，使得吸入侧点与压力侧点之间的距离 可以变化。 本发明还涉及包括这种风力涡轮机叶片的风力涡轮机和涉及包括这种风力涡轮机叶片的风力涡轮机的方法。

    Wind turbine blade and blade element combination and method of changing the aerodynamic profile of a wind turbine blade
    9.
    发明授权
    Wind turbine blade and blade element combination and method of changing the aerodynamic profile of a wind turbine blade 有权
    风力涡轮机叶片和叶片元件组合以及改变风力涡轮机叶片的空气动力学特性的方法

    公开(公告)号：US08550777B2

    公开(公告)日：2013-10-08

    申请号：US12733398

    申请日：2008-08-29

    申请人： Casper Kildegaard

    发明人： Casper Kildegaard

    IPC分类号： F03D1/02

    CPC分类号： F03D1/0675 ,  F03D1/065 ,  F05B2240/301 ,  F05B2250/70 ,  Y02E10/721

    摘要： A blade element (42; 44; 46; 48; 150; 250; 350) for mounting on a wind turbine blade (10) is provided. The blade (10) has a longitudinal direction (L) and a chord extending transversely to the longitudinal direction between a leading edge (18) and a trailing edge (20). The blade (10) has an airfoil profile with a thickness between a suction side and a pressure side along at least a part of the longitudinal direction (L) and with a position of maximum thickness between the leading edge (18) and the trailing edge (20). The blade element (10) has a shape so that, by mounting in a first longitudinal part of the wind turbine blade (10), it changes the profile of the first longitudinal part from a first airfoil profile (100; 200; 300) with an essentially pointed trailing edge (100; 200; 300) and a first chord length (c11; c21; c31) to a changed airfoil profile with a blunt trailing edge (153; 253; 353). The changed airfoil profile is a truncated profile of an imaginary airfoil profile (160; 260; 360) with an essentially pointed trailing edge and a second chord length (c12; c22; c32), which is larger than the first chord length (c11; c21; c31).

    摘要翻译： 提供了用于安装在风力涡轮机叶片（10）上的叶片元件（42; 44; 46; 48; 150; 250; 350）。 刀片（10）具有纵向方向（L）和在前缘（18）和后缘（20）之间横向于纵向延伸的弦线。 叶片（10）具有沿着纵向方向（L）的至少一部分具有在吸力侧和压力侧之间的厚度的翼型轮廓，并且在前缘（18）和后缘（18）之间具有最大厚度的位置 （20）。 叶片元件（10）具有这样的形状，使得通过安装在风力涡轮机叶片（10）的第一纵向部分中，它使第一纵向部分的轮廓从第一翼型轮廓（100; 200; 300）与第 基本上尖的后缘（100; 200; 300）和第一和弦长度（c11; c21; c31）到具有钝的后缘（153; 253; 353）的改变的翼型轮廓。 改变的翼型轮廓是具有基本上尖的后缘和第二弦长（c12; c22; c32）的假想翼型轮廓（160; 260; 360）的截头轮廓，其大于第一弦长（c11; c21; c31）。

    Wind turbine blade and hub assembly
    10.
    发明授权
    Wind turbine blade and hub assembly 有权
    风力发电机叶片和轮毂总成

    公开(公告)号：US08545182B2

    公开(公告)日：2013-10-01

    申请号：US12812625

    申请日：2009-01-13

    申请人： Tommy Sørensen

    发明人： Tommy Sørensen

    IPC分类号： B64C11/06

    CPC分类号： F03D1/0658 ,  F05B2260/301 ,  F16C19/18 ,  F16C35/06 ,  F16C2300/14 ,  Y02E10/721 ,  Y02E10/722

    摘要： This invention relates to a wind turbine blade with at least two connection members such as bushings and/or threaded bars in the root of the blade for attaching the blade to a hub. The connection members are placed along the blade surface and at least some of the connection members are non-parallel and hence oriented in different directions. Hereby is obtained that the root section of the blade can be shortened and the maximum chord of the wind turbine blade can be moved closer to the hub, whereby the part of the blade exploiting the wind is increased and the power output similarly increased.The present invention further relates to a pitch bearing and a hub comprising a bearing ring with two or more holes for positioning fastening members for attaching a wind turbine blade to the bearing. Here, correspondingly, at least two of the holes are oriented in different angles so that the fastening members positioned in the holes are non-parallel and extend in different directions.

    摘要翻译： 本发明涉及一种风力涡轮机叶片，其具有至少两个连接构件，例如在叶片的根部中的衬套和/或螺纹杆，用于将叶片附接到轮毂。 连接构件沿着叶片表面放置，并且至少一些连接构件是不平行的并且因此在不同方向上定向。 由此，可以缩短叶片的根部，并且可以使风力涡轮机叶片的最大弦弦更靠近轮毂移动，从而增加叶片利用风的部分，同时增加功率输出。 本发明还涉及一种变桨轴承和轮毂，其包括具有两个或更多个孔的轴承环，用于定位用于将风力涡轮机叶片附接到轴承的紧固构件。 这里，相应地，至少两个孔以不同的角度定向，使得定位在孔中的紧固构件不平行并且在不同方向上延伸。