公开(公告)号：US07632068B2

公开(公告)日：2009-12-15

申请号：US10551406

申请日：2004-03-31

Applicant: Dan Christian Bak ,  Thomas Buhl ,  Peter Fuglsang ,  Helge Aagaard Madsen ,  Flemming Rasmussen

Inventor： Dan Christian Bak ,  Thomas Buhl ,  Peter Fuglsang ,  Helge Aagaard Madsen ,  Flemming Rasmussen

IPC: F03B3/14

CPC classification number: F03D7/0232 ,  F03D1/0641 ,  F05B2240/31 ,  F05B2240/311 ,  F05B2260/70 ,  F05B2260/76 ,  F05B2280/5006 ,  Y02E10/721 ,  Y02E10/723

Abstract: The present invention relates to a design concept by which the power, loads and/or stability of a wind turbine may be controlled by typically fast variation of the geometry of the blades using active geometry control (e.g. smart materials or by embedded mechanical actuators), or using passive geometry control (e.g. changes arising from loading and/or deformation of the blade) or by a combination of the two methods. The invention relates in particular to a wind turbine blade, a wind turbine and a method of controlling a wind turbine.

Abstract translation: 本发明涉及一种设计概念，通过该设计概念，风力涡轮机的功率，负载和/或稳定性可以通过使用主动几何控制（例如智能材料或嵌入式机械致动器）的叶片的几何形状的典型快速变化来控制， 或使用被动几何控制（例如由叶片的加载和/或变形引起的变化）或两种方法的组合。 本发明具体涉及风力涡轮机叶片，风力涡轮机和控制风力涡轮机的方法。

公开(公告)号：US20090290982A1

公开(公告)日：2009-11-26

申请号：US12307474

申请日：2007-07-06

Applicant: Helge Aagaard Madsen ,  Flemming Rasmussen ,  Thomas Buhl ,  Morten Hartvig Hansen ,  Dan Christian Bak ,  Mac Gaunaa ,  Peter Bjørn Andersen

Inventor： Helge Aagaard Madsen ,  Flemming Rasmussen ,  Thomas Buhl ,  Morten Hartvig Hansen ,  Dan Christian Bak ,  Mac Gaunaa ,  Peter Bjørn Andersen

IPC: F03D1/06 ,  B29C47/00

CPC classification number: F03D1/0633 ,  F03D1/0675 ,  F03D7/0232 ,  F05B2230/24 ,  F05B2240/31 ,  F05B2240/311 ,  F05B2280/4003 ,  F05B2280/4004 ,  F05B2280/6003 ,  F05B2280/6013 ,  F05B2280/702 ,  F05C2225/00 ,  F05C2225/02 ,  F05C2253/04 ,  F05C2253/16 ,  F05C2253/22 ,  Y02E10/721 ,  Y02E10/723 ,  Y02P70/523

Abstract: A deformable trailing edge section (3) of a wind turbine blade (1), at least part of said section (3) being formed in a deformable material. The blade section (3) comprises one or more cavities (5) being in connection with or connectable to a fluid source in a way that allows fluid to stream from the fluid source to the cavity or cavities (5), so that the shape of the deformable trailing edge section (3) and thereby the camber of the blade cross-section (3) is changeable by the pressure of fluid in the cavity or cavities (5) with insignificant changes of the thickness and chord wise length of the deformable trailing edge section. Furthermore a wind turbine blade (1) is described, having at least one of such trailing edge section (s) (3) and to a system (11) for mounting a blade section (3) on a main blade (2) of a wind turbine. In addition a method of manufacturing a deformable trailing edge section (3) of a wind turbine blade (1) is disclosed.

Abstract translation: 风力涡轮机叶片（1）的可变形的后缘部分（3），所述部分（3）的至少一部分形成为可变形材料。 叶片部分（3）包括一个或多个空腔（5），其以允许流体从流体源流到空腔（5）的方式与流体源连接或连接，使得形状 可变形的后缘部分（3）以及由此的叶片横截面（3）的外倾可以通过空腔或空腔（5）中的流体的压力而变化，其中可变形拖尾的厚度和弦的长度没有显着的变化 边缘部分。 此外，描述了风力涡轮机叶片（1），其具有这种后缘部分（3）中的至少一个和用于将叶片部分（3）安装在主叶片（2）上的系统（11） 风力发电机。 另外，公开了制造风力涡轮机叶片（1）的可变形后缘部分（3）的方法。

公开(公告)号：US06672837B1

公开(公告)日：2004-01-06

申请号：US09701493

申请日：2001-06-13

Applicant: Herman F. Veldkamp ,  Lars Risager ,  Flemming Rasmussen

Inventor： Herman F. Veldkamp ,  Lars Risager ,  Flemming Rasmussen

IPC: F04D2900

CPC classification number: F16F7/10 ,  F03D80/00 ,  F05B2210/14 ,  F05B2240/14 ,  F05B2240/912 ,  F05B2260/96 ,  F05B2260/964 ,  Y02E10/726 ,  Y02E10/728 ,  Y10S416/50

Abstract: The present invention relates to a wind turbine with oscillation damping means provided at the nacelle and being designed for damping edgewise oscillations of the rotor blades in the rotational plane of the rotor. In particular, the invention relates to a wind turbine in which the oscillation damping means are provided at the end of the nacelle being opposite to the end from which the rotor extends and are designed for damping oscillations of the first eigenfrequency of the rotor blades in the rotational plane, especially oscillations being perpendicular to the rotational axis of the rotor. The damping means are advantageously designed to dampen oscillations of a frequency being substantially equal to the first eigenfrequency in the rotational plane of the at least one blade minus the frequency of rotation of the rotor. The oscillation damping means of the present invention are preferably capable of damping oscillations being substantially horizontal and substantially perpendicular to the rotation axis.

Abstract translation: 本发明涉及一种风力涡轮机，其具有设置在机舱处的振动阻尼装置，并被设计成用于在转子的旋转平面中阻尼转子叶片的沿边振荡。 特别地，本发明涉及一种风力涡轮机，其中振动阻尼装置设置在机舱的端部处，其与转子延伸的端部相对，并且被设计成用于阻尼转子叶片的第一本征频率的振荡 旋转平面，特别是垂直于转子旋转轴线的振荡。 阻尼装置有利地被设计成抑制基本上等于至少一个叶片的旋转平面中的第一本征频率的频率的振荡减去转子的旋转频率的振荡。 本发明的振动阻尼装置优选能够阻尼基本上水平并基本上垂直于旋转轴线的振荡。

公开(公告)号：US06514043B1

公开(公告)日：2003-02-04

申请号：US09701731

申请日：2001-03-05

Applicant: Flemming Rasmussen ,  Per Vølund ,  Jørgen Thirstrup Petersen ,  Bjørn Johansen ,  Preben Ellebæk

Inventor： Flemming Rasmussen ,  Per Vølund ,  Jørgen Thirstrup Petersen ,  Bjørn Johansen ,  Preben Ellebæk

IPC: B63H106

CPC classification number: F03D7/0224 ,  B64C27/32 ,  F03D1/0658 ,  F05B2260/77 ,  Y02E10/721 ,  Y02E10/723

Abstract: The present invention relates to a hub assembly of a rotor for holding at least one wing, wherein the at least one wing is connected/mounted to the hub assembly in at least two suspension points. The hub assembly may be applied to any kind of either energy extracting devices such as wind turbines or the like or lift producing devices such as helicopter rotors or propellers. The invention is suited for rotors in general and is able to enable coning movement of wings connected/mounted to the hub assembly, enable teetering movement of the rotor and enable alteration of the pitch angle of the wings connected/mounted to the hub assembly. The hub assembly according to the present invention provides a hub where the pitching of the wings can occur synchronously/simultaneously due to an interconnection of the wings attached/mounted to the hub assembly and where coning of the wings may be applied at the same time with pitching of the wings and teetering of the rotor.

Abstract translation: 本发明涉及一种用于保持至少一个翼的转子的轮毂组件，其中至少一个翼在至少两个悬挂点处连接/安装到轮毂组件。 轮毂组件可以应用于任何一种能量提取装置，例如风力涡轮机等，或提升产生装置，例如直升机转子或螺旋桨。 本发明通常适用于转子，并且能够使连接/安装到轮毂组件的翼的锥形运动能够使得转子的跷跷板运动能够改变连接/安装到轮毂组件的翼的桨距角。 根据本发明的轮毂组件提供了一种毂，其中翼的俯仰可以同时/同时地发生，这是由于连接/安装到轮毂组件的翼的互连，并且翼的同时可以同时施加翼 俯仰翼子和转子的跷跷板。

公开(公告)号：US08419363B2

公开(公告)日：2013-04-16

申请号：US12307474

申请日：2007-07-06

Applicant: Helge Aagaard Madsen ,  Flemming Rasmussen ,  Thomas Buhl ,  Morten Hartvig Hansen ,  Dan Christian Bak ,  Mac Gaunaa ,  Peter Bjørn Andersen

Inventor： Helge Aagaard Madsen ,  Flemming Rasmussen ,  Thomas Buhl ,  Morten Hartvig Hansen ,  Dan Christian Bak ,  Mac Gaunaa ,  Peter Bjørn Andersen

IPC: B64C9/00

CPC classification number: F03D1/0633 ,  F03D1/0675 ,  F03D7/0232 ,  F05B2230/24 ,  F05B2240/31 ,  F05B2240/311 ,  F05B2280/4003 ,  F05B2280/4004 ,  F05B2280/6003 ,  F05B2280/6013 ,  F05B2280/702 ,  F05C2225/00 ,  F05C2225/02 ,  F05C2253/04 ,  F05C2253/16 ,  F05C2253/22 ,  Y02E10/721 ,  Y02E10/723 ,  Y02P70/523

Abstract: A deformable trailing edge section (3) of a wind turbine blade (1), at least part of said section (3) being formed in a deformable material. The blade section (3) comprises one or more cavities (5) being in connection with or connectable to a fluid source in a way that allows fluid to stream from the fluid source to the cavity or cavities (5), so that the shape of the deformable trailing edge section (3) and thereby the camber of the blade cross-section (3) is changeable by the pressure of fluid in the cavity or cavities (5) with insignificant changes of the thickness and chord wise length of the deformable trailing edge section. Furthermore a wind turbine blade (1) is described, having at least one of such trailing edge section (s) (3) and to a system (11) for mounting a blade section (3) on a main blade (2) of a wind turbine. In addition a method of manufacturing a deformable trailing edge section (3) of a wind turbine blade (1) is disclosed.

Abstract translation: 风力涡轮机叶片（1）的可变形的后缘部分（3），所述部分（3）的至少一部分形成为可变形材料。 叶片部分（3）包括一个或多个空腔（5），其以允许流体从流体源流向空腔（5）的方式与流体源连接或连接，使得形状 可变形的后缘部分（3）以及由此的叶片横截面（3）的外倾可以通过空腔或空腔（5）中的流体的压力而变化，其中可变形拖尾的厚度和弦的长度没有显着的变化 边缘部分。 此外，描述了风力涡轮机叶片（1），其具有这种后缘部分（3）中的至少一个和用于将叶片部分（3）安装在主叶片（2）上的系统（11） 风力发电机。 另外，公开了制造风力涡轮机叶片（1）的可变形后缘部分（3）的方法。

公开(公告)号：US20070036653A1

公开(公告)日：2007-02-15

申请号：US10551406

申请日：2004-03-31

Applicant: Dan Bak ,  Thomas Buhl ,  Peter Fuglsang ,  Helge Madsen ,  Flemming Rasmussen

Inventor： Dan Bak ,  Thomas Buhl ,  Peter Fuglsang ,  Helge Madsen ,  Flemming Rasmussen

IPC: B64C27/54

CPC classification number: F03D7/0232 ,  F03D1/0641 ,  F05B2240/31 ,  F05B2240/311 ,  F05B2260/70 ,  F05B2260/76 ,  F05B2280/5006 ,  Y02E10/721 ,  Y02E10/723

Abstract: The present invention relates to a design concept by which the power, loads and/or stability of a wind turbine may be controlled by typically fast variation of the geometry of the blades using active geometry control (e.g. smart materials or by embedded mechanical actuators), or using passive geometry control (e.g. changes arising from loading and/or deformation of the blade) or by a combination of the two methods. The invention relates in particular to a wind turbine blade, a wind turbine and a method of controlling a wind turbine.

Abstract translation: 本发明涉及一种设计概念，通过该设计概念，风力涡轮机的功率，负载和/或稳定性可以通过使用主动几何控制（例如智能材料或嵌入式机械致动器）的叶片的几何形状的典型快速变化来控制， 或使用被动几何控制（例如由叶片的加载和/或变形引起的变化）或两种方法的组合。 本发明具体涉及风力涡轮机叶片，风力涡轮机和控制风力涡轮机的方法。