公开(公告)号：US20160237986A1

公开(公告)日：2016-08-18

申请号：US15141252

申请日：2016-04-28

Applicant: Vestas Wind Systems A/S

Inventor： Mazyar Abolfazlian ,  Morten Mogensen

IPC: F03D1/00 ,  B66C23/20 ,  F03D80/80 ,  F03D9/00 ,  F03D80/60

CPC classification number: F03D9/25 ,  B66C23/207 ,  F01D25/12 ,  F03D13/20 ,  F03D80/00 ,  F03D80/50 ,  F03D80/60 ,  F03D80/80 ,  F03D80/88 ,  F05B2240/14 ,  F05B2240/916 ,  F05B2260/20 ,  F05B2260/201 ,  Y02B10/30 ,  Y02E10/726 ,  Y02E10/728 ,  Y02T50/675

Abstract: A wind turbine for generating electrical energy may include a tower, a nacelle at the top of the tower, and a rotor coupled to a generator within the nacelle. The wind turbine further includes a cooler including a spoiler and at least one cooler panel projecting above a roof of the nacelle. A heliplatform includes a support structure extending from the nacelle and at least partially integrated with the cooler. The wind turbine may also include a crane coupled to the nacelle and configured to move between a first stowed position underneath the nacelle roof and a second operational position. In the operational position, the crane is selectively positionable over the heliplatform. A method of using the wind turbine and crane is also disclosed.

公开(公告)号：US09255479B2

公开(公告)日：2016-02-09

申请号：US13705573

申请日：2012-12-05

Applicant: ALSTOM Technology Ltd.

Inventor： Ernst Pauli ,  Sergey Shchukin ,  Daniel Seng

IPC: F04D29/58 ,  F01D5/08 ,  F04D29/053 ,  F04D29/32

CPC classification number: F01D5/08 ,  F01D5/082 ,  F04D29/053 ,  F04D29/321 ,  F04D29/584 ,  F05B2260/201 ,  F05B2260/2241 ,  F05D2260/201 ,  F05D2260/22141

Abstract: A high-pressure compressor (12), in particular in a gas turbine (10), has a compressor rotor (17) which is surrounded by a stator (18, 19) thereby forming a main flow channel (25) and which is delimited at the compressor outlet by an end face (30) substantially extending in the radial direction, along which end face cooling air (21) is conveyed in the radial direction for the purpose of cooling. A prolonged service life is achieved in that the end face (30) is provided with a first system (23, 24) for improving the heat transfer between the cooling air (21) and the end face (30).

Abstract translation: 特别是在燃气轮机（10）中的高压压缩机（12）具有由定子（18,19）围绕的压缩机转子（17），从而形成主流道（25）并被界定 在压缩机出口处，通过沿径向方向大致延伸的端面（30），为了冷却目的沿其沿径向方向输送端面冷却空气（21）。 实现了延长的使用寿命，其中端面（30）设置有用于改善冷却空气（21）和端面（30）之间的热传递的第一系统（23,24）。

公开(公告)号：US20150308408A1

公开(公告)日：2015-10-29

申请号：US14643069

申请日：2015-03-10

Applicant: SIEMENS AKTIENGESELLSCHAFT

Inventor： UFFE ERIKSEN ,  STEFFEN LORENTZEN ,  THORKIL MUNK-HANSEN ,  CLAUS THYGESEN

IPC: F03D7/02 ,  F03D11/00

CPC classification number: F03D7/0296 ,  F03D80/60 ,  F05B2240/14 ,  F05B2260/201 ,  F05B2260/964 ,  Y02E10/72

Abstract: An apparatus for dampening of acoustic noise generated by air-cooling of at least one wind turbine component provided with the nacelle of a wind turbine is provided. Apparatus for dampening of acoustic noise generated by air-cooling of at least one wind turbine component provided with the nacelle of a wind turbine, comprising at least one acoustic dampening means, with the acoustic dampening means including at least one acoustic dampening channel structure having at least one acoustic dampening channel connected with at least one inlet opening of the acoustic dampening channel structure and at least one outlet opening of the acoustic dampening channel structure.

Abstract translation: 提供一种用于抑制由设置有风力涡轮机的机舱的至少一个风力涡轮机部件的空气冷却产生的声学噪声的装置。 用于衰减由设置有风力涡轮机的机舱的至少一个风力涡轮机部件的空气冷却产生的声学噪声的装置，包括至少一个声学阻尼装置，所述声学阻尼装置包括至少一个声学阻尼通道结构， 至少一个与所述声学阻尼通道结构的至少一个入口连接的声学阻尼通道和所述声学阻尼通道结构的至少一个出口。

公开(公告)号：US08546972B2

公开(公告)日：2013-10-01

申请号：US13384239

申请日：2009-09-17

Applicant: Yunhe Deng

Inventor： Yunhe Deng

IPC: F03D9/00 ,  H02P9/04

CPC classification number: H02K19/38 ,  F03D3/005 ,  F03D3/02 ,  F03D3/065 ,  F03D9/25 ,  F03D13/20 ,  F03D80/60 ,  F03D80/70 ,  F03D80/88 ,  F05B2240/212 ,  F05B2240/31 ,  F05B2240/912 ,  F05B2240/916 ,  F05B2260/201 ,  H02K7/183 ,  H02K9/04 ,  H02K16/00 ,  Y02E10/728 ,  Y02E10/74 ,  Y02P70/523 ,  Y02T50/675

Abstract: A vertical wind power generator comprises a tower column (1), at least one generator unit (2), at least two blades (3), an excitation control device (16), a rotation rectifying device (161), a bidirectional frequency converter (15), flanges (7-13), bearings (4-6), a cooling system, a crane (80) and a lift system. The generator unit (2) comprises a bracket (201), a generator (202) and an exciter (203). The bracket (201) comprises an outer bracket (2011) and an inner bracket (2012). The generator (202) comprises a stator (2021) and a rotor (2022). The exciter (203) comprises a stator (2031) and a rotor (2032). The vertical wind power generator can be manufactured at reduced cost, be rapidly started, improve the utilization efficiency of wind power, have a better cooling effect on the generator (202) and increase its operating life, and therefore reduce maintenance cost and time.

Abstract translation: 一种垂直风力发电机包括塔柱（1），至少一个发电机单元（2），至少两个叶片（3），励磁控制装置（16），旋转整流装置（161），双向变频器 （15），法兰（7-13），轴承（4-6），冷却系统，起重机（80）和升降系统。 发电机单元（2）包括支架（201），发电机（202）和励磁机（203）。 支架（201）包括外支架（2011）和内支架（2012）。 发电机（202）包括定子（2021）和转子（2022）。 励磁机（203）包括定子（2031）和转子（2032）。 立式风力发电机可以降低成本，快速启动，提高风力发电的利用效率，对发电机组（202）的降温效果更好，延长使用寿命，降低维护成本和时间。

公开(公告)号：US08476784B2

公开(公告)日：2013-07-02

申请号：US13252468

申请日：2011-10-04

Applicant: Shinsuke Sato ,  Shigeto Hirai ,  Tatsuo Ishiguro

Inventor： Shinsuke Sato ,  Shigeto Hirai ,  Tatsuo Ishiguro

IPC: F03D9/00

CPC classification number: F03D1/0691 ,  F03D1/0675 ,  F03D9/25 ,  F03D13/20 ,  F03D80/60 ,  F03D80/80 ,  F03D80/88 ,  F05B2240/14 ,  F05B2240/221 ,  F05B2240/30 ,  F05B2240/912 ,  F05B2260/201 ,  Y02E10/721 ,  Y02E10/728

Abstract: In a wind turbine generating apparatus, a heat generating device is provided inside the rotor head and has a hermetically-sealed structure from outside. A rotor head cooling air passage is formed through the periphery of the heat generating device to the inside of a wind turbine blade. A cooling air introduction portion through which cooling air flows and an air outlet from which the cooling air is discharged are provided in the rotor head cooling air passage to thereby form the air outlet in the wind turbine blade.

Abstract translation: 在风力涡轮发电装置中，在转子头内部设置有发热装置，并且具有从外部的密封结构。 转子头冷却空气通道通过发热装置的周边形成到风力涡轮机叶片的内部。 在转子头冷却风通道中设置有冷却空气流过的冷却空气导入部和排出冷却空气的空气出口，从而在风力涡轮机叶片中形成空气出口。

公开(公告)号：US20120280511A1

公开(公告)日：2012-11-08

申请号：US13520396

申请日：2010-03-26

Applicant: Uffe Eriksen

Inventor： Uffe Eriksen

IPC: F03D9/00 ,  G05D23/19 ,  F16C33/00

CPC classification number: F16C37/00 ,  F03D80/60 ,  F03D80/70 ,  F05B2240/50 ,  F05B2260/201 ,  F16C37/007 ,  F16C2360/31 ,  Y02E10/721 ,  Y02E10/722

Abstract: A direct drive wind turbine with a cooling system has a generator with a rotor and a stator and a bearing with an inner ring and an outer ring connecting the rotor and the stator rotatively. The cooling system includes at least one heat sink which is in thermal communication with the inner ring of the bearing and a heat dissipater which is in thermal communication with the heat sink.

Abstract translation: 具有冷却系统的直接驱动风力涡轮机具有带有转子和定子的发电机以及具有内环的轴承以及将转子和定子相互连接的外圈。 冷却系统包括至少一个与轴承的内圈热连通的散热器和与散热器热连通的散热器。

公开(公告)号：US20100071379A1

公开(公告)日：2010-03-25

申请号：US12238174

申请日：2008-09-25

Applicant: Gregory O. Woodcock ,  Timothy Ertz ,  Brian Koch

Inventor： Gregory O. Woodcock ,  Timothy Ertz ,  Brian Koch

IPC: F02C1/00

CPC classification number: F23R3/06 ,  F05B2260/201 ,  F05B2260/202 ,  F05B2260/203 ,  F23R2900/03041 ,  Y02T50/675

Abstract: A combustor for an engine assembly includes a cylindrical wall forming a combustion chamber in which an air and fuel mixture is combusted; and a plurality of effusion cooling holes formed in the cylindrical wall, the plurality of effusion cooling holes oriented such that cooling air flowing therethrough cools the cylindrical wall with effusion cooling, convection cooling, and impingement cooling.

Abstract translation: 用于发动机组件的燃烧器包括形成空气和燃料混合物燃烧的燃烧室的圆柱形壁; 以及形成在圆筒壁上的多个排出冷却孔，多个排出冷却孔的取向使得流过的冷却空气通过喷出冷却，对流冷却和冲击冷却来冷却圆筒壁。

公开(公告)号：US20060101801A1

公开(公告)日：2006-05-18

申请号：US10992184

申请日：2004-11-18

Applicant: Robert Bland

Inventor： Robert Bland

IPC: F23R3/04

CPC classification number: F23R3/26 ,  F05B2260/201 ,  F23R3/04

Abstract: Embodiments of the invention relate to a combustor flow sleeve for a turbine engine. The flow sleeve can be configured to optimize cooling and airflow distribution. The flow sleeve can include first and second sets of openings. A first set of openings can be provided for impingement cooling the areas of the liner that are subjected to high thermal loads. The second set of openings can be provided to more evenly distribute the airflow into the combustor head-end. By focusing the cooling on the areas of need and by making the airflow more uniform, embodiments of the invention can reduce the system pressure drop and enhance the performance and power of the engine.

公开(公告)号：US20010029738A1

公开(公告)日：2001-10-18

申请号：US09826927

申请日：2001-04-06

Inventor： Anthony Pidcock ,  Desmond Close ,  Michael P. Spooner

IPC: F02C001/00

CPC classification number: F23R3/002 ,  F05B2260/201 ,  F05B2260/202 ,  F23R3/08

Abstract: A wall structure for a gas turbine combustor arranged to have a general direction of fluid flow therethrough includes inner and outer walls defining a space therebetween. The inner wall is made up of a plurality of tiles having axial edges aligned generally with the direction of fluid flow, a gap being defined between axial edges of adjacent tiles. Orifices are provided within the axial edges to direct leakage air passing through the gaps to give the leakage air a flow component in the general direction of fluid flow through the combustor.

Abstract translation: 用于燃气轮机燃烧器的壁结构，其布置成具有流体流动的大致方向，其中包括限定其间的空间的内壁和外壁。 内壁由多个瓦片组成，其多个瓦片具有大致与流体流动方向对齐的轴向边缘，间隙限定在相邻瓦片的轴向边缘之间。 在轴向边缘内设置有孔口，以引导通过间隙的泄漏空气，使得泄漏空气在流体通过燃烧器的流体的大致方向上流动。

公开(公告)号：US5598697A

公开(公告)日：1997-02-04

申请号：US505633

申请日：1995-07-21

Applicant: Christine J. M. Ambrogi ,  Denis R. H. Ansart ,  Serge M. Meunier ,  Denis J. M. Sandelis

Inventor： Christine J. M. Ambrogi ,  Denis R. H. Ansart ,  Serge M. Meunier ,  Denis J. M. Sandelis

IPC: F23R3/00

CPC classification number: F23R3/002 ,  F05B2260/201 ,  F05B2260/202 ,  F05B2260/222

Abstract: A wall structure for a wall bounding a combustion chamber of a gas turbine engine is disclosed having a first wall with an inner surface facing towards the interior of the combustion chamber and an outer surface facing away from the interior of the combustion chamber such that the inner surface forms a boundary of the combustion chamber and the outer surface has a surface roughness to prevent the formation of a fluid flow cooling layer which would cool the outer surface. The invention also has a second wall spaced from the outer surface of the first wall in a direction away from the interior of the combustion chamber so as to define a cooling fluid circulatory space between the first and second walls. A plurality of first perforations extend through the first wall in communication with the cooling fluid circulatory space to enable passage of cooling fluid from the space through the first perforations to form a cooling fluid film on the inner surface of the first wall.

Abstract translation: 公开了一种用于限定燃气涡轮发动机的燃烧室的壁的壁结构，其具有面向燃烧室内部的内表面的第一壁和远离燃烧室内部的外表面， 表面形成燃烧室的边界，并且外表面具有表面粗糙度，以防止形成冷却外表面的流体流动冷却层。 本发明还具有在远离燃烧室内部的方向上与第一壁的外表面隔开的第二壁，以便限定第一和第二壁之间的冷却流体循环空间。 多个第一穿孔延伸穿过与冷却流体循环空间连通的第一壁，以使冷却流体能够从空间通过第一穿孔，以在第一壁的内表面上形成冷却流体膜。