公开(公告)号：EP2365219A2

公开(公告)日：2011-09-14

申请号：EP11157343.2

申请日：2011-03-08

申请人： General Electric Company

发明人： Saddoughi, Seyed Gholamali ,  Badding, Bruce John ,  Giguere, Philippe ,  Boespflug, Matthew Patrick ,  Bennett, Jr., Grover Andrew ,  Gupta, Anurag

IPC分类号： F03D11/00

CPC分类号： F03D1/0675 ,  F03D80/40 ,  F05B2240/122 ,  F05D2270/172 ,  Y02E10/721

摘要： A system for deicing a wind turbine blade includes an electrically powered active plasma actuator (10) applied to a desired portion of a wind turbine blade (30). The activated plasma actuator (10) energizes the air (22,26) in the vicinity of the plasma actuator (10) to increase the surface temperature of the wind turbine blade (30) in the vicinity of the plasma actuator (10) sufficiently to reduce or eliminate the collection of ice on a desired portion of the wind turbine blade (30).

摘要翻译： 用于除风风力涡轮机叶片的系统包括施加到风力涡轮机叶片（30）的期望部分的电动有源等离子体致动器（10）。 活化的等离子体致动器（10）激发等离子体致动器（10）附近的空气（22,26），以使等离子体致动器（10）附近的风力涡轮机叶片（30）的表面温度充分增加， 减少或消除在风力涡轮机叶片（30）的期望部分上的冰的收集。

公开(公告)号：EP2365219A3

公开(公告)日：2014-04-30

申请号：EP11157343.2

申请日：2011-03-08

申请人： General Electric Company

发明人： Saddoughi, Seyed Gholamali ,  Badding, Bruce John ,  Giguere, Philippe ,  Boespflug, Matthew Patrick ,  Bennett, Jr., Grover Andrew ,  Gupta, Anurag

IPC分类号： F03D11/00 ,  F03D1/06

CPC分类号： F03D1/0675 ,  F03D80/40 ,  F05B2240/122 ,  F05D2270/172 ,  Y02E10/721

摘要： A system for deicing a wind turbine blade includes an electrically powered active plasma actuator (10) applied to a desired portion of a wind turbine blade (30). The activated plasma actuator (10) energizes the air (22,26) in the vicinity of the plasma actuator (10) to increase the surface temperature of the wind turbine blade (30) in the vicinity of the plasma actuator (10) sufficiently to reduce or eliminate the collection of ice on a desired portion of the wind turbine blade (30).

公开(公告)号：EP2518294A2

公开(公告)日：2012-10-31

申请号：EP12165617.7

申请日：2012-04-26

申请人： General Electric Company

发明人： Elkady, Ahmed Mostafa ,  Idahosa, Uyigue Omoma ,  Boespflug, Matthew Patrick ,  Bennet, Grover Andrew ,  Herbon, John Thomas ,  Karim, Hasan ,  Myers, Geoffrey Davis ,  Saddoughi, Seyed Gholamali

IPC分类号： F02C3/20

CPC分类号： F02C3/34 ,  F01K23/10 ,  F02C3/14 ,  F02C3/20 ,  F05D2240/35 ,  F05D2270/082 ,  Y02E20/344

摘要： A system 50 and a method of generating energy in a power plant using a turbine 64 are provided. The system 50 includes an air separation unit 12 providing an oxygen output; a plasma generator 54 that is capable of generating plasma 60; and a combustor 14 configured to receive oxygen and to combust a fuel stream 58 in the presence of the plasma 60, so as to maintain a stable flame, generating an exhaust gas 62. The system 50 can further include a water condensation system 16, fluidly-coupled to the combustor 14, that is capable of producing a high-content carbon dioxide stream 70 that is substantially free of oxygen. The method of generating energy in a power plant includes the steps of operating an air separation unit 12 to separate oxygen from air, combusting a fuel stream 58 in a combustor 14 in the presence of oxygen, and generating an exhaust gas 62 from the combustion. The exhaust gas 62 can be used in a turbine 64 to generate electricity. A plasma 60 is generated inside the combustor 14, and a stable flame is maintained in the combustor 14.

公开(公告)号：EP2518294A3

公开(公告)日：2017-05-03

申请号：EP12165617.7

申请日：2012-04-26

申请人： General Electric Company

发明人： Elkady, Ahmed Mostafa ,  Idahosa, Uyigue Omoma ,  Boespflug, Matthew Patrick ,  Bennet, Grover Andrew ,  Herbon, John Thomas ,  Karim, Hasan ,  Myers, Geoffrey Davis ,  Saddoughi, Seyed Gholamali

IPC分类号： F02C3/20 ,  F02C3/14 ,  F02C3/34 ,  F01K23/10

CPC分类号： F02C3/34 ,  F01K23/10 ,  F02C3/14 ,  F02C3/20 ,  F05D2240/35 ,  F05D2270/082 ,  Y02E20/344

摘要： A system 50 and a method of generating energy in a power plant using a turbine 64 are provided. The system 50 includes an air separation unit 12 providing an oxygen output; a plasma generator 54 that is capable of generating plasma 60; and a combustor 14 configured to receive oxygen and to combust a fuel stream 58 in the presence of the plasma 60, so as to maintain a stable flame, generating an exhaust gas 62. The system 50 can further include a water condensation system 16, fluidly-coupled to the combustor 14, that is capable of producing a high-content carbon dioxide stream 70 that is substantially free of oxygen. The method of generating energy in a power plant includes the steps of operating an air separation unit 12 to separate oxygen from air, combusting a fuel stream 58 in a combustor 14 in the presence of oxygen, and generating an exhaust gas 62 from the combustion. The exhaust gas 62 can be used in a turbine 64 to generate electricity. A plasma 60 is generated inside the combustor 14, and a stable flame is maintained in the combustor 14.

摘要翻译： 本发明提供一种系统50和使用涡轮64中的动力装置中产生能量的方法。 该系统包括50至空气分离单元12提供氧气，以输出; 等离子体发生器54确实能够产生等离子体60的; 和燃烧器14配置成接收氧和在等离子体60的存在下燃烧燃料流58，以维持稳定的火焰，在废气62的系统50生成可进一步包括水冷凝系统16流体地 - 偶联到燃烧器14，确实能够产生高含量的二氧化碳流70的所做的是基本上不含氧的。 在动力设备中产生的能量的方法包括在空气分离单元12从空气操作以单独的氧，在氧的存在下，在燃烧器14中燃烧燃料流58从燃烧的步骤，和排气气体62的生成。 废气62可在涡轮机64用于发电。 等离子体60被燃烧器14的内部产生，并且稳定的火焰保持在燃烧器14日

公开(公告)号：EP2623867A1

公开(公告)日：2013-08-07

申请号：EP12194222.1

申请日：2012-11-26

申请人： General Electric Company

发明人： Boespflug, Matthew Patrick ,  Saddoughi, Seyed Gholamali ,  Bennett, Grover Andrew ,  Herbon, John Thomas

IPC分类号： F23R3/14 ,  F23R3/28 ,  F23C7/00

CPC分类号： F23C7/004 ,  F23C2900/07001 ,  F23D2212/10 ,  F23D2212/20 ,  F23D2900/00008 ,  F23R3/14 ,  F23R3/286 ,  Y02T50/675

摘要： A fuel nozzle assembly (118) for use with a turbine engine includes at least one fuel conduit (212/216) coupled to at least one fuel source. The fuel nozzle assembly also includes at least one swirler (222) that includes at least one wall (230) having a porous portion (234/236). The at least one wall is coupled to the at least one fuel conduit. The porous portion is formed from a material (300) having a porosity that facilitates fuel flow (246/248) therethrough. At least one fuel flow path is thereby defined through the porous portion of the at least one wall.

摘要翻译： 用于涡轮发动机的燃料喷嘴组件（118）包括联接到至少一个燃料源的至少一个燃料管道（212/216）。 燃料喷嘴组件还包括至少一个旋流器（222），其包括具有多孔部分（234/236）的至少一个壁（230）。 所述至少一个壁联接到所述至少一个燃料管道。 多孔部分由具有促进燃料流动的孔隙率（246/248）的材料（300）形成。 由此至少一个燃料流动路径通过至少一个壁的多孔部分被限定。