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公开(公告)号：US09816391B2
公开(公告)日：2017-11-14
申请号：US14493378
申请日：2014-09-23
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Sanji Ekanayake , Alston Ilford Scipio , Julio Enrique Mestroni , Timothy Joseph Rehg
CPC classification number: F01D25/002 , B05B7/0892 , B08B3/02 , B08B9/00
Abstract: The present application thus provides a cleaning system for use with a compressor of a turbine engine. The cleaning system may include a wash nozzle positioned about the compressor and a spheroid injection port to inject a number of spheroids therein.
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公开(公告)号：US09863285B2
公开(公告)日：2018-01-09
申请号：US14662836
申请日：2015-03-19
Applicant: General Electric Company
Inventor： Sanji Ekanayake , Thomas John Freeman , John David Memmer , Timothy Joseph Rehg , Alston Ilford Scipio
CPC classification number: F01K23/10 , F02C3/10 , F02C6/00 , F02C6/02 , F02C6/08 , F02C6/18 , F02C9/18 , Y02E20/14 , Y02E20/16
Abstract: A power generation system may include a generator; a gas turbine system for powering the generator, the gas turbine system including a turbine component, an integral compressor and a combustor to which air from the integral compressor and fuel are supplied, the combustor arranged to supply hot combustion gases to the turbine component, and the integral compressor having a flow capacity greater than an intake capacity of at least one of the combustor and the turbine component, creating an excess air flow. A first control valve system controls flow of the excess air flow along an excess air flow path to a supplemental gas turbine system. The excess air flow may be combusted with a fuel and supplied to the supplemental gas turbine system. An eductor may be positioned in the excess air flow path for using the excess air flow as a motive force to augment the excess air flow with additional gas.
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3.发明申请POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS GAS FLOW FOR SUPPLEMENTAL GAS TURBINE SYSTEM 有权具有压缩机功能的发电系统创造更多气体补给气体系统的气体流量公开(公告)号：US20160273402A1
公开(公告)日：2016-09-22
申请号：US14662836
申请日：2015-03-19
Applicant: General Electric Company
Inventor： Sanji Ekanayake , Thomas John Freeman , John David Memmer , Timothy Joseph Rehg , Alston Ilford Scipio
CPC classification number: F01K23/10 , F02C3/10 , F02C6/00 , F02C6/02 , F02C6/08 , F02C6/18 , F02C9/18 , Y02E20/14 , Y02E20/16
Abstract: A power generation system may include a generator; a gas turbine system for powering the generator, the gas turbine system including a turbine component, an integral compressor and a combustor to which air from the integral compressor and fuel are supplied, the combustor arranged to supply hot combustion gases to the turbine component, and the integral compressor having a flow capacity greater than an intake capacity of at least one of the combustor and the turbine component, creating an excess air flow. A first control valve system controls flow of the excess air flow along an excess air flow path to a supplemental gas turbine system. The excess air flow may be combusted with a fuel and supplied to the supplemental gas turbine system. An eductor may be positioned in the excess air flow path for using the excess air flow as a motive force to augment the excess air flow with additional gas.
Abstract translation: 发电系统可以包括发电机; 用于为发电机供电的燃气轮机系统，所述燃气涡轮机系统包括涡轮机部件，一体式压缩机和燃烧器，供应来自所述一体式压缩机和燃料的空气，所述燃烧器布置成将热燃烧气体供应到所述涡轮机部件，以及 所述整体式压缩机具有大于所述燃烧器和所述涡轮机部件中的至少一个的进气容量的流量，从而产生过量的气流。 第一控制阀系统控制过量空气流沿着多余的气流路径流向补充燃气轮机系统。 过量空气流可以与燃料一起燃烧并供应到辅助燃气轮机系统。 喷射器可以定位在过量空气流动路径中，以使用过量的气流作为动力，以用额外的气体来增加过量的气流。
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4.发明申请POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND TURBO-EXPANDER USING SAME 审中-公开具有压缩机的发电系统创造出更高的空气流量和使用其的涡轮膨胀机公开(公告)号：US20160273403A1
公开(公告)日：2016-09-22
申请号：US14662847
申请日：2015-03-19
Applicant: General Electric Company
Inventor： Sanji Ekanayake , Kihyung Kim , Timothy Joseph Rehg , Alston Ilford Scipio , Leslie Yung Min Tong
CPC classification number: F01K23/10 , F02C3/04 , F02C3/10 , F02C3/13 , F02C3/32 , F02C6/08 , F02C9/18 , F05D2220/72 , F05D2230/80 , F05D2260/601 , F05D2260/606 , Y02E20/14 , Y02E20/16
Abstract: A power generation system may include a generator, and a gas turbine system for powering the generator, the gas turbine system including a turbine component, an integral compressor and a combustor to which air from the integral compressor and fuel are supplied, the combustor arranged to supply hot combustion gases to the turbine component, and the integral compressor having a flow capacity greater than an intake capacity of at least one of the combustor and the turbine component, creating an excess air flow. A turbo-expander may also power the generator. A first control valve control flow of the excess air flow along an excess air flow path to an inlet of the turbo-expander. An educator may be positioned in the excess air flow path for using the excess air flow as a motive force to augment the excess air flow with additional air. A discharge of the turbo-expander is supplied to an exhaust of the turbine component for an HRSG.
Abstract translation: 发电系统可以包括发电机和用于为发电机供电的燃气轮机系统，所述燃气涡轮机系统包括涡轮机部件，整体式压缩机和燃烧器，来自所述整体式压缩机和燃料的空气被供应到所述燃烧器，所述燃烧器布置成 向涡轮机部件供应热燃烧气体，并且整体压缩机具有大于燃烧器和涡轮机部件中的至少一个的进气容量的流量，产生过量空气流。 涡轮膨胀机也可以为发电机供电。 第一控制阀控制沿着过量空气流动路径的过量气流到涡轮膨胀机的入口的流动。 教育者可以定位在过量气流路径中，以使用过量的气流作为增加额外空气的过量气流的动力。 涡轮膨胀机的排放被供给到用于HRSG的涡轮机部件的排气口。
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