EA200200007A1 - Система наддува для газовых турбин - Google Patents

Система наддува для газовых турбин

Info

Publication number
EA200200007A1
EA200200007A1 EA200200007A EA200200007A EA200200007A1 EA 200200007 A1 EA200200007 A1 EA 200200007A1 EA 200200007 A EA200200007 A EA 200200007A EA 200200007 A EA200200007 A EA 200200007A EA 200200007 A1 EA200200007 A1 EA 200200007A1
Authority
EA
Eurasian Patent Office
Prior art keywords
turbine
regulator
generator
blower fan
gas turbine
Prior art date
Application number
EA200200007A
Other languages
English (en)
Other versions
EA005393B1 (ru
Inventor
Уилльям Л. Копко
Original Assignee
Инханст Тэрбайн Аутпут Холдинг, Ллс.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US09/388,927 external-priority patent/US6308512B1/en
Priority claimed from US09/475,154 external-priority patent/US6442942B1/en
Application filed by Инханст Тэрбайн Аутпут Холдинг, Ллс. filed Critical Инханст Тэрбайн Аутпут Холдинг, Ллс.
Publication of EA200200007A1 publication Critical patent/EA200200007A1/ru
Publication of EA005393B1 publication Critical patent/EA005393B1/ru

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/36—Open cycles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • F02C7/141—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
    • F02C7/143—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid before or between the compressor stages
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00—Combustion technologies with mitigation potential
    • Y02E20/16—Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Control Of Turbines (AREA)

Abstract

В заявке описана система наддува для газотурбинных установок (11), вырабатывающих электрическую энергию. Система включает нагнетательный вентилятор (30, 32) и регулятор (50), который ограничивает выходную мощность турбины и защищает генератор (28) от перегрузки при низких температурах окружающего воздуха. Регулятор может ограничивать выходную мощность турбины, контролируя работу камеры сгорания, температуру воздуха на входе в турбину, давление, создаваемое нагнетательным вентилятором, и другими способами. Предлагаемую в изобретении систему наддува можно использовать для модернизации существующих газотурбинных энергетических установок, не заменяя при этом генератора и другого связанного с ним оборудования.Международная заявка была опубликована вместе с отчетом о международном поиске.
EA200200007A 1999-06-10 2000-06-09 Газотурбинная установка для выработки электрической энергии и система наддува для газотурбинной установки EA005393B1 (ru)

Applications Claiming Priority (8)

Application Number Priority Date Filing Date Title
US13884899P 1999-06-10 1999-06-10
US13989499P 1999-06-22 1999-06-22
US09/388,927 US6308512B1 (en) 1999-06-10 1999-09-02 Supercharging system for gas turbines
US15227799P 1999-09-03 1999-09-03
US15920799P 1999-10-13 1999-10-13
US09/475,154 US6442942B1 (en) 1999-06-10 1999-12-30 Supercharging system for gas turbines
US19530200P 2000-04-10 2000-04-10
PCT/US2000/015821 WO2001000975A1 (en) 1999-06-10 2000-06-09 Supercharging system for gas turbines

Publications (2)

Publication Number Publication Date
EA200200007A1 true EA200200007A1 (ru) 2002-06-27
EA005393B1 EA005393B1 (ru) 2005-02-24

Family

ID=27568921

Family Applications (1)

Application Number Title Priority Date Filing Date
EA200200007A EA005393B1 (ru) 1999-06-10 2000-06-09 Газотурбинная установка для выработки электрической энергии и система наддува для газотурбинной установки

Country Status (9)

Country Link
EP (1) EP1206634A4 (ru)
JP (1) JP2003529701A (ru)
KR (1) KR100874508B1 (ru)
CN (1) CN1304740C (ru)
AU (1) AU775318B2 (ru)
BR (1) BR0011468B1 (ru)
CA (1) CA2376788A1 (ru)
EA (1) EA005393B1 (ru)
MX (1) MXPA01012754A (ru)

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RU2474714C2 (ru) * 2008-09-08 2013-02-10 Вольво Ластвагнар Аб Способ и система бортовой диагностики
KR101011335B1 (ko) * 2009-01-15 2011-01-28 김한기 스팀 발생장치
KR101434119B1 (ko) * 2011-01-21 2014-08-25 미츠비시 쥬고교 가부시키가이샤 발전 플랜트
TWI563164B (en) * 2011-03-22 2016-12-21 Exxonmobil Upstream Res Co Integrated systems incorporating inlet compressor oxidant control apparatus and related methods of generating power
WO2013116185A1 (en) * 2012-01-30 2013-08-08 Kraft Robert J Gas turbine energy storage and energy supplementing systems and methods of making and using the same
US20130318941A1 (en) * 2012-05-31 2013-12-05 General Electric Company Supercharged Combined Cycle System With Air Flow Bypass
US9771864B2 (en) * 2012-05-31 2017-09-26 General Electric Company Gas turbine compressor inlet pressurization and flow control system
US9239007B2 (en) * 2012-05-31 2016-01-19 General Electric Company Gas turbine compressor inlet pressurization having a torque converter system
CN102797833A (zh) * 2012-08-31 2012-11-28 长城汽车股份有限公司 车辆生热构件用冷却节能装置
JP6291245B2 (ja) * 2012-12-20 2018-03-14 ゼネラル・エレクトリック・カンパニイ Ｈｒｓｇおよびファンへの空気流バイパスを備えた過給結合サイクルシステム
US9567913B2 (en) * 2013-01-28 2017-02-14 General Electric Company Systems and methods to extend gas turbine hot gas path parts with supercharged air flow bypass
US9581089B2 (en) 2013-05-10 2017-02-28 General Electric Company Gas dosage control for gas engine
EP2910742A1 (de) * 2014-02-20 2015-08-26 Siemens Aktiengesellschaft Verfahren zum Kuppeln einer Dampfturbine und einer Gasturbine mit einem gewünschten Differenzwinkel
US10030558B2 (en) * 2015-06-29 2018-07-24 General Electric Company Power generation system exhaust cooling
RU2621448C2 (ru) * 2015-10-06 2017-06-06 федеральное государственное автономное образовательное учреждение высшего образования "Самарский государственный аэрокосмический университет имени академика С.П. Королева (национальный исследовательский университет)" (СГАУ) Способ работы комбинированной газопаровой установки
RU2628851C1 (ru) * 2016-10-25 2017-08-22 федеральное государственное бюджетное образовательное учреждение высшего образования "Национальный исследовательский университет "МЭИ" (ФГБОУ ВО "НИУ "МЭИ") Газотурбинная установка
CN106499666A (zh) * 2016-11-28 2017-03-15 沈阳透平机械股份有限公司 流量系数0.0242管线压缩机模型级及叶轮设计方法
US20180171877A1 (en) * 2016-12-15 2018-06-21 General Electric Company Power Generation System and Method for Operating Same
RU2637345C1 (ru) * 2017-03-16 2017-12-04 федеральное государственное бюджетное образовательное учреждение высшего образования "Национальный исследовательский университет "МЭИ" (ФГБОУ ВО "НИУ "МЭИ") Устройство управления теплосиловой установкой
JP6947608B2 (ja) * 2017-11-07 2021-10-13 株式会社クボタ 廃棄物処理設備及び廃棄物処理設備の運転方法
CN108593323A (zh) * 2018-04-26 2018-09-28 上海交通大学 一种燃驱压缩机组性能测试系统
CN108915872B (zh) * 2018-07-04 2021-04-13 贵溪发电有限责任公司 一种提高火力发电厂发电效率的方法
CN108915871B (zh) * 2018-07-04 2021-05-25 智腾机械设备（上海）有限公司 一种发电式燃气轮机
KR102038071B1 (ko) * 2019-06-06 2019-10-29 (주)케이알터빈에너지 다수개의 증기터빈과 발전기를 이용한 발전장치
KR20210064481A (ko) * 2019-11-25 2021-06-03 현대자동차주식회사 하이브리드 차량의 제어 장치 및 방법
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CN114810231B (zh) * 2021-01-28 2023-08-01 华能北京热电有限责任公司 一种燃气–蒸汽联合循环机组燃气增压机变频控制方法

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Also Published As

Publication number Publication date
EA005393B1 (ru) 2005-02-24
JP2003529701A (ja) 2003-10-07
AU775318B2 (en) 2004-07-29
EP1206634A4 (en) 2005-10-12
KR100874508B1 (ko) 2008-12-18
KR20020038921A (ko) 2002-05-24
MXPA01012754A (es) 2003-09-04
EP1206634A1 (en) 2002-05-22
CN1304740C (zh) 2007-03-14
BR0011468B1 (pt) 2010-08-24
AU7823200A (en) 2001-01-31
CN1355869A (zh) 2002-06-26
CA2376788A1 (en) 2001-01-04
BR0011468A (pt) 2002-03-19

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Legal Events

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MM4A Lapse of a eurasian patent due to non-payment of renewal fees within the time limit in the following designated state(s)

Designated state(s): AM AZ BY KG MD TJ TM

MM4A Lapse of a eurasian patent due to non-payment of renewal fees within the time limit in the following designated state(s)

Designated state(s): KZ RU