RU2566621C2 - Способ работы газовой турбины с последовательным сгоранием и газовая турбина для осуществления указанного способа - Google Patents

Способ работы газовой турбины с последовательным сгоранием и газовая турбина для осуществления указанного способа Download PDF

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Publication number
RU2566621C2
RU2566621C2 RU2013146093/06A RU2013146093A RU2566621C2 RU 2566621 C2 RU2566621 C2 RU 2566621C2 RU 2013146093/06 A RU2013146093/06 A RU 2013146093/06A RU 2013146093 A RU2013146093 A RU 2013146093A RU 2566621 C2 RU2566621 C2 RU 2566621C2
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RU
Russia
Prior art keywords
combustion chamber
temperature
combustion
gas turbine
inlet
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RU2013146093/06A
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English (en)
Russian (ru)
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RU2013146093A (ru
Inventor
Андреа КИАНИ
Аднан ЭРОГЛУ
Дуглас Энтони ПЕННЕЛЛ
Николя ТРЭН
Эвальд ФРАЙТАГ
Original Assignee
Альстом Текнолоджи Лтд
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Publication of RU2013146093A publication Critical patent/RU2013146093A/ru
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    • 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
    • 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
    • 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
    • F02C7/22—Fuel supply systems
    • F02C7/228—Dividing fuel between various burners
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/08—Purpose of the control system to produce clean exhaust gases
    • 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]

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
RU2013146093/06A 2012-10-22 2013-10-15 Способ работы газовой турбины с последовательным сгоранием и газовая турбина для осуществления указанного способа RU2566621C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP12189430 2012-10-22
EP12189430.7 2012-10-22

Publications (2)

Publication Number Publication Date
RU2013146093A RU2013146093A (ru) 2015-04-20
RU2566621C2 true RU2566621C2 (ru) 2015-10-27

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RU2013146093/06A RU2566621C2 (ru) 2012-10-22 2013-10-15 Способ работы газовой турбины с последовательным сгоранием и газовая турбина для осуществления указанного способа

Country Status (7)

Country Link
US (1) US9518511B2 (enExample)
EP (1) EP2722508B1 (enExample)
JP (1) JP6000220B2 (enExample)
KR (1) KR101555500B1 (enExample)
CN (1) CN103775215B (enExample)
CA (1) CA2829613C (enExample)
RU (1) RU2566621C2 (enExample)

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EP3015661A1 (en) 2014-10-28 2016-05-04 Alstom Technology Ltd Combined cycle power plant
EP3037728B1 (en) * 2014-12-22 2020-04-29 Ansaldo Energia Switzerland AG Axially staged mixer with dilution air injection
EP3037726B1 (en) 2014-12-22 2018-09-26 Ansaldo Energia Switzerland AG Separate feedings of cooling and dilution air
EP3061944A1 (en) * 2015-02-26 2016-08-31 General Electric Technology GmbH Method for controlling the operation of a gas turbine with sequential combustion
US10330015B2 (en) * 2015-09-25 2019-06-25 General Electric Company Transient emission temperature control of turbine systems
CN109416181B (zh) 2016-05-12 2021-05-28 西门子公司 用于减少排放的选择性燃烧器控制方法
EP3447379B1 (en) * 2017-08-25 2022-01-26 Ansaldo Energia IP UK Limited Method for operating a gas turbine plant and gas turbine plant
EP3683426B1 (en) * 2019-01-15 2023-05-03 Ansaldo Energia Switzerland AG Method for operating a gas turbine power plant and gas turbine power plant
EP3845813B1 (en) * 2019-12-31 2024-04-03 Ansaldo Energia Switzerland AG Method for operating a gas turbine assembly and gas turbine assembly
EP3845740B1 (en) * 2019-12-31 2024-04-03 ANSALDO ENERGIA S.p.A. Gas turbine assembly
KR102804270B1 (ko) * 2023-03-29 2025-05-08 석 규 이 가스터빈 압축실과 연소실과 배기관에서 폭명기를 발생시키고 압축실과 연소실과 배기관의 압력을 급상승시켜 추력과 출력을 상승시키는 가스터빈 폭명기시스템

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RU2229030C2 (ru) * 2002-02-20 2004-05-20 Общество с ограниченной ответственностью "Интербизнеспроект" Способ повышения эффективности работы газотурбинной установки
EP1531305A1 (en) * 2003-11-12 2005-05-18 United Technologies Corporation Multi-point fuel injector
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Also Published As

Publication number Publication date
EP2722508A1 (en) 2014-04-23
CA2829613A1 (en) 2014-04-22
CA2829613C (en) 2016-02-23
CN103775215A (zh) 2014-05-07
JP2014084873A (ja) 2014-05-12
US20140109586A1 (en) 2014-04-24
US9518511B2 (en) 2016-12-13
RU2013146093A (ru) 2015-04-20
JP6000220B2 (ja) 2016-09-28
CN103775215B (zh) 2016-10-05
KR101555500B1 (ko) 2015-10-06
EP2722508B1 (en) 2018-06-13
KR20140051089A (ko) 2014-04-30

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Effective date: 20170518