RU2562681C2 - Газовая турбина с уменьшенными выбросами при частичной нагрузке - Google Patents

Газовая турбина с уменьшенными выбросами при частичной нагрузке Download PDF

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Publication number
RU2562681C2
RU2562681C2 RU2011144106/06A RU2011144106A RU2562681C2 RU 2562681 C2 RU2562681 C2 RU 2562681C2 RU 2011144106/06 A RU2011144106/06 A RU 2011144106/06A RU 2011144106 A RU2011144106 A RU 2011144106A RU 2562681 C2 RU2562681 C2 RU 2562681C2
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RU
Russia
Prior art keywords
turbine
combustion chamber
load
fuel
temperature
Prior art date
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RU2011144106/06A
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English (en)
Russian (ru)
Other versions
RU2011144106A (ru
Inventor
Аднан ЭРОГЛУ
Клаус КНАП
Петер ФЛОР
Ганс Петер КНЁПФЕЛЬ
Вэйцюнь ГЭН
Original Assignee
Альстом Текнолоджи Лтд
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Publication date
Application filed by Альстом Текнолоджи Лтд filed Critical Альстом Текнолоджи Лтд
Publication of RU2011144106A publication Critical patent/RU2011144106A/ru
Application granted granted Critical
Publication of RU2562681C2 publication Critical patent/RU2562681C2/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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/003—Gas-turbine plants with heaters between turbine stages
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C6/00—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion
    • F23C6/04—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection
    • F23C6/042—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection with fuel supply in stages
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N1/00—Regulating fuel supply
    • F23N1/02—Regulating fuel supply conjointly with air supply
    • F23N1/022—Regulating fuel supply conjointly with air supply using electronic means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R7/00—Intermittent or explosive combustion chambers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N2237/00—Controlling
    • F23N2237/02—Controlling two or more burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N2241/00—Applications
    • F23N2241/20—Gas turbines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03341—Sequential combustion chambers or burners
    • 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]

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
RU2011144106/06A 2009-04-01 2010-03-12 Газовая турбина с уменьшенными выбросами при частичной нагрузке RU2562681C2 (ru)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
CH00536/09A CH700796A1 (de) 2009-04-01 2009-04-01 Verfahren zum CO-emissionsarmen Betrieb einer Gasturbine mit sequentieller Verbrennung und Gasturbine mit verbessertem Teillast- Emissionsverhalten.
CH00536/09 2009-04-01
PCT/EP2010/053171 WO2010112318A1 (de) 2009-04-01 2010-03-12 Gasturbine mit verbessertem teillast-emissionsverhalten

Publications (2)

Publication Number Publication Date
RU2011144106A RU2011144106A (ru) 2013-05-10
RU2562681C2 true RU2562681C2 (ru) 2015-09-10

Family

ID=40848719

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2011144106/06A RU2562681C2 (ru) 2009-04-01 2010-03-12 Газовая турбина с уменьшенными выбросами при частичной нагрузке

Country Status (7)

Country Link
US (2) US8434312B2 (enExample)
EP (1) EP2414653B1 (enExample)
JP (1) JP5680053B2 (enExample)
CH (1) CH700796A1 (enExample)
ES (1) ES2627679T3 (enExample)
RU (1) RU2562681C2 (enExample)
WO (1) WO2010112318A1 (enExample)

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US10316696B2 (en) 2015-05-08 2019-06-11 General Electric Company System and method for improving exhaust energy recovery
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US10330015B2 (en) * 2015-09-25 2019-06-25 General Electric Company Transient emission temperature control of turbine systems
US10920676B2 (en) * 2016-11-17 2021-02-16 General Electric Company Low partial load emission control for gas turbine system
HUE050483T2 (hu) * 2017-03-14 2020-12-28 Gen Electric Módszer és rendszer egy szekvenciális gázturbinamotor vezérlésére
US11092085B2 (en) * 2017-03-14 2021-08-17 General Electric Company Method and system for controlling a sequential gas turbine engine
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EP3524799A1 (de) 2018-02-13 2019-08-14 Siemens Aktiengesellschaft Verfahren zum betreiben einer brenneranordnung einer gasturbine
EP3578762A1 (en) * 2018-06-08 2019-12-11 General Electric Technology GmbH Method for determining an outlet temperature of an upstream combustion stage in a gas turbine engine having at least two serially arranged combustion stages
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
JP7231493B2 (ja) * 2019-06-12 2023-03-01 三菱重工業株式会社 制御装置、ガスタービン、制御方法及びプログラム
EP3772616B1 (en) * 2019-08-08 2024-02-07 Ansaldo Energia Switzerland AG Method for operating a gas turbine assembly comprising a sequential combustor
EP3822468B1 (en) * 2019-11-18 2024-04-03 Ansaldo Energia Switzerland AG Gas turbine engine operable at very low partial load and method of controlling a gas turbine engine
US11203986B1 (en) * 2020-06-08 2021-12-21 General Electric Company Systems and methods for extended emissions compliant operation of a gas turbine engine
CN112627989A (zh) * 2021-01-08 2021-04-09 大连欧谱纳透平动力科技有限公司 控制小型燃气轮机排气温度和氮氧化物浓度的系统及方法
CN114001374B (zh) * 2021-11-12 2024-12-03 西安热工研究院有限公司 一种适用于气液两相双燃料旋转爆震燃烧室
EP4206452A1 (en) * 2021-12-30 2023-07-05 Ansaldo Energia Switzerland AG Method for operating a gas turbine assembly for a power plant and gas turbine assembly for a power plant

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Also Published As

Publication number Publication date
EP2414653B1 (de) 2017-03-01
US20130219904A1 (en) 2013-08-29
JP5680053B2 (ja) 2015-03-04
RU2011144106A (ru) 2013-05-10
EP2414653A1 (de) 2012-02-08
US8794008B2 (en) 2014-08-05
JP2012522922A (ja) 2012-09-27
ES2627679T3 (es) 2017-07-31
US8434312B2 (en) 2013-05-07
WO2010112318A1 (de) 2010-10-07
CH700796A1 (de) 2010-10-15
US20120017601A1 (en) 2012-01-26

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PD4A Correction of name of patent owner
PC41 Official registration of the transfer of exclusive right

Effective date: 20170426

MM4A The patent is invalid due to non-payment of fees

Effective date: 20190313