IT1396516B1 - Metodo di controllo di modo basato su temperatura di scarico per turbina a gas e turbina a gas - Google Patents

Metodo di controllo di modo basato su temperatura di scarico per turbina a gas e turbina a gas

Info

Publication number
IT1396516B1
IT1396516B1 ITCO2009A000054A ITCO20090054A IT1396516B1 IT 1396516 B1 IT1396516 B1 IT 1396516B1 IT CO2009A000054 A ITCO2009A000054 A IT CO2009A000054A IT CO20090054 A ITCO20090054 A IT CO20090054A IT 1396516 B1 IT1396516 B1 IT 1396516B1
Authority
IT
Italy
Prior art keywords
gas turbine
mode control
control based
exhaust temperature
turbine
Prior art date
Application number
ITCO2009A000054A
Other languages
English (en)
Inventor
Claudio Botarelli
Original Assignee
Nuovo Pignone Spa
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 to ITCO2009A000054A priority Critical patent/IT1396516B1/it
Application filed by Nuovo Pignone Spa filed Critical Nuovo Pignone Spa
Priority to US13/512,185 priority patent/US8820089B2/en
Priority to CA2781917A priority patent/CA2781917C/en
Priority to KR1020127016658A priority patent/KR20120096056A/ko
Priority to EP10781496.4A priority patent/EP2504546B1/en
Priority to JP2012540368A priority patent/JP5789265B2/ja
Priority to CN201080062653.2A priority patent/CN102713208B/zh
Priority to PCT/EP2010/067791 priority patent/WO2011064142A1/en
Priority to AU2010323283A priority patent/AU2010323283B2/en
Priority to RU2012122725/06A priority patent/RU2539930C2/ru
Publication of ITCO20090054A1 publication Critical patent/ITCO20090054A1/it
Application granted granted Critical
Publication of IT1396516B1 publication Critical patent/IT1396516B1/it

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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/32—Control of fuel supply characterised by throttling of fuel
    • F02C9/34—Joint control of separate flows to main and auxiliary burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N5/00—Systems for controlling combustion
    • F23N5/003—Systems for controlling combustion using detectors sensitive to combustion gas properties
    • 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
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/36—Supply of different fuels
    • 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
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/301—Pressure
    • 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
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/303—Temperature
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N2221/00—Pretreatment or prehandling
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N2237/00—Controlling
    • F23N2237/08—Controlling two or more different types of fuel simultaneously
    • 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
    • F23R2900/00002—Gas turbine combustors adapted for fuels having low heating value [LHV]

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Supercharger (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
ITCO2009A000054A 2009-11-27 2009-11-27 Metodo di controllo di modo basato su temperatura di scarico per turbina a gas e turbina a gas IT1396516B1 (it)

Priority Applications (10)

Application Number Priority Date Filing Date Title
ITCO2009A000054A IT1396516B1 (it) 2009-11-27 2009-11-27 Metodo di controllo di modo basato su temperatura di scarico per turbina a gas e turbina a gas
CA2781917A CA2781917C (en) 2009-11-27 2010-11-19 Exhaust temperature based mode control method for gas turbine and gas turbine
KR1020127016658A KR20120096056A (ko) 2009-11-27 2010-11-19 가스 터빈용 배기 온도 기반 모드 제어 방법 및 가스 터빈
EP10781496.4A EP2504546B1 (en) 2009-11-27 2010-11-19 Exhaust temperature based mode control method for gas turbine and gas turbine
US13/512,185 US8820089B2 (en) 2009-11-27 2010-11-19 Exhaust temperature based mode control method for gas turbine and gas turbine
JP2012540368A JP5789265B2 (ja) 2009-11-27 2010-11-19 排気温度に基づくガスタービン用モード制御方法およびガスタービン
CN201080062653.2A CN102713208B (zh) 2009-11-27 2010-11-19 用于燃气涡轮的基于废气温度的模式控制方法和燃气涡轮
PCT/EP2010/067791 WO2011064142A1 (en) 2009-11-27 2010-11-19 Exhaust temperature based mode control method for gas turbine and gas turbine
AU2010323283A AU2010323283B2 (en) 2009-11-27 2010-11-19 Exhaust temperature based mode control method for gas turbine and gas turbine
RU2012122725/06A RU2539930C2 (ru) 2009-11-27 2010-11-19 Способ управления режимом работы газовой турбины на основе температуры выхлопного газа и газовая турбина

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ITCO2009A000054A IT1396516B1 (it) 2009-11-27 2009-11-27 Metodo di controllo di modo basato su temperatura di scarico per turbina a gas e turbina a gas

Publications (2)

Publication Number Publication Date
ITCO20090054A1 ITCO20090054A1 (it) 2011-05-28
IT1396516B1 true IT1396516B1 (it) 2012-12-14

Family

ID=42333395

Family Applications (1)

Application Number Title Priority Date Filing Date
ITCO2009A000054A IT1396516B1 (it) 2009-11-27 2009-11-27 Metodo di controllo di modo basato su temperatura di scarico per turbina a gas e turbina a gas

Country Status (10)

Country Link
US (1) US8820089B2 (it)
EP (1) EP2504546B1 (it)
JP (1) JP5789265B2 (it)
KR (1) KR20120096056A (it)
CN (1) CN102713208B (it)
AU (1) AU2010323283B2 (it)
CA (1) CA2781917C (it)
IT (1) IT1396516B1 (it)
RU (1) RU2539930C2 (it)
WO (1) WO2011064142A1 (it)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
MX352291B (es) * 2010-07-02 2017-11-16 Exxonmobil Upstream Res Company Star Sistemas y métodos de generación de potencia de triple ciclo de baja emisión.
MY160833A (en) * 2010-07-02 2017-03-31 Exxonmobil Upstream Res Co Stoichiometric combustion of enriched air with exhaust gas recirculation
US20150075170A1 (en) * 2013-09-17 2015-03-19 General Electric Company Method and system for augmenting the detection reliability of secondary flame detectors in a gas turbine
EP2921673A1 (de) * 2014-03-20 2015-09-23 Siemens Aktiengesellschaft Variable Grenzleistungsregelung für Gasturbinen
EP2952811A1 (en) * 2014-06-02 2015-12-09 Siemens Aktiengesellschaft Method and device to control a fuel split in a combustion device
US9909508B2 (en) * 2014-06-26 2018-03-06 General Electric Company Automatic combustion system characterization
EP3015658A1 (de) * 2014-10-27 2016-05-04 Siemens Aktiengesellschaft Turbinenregelungseinheit mit einem temperaturbeanspruchungsregler als führungsregler
US9791351B2 (en) * 2015-02-06 2017-10-17 General Electric Company Gas turbine combustion profile monitoring
US20180283287A1 (en) 2015-04-30 2018-10-04 Nuovo Pignone Tecnologie Srl Ultra-low nox emission gas turbine engine in mechanical drive applications
CN105241669B (zh) * 2015-09-09 2017-09-01 哈尔滨工业大学 基于比较编码的燃气轮机燃烧系统在线监测方法
US10061298B2 (en) * 2016-04-27 2018-08-28 General Electric Company Control of machinery with calibrated performance model
US11112118B2 (en) * 2016-06-27 2021-09-07 General Electric Company Gas turbine lower heating value methods and systems
FR3061240B1 (fr) * 2016-12-22 2019-05-31 Safran Aircraft Engines Procede ameliore de regulation d'un circuit d'alimentation
RU2696919C1 (ru) * 2018-04-18 2019-08-07 Акционерное общество "РОТЕК" (АО "РОТЕК") Способ и система оценки технического состояния узлов газовой турбины по температурным полям
RU195793U1 (ru) * 2019-11-21 2020-02-05 Хайдер Ибрагим Куса Мобильное зарядное устройство
CN117153282B (zh) * 2023-09-11 2024-04-16 中国航发燃气轮机有限公司 燃气轮机燃烧室基准温度计算方法、装置、介质及设备

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3924140A (en) * 1972-03-14 1975-12-02 Westinghouse Electric Corp System for monitoring and controlling industrial gas turbine power plants including facility for dynamic calibration control instrumentation
FR2308785A1 (fr) * 1975-04-24 1976-11-19 France Etat Perfectionnements aux installations motrices comportant un moteur a combustion interne suralimente
JPS61241425A (ja) * 1985-04-17 1986-10-27 Hitachi Ltd ガスタ−ビンの燃料ガス制御方法及び制御装置
US6092362A (en) * 1996-11-27 2000-07-25 Hitachi, Ltd. Gas-turbine combustor with load-responsive premix burners
RU2248453C2 (ru) * 1998-08-31 2005-03-20 III Вильям Скотт Роллинс Электростанция и способ получения энергии с комбинированием циклов
JP3783442B2 (ja) * 1999-01-08 2006-06-07 株式会社日立製作所 ガスタービンの制御方法
US6226974B1 (en) * 1999-06-25 2001-05-08 General Electric Co. Method of operation of industrial gas turbine for optimal performance
US6442941B1 (en) * 2000-09-11 2002-09-03 General Electric Company Compressor discharge bleed air circuit in gas turbine plants and related method
JP2002130852A (ja) * 2000-10-18 2002-05-09 Shigeto Matsuo 多系統空気冷凍システム
JP2002181399A (ja) * 2000-12-11 2002-06-26 Shigeto Matsuo 自冷式空気冷凍システム
US6715916B2 (en) * 2001-02-08 2004-04-06 General Electric Company System and method for determining gas turbine firing and combustion reference temperatures having correction for water content in fuel
US6687596B2 (en) * 2001-08-31 2004-02-03 General Electric Company Diagnostic method and system for turbine engines
JP3684208B2 (ja) * 2002-05-20 2005-08-17 株式会社東芝 ガスタービン制御装置
RU2237815C2 (ru) * 2002-06-07 2004-10-10 Морев Валерий Григорьевич Способ получения полезной энергии в комбинированном цикле (его варианты) и устройство для его осуществления
US6779346B2 (en) * 2002-12-09 2004-08-24 General Electric Company Control of gas turbine combustion temperature by compressor bleed air
US7246002B2 (en) * 2003-11-20 2007-07-17 General Electric Company Method for controlling fuel splits to gas turbine combustor
JP4119909B2 (ja) * 2005-09-14 2008-07-16 三菱重工業株式会社 ガスタービンの燃焼制御装置
EP1840354B1 (de) * 2006-03-28 2017-11-29 Ansaldo Energia IP UK Limited Verfahren zum Betrieb einer Gasturbinenanlage sowie Gasturbinenanlage zur Durchführung des Verfahrens
US7878004B2 (en) 2006-04-20 2011-02-01 Siemens Aktiengesellschaft Method and device for optimizing a light-up procedure of a gas turbine engine
JP4831820B2 (ja) * 2006-05-22 2011-12-07 三菱重工業株式会社 ガスタービン出力学習回路及びこれを備えたガスタービンの燃焼制御装置
EP1860302A1 (en) 2006-05-22 2007-11-28 Siemens Aktiengesellschaft Gas turbine engine starting method and control device
US9043118B2 (en) 2007-04-02 2015-05-26 General Electric Company Methods and systems for model-based control of gas turbines
ITMI20080164A1 (it) 2008-02-04 2009-08-05 Nuovo Pignone Spa Metodo per l'avviamento di una turbina a gas
EP2107305A1 (en) * 2008-04-01 2009-10-07 Siemens Aktiengesellschaft Gas turbine system and method

Also Published As

Publication number Publication date
CA2781917C (en) 2017-10-10
US8820089B2 (en) 2014-09-02
JP5789265B2 (ja) 2015-10-07
JP2013512379A (ja) 2013-04-11
CN102713208B (zh) 2014-11-26
EP2504546B1 (en) 2016-02-17
CN102713208A (zh) 2012-10-03
WO2011064142A1 (en) 2011-06-03
RU2012122725A (ru) 2014-01-10
US20130042624A1 (en) 2013-02-21
AU2010323283A1 (en) 2012-06-14
ITCO20090054A1 (it) 2011-05-28
RU2539930C2 (ru) 2015-01-27
AU2010323283B2 (en) 2016-07-07
EP2504546A1 (en) 2012-10-03
CA2781917A1 (en) 2011-06-03
KR20120096056A (ko) 2012-08-29

Similar Documents

Publication Publication Date Title
IT1396517B1 (it) Metodo di controllo di modo basato su temperatura di scarico per turbina a gas e turbina a gas
IT1396516B1 (it) Metodo di controllo di modo basato su temperatura di scarico per turbina a gas e turbina a gas
BRPI0924985A2 (pt) "método para controle de uma temperatura de gás de exaustão"
GB0917319D0 (en) An apparatus and method of operating a gas turbine engine
GB0722398D0 (en) A method of monitoring a gas turbine engine
EP2309109A4 (en) GAS TURBINE AND METHOD FOR OPERATING A GAS TURBINE
GB201101304D0 (en) System and method of operating gas turbine engine with an alternative working fluid
IT1396515B1 (it) Soglia basata su temperatura di scarico per metodo di controllo e turbina
GB2468346B (en) Cooling system for an aero gas turbine engine
EP2519724A4 (en) GAS TURBINE AND COOLING SYSTEM
EP2419621A4 (en) SYSTEM AND METHOD FOR MANAGING HEAT PROBLEMS IN GAS TURBINE ENGINES
GB201101287D0 (en) System and method of operating a gas turbine engine with an alternate working fluid
IT1396514B1 (it) Metodo di controllo di turbina basato su rapporto tra temperatura di scarico e pressione di turbina
EP2659095A4 (en) GAS TURBINE AND COOLING FLOW CIRCUIT THEREFOR
EP2426338A4 (en) PLATE-SHAPED ELEMENTS, METHOD FOR THE PRODUCTION THEREOF, GAS TURBINE BURNER AND GAS TURBINE
EP2333248A4 (en) GAS TURBINE AND OPERATING METHOD THEREFOR
EP2270337A4 (en) BLADE OF A GAS TURBINE ENGINE FOR AN AIRCRAFT, AND METHOD OF MANUFACTURING THE SAME
EP2351967A4 (en) CONNECTION STRUCTURE FOR COMBUSTION CHAMBER, COMBUSTION CHAMBER TERMINAL PIPE, METHOD FOR DESIGNING COMBUSTION CHAMBER TERMINAL PIPE, AND GAS TURBINE
EP2519723A4 (en) GAS TURBINE MOTOR AND HEAT EXCHANGE SYSTEM
DE102009038772A8 (de) Abgasnutzturbine für ein Turbo-Compound-System
EP2359082A4 (en) GAS TURBINE REGENERATING APPARATUS AND METHOD OF MANUFACTURING
GB0916696D0 (en) Exhaust gas recirculation cooling system, integrated exhaust gas recirculation coller and method of operating and engine with an exhaust gas recircualtion
BRPI1013738A2 (pt) válvula de recirculação de gás de escapamento e método de resfriamento.
GB2473651B (en) Gas turbine aircraft engines and operation thereof
EP2458167A4 (en) DEFROSTING TEMPERATURE MEASURING DEVICE AND DEFROSTING TEMPERATURE MEASURING PROCEDURE