NO20053516L - Fremgangsmate for korrigert parameterregulering for toakslet gassturbin. - Google Patents

Fremgangsmate for korrigert parameterregulering for toakslet gassturbin.

Info

Publication number
NO20053516L
NO20053516L NO20053516A NO20053516A NO20053516L NO 20053516 L NO20053516 L NO 20053516L NO 20053516 A NO20053516 A NO 20053516A NO 20053516 A NO20053516 A NO 20053516A NO 20053516 L NO20053516 L NO 20053516L
Authority
NO
Norway
Prior art keywords
regulates
control
gas turbine
turbine
procedure
Prior art date
Application number
NO20053516A
Other languages
English (en)
Norwegian (no)
Inventor
Stefano Groppi
Andrea Casoni
Alessandro Russo
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
Application filed by Nuovo Pignone Spa filed Critical Nuovo Pignone Spa
Publication of NO20053516L publication Critical patent/NO20053516L/no

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00Regulating or controlling by varying flow
    • F01D17/02Arrangement of sensing elements
    • F01D17/08Arrangement of sensing elements responsive to condition of working-fluid, e.g. pressure
    • F01D17/085Arrangement of sensing elements responsive to condition of working-fluid, e.g. pressure to temperature
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00Regulating or controlling by varying flow
    • F01D17/10Final actuators
    • F01D17/105Final actuators by passing part of the fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D21/00Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/12Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to temperature
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26Control of fuel supply
    • F02C9/28Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00Control
    • F05D2270/01Purpose of the control system
    • F05D2270/08Purpose of the control system to produce clean exhaust gases
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00Control
    • F05D2270/01Purpose of the control system
    • F05D2270/11Purpose of the control system to prolong engine life
    • F05D2270/112Purpose of the control system to prolong engine life by limiting temperatures
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00Control
    • F05D2270/30Control parameters, e.g. input parameters
    • F05D2270/303Temperature

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Control Of Turbines (AREA)
  • Supercharger (AREA)
NO20053516A 2002-12-17 2005-07-18 Fremgangsmate for korrigert parameterregulering for toakslet gassturbin. NO20053516L (no)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IT002660A ITMI20022660A1 (it) 2002-12-17 2002-12-17 Metodo di controllo a parametri per una turbina a gas a doppio albero.
PCT/EP2003/014174 WO2004055340A1 (fr) 2002-12-17 2003-12-10 Procede de commande de parametres corriges destine a une turbine a gaz a deux corps

Publications (1)

Publication Number Publication Date
NO20053516L true NO20053516L (no) 2005-07-18

Family

ID=32587867

Family Applications (1)

Application Number Title Priority Date Filing Date
NO20053516A NO20053516L (no) 2002-12-17 2005-07-18 Fremgangsmate for korrigert parameterregulering for toakslet gassturbin.

Country Status (10)

Country Link
US (1) US7634914B2 (fr)
EP (1) EP1581732B1 (fr)
JP (1) JP4546836B2 (fr)
KR (1) KR101034921B1 (fr)
CN (2) CN101187317B (fr)
AU (1) AU2003296644A1 (fr)
DE (1) DE60332557D1 (fr)
IT (1) ITMI20022660A1 (fr)
NO (1) NO20053516L (fr)
WO (1) WO2004055340A1 (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7577549B2 (en) * 2005-07-18 2009-08-18 General Electric Company System and method for trending exhaust gas temperature in a turbine engine
US7549292B2 (en) * 2005-10-03 2009-06-23 General Electric Company Method of controlling bypass air split to gas turbine combustor
US9115648B2 (en) * 2009-04-10 2015-08-25 General Electric Company Corrected megawatt backup curve methodology
IT1396514B1 (it) * 2009-11-27 2012-12-14 Nuovo Pignone Spa Metodo di controllo di turbina basato su rapporto tra temperatura di scarico e pressione di turbina
CN102563805B (zh) * 2011-12-22 2013-11-27 广东美的制冷设备有限公司 推算空调器的压缩机排气温度的控制方法
JP6134616B2 (ja) * 2013-09-06 2017-05-24 三菱日立パワーシステムズ株式会社 2軸ガスタービン
CN107882641B (zh) * 2017-10-11 2019-10-18 中国航发西安动力控制科技有限公司 一种双转子发动机的控制方法

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1231369A (en) * 1912-07-17 1917-06-26 Andrew J Johnson Burner.
US4314441A (en) * 1977-07-22 1982-02-09 Westinghouse Electric Corp. Gas turbine power plant control apparatus including an ambient temperature responsive control system
US4809497A (en) * 1983-06-15 1989-03-07 Sunstrand Corporation Gas turbine engine/load compressor power plants
JP3039947B2 (ja) * 1990-03-19 2000-05-08 株式会社日立製作所 ガスタービンの燃料制御装置
JPH07189746A (ja) * 1993-12-28 1995-07-28 Hitachi Ltd ガスタービン燃焼器の制御方法
US5622042A (en) * 1995-02-27 1997-04-22 Compressor Controls Corporation Method for predicting and using the exhaust gas temperatures for control of two and three shaft gas turbines
JPH11159756A (ja) * 1997-12-01 1999-06-15 Mitsubishi Heavy Ind Ltd 油焚dln燃焼器の水噴射制御装置
JPH11343868A (ja) * 1998-06-02 1999-12-14 Hitachi Ltd ガスタービン制御装置
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
JP2002259505A (ja) * 2001-02-27 2002-09-13 Hitachi Ltd 発電設備のデータ提供システム
JP2003206749A (ja) * 2002-01-17 2003-07-25 Mitsubishi Heavy Ind Ltd タービン設備及びその運転方法

Also Published As

Publication number Publication date
US20060242963A1 (en) 2006-11-02
CN101187317A (zh) 2008-05-28
JP4546836B2 (ja) 2010-09-22
KR20050086916A (ko) 2005-08-30
DE60332557D1 (de) 2010-06-24
AU2003296644A1 (en) 2004-07-09
KR101034921B1 (ko) 2011-05-17
EP1581732A1 (fr) 2005-10-05
ITMI20022660A1 (it) 2004-06-18
WO2004055340A1 (fr) 2004-07-01
JP2006509957A (ja) 2006-03-23
CN101187317B (zh) 2012-05-30
US7634914B2 (en) 2009-12-22
CN1745233A (zh) 2006-03-08
EP1581732B1 (fr) 2010-05-12
CN100347427C (zh) 2007-11-07

Similar Documents

Publication Publication Date Title
NO20053516L (no) Fremgangsmate for korrigert parameterregulering for toakslet gassturbin.
WO2008123904A3 (fr) Frein moteur pour co-réduction de chargement partiel
CA2451049A1 (fr) Controle de la temperature de combustion d'une turbine a gaz par prelevement d'air sur compresseur
ES2312098T3 (es) Procedimiento de valoracion de las fugas de productos en los sistemas de hermeticidad de los compresores por recuperacion y reciclado como combustible.
US6792756B2 (en) Gas supply control device for a gas storage power plant
CA2408704A1 (fr) Methode et dispositif de commande de la pression du carburant dans une turbine a gaz
EP1382910A3 (fr) Dispositif de commande pour brûleur à gaz
EP1063402A3 (fr) Méthode d'operation optimalisé pour une turbine à gaz industrielle
NO20063395L (no) Teknisk kraftanlegg med sekvensiell forbrenning og reduserte utslipp av CO2, og en fremgangsmate for drift av et anlegg av denne type
EP1746347A3 (fr) Procédé et système pour une chambre à combustion étagée
MY156015A (en) Exhaust temperature based mode control method for gas turbine and gas turbine
EP1788210A3 (fr) Procédé et appareil de commande de gaz d'échappement à l'aide d'un brûleur alimenté en carburant d'un assemblage de diminution d'émission
WO2006107828A3 (fr) Systeme de regulation des gaz a ailette toroidale d'intersection
RU2012136111A (ru) Способ эксплуатации газотурбинной установки и газотурбинная установка для реализации данного способа
RU2008135804A (ru) Газотурбинная система и способ ее эксплуатации
WO2009060889A1 (fr) Dispositif de commande de fonctionnement et procédé de commande de fonctionnement d'une turbine à gaz
EP1770331A3 (fr) Procédé pour contrôler la partition de l'air de dérivation vers la chambre de combustion de turbine
ATE449242T1 (de) Sequentielles steuerventil
WO2007031839A3 (fr) Moteur à combustion interne et procédé de commande associé
US20140123651A1 (en) System for providing fuel to a combustor assembly in a gas turbine engine
EP2654116A4 (fr) Système de génération d'énergie et son procédé de fonctionnement
DE60201435D1 (de) Drosselklappeanordnung
NO20072073L (no) Fremgangsmate for konsentrering av karbondioksyd som er tilstede i avgasser fra et kraftgenereringsanlegg
WO2004086547A3 (fr) Systeme d'humidification de gaz d'entree cathode et procede pour un systeme de pile a combustible
US20150345393A1 (en) Systems and methods for utilizing gas turbine compartment ventilation discharge air

Legal Events

Date Code Title Description
FC2A Withdrawal, rejection or dismissal of laid open patent application