ATE196342T1 - Die kraftstoffzufuhr für eine gasturbine wird in abhängigkeit von der berechneten turbinenauslasstemperatur geregelt - Google Patents

Die kraftstoffzufuhr für eine gasturbine wird in abhängigkeit von der berechneten turbinenauslasstemperatur geregelt

Info

Publication number
ATE196342T1
ATE196342T1 AT96300839T AT96300839T ATE196342T1 AT E196342 T1 ATE196342 T1 AT E196342T1 AT 96300839 T AT96300839 T AT 96300839T AT 96300839 T AT96300839 T AT 96300839T AT E196342 T1 ATE196342 T1 AT E196342T1
Authority
AT
Austria
Prior art keywords
temperature
egt
turbine
combustion chamber
measured
Prior art date
Application number
AT96300839T
Other languages
English (en)
Inventor
Saul Mirsky
Naum Staroselsky
Original Assignee
Compressor Controls Corp
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 Compressor Controls Corp filed Critical Compressor Controls Corp
Application granted granted Critical
Publication of ATE196342T1 publication Critical patent/ATE196342T1/de

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
    • 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
    • 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
    • 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
    • F05D2270/11—Purpose of the control system to prolong engine life
    • F05D2270/112—Purpose of the control system to prolong engine life by limiting temperatures

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Blast Furnaces (AREA)
AT96300839T 1995-02-27 1996-02-07 Die kraftstoffzufuhr für eine gasturbine wird in abhängigkeit von der berechneten turbinenauslasstemperatur geregelt ATE196342T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/395,599 US5622042A (en) 1995-02-27 1995-02-27 Method for predicting and using the exhaust gas temperatures for control of two and three shaft gas turbines

Publications (1)

Publication Number Publication Date
ATE196342T1 true ATE196342T1 (de) 2000-09-15

Family

ID=23563702

Family Applications (1)

Application Number Title Priority Date Filing Date
AT96300839T ATE196342T1 (de) 1995-02-27 1996-02-07 Die kraftstoffzufuhr für eine gasturbine wird in abhängigkeit von der berechneten turbinenauslasstemperatur geregelt

Country Status (7)

Country Link
US (1) US5622042A (de)
EP (1) EP0728919B1 (de)
AT (1) ATE196342T1 (de)
CA (1) CA2168422A1 (de)
DE (1) DE69610233T2 (de)
NO (1) NO960279L (de)
RU (1) RU2170358C2 (de)

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US6633828B2 (en) 2001-03-21 2003-10-14 Honeywell International Inc. Speed signal variance detection fault system and method
JP2002309963A (ja) * 2001-04-17 2002-10-23 Mitsubishi Heavy Ind Ltd ガスタービンプラント
US6952639B2 (en) * 2002-11-12 2005-10-04 General Electric Company Method and system for temperature estimation of gas turbine combustion cans
US20040114666A1 (en) * 2002-12-17 2004-06-17 Hardwicke Canan Uslu Temperature sensing structure, method of making the structure, gas turbine engine and method of controlling temperature
ITMI20022660A1 (it) * 2002-12-17 2004-06-18 Nuovo Pignone Spa Metodo di controllo a parametri per una turbina a gas a doppio albero.
US6912856B2 (en) * 2003-06-23 2005-07-05 General Electric Company Method and system for controlling gas turbine by adjusting target exhaust temperature
US7246002B2 (en) * 2003-11-20 2007-07-17 General Electric Company Method for controlling fuel splits to gas turbine combustor
EP1655590B1 (de) * 2004-11-09 2016-02-03 Alstom Technology Ltd Verfahren zur Bestimmung einer über einen Strömungsquerschnitt massengemittelten Temperatur einer Gasströmung in einer Gasturbine
FR2890939B1 (fr) * 2005-09-22 2007-10-19 Airbus Sas Procede et dispositif pour fournir a un pilote d'un aeronef multimoteur des informations relatives auxdits moteurs
RU2305788C2 (ru) * 2005-10-24 2007-09-10 Открытое акционерное общество "Авиадвигатель" Способ аварийной защиты газотурбинного двигателя при отказах и неисправностях
RU2315885C1 (ru) * 2006-03-24 2008-01-27 Открытое акционерное общество "Авиадвигатель" Способ защиты газотурбинного двигателя от перегрева
RU2316663C1 (ru) * 2006-06-13 2008-02-10 Открытое акционерное общество "Авиадвигатель" Способ дозирования топлива на запуске газотурбинного двигателя
RU2329388C1 (ru) * 2006-10-05 2008-07-20 Открытое акционерное общество "СТАР" Способ защиты газотурбинного двигателя
RU2444640C2 (ru) * 2007-08-01 2012-03-10 Ансальдо Энергия С.П.А. Устройство и способ регулирования температуры выхлопа газовой турбины
RU2341690C1 (ru) * 2007-10-02 2008-12-20 Закрытое Акционерное Общество "Система Комплекс" Способ регулирования технологических параметров энергоустановки
RU2430252C1 (ru) * 2010-03-23 2011-09-27 Закрытое акционерное общество "Научно-производственная фирма "Система-Сервис" Способ определения погасания камеры сгорания газотурбинных двигателей
EP2562369B1 (de) * 2011-08-22 2015-01-14 Alstom Technology Ltd Verfahren zum Betrieb einer Gasturbinenanlage sowie Gasturbinenanlage zur Durchführung des Verfahrens
GB201219815D0 (en) * 2012-11-05 2012-12-19 Rolls Royce Plc Engine control parameter trimming
EP2840245A1 (de) * 2013-08-20 2015-02-25 Alstom Technology Ltd Verfahren zur Steuerung einer Gasturbinenbaugruppe
RU2592360C2 (ru) * 2014-11-27 2016-07-20 Открытое акционерное общество "Уфимское моторостроительное производственное объединение" ОАО УМПО Способ регулирования авиационного турбореактивного двигателя

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US2809492A (en) * 1952-12-23 1957-10-15 Simmonds Aerocessories Inc Apparatus for measuring and/or controlling fuel/air ratio of gas turbines without direct gravimetric fuel metering
US3379584A (en) * 1964-09-04 1968-04-23 Texas Instruments Inc Semiconductor wafer with at least one epitaxial layer and methods of making same
US3377848A (en) * 1966-08-22 1968-04-16 Gen Electric Temperature indicating means for gas turbine engines
US3667218A (en) * 1970-03-27 1972-06-06 Gen Electric Gas turbine temperature adaptive control
US3789665A (en) * 1972-02-22 1974-02-05 Avco Corp Inferred measurement of the turbine inlet temperature of a gas turbine engine
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Also Published As

Publication number Publication date
DE69610233D1 (de) 2000-10-19
EP0728919B1 (de) 2000-09-13
NO960279D0 (no) 1996-01-24
US5622042A (en) 1997-04-22
NO960279L (no) 1996-08-28
EP0728919A1 (de) 1996-08-28
RU2170358C2 (ru) 2001-07-10
CA2168422A1 (en) 1996-08-28
DE69610233T2 (de) 2001-01-25

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