DE60209928D1 - Verfahren zum starten einer gasturbine - Google Patents

Verfahren zum starten einer gasturbine

Info

Publication number
DE60209928D1
DE60209928D1 DE60209928T DE60209928T DE60209928D1 DE 60209928 D1 DE60209928 D1 DE 60209928D1 DE 60209928 T DE60209928 T DE 60209928T DE 60209928 T DE60209928 T DE 60209928T DE 60209928 D1 DE60209928 D1 DE 60209928D1
Authority
DE
Germany
Prior art keywords
starting
gas turbine
turbine
gas
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Lifetime
Application number
DE60209928T
Other languages
English (en)
Other versions
DE60209928T2 (de
Inventor
Richard O'connor
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Pratt and Whitney Canada Corp
Original Assignee
Pratt and Whitney Canada 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 Pratt and Whitney Canada Corp filed Critical Pratt and Whitney Canada Corp
Application granted granted Critical
Publication of DE60209928D1 publication Critical patent/DE60209928D1/de
Publication of DE60209928T2 publication Critical patent/DE60209928T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • 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
    • F02C7/26—Starting; Ignition
    • 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
    • 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
    • F05D2270/304—Spool rotational speed
DE60209928T 2001-12-14 2002-11-07 Verfahren zum starten einer gasturbine Expired - Lifetime DE60209928T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US16869 2001-12-14
US10/016,869 US6810676B2 (en) 2001-12-14 2001-12-14 Method of engine starting in a gas turbine engine
PCT/CA2002/001699 WO2003052250A1 (en) 2001-12-14 2002-11-07 Method of starting a gas turbine engine

Publications (2)

Publication Number Publication Date
DE60209928D1 true DE60209928D1 (de) 2006-05-11
DE60209928T2 DE60209928T2 (de) 2006-12-14

Family

ID=21779437

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60209928T Expired - Lifetime DE60209928T2 (de) 2001-12-14 2002-11-07 Verfahren zum starten einer gasturbine

Country Status (6)

Country Link
US (2) US6810676B2 (de)
EP (1) EP1454046B1 (de)
JP (1) JP4118811B2 (de)
CA (1) CA2466568C (de)
DE (1) DE60209928T2 (de)
WO (1) WO2003052250A1 (de)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6834226B2 (en) * 2002-09-13 2004-12-21 Elliott Energy Systems, Inc. Multiple control loop acceleration of turboalternator after reaching self-sustaining speed previous to reaching synchronous speed
JP4650785B2 (ja) * 2004-11-18 2011-03-16 株式会社Ｉｈｉ ガスタービンエンジンの燃料制御方法および装置
US7506517B2 (en) * 2004-11-23 2009-03-24 Honeywell International, Inc. System and method for turbine engine startup profile characterization
US8443583B2 (en) * 2006-06-15 2013-05-21 Indiana University Research And Technology Corp. Pilot fuel injection for a wave rotor engine
EP1956294A1 (de) * 2007-02-06 2008-08-13 Siemens Aktiengesellschaft Feuerungsanlage und Verfahren zum Betrieb einer Feuerungsanlage
US7840333B2 (en) * 2007-03-30 2010-11-23 Hamilton Sundstrand Corporation Event-driven starter controller
US7861534B2 (en) * 2007-05-03 2011-01-04 Pratt & Whitney Canada Corp. Method of starting turbine engine from low engine speed
US8297036B2 (en) * 2008-06-11 2012-10-30 United Technologies Corporation Method and apparatus for determining failures of gas shutoff valves in gas turbines
US8321120B2 (en) * 2009-01-16 2012-11-27 Honeywell International Inc. System and method for starting a gas turbine engine with inoperable exhaust gas turbine temperature sensor
US8467949B2 (en) * 2009-05-29 2013-06-18 Honeywell International Inc. Methods and systems for turbine line replaceable unit fault detection and isolation during engine startup
JP2011043136A (ja) * 2009-08-24 2011-03-03 Honda Motor Co Ltd ガスタービン・エンジンの始動時燃料制御装置
US8925328B2 (en) * 2009-10-26 2015-01-06 Siemens Energy, Inc. Gas turbine starting process
US8833085B2 (en) * 2010-01-27 2014-09-16 General Electric Company System and method for gas turbine startup control
US9086018B2 (en) * 2010-04-23 2015-07-21 Hamilton Sundstrand Corporation Starting a gas turbine engine to maintain a dwelling speed after light-off
US8355819B2 (en) 2010-10-05 2013-01-15 General Electric Company Method, apparatus and system for igniting wide range of turbine fuels
EP2442031A1 (de) * 2010-10-13 2012-04-18 Siemens Aktiengesellschaft Verbrennungsvorrichtung mit gepulstem Kraftstoffsplit
US9926848B2 (en) * 2011-01-06 2018-03-27 Hamilton Sundstand Corporation Turbomachine fuel delivery method and assembly
FR2970304B1 (fr) * 2011-01-11 2013-02-08 Turbomeca Procede de demarrage d'une turbomachine
US8467918B2 (en) * 2011-07-05 2013-06-18 Universal Avionics Systems Corporation Heuristic method for computing performance of an aircraft
US8666633B2 (en) 2012-02-07 2014-03-04 Honeywell International Inc. Engine systems with efficient start control logic
US9541005B2 (en) * 2012-09-28 2017-01-10 Pratt & Whitney Canada Corp. Adaptive fuel manifold filling function for improved engine start
US10641179B2 (en) 2016-11-07 2020-05-05 General Electric Company System and method for starting gas turbine engines
US10422287B2 (en) * 2017-03-20 2019-09-24 General Electric Company Systems and methods for closed loop control of OBB valve for power generation systems
US10801416B2 (en) 2017-05-03 2020-10-13 Pratt & Whitney Canada Corp. Method and system for setting fuel flow for engine start as a function of aircraft speed
US10352189B2 (en) 2017-05-10 2019-07-16 Pratt & Whitney Canada Corp. Method and system for setting an acceleration schedule for engine start
US11181274B2 (en) * 2017-08-21 2021-11-23 General Electric Company Combustion system and method for attenuation of combustion dynamics in a gas turbine engine
US11506076B2 (en) * 2020-01-23 2022-11-22 Pratt & Whitney Canada Corp. Methods and systems for starting an engine
DE102020116071A1 (de) 2020-06-18 2021-12-23 Prominent Gmbh Verfahren zum Steuern eines mit einer Dosierpumpe förderbaren Volumens
US11898500B2 (en) * 2020-12-22 2024-02-13 Textron Innovations Inc. Inlet configuration enabling rapid in-flight engine restart
US20230193834A1 (en) * 2021-12-21 2023-06-22 Rolls-Royce Plc Method of controlling an aircraft propulsion system with a variable inlet guide vane, and propulsion system with a variable inlet guide vane scheduling manager

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3059427A (en) * 1956-10-15 1962-10-23 Robert J Thorpe Apparatus for controlling the fuel supply to an internal combustion engine during starting
US3667218A (en) 1970-03-27 1972-06-06 Gen Electric Gas turbine temperature adaptive control
US3844112A (en) 1973-06-27 1974-10-29 Curtiss Wright Corp Gas turbine start-up fuel control system
US4044554A (en) 1976-07-19 1977-08-30 General Motors Corporation Gas turbine engine fuel control
US4350008A (en) 1979-12-26 1982-09-21 United Technologies Corporation Method of starting turbine engines
US4464895A (en) * 1982-05-26 1984-08-14 Chandler Evans Inc. Gas turbine engine starting technique and control
US4566266A (en) 1984-02-13 1986-01-28 Dresser Industries, Inc. Automatic temperature compensated fuel flow regulation
GB8911806D0 (en) 1989-05-23 1989-07-12 Rolls Royce Plc Gas turbine engine fuel control system with enhanced relight capability
US5107674A (en) 1990-03-30 1992-04-28 General Electric Company Control for a gas turbine engine
US5165223A (en) * 1990-12-10 1992-11-24 Sundstrand Corporation Process for starting a gas turbine and gas turbine
GB2260577B (en) 1991-10-16 1994-10-05 Rolls Royce Plc Gas turbine engine starting
DE4221805A1 (de) 1992-07-03 1994-01-05 Mak System Gmbh Verfahren und Einrichtung zum Starten einer Gasturbine
GB9410760D0 (en) 1994-05-27 1994-07-27 Rolls Royce Plc Gas turbine engine fuel control system
US5718111A (en) 1995-08-04 1998-02-17 Alliedsignal Inc. Fuzzy start logic for jet engines
US5907949A (en) * 1997-02-03 1999-06-01 United Technologies Corporation Starting fuel control method for a turbine engine
US6062016A (en) * 1997-04-21 2000-05-16 Capstone Turbine Corporation Gas turbine engine fixed speed light-off method
US6182438B1 (en) 1999-07-08 2001-02-06 Moog Inc. Method and apparatus for starting a gas turbine engine
US6810677B2 (en) * 2001-08-27 2004-11-02 Elliot Energy Systems, Inc. Method for gas turbine light-off

Also Published As

Publication number Publication date
CA2466568C (en) 2011-04-19
DE60209928T2 (de) 2006-12-14
EP1454046A1 (de) 2004-09-08
US6988368B2 (en) 2006-01-24
US6810676B2 (en) 2004-11-02
US20050028533A1 (en) 2005-02-10
CA2466568A1 (en) 2003-06-26
JP4118811B2 (ja) 2008-07-16
JP2005513319A (ja) 2005-05-12
WO2003052250A1 (en) 2003-06-26
EP1454046B1 (de) 2006-03-15
US20030110777A1 (en) 2003-06-19

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