DE60239652D1 - Vorrichtung und Methode um das Erlöschen einer Turbinenbrennkammerflamme festzustellen - Google Patents

Vorrichtung und Methode um das Erlöschen einer Turbinenbrennkammerflamme festzustellen

Info

Publication number
DE60239652D1
DE60239652D1 DE60239652T DE60239652T DE60239652D1 DE 60239652 D1 DE60239652 D1 DE 60239652D1 DE 60239652 T DE60239652 T DE 60239652T DE 60239652 T DE60239652 T DE 60239652T DE 60239652 D1 DE60239652 D1 DE 60239652D1
Authority
DE
Germany
Prior art keywords
extinction
determining
turbine combustor
combustor flame
flame
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
DE60239652T
Other languages
German (de)
English (en)
Inventor
Peter Thomas Harrison
Kail Lester Linebrink
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of DE60239652D1 publication Critical patent/DE60239652D1/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
    • 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
    • F02C7/262—Restarting after flame-out
    • 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
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N5/00—Systems for controlling combustion
    • F23N5/24—Preventing development of abnormal or undesired conditions, i.e. safety arrangements
    • 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
    • F05D2270/09—Purpose of the control system to cope with emergencies
    • F05D2270/092—Purpose of the control system to cope with emergencies in particular blow-out and relight
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N2241/00—Applications
    • F23N2241/20—Gas turbines
    • 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
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
DE60239652T 2001-05-17 2002-05-15 Vorrichtung und Methode um das Erlöschen einer Turbinenbrennkammerflamme festzustellen Expired - Lifetime DE60239652D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/859,612 US6442943B1 (en) 2001-05-17 2001-05-17 Methods and apparatus for detecting turbine engine flameout

Publications (1)

Publication Number Publication Date
DE60239652D1 true DE60239652D1 (de) 2011-05-19

Family

ID=25331330

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60239652T Expired - Lifetime DE60239652D1 (de) 2001-05-17 2002-05-15 Vorrichtung und Methode um das Erlöschen einer Turbinenbrennkammerflamme festzustellen

Country Status (4)

Country Link
US (1) US6442943B1 (https=)
EP (1) EP1258617B1 (https=)
JP (1) JP4113728B2 (https=)
DE (1) DE60239652D1 (https=)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6978597B2 (en) * 2002-03-20 2005-12-27 Ebara Corporation Flame detecting apparatus for gas turbine
US7386982B2 (en) * 2004-10-26 2008-06-17 General Electric Company Method and system for detecting ignition failure in a gas turbine engine
EP1953454A1 (en) * 2007-01-30 2008-08-06 Siemens Aktiengesellschaft Method of detecting a partial flame failure in a gas turbine engine and a gas turbine engine
US7902999B2 (en) * 2008-04-18 2011-03-08 Honeywell International Inc. Gas turbine engine rotor lock prevention system and method
US8151573B2 (en) * 2008-11-06 2012-04-10 Honeywell International Inc. Turbomachine flameout confirmation
FR2951540B1 (fr) * 2009-10-19 2012-06-01 Turbomeca Test de non-extinction pour chambre de combustion de turbomachine
US8457835B2 (en) 2011-04-08 2013-06-04 General Electric Company System and method for use in evaluating an operation of a combustion machine
CN103089454B (zh) * 2013-02-04 2015-07-15 哈尔滨东安发动机（集团）有限公司 微型燃气轮机数字式控制装置
CN103114914B (zh) * 2013-02-04 2015-10-28 哈尔滨东安发动机（集团）有限公司 微型燃气轮机的控制方法
WO2015031318A1 (en) * 2013-08-27 2015-03-05 United Technologies Corporation Gas turbine flameout detection
US10371002B2 (en) * 2016-06-14 2019-08-06 General Electric Company Control system for a gas turbine engine
IT201700028052A1 (it) * 2017-03-14 2018-09-14 Nuovo Pignone Tecnologie Srl Metodo per rilevare estinzione di fiamma in un bruciatore e sistema a turbina
US11397135B2 (en) 2017-03-14 2022-07-26 General Electric Company Method of detecting flameout in a combustor and turbine system
US11421601B2 (en) 2019-03-28 2022-08-23 Woodward, Inc. Second stage combustion for igniter
WO2021262853A1 (en) * 2020-06-23 2021-12-30 Woodward, Inc. Ignition system for power generation engine

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1415681A (en) * 1972-06-24 1975-11-26 Rolls Royce Flame-out control in gas turbine engine
US4044554A (en) 1976-07-19 1977-08-30 General Motors Corporation Gas turbine engine fuel control
US4783957A (en) 1986-12-23 1988-11-15 Sundstrand Corporation Fuel control circuit for a turbine engine
US5235802A (en) 1991-04-18 1993-08-17 United Technologies Corporation Flame failure detection method
US5170621A (en) 1991-04-18 1992-12-15 United Technologies Corporation Flame failure detection
US5551227A (en) * 1994-12-22 1996-09-03 General Electric Company System and method of detecting partial flame out in a gas turbine engine combustor
US5581995A (en) * 1995-03-14 1996-12-10 United Technologies Corporation Method and apparatus for detecting burner blowout
US5828797A (en) 1996-06-19 1998-10-27 Meggitt Avionics, Inc. Fiber optic linked flame sensor
US5961314A (en) 1997-05-06 1999-10-05 Rosemount Aerospace Inc. Apparatus for detecting flame conditions in combustion systems

Also Published As

Publication number Publication date
EP1258617A2 (en) 2002-11-20
JP4113728B2 (ja) 2008-07-09
EP1258617A3 (en) 2009-03-25
JP2003003864A (ja) 2003-01-08
EP1258617B1 (en) 2011-04-06
US6442943B1 (en) 2002-09-03

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