GB8329218D0 - Reheat combustion system for gas turbine engine - Google Patents

Reheat combustion system for gas turbine engine

Info

Publication number
GB8329218D0
GB8329218D0 GB838329218A GB8329218A GB8329218D0 GB 8329218 D0 GB8329218 D0 GB 8329218D0 GB 838329218 A GB838329218 A GB 838329218A GB 8329218 A GB8329218 A GB 8329218A GB 8329218 D0 GB8329218 D0 GB 8329218D0
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
combustion system
reheat combustion
reheat
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.)
Pending
Application number
GB838329218A
Other languages
English (en)
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.)
FFOWCS WILLIAMS J E
Original Assignee
FFOWCS WILLIAMS J E
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 FFOWCS WILLIAMS J E filed Critical FFOWCS WILLIAMS J E
Priority to GB838329218A priority Critical patent/GB8329218D0/en
Publication of GB8329218D0 publication Critical patent/GB8329218D0/en
Priority to GB08426577A priority patent/GB2165964B/en
Priority to US06/665,154 priority patent/US4557106A/en
Priority to DE19843439903 priority patent/DE3439903A1/de
Priority to FR8416693A priority patent/FR2554170B1/fr
Priority to JP59232268A priority patent/JPS60111027A/ja
Priority to IT23443/84A priority patent/IT1178620B/it
Pending legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M20/00—Details of combustion chambers, not otherwise provided for, e.g. means for storing heat from flames
    • F23M20/005—Noise absorbing means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N5/00—Systems for controlling combustion
    • F23N5/16—Systems for controlling combustion using noise-sensitive detectors
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
    • 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
    • F05D2260/00—Function
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise
    • F05D2260/962—Preventing, counteracting or reducing vibration or noise by means of "anti-noise"
    • 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
    • F05D2270/14—Purpose of the control system to control thermoacoustic behaviour in the combustion chambers
    • 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
    • F23R2900/00013—Reducing thermo-acoustic vibrations by active means
    • 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
    • F23R2900/00014—Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators
    • 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 Combustion (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
GB838329218A 1983-11-02 1983-11-02 Reheat combustion system for gas turbine engine Pending GB8329218D0 (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
GB838329218A GB8329218D0 (en) 1983-11-02 1983-11-02 Reheat combustion system for gas turbine engine
GB08426577A GB2165964B (en) 1983-11-02 1984-10-19 Combustion system for a gas turbine engine
US06/665,154 US4557106A (en) 1983-11-02 1984-10-26 Combustion system for a gas turbine engine
DE19843439903 DE3439903A1 (de) 1983-11-02 1984-10-31 Verbrennungssystem fuer ein gasturbinentriebwerk
FR8416693A FR2554170B1 (fr) 1983-11-02 1984-10-31 Systeme de combustion pour moteur a turbine a gaz
JP59232268A JPS60111027A (ja) 1983-11-02 1984-11-02 ガスタービン・エンジンの燃焼系
IT23443/84A IT1178620B (it) 1983-11-02 1984-11-02 Complesso di combustione per motore a turbina a gas

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB838329218A GB8329218D0 (en) 1983-11-02 1983-11-02 Reheat combustion system for gas turbine engine

Publications (1)

Publication Number Publication Date
GB8329218D0 true GB8329218D0 (en) 1983-12-07

Family

ID=10551095

Family Applications (2)

Application Number Title Priority Date Filing Date
GB838329218A Pending GB8329218D0 (en) 1983-11-02 1983-11-02 Reheat combustion system for gas turbine engine
GB08426577A Expired GB2165964B (en) 1983-11-02 1984-10-19 Combustion system for a gas turbine engine

Family Applications After (1)

Application Number Title Priority Date Filing Date
GB08426577A Expired GB2165964B (en) 1983-11-02 1984-10-19 Combustion system for a gas turbine engine

Country Status (6)

Country Link
US (1) US4557106A (enExample)
JP (1) JPS60111027A (enExample)
DE (1) DE3439903A1 (enExample)
FR (1) FR2554170B1 (enExample)
GB (2) GB8329218D0 (enExample)
IT (1) IT1178620B (enExample)

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US5117642A (en) * 1989-12-18 1992-06-02 Kabushiki Kaisha Toshiba Low noise refrigerator and noise control method thereof
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JPH07501137A (ja) * 1991-11-15 1995-02-02 シーメンス アクチエンゲゼルシヤフト ガスタービン設備の燃焼室内の燃焼振動抑制装置
US5287697A (en) * 1992-01-02 1994-02-22 General Electric Company Variable area bypass injector seal
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DE69524883T2 (de) * 1994-10-13 2002-09-19 The Boeing Co., Seattle System zur lärmverringerung eines düsentriebwerks mittels elektropneumatischer wandler
US5575144A (en) * 1994-11-28 1996-11-19 General Electric Company System and method for actively controlling pressure pulses in a gas turbine engine combustor
US5719791A (en) * 1995-03-17 1998-02-17 Georgia Tech Research Corporation Methods, apparatus and systems for real time identification and control of modes of oscillation
FR2732407B1 (fr) * 1995-03-29 1997-04-30 Snecma Procede pour eviter les instabilites dues a la combustion dans un turboreacteur
US5685157A (en) * 1995-05-26 1997-11-11 General Electric Company Acoustic damper for a gas turbine engine combustor
DE59711378D1 (de) * 1997-11-24 2004-04-08 Alstom Switzerland Ltd Verfahren zum Minimieren thermoakustischer Schwingungen in Gasturbinenbrennkammern
EP0918194A1 (de) * 1997-11-24 1999-05-26 Abb Research Ltd. Verfahren zur Auslegung eines Verbrennungssystems und Verfahren und Vorrichtung zur Bestimmung von Brennereigenschaften
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DE59810032D1 (de) * 1998-09-10 2003-12-04 Alstom Switzerland Ltd Verfahren zum Minimieren thermoakustischer Schwingungen in Gasturbinenbrennkammern
DE59810033D1 (de) * 1998-09-16 2003-12-04 Alstom Switzerland Ltd Verfahren zum Minimieren thermoakustischer Schwingungen in Gasturbinenbrennkammern
US6354071B2 (en) * 1998-09-25 2002-03-12 General Electric Company Measurement method for detecting and quantifying combustor dynamic pressures
DE19928226A1 (de) * 1999-05-07 2001-02-01 Abb Alstom Power Ch Ag Verfahren zur Unterdrückung bzw. Kontrolle von thermoakustischen Schwingungen in einem Verbrennungs-System sowie Verbrennungssystem zur Durchführung des Verfahrens
DE10000415A1 (de) * 2000-01-07 2001-09-06 Alstom Power Schweiz Ag Baden Verfahren und Vorrichtung zur Unterdrückung von Strömungswirbeln innerhalb einer Strömungskraftmaschine
US6530228B2 (en) * 2001-05-07 2003-03-11 The United States Of America As Represented By The Secretary Of The Navy Method and device for modulation of a flame
US7017415B2 (en) * 2001-09-27 2006-03-28 Siemens Westinghouse Power Corporation Apparatus for sensing pressure fluctuations in a hostile environment
US6843061B2 (en) 2002-02-15 2005-01-18 Siemens Westinghouse Power Corporation Gas turbine with flexible combustion sensor connection
DE10213682A1 (de) * 2002-03-27 2003-10-09 Alstom Switzerland Ltd Verfahren und Vorrichtung zur Kontrolle von thermoakustischen Instabilitäten bzw. Schwingungen in einem Verbrennungssystem
US6742341B2 (en) * 2002-07-16 2004-06-01 Siemens Westinghouse Power Corporation Automatic combustion control for a gas turbine
US6640549B1 (en) * 2002-12-03 2003-11-04 The United States Of America As Represented By The Secretary Of The Navy Method and device for modulation of a flame
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US20140360203A1 (en) * 2011-12-29 2014-12-11 Delafield Pty Ltd Rijke type combustion arrangement and method
US9255835B2 (en) 2012-08-22 2016-02-09 Siemens Energy, Inc. System for remote vibration detection on combustor basket and transition in gas turbines
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Also Published As

Publication number Publication date
FR2554170B1 (fr) 1987-11-20
GB2165964B (en) 1987-11-11
US4557106A (en) 1985-12-10
GB2165964A (en) 1986-04-23
JPS60111027A (ja) 1985-06-17
JPH0472982B2 (enExample) 1992-11-19
GB8426577D0 (en) 1984-11-28
DE3439903A1 (de) 1985-05-09
FR2554170A1 (fr) 1985-05-03
IT1178620B (it) 1987-09-09
IT8423443A0 (it) 1984-11-02
IT8423443A1 (it) 1986-05-02

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