IT8423443A0 - Complesso di combustione per motore a turbina a gas. - Google Patents

Complesso di combustione per motore a turbina a gas.

Info

Publication number
IT8423443A0
IT8423443A0 IT8423443A IT2344384A IT8423443A0 IT 8423443 A0 IT8423443 A0 IT 8423443A0 IT 8423443 A IT8423443 A IT 8423443A IT 2344384 A IT2344384 A IT 2344384A IT 8423443 A0 IT8423443 A0 IT 8423443A0
Authority
IT
Italy
Prior art keywords
gas turbine
turbine engine
combustion
complex
combustion complex
Prior art date
Application number
IT8423443A
Other languages
English (en)
Other versions
IT8423443A1 (it
IT1178620B (it
Inventor
John Eirwyn Ffowcs Williams
Philip Joseph Dines
Maria Anna Heckl
Original Assignee
Hecki Maria Anna
John Eirwyn Ffowcs Williams
Dines Philip
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 Hecki Maria Anna, John Eirwyn Ffowcs Williams, Dines Philip filed Critical Hecki Maria Anna
Publication of IT8423443A0 publication Critical patent/IT8423443A0/it
Publication of IT8423443A1 publication Critical patent/IT8423443A1/it
Application granted granted Critical
Publication of IT1178620B publication Critical patent/IT1178620B/it

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)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Control Of Combustion (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
IT23443/84A 1983-11-02 1984-11-02 Complesso di combustione per motore a turbina a gas IT1178620B (it)

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 (3)

Publication Number Publication Date
IT8423443A0 true IT8423443A0 (it) 1984-11-02
IT8423443A1 IT8423443A1 (it) 1986-05-02
IT1178620B IT1178620B (it) 1987-09-09

Family

ID=10551095

Family Applications (1)

Application Number Title Priority Date Filing Date
IT23443/84A IT1178620B (it) 1983-11-02 1984-11-02 Complesso di combustione per motore a turbina a gas

Country Status (6)

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

Families Citing this family (57)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5082421A (en) * 1986-04-28 1992-01-21 Rolls-Royce Plc Active control of unsteady motion phenomena in turbomachinery
GB8610297D0 (en) * 1986-04-28 1986-10-01 Rolls Royce Turbomachinery
GB8708595D0 (en) * 1987-04-10 1987-05-13 Rolls Royce Plc Gas turbine fuel control system
US4967550A (en) * 1987-04-28 1990-11-06 Rolls-Royce Plc Active control of unsteady motion phenomena in turbomachinery
US5127235A (en) * 1989-12-18 1992-07-07 Kabushiki Kaisha Toshiba Low noise refrigerator and noise control method thereof
US5117642A (en) * 1989-12-18 1992-06-02 Kabushiki Kaisha Toshiba Low noise refrigerator and noise control method thereof
GB2239961A (en) * 1990-01-02 1991-07-17 Gen Electric Control of combustion-induced instabilities
GB9003959D0 (en) * 1990-02-21 1990-04-18 Ross Colin F Active control of internal combustion engine performance
WO1993010401A1 (de) * 1991-11-15 1993-05-27 Siemens Aktiengesellschaft Einrichtung zur unterdrückung von verbrennungsschwingungen in einer brennkammer einer gasturbinenanlage
US5287697A (en) * 1992-01-02 1994-02-22 General Electric Company Variable area bypass injector seal
US5609136A (en) * 1994-06-28 1997-03-11 Cummins Engine Company, Inc. Model predictive control for HPI closed-loop fuel pressure control system
EP0786131B1 (en) * 1994-10-13 2002-01-02 The Boeing Company Jet engine fan noise reduction system utilizing electro pneumatic transducers
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
EP0918152A1 (de) * 1997-11-24 1999-05-26 Abb Research Ltd. Verfahren und Vorrichtung zur Kontrolle thermoakustischer Schwingungen in einem Verbrennungssystem
EP0918153B1 (de) * 1997-11-24 2004-03-03 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
EP0985810B1 (de) 1998-09-10 2003-10-29 ALSTOM (Switzerland) Ltd Verfahren zum Minimieren thermoakustischer Schwingungen in Gasturbinenbrennkammern
EP0987495B1 (de) * 1998-09-16 2003-10-29 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
US6694832B1 (en) 2003-02-27 2004-02-24 General Electric Company Kit and method for setting probe depth
US6978680B2 (en) * 2003-02-27 2005-12-27 General Electric Company Dynamic pressure probe holder and method of obtaining a dynamic pressure signal
US6976351B2 (en) * 2003-04-04 2005-12-20 General Electric Company Methods and apparatus for monitoring gas turbine combustion dynamics
GB2407152A (en) * 2003-10-14 2005-04-20 Alstom Apparatus and method for testing combustion
US7334409B2 (en) * 2004-05-19 2008-02-26 Alltech, Inc. Retractable afterburner for jet engine
US7377114B1 (en) * 2004-06-02 2008-05-27 Kevin P Pearce Turbine engine pulsed fuel injection utilizing stagger injector operation
US8768602B2 (en) * 2004-10-20 2014-07-01 Yamaha Hatsudoki Kabushiki Kaisha Straddle-type vehicle and combustion controller for straddle-type vehicle
WO2006059982A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Remote engine fuel control and electronic engine control for turbine engine
US20060283190A1 (en) * 2005-06-16 2006-12-21 Pratt & Whitney Canada Corp. Engine status detection with external microphone
US20070255563A1 (en) * 2006-04-28 2007-11-01 Pratt & Whitney Canada Corp. Machine prognostics and health monitoring using speech recognition techniques
US20080127728A1 (en) * 2006-11-30 2008-06-05 General Electric Company Mechanical response based detonation velocity measurement system
GB0710153D0 (en) * 2007-05-26 2007-07-04 Rolls Royce Plc Method and apparatus for suppressing aeroengine contrails
US8028512B2 (en) 2007-11-28 2011-10-04 Solar Turbines Inc. Active combustion control for a turbine engine
GB0823085D0 (en) * 2008-12-19 2009-01-28 Rolls Royce Plc Combustor Rumble
GB201119036D0 (en) * 2011-11-03 2011-12-14 Univ Oxford Brookes A method of controlling a dynamic physical system
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
US9255526B2 (en) 2012-08-23 2016-02-09 Siemens Energy, Inc. System and method for on line monitoring within a gas turbine combustor section
EP3090144A4 (en) * 2013-12-12 2017-09-27 Morris, Robert, J. Active flutter control of variable pitch blades
US9885609B2 (en) * 2014-05-23 2018-02-06 United Technologies Corporation Gas turbine engine optical system
CN105631215B (zh) * 2015-12-29 2018-07-13 中国航空工业集团公司沈阳发动机设计研究所 一种航空发动机加力燃烧室供油量的计算方法
GB2558228B (en) 2016-12-22 2020-05-20 Rolls Royce Plc Aircraft electrically-assisted propulsion control system
US11092083B2 (en) * 2017-02-10 2021-08-17 General Electric Company Pressure sensor assembly for a turbine engine
US11421877B2 (en) * 2017-08-29 2022-08-23 General Electric Company Vibration control for a gas turbine engine
US11841139B2 (en) 2020-02-22 2023-12-12 Honeywell International Inc. Resonance prevention using combustor damping rates
CN114070904B (zh) 2020-07-30 2023-12-05 北京小米移动软件有限公司 电子设备
DE102022126449B3 (de) 2022-10-12 2024-02-08 Rocket Factory Augsburg AG Vorrichtung zur Steuerung eines Masseflusses und System mit einer Vorrichtung zur Steuerung eines Masseflusses

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3053047A (en) * 1953-05-27 1962-09-11 Bendix Corp Fuel feed and power control system for gas turbine engines
US2911788A (en) * 1956-12-14 1959-11-10 United Aircraft Corp Screech sensing device
US2941356A (en) * 1957-03-01 1960-06-21 United Aircraft Corp Variable pressure wave absorption for combustion chambers
US3245219A (en) * 1958-11-24 1966-04-12 Henry E Warden Stall-surge sonic sensor and control apparatus for turbo-compressor type gas engines
US3620013A (en) * 1969-10-31 1971-11-16 James H Rogers Noise abatement methods relating to flame and jet production and associated apparatus
US3936606A (en) * 1971-12-07 1976-02-03 Wanke Ronald L Acoustic abatement method and apparatus
GB1456018A (en) * 1972-11-24 1976-11-17 Nat Res Dev Active control of sound waves
GB1495015A (en) * 1975-09-01 1977-12-14 British Petroleum Co Monitoring and/or control of burners
US4083433A (en) * 1976-11-16 1978-04-11 Westinghouse Electric Corporation Active vibration damper with electrodynamic sensor and drive units
FR2490786A1 (fr) * 1980-09-25 1982-03-26 Centre Nat Rech Scient Procede de commande d'une flamme de combustion et sonde microphonique permettant sa mise en oeuvre
DE3209617C2 (de) * 1982-03-17 1985-10-10 Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt e.V., 5000 Köln Geräuscharme Turboarbeitsmaschine

Also Published As

Publication number Publication date
FR2554170B1 (fr) 1987-11-20
IT8423443A1 (it) 1986-05-02
JPH0472982B2 (it) 1992-11-19
GB2165964B (en) 1987-11-11
JPS60111027A (ja) 1985-06-17
DE3439903A1 (de) 1985-05-09
GB8329218D0 (en) 1983-12-07
IT1178620B (it) 1987-09-09
GB8426577D0 (en) 1984-11-28
GB2165964A (en) 1986-04-23
US4557106A (en) 1985-12-10
FR2554170A1 (fr) 1985-05-03

Similar Documents

Publication Publication Date Title
IT8423443A0 (it) Complesso di combustione per motore a turbina a gas.
IT8422791A0 (it) Combustore schermato specialmente per turbomotori a gas.
IT8321934A0 (it) Carburatore per turbomotore a gas.
IT8423428A0 (it) Turbocompressore a gas di scarico per un motore endotermico.
IT8020445A0 (it) Motore a turbina a gas.
BR8003008A (pt) Motor de turbina a gas
IT8019702A0 (it) Cappottatura di motore a turbina agas.
IT8420753A0 (it) Impianto di comando per motore a turbina a gas.
IT1142986B (it) Motore endotermico con un turbocompressore a gas di scarico
IT8222204A0 (it) Per turbomotori a gas.struttura di tenuta particolarmente
IT7921628A0 (it) Motore a turbina a gas.
IT7821288A0 (it) Motore per turbina a gas.
IT8124388A0 (it) Struttura di carcassa per motore di turbina a gas.
IT8119348A0 (it) Complesso di aspirazione per turbomotori a gas.
IT8321090A0 (it) Prediffusore per motori a turbina a gas.
IT8423829A0 (it) Pala per turbomotore a gas.
IT8321087A0 (it) Struttura di diffusione per un motore a turbina a gas.
IT8521926A0 (it) Ugello di scarico orientabile per un motore a turbina a gas.
IT8483636A0 (it) Comando accessorio per motore a turbina.
IT8025620A0 (it) Motore a turbina a gas modulare.
DE3585231D1 (de) Gasturbinenmotor.
IT1077139B (it) Impianto di accensione per motore a turbina a gas
IT8123606A0 (it) Ugello di combustibile per turbomotore a gas.
IT7927234A0 (it) Assieme di palette direttrici di distributore per motore a turbina a gas.
SE8402053L (sv) Avgasstyrning for en tvataktsforbrenningsmotor

Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19971031