IT1178620B - Complesso di combustione per motore a turbina a gas - Google Patents
Complesso di combustione per motore a turbina a gasInfo
- Publication number
- IT1178620B IT1178620B IT23443/84A IT2344384A IT1178620B IT 1178620 B IT1178620 B IT 1178620B IT 23443/84 A IT23443/84 A IT 23443/84A IT 2344384 A IT2344384 A IT 2344384A IT 1178620 B IT1178620 B IT 1178620B
- Authority
- IT
- Italy
- Prior art keywords
- gas turbine
- turbine engine
- combustion
- complex
- combustion complex
- Prior art date
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)
- Combined Controls Of Internal Combustion Engines (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
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 IT8423443A0 (it) | 1984-11-02 |
IT8423443A1 IT8423443A1 (it) | 1986-05-02 |
IT1178620B true 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)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB8610297D0 (en) * | 1986-04-28 | 1986-10-01 | Rolls Royce | Turbomachinery |
US5082421A (en) * | 1986-04-28 | 1992-01-21 | Rolls-Royce Plc | Active control of unsteady motion phenomena in 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 |
US5117642A (en) * | 1989-12-18 | 1992-06-02 | Kabushiki Kaisha Toshiba | Low noise refrigerator and noise control method thereof |
US5127235A (en) * | 1989-12-18 | 1992-07-07 | Kabushiki Kaisha Toshiba | Low noise refrigerator and noise control method thereof |
DE4040745A1 (de) * | 1990-01-02 | 1991-07-04 | Gen Electric | Aktive regelung von durch verbrennung hervorgerufene instabilitaeten |
GB9003959D0 (en) * | 1990-02-21 | 1990-04-18 | Ross Colin F | Active control of internal combustion engine performance |
CZ114994A3 (en) * | 1991-11-15 | 1994-08-17 | Siemens Ag | Device for suppressing vibrations induced by combustion within a combustion chamber |
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 |
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 |
EP0918152A1 (de) * | 1997-11-24 | 1999-05-26 | Abb Research Ltd. | Verfahren und Vorrichtung zur Kontrolle thermoakustischer Schwingungen in einem Verbrennungssystem |
EP0918194A1 (de) * | 1997-11-24 | 1999-05-26 | Abb Research Ltd. | Verfahren zur Auslegung eines Verbrennungssystems und Verfahren und Vorrichtung zur Bestimmung von Brennereigenschaften |
DE59711378D1 (de) * | 1997-11-24 | 2004-04-08 | Alstom Switzerland Ltd | Verfahren zum Minimieren thermoakustischer Schwingungen in Gasturbinenbrennkammern |
EP0985810B1 (de) * | 1998-09-10 | 2003-10-29 | 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 |
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 |
JPWO2006043622A1 (ja) * | 2004-10-20 | 2008-05-22 | ヤマハ発動機株式会社 | 鞍乗型車両及び鞍乗型車両用燃焼制御装置 |
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 |
WO2013096989A1 (en) * | 2011-12-29 | 2013-07-04 | 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 |
WO2015119706A2 (en) * | 2013-12-12 | 2015-08-13 | 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)
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 |
-
1983
- 1983-11-02 GB GB838329218A patent/GB8329218D0/en active Pending
-
1984
- 1984-10-19 GB GB08426577A patent/GB2165964B/en not_active Expired
- 1984-10-26 US US06/665,154 patent/US4557106A/en not_active Expired - Lifetime
- 1984-10-31 FR FR8416693A patent/FR2554170B1/fr not_active Expired
- 1984-10-31 DE DE19843439903 patent/DE3439903A1/de not_active Withdrawn
- 1984-11-02 IT IT23443/84A patent/IT1178620B/it active
- 1984-11-02 JP JP59232268A patent/JPS60111027A/ja active Granted
Also Published As
Publication number | Publication date |
---|---|
FR2554170A1 (fr) | 1985-05-03 |
GB8426577D0 (en) | 1984-11-28 |
IT8423443A1 (it) | 1986-05-02 |
JPH0472982B2 (it) | 1992-11-19 |
IT8423443A0 (it) | 1984-11-02 |
US4557106A (en) | 1985-12-10 |
FR2554170B1 (fr) | 1987-11-20 |
JPS60111027A (ja) | 1985-06-17 |
GB2165964A (en) | 1986-04-23 |
DE3439903A1 (de) | 1985-05-09 |
GB2165964B (en) | 1987-11-11 |
GB8329218D0 (en) | 1983-12-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
TA | Fee payment date (situation as of event date), data collected since 19931001 |
Effective date: 19971031 |