CH701628B1 - Gasturbinenmaschinensteuersystem mit akustischem Treiber und/oder strömungsbeeinflussender Vorrichtung zur Steuerung der Verbrennungsdynamik. - Google Patents
Gasturbinenmaschinensteuersystem mit akustischem Treiber und/oder strömungsbeeinflussender Vorrichtung zur Steuerung der Verbrennungsdynamik. Download PDFInfo
- Publication number
- CH701628B1 CH701628B1 CH01289/10A CH12892010A CH701628B1 CH 701628 B1 CH701628 B1 CH 701628B1 CH 01289/10 A CH01289/10 A CH 01289/10A CH 12892010 A CH12892010 A CH 12892010A CH 701628 B1 CH701628 B1 CH 701628B1
- Authority
- CH
- Switzerland
- Prior art keywords
- combustion dynamics
- flow
- acoustic
- gas turbine
- control system
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 95
- 238000010926 purge Methods 0.000 claims abstract description 30
- 238000004458 analytical method Methods 0.000 claims abstract description 15
- 238000000034 method Methods 0.000 claims description 26
- 239000000446 fuel Substances 0.000 claims description 8
- 230000003993 interaction Effects 0.000 claims description 5
- 230000002452 interceptive effect Effects 0.000 claims description 3
- 239000000203 mixture Substances 0.000 claims description 3
- 239000007789 gas Substances 0.000 description 31
- 239000003570 air Substances 0.000 description 26
- 238000010586 diagram Methods 0.000 description 7
- 239000000567 combustion gas Substances 0.000 description 6
- 230000008901 benefit Effects 0.000 description 5
- 230000008569 process Effects 0.000 description 5
- 230000004913 activation Effects 0.000 description 3
- 230000008859 change Effects 0.000 description 3
- 238000003672 processing method Methods 0.000 description 3
- 230000009467 reduction Effects 0.000 description 3
- 238000005070 sampling Methods 0.000 description 3
- 238000004891 communication Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000008030 elimination Effects 0.000 description 2
- 238000003379 elimination reaction Methods 0.000 description 2
- 239000000284 extract Substances 0.000 description 2
- 230000003094 perturbing effect Effects 0.000 description 2
- 238000001228 spectrum Methods 0.000 description 2
- 239000012080 ambient air Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Classifications
-
- 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
- F23N5/242—Preventing development of abnormal or undesired conditions, i.e. safety arrangements using electronic means
-
- 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
- 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
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/26—Controlling the air flow
-
- 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
- F23N—REGULATING OR CONTROLLING COMBUSTION
- F23N2241/00—Applications
- F23N2241/20—Gas turbines
-
- 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
-
- 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)
- Testing Of Engines (AREA)
- Regulation And Control Of Combustion (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/539,763 US8326513B2 (en) | 2009-08-12 | 2009-08-12 | Gas turbine combustion dynamics control system and method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CH701628A2 CH701628A2 (de) | 2011-02-15 |
| CH701628B1 true CH701628B1 (de) | 2015-08-14 |
Family
ID=43448471
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CH01289/10A CH701628B1 (de) | 2009-08-12 | 2010-08-10 | Gasturbinenmaschinensteuersystem mit akustischem Treiber und/oder strömungsbeeinflussender Vorrichtung zur Steuerung der Verbrennungsdynamik. |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US8326513B2 (enExample) |
| JP (1) | JP5820574B2 (enExample) |
| CN (1) | CN101994574B (enExample) |
| CH (1) | CH701628B1 (enExample) |
| DE (1) | DE102010036802A1 (enExample) |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20130006581A1 (en) * | 2011-06-30 | 2013-01-03 | General Electric Company | Combustor health and performance monitoring system for gas turbines using combustion dynamics |
| EP2783092B1 (en) | 2011-11-22 | 2018-11-14 | Electric Power Research Institute, Inc | System and method for anomaly detection |
| FR2989736B1 (fr) * | 2012-04-18 | 2014-05-16 | Ge Energy Products France Snc | Procede de purge d'une turbine a gaz |
| US9803560B2 (en) * | 2013-03-15 | 2017-10-31 | Ansaldo Energia Ip Uk Limited | Dynamic tuning of a gas turbine engine to detect and prevent lean blowout |
| US9423317B2 (en) * | 2013-12-31 | 2016-08-23 | Inventus Holdings, Llc | Combustion chamber measurement system |
| US9798318B2 (en) * | 2014-04-14 | 2017-10-24 | General Electric Company | Online frequency response characterization system and method |
| US10024335B2 (en) | 2014-06-26 | 2018-07-17 | General Electric Company | Apparatus for transferring energy between a rotating element and fluid |
| EP3301278A1 (en) * | 2016-09-30 | 2018-04-04 | Siemens Aktiengesellschaft | Gas turbine arrangement with controlled bleed air injection into combustor, and method of operation |
| US11092083B2 (en) | 2017-02-10 | 2021-08-17 | General Electric Company | Pressure sensor assembly for a turbine engine |
| FR3080437B1 (fr) * | 2018-04-24 | 2020-04-17 | Safran Aircraft Engines | Systeme d'injection pour une chambre annulaire de combustion de turbomachine |
| US11867397B2 (en) | 2019-05-10 | 2024-01-09 | Electric Power Research Institute, Inc. | Gas turbine |
| US12173899B2 (en) * | 2022-03-07 | 2024-12-24 | Baker Hughes Holdings Llc | Combustion quality spectrum |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH05157239A (ja) * | 1991-12-04 | 1993-06-22 | Hitachi Ltd | ガスタービン用燃焼器 |
| JPH0777063A (ja) * | 1993-09-09 | 1995-03-20 | Hitachi Ltd | 燃焼制御装置 |
| US6522991B2 (en) | 2001-05-04 | 2003-02-18 | United Technologies Corporation | Suppressing oscillations in processes such as gas turbine combustion |
| US7454892B2 (en) * | 2002-10-30 | 2008-11-25 | Georgia Tech Research Corporation | Systems and methods for detection and control of blowout precursors in combustors using acoustical and optical sensing |
| 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 |
| US7775052B2 (en) * | 2004-05-07 | 2010-08-17 | Delavan Inc | Active combustion control system for gas turbine engines |
| US7484369B2 (en) * | 2004-05-07 | 2009-02-03 | Rosemount Aerospace Inc. | Apparatus for observing combustion conditions in a gas turbine engine |
| US7278266B2 (en) * | 2004-08-31 | 2007-10-09 | General Electric Company | Methods and apparatus for gas turbine engine lean blowout avoidance |
| US7340900B2 (en) | 2004-12-15 | 2008-03-11 | General Electric Company | Method and apparatus for decreasing combustor acoustics |
| US7966801B2 (en) | 2006-12-07 | 2011-06-28 | General Electric Company | Apparatus and method for gas turbine active combustion control system |
-
2009
- 2009-08-12 US US12/539,763 patent/US8326513B2/en active Active
-
2010
- 2010-08-02 DE DE102010036802A patent/DE102010036802A1/de not_active Withdrawn
- 2010-08-04 JP JP2010175034A patent/JP5820574B2/ja not_active Expired - Fee Related
- 2010-08-10 CH CH01289/10A patent/CH701628B1/de not_active IP Right Cessation
- 2010-08-12 CN CN201010258300.1A patent/CN101994574B/zh not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| US8326513B2 (en) | 2012-12-04 |
| US20110040469A1 (en) | 2011-02-17 |
| JP5820574B2 (ja) | 2015-11-24 |
| JP2011038763A (ja) | 2011-02-24 |
| CN101994574A (zh) | 2011-03-30 |
| CN101994574B (zh) | 2014-10-15 |
| CH701628A2 (de) | 2011-02-15 |
| DE102010036802A1 (de) | 2011-02-17 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| NV | New agent |
Representative=s name: GENERAL ELECTRIC TECHNOLOGY GMBH GLOBAL PATENT, CH |
|
| PL | Patent ceased |