KR940002550A - 이차 버너 - Google Patents
이차 버너 Download PDFInfo
- Publication number
- KR940002550A KR940002550A KR1019930012484A KR930012484A KR940002550A KR 940002550 A KR940002550 A KR 940002550A KR 1019930012484 A KR1019930012484 A KR 1019930012484A KR 930012484 A KR930012484 A KR 930012484A KR 940002550 A KR940002550 A KR 940002550A
- Authority
- KR
- South Korea
- Prior art keywords
- combustion chamber
- burner
- air passage
- secondary burner
- damping
- 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
- 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
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2260/00—Function
- F05B2260/96—Preventing, counteracting or reducing vibration or 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
- F05D2240/00—Components
- F05D2240/35—Combustors or associated equipment
-
- 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
-
- 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
- F23R2900/03341—Sequential combustion chambers or burners
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
- Gas Burners (AREA)
- Spray-Type Burners (AREA)
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
Abstract
가스터어빈 연소실에 사용하는 이차 버너에 있어서 연소실벽(1)에 내부에 배열된 연료공급부(2,3)는 환성 공기 통로(4)에 의해 둘러싸여 있다. 상기 공기 통로(4)는 적어도 하나의 공급관(5)에 의해 직통형 헬름홀쯔 공명기(6)와 연통한다. 상기 헬름홀쯔 공명기의 댐핑관의 출구는 환상통로로 형성되어 있고, 이차 연소실(9)의 버너 마우스(8) 영역에 위치한다.
Description
본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음
제1도는 이차 버너의 부분 종단면도,
제2도는 헬름홀츠 공명기의 원리를 보여주는 도면.
Claims (3)
- 연소실벽에 배열된 연료공급부가 환상 공기 통로에 의해 둘러싸여 있는, 가스터어빈 연소실용 이차 버너에 있어서, 상기 공기 통로는 하나 이상의 공급관에 의해 직통형 헬름홀쯔 공명기와 연통하고, 상기 헬름홀쯔 공명기의 하나 이상의 댐핑관으로 부터의 출구는 이차 연소실의 버너 마우스 영역에 위치됨으로 특징으로 하는 이차 버너.
- 제1항에 있어서, 상기 댐핑관이 환상 통로로 형성됨을 특징으로 하는 이차 버너.
- 연소실에서의 이차 버너용 직통형 홀름홀쯔 공명기에 있어서, 공급관, 공명 체적부 및 상기 댐핑관의 입출구 단부는 만곡되어 짐을 특징으로 하는 이차 버너용 직통형 헬름홀쯔 공명기.※ 참고사항 : 최초출원 내용에 의하여 공개하는 것임.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP92111347.8 | 1992-07-03 | ||
EP92111347A EP0577862B1 (de) | 1992-07-03 | 1992-07-03 | Nachbrenner |
Publications (1)
Publication Number | Publication Date |
---|---|
KR940002550A true KR940002550A (ko) | 1994-02-17 |
Family
ID=8209779
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
KR1019930012484A KR940002550A (ko) | 1992-07-03 | 1993-07-03 | 이차 버너 |
Country Status (6)
Country | Link |
---|---|
US (1) | US5431018A (ko) |
EP (1) | EP0577862B1 (ko) |
JP (1) | JPH0694227A (ko) |
KR (1) | KR940002550A (ko) |
CA (1) | CA2098810A1 (ko) |
DE (1) | DE59208193D1 (ko) |
Families Citing this family (53)
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EP0974788B1 (de) * | 1998-07-23 | 2014-11-26 | Alstom Technology Ltd | Vorrichtung zur gezielten Schalldämpfung innerhalb einer Strömungsmaschine |
DE59809097D1 (de) | 1998-09-30 | 2003-08-28 | Alstom Switzerland Ltd | Brennkammer für eine Gasturbine |
DE19905995A1 (de) | 1999-02-15 | 2000-08-17 | Asea Brown Boveri | Brennstofflanze zum Eindüsen von flüssigen und/oder gasförmigen Brennstoffen in eine Brennkammer sowie Verfahren zum Betrieb einer solchen Brennstofflanze |
DE19905996A1 (de) | 1999-02-15 | 2000-08-17 | Abb Alstom Power Ch Ag | Brennstofflanze zum Eindüsen von flüssigen und/oder gasförmigen Brennstoffen in eine Brennkammer |
US6351947B1 (en) | 2000-04-04 | 2002-03-05 | Abb Alstom Power (Schweiz) | Combustion chamber for a gas turbine |
DE10056243A1 (de) * | 2000-11-14 | 2002-05-23 | Alstom Switzerland Ltd | Brennkammer und Verfahren zum Betrieb dieser Brennkammer |
EP1342953A1 (de) * | 2002-03-07 | 2003-09-10 | Siemens Aktiengesellschaft | Gasturbine |
RU2212589C1 (ru) * | 2002-06-28 | 2003-09-20 | Козырев Александр Валентинович | Камера сгорания теплового двигателя |
EP1601913A1 (de) * | 2003-03-07 | 2005-12-07 | Alstom Technology Ltd | Vormischbrenner |
EP1557609B1 (en) * | 2004-01-21 | 2016-03-16 | Siemens Aktiengesellschaft | Device and method for damping thermoacoustic oscillations in a combustion chamber |
EP1559874B1 (de) * | 2004-02-02 | 2013-07-31 | Siemens Aktiengesellschaft | Diffusor und Turbine |
US7788926B2 (en) * | 2006-08-18 | 2010-09-07 | Siemens Energy, Inc. | Resonator device at junction of combustor and combustion chamber |
US8127546B2 (en) | 2007-05-31 | 2012-03-06 | Solar Turbines Inc. | Turbine engine fuel injector with helmholtz resonators |
KR100905254B1 (ko) | 2007-11-06 | 2009-06-29 | 홍정구 | 연소기의 불안정 연소 영역에 대한 저감장치 및 저감방법 |
US8516819B2 (en) | 2008-07-16 | 2013-08-27 | Siemens Energy, Inc. | Forward-section resonator for high frequency dynamic damping |
EP2187125A1 (de) * | 2008-09-24 | 2010-05-19 | Siemens Aktiengesellschaft | Vorrichtung und Verfahren zur Dämpfung von Verbrennungsschwingungen |
US8789372B2 (en) | 2009-07-08 | 2014-07-29 | General Electric Company | Injector with integrated resonator |
US8474265B2 (en) * | 2009-07-29 | 2013-07-02 | General Electric Company | Fuel nozzle for a turbine combustor, and methods of forming same |
EP2480773B1 (de) * | 2009-09-24 | 2014-12-31 | Siemens Aktiengesellschaft | Brennstoffleitungssystem, verfahren zum betrieb einer gasturbine und ein verfahren zum spülen des brennstoffleitungssystems einer gasturbine |
WO2011054739A2 (en) | 2009-11-07 | 2011-05-12 | Alstom Technology Ltd | Reheat burner injection system |
EP2496884B1 (en) | 2009-11-07 | 2016-12-28 | General Electric Technology GmbH | Reheat burner injection system |
EP2496883B1 (en) | 2009-11-07 | 2016-08-10 | Alstom Technology Ltd | Premixed burner for a gas turbine combustor |
EP2496885B1 (en) | 2009-11-07 | 2019-05-29 | Ansaldo Energia Switzerland AG | Burner with a cooling system allowing an increased gas turbine efficiency |
WO2011054757A2 (en) | 2009-11-07 | 2011-05-12 | Alstom Technology Ltd | Reheat burner injection system with fuel lances |
US9127837B2 (en) * | 2010-06-22 | 2015-09-08 | Carrier Corporation | Low pressure drop, low NOx, induced draft gas heaters |
CH703357A1 (de) | 2010-06-25 | 2011-12-30 | Alstom Technology Ltd | Wärmebelastetes, gekühltes bauteil. |
EP2474784A1 (en) | 2011-01-07 | 2012-07-11 | Siemens Aktiengesellschaft | Combustion system for a gas turbine comprising a resonator |
US8938971B2 (en) | 2011-05-11 | 2015-01-27 | Alstom Technology Ltd | Flow straightener and mixer |
RU2550370C2 (ru) | 2011-05-11 | 2015-05-10 | Альстом Текнолоджи Лтд | Центробежная форсунка с выступающими частями |
US9341375B2 (en) | 2011-07-22 | 2016-05-17 | General Electric Company | System for damping oscillations in a turbine combustor |
US9103551B2 (en) | 2011-08-01 | 2015-08-11 | General Electric Company | Combustor leaf seal arrangement |
US8966903B2 (en) | 2011-08-17 | 2015-03-03 | General Electric Company | Combustor resonator with non-uniform resonator passages |
EP2642203A1 (en) * | 2012-03-20 | 2013-09-25 | Alstom Technology Ltd | Annular Helmholtz damper |
US20130305739A1 (en) * | 2012-05-18 | 2013-11-21 | General Electric Company | Fuel nozzle cap |
US20130305725A1 (en) * | 2012-05-18 | 2013-11-21 | General Electric Company | Fuel nozzle cap |
CA2830031C (en) | 2012-10-23 | 2016-03-15 | Alstom Technology Ltd. | Burner for a can combustor |
JP6231114B2 (ja) | 2012-10-24 | 2017-11-15 | ゼネラル エレクトリック テクノロジー ゲゼルシャフト ミット ベシュレンクテル ハフツングGeneral Electric Technology GmbH | 希釈ガス混合器を備えた2段燃焼 |
EP2725302A1 (en) | 2012-10-25 | 2014-04-30 | Alstom Technology Ltd | Reheat burner arrangement |
WO2014131876A1 (de) * | 2013-02-28 | 2014-09-04 | Siemens Aktiengesellschaft | Dämpfungsvorrichtung für eine gasturbine, gasturbine und verfahren zur dämpfung thermoakustischer schwingungen |
CN105121962B (zh) * | 2013-04-25 | 2018-06-22 | 安萨尔多能源瑞士股份公司 | 具有稀释气体的连续燃烧 |
EP2837883B1 (en) | 2013-08-16 | 2018-04-04 | Ansaldo Energia Switzerland AG | Premixed can annular combustor with mixing lobes for the second stage of a sequential gas turbine |
US20150113991A1 (en) * | 2013-10-25 | 2015-04-30 | Alstom Technology Ltd | Damping device for a combustor of a gas turbine |
US20150167980A1 (en) * | 2013-12-18 | 2015-06-18 | Jared M. Pent | Axial stage injection dual frequency resonator for a combustor of a gas turbine engine |
EP2933559A1 (en) | 2014-04-16 | 2015-10-21 | Alstom Technology Ltd | Fuel mixing arragement and combustor with such a fuel mixing arrangement |
EP3023696B1 (en) | 2014-11-20 | 2019-08-28 | Ansaldo Energia Switzerland AG | Lobe lance for a gas turbine combustor |
EP3029378B1 (en) | 2014-12-04 | 2019-08-28 | Ansaldo Energia Switzerland AG | Sequential burner for an axial gas turbine |
EP3306197B1 (en) * | 2016-10-08 | 2020-01-29 | Ansaldo Energia Switzerland AG | Dual fuel injector for a sequential burner of a sequential gas turbine |
US10220474B2 (en) * | 2016-12-02 | 2019-03-05 | General Electricd Company | Method and apparatus for gas turbine combustor inner cap and high frequency acoustic dampers |
DE102017223249A1 (de) | 2016-12-19 | 2018-06-21 | Brigham Young University | Kompakter akustischer Resonator für geschlossene Systeme |
US20180174566A1 (en) * | 2016-12-19 | 2018-06-21 | Caterpillar Inc. | Compact acoustic resonator for enclosed systems |
EP3354984B1 (en) | 2017-01-31 | 2020-09-09 | Ansaldo Energia Switzerland AG | Lobed injector for a gas turbine combustor |
EP3438540A1 (en) | 2017-07-31 | 2019-02-06 | Siemens Aktiengesellschaft | A burner including an acoustic damper |
CN114165813B (zh) * | 2021-12-03 | 2022-08-30 | 北京航空航天大学 | 一种双油路供油的气动辅助一体化支板稳定器 |
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GB648699A (en) * | 1947-10-17 | 1951-01-10 | Arthur Holmes Fletcher | Improvements in or relating to gas-turbine engine fuel systems and liquid fuel injectors therefor |
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US4409787A (en) * | 1979-04-30 | 1983-10-18 | General Electric Company | Acoustically tuned combustor |
DE3324805A1 (de) * | 1983-07-09 | 1985-01-17 | Betriebsforschungsinstitut VDEh - Institut für angewandte Forschung GmbH, 4000 Düsseldorf | Einrichtung zur vermeidung von druckschwingungen bei brennkammern |
JPS60213721A (ja) * | 1984-04-09 | 1985-10-26 | Matsushita Electric Ind Co Ltd | パルス燃焼器用マフラ |
DE3432607A1 (de) * | 1984-09-05 | 1986-03-13 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Einrichtung zum daempfen von brennkammerschwingungen bei fluessigkeitsraketentriebwerken |
US4570610A (en) * | 1984-12-28 | 1986-02-18 | Gas Research Institute | Pulse combustion burner for cooking surface |
US5123835A (en) * | 1991-03-04 | 1992-06-23 | The United States Of America As Represented By The United States Department Of Energy | Pulse combustor with controllable oscillations |
-
1992
- 1992-07-03 EP EP92111347A patent/EP0577862B1/de not_active Expired - Lifetime
- 1992-07-03 DE DE59208193T patent/DE59208193D1/de not_active Expired - Fee Related
-
1993
- 1993-06-18 CA CA002098810A patent/CA2098810A1/en not_active Abandoned
- 1993-06-18 US US08/078,031 patent/US5431018A/en not_active Expired - Fee Related
- 1993-07-02 JP JP5164642A patent/JPH0694227A/ja active Pending
- 1993-07-03 KR KR1019930012484A patent/KR940002550A/ko not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
US5431018A (en) | 1995-07-11 |
EP0577862A1 (de) | 1994-01-12 |
JPH0694227A (ja) | 1994-04-05 |
EP0577862B1 (de) | 1997-03-12 |
CA2098810A1 (en) | 1994-01-04 |
DE59208193D1 (de) | 1997-04-17 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WITN | Application deemed withdrawn, e.g. because no request for examination was filed or no examination fee was paid |