KR830006575A - 가스터어빈용 연소방법 및 가스터어빈연소기 - Google Patents
가스터어빈용 연소방법 및 가스터어빈연소기 Download PDFInfo
- Publication number
- KR830006575A KR830006575A KR1019810003038A KR810003038A KR830006575A KR 830006575 A KR830006575 A KR 830006575A KR 1019810003038 A KR1019810003038 A KR 1019810003038A KR 810003038 A KR810003038 A KR 810003038A KR 830006575 A KR830006575 A KR 830006575A
- Authority
- KR
- South Korea
- Prior art keywords
- combustion
- gas turbine
- gas
- inner cylinder
- fuel
- Prior art date
Links
- 238000009841 combustion method Methods 0.000 title claims 5
- 238000002485 combustion reaction Methods 0.000 claims description 9
- 239000000446 fuel Substances 0.000 claims description 9
- 239000012530 fluid Substances 0.000 claims 2
- 238000011144 upstream manufacturing Methods 0.000 claims 2
- 238000010790 dilution Methods 0.000 claims 1
- 239000012895 dilution Substances 0.000 claims 1
- 238000009751 slip forming Methods 0.000 claims 1
- 230000008961 swelling Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 4
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
-
- 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
- F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
-
- 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
- F23R3/34—Feeding into different combustion zones
- F23R3/346—Feeding into different combustion zones for staged combustion
-
- 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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E20/00—Combustion technologies with mitigation potential
- Y02E20/34—Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Abstract
내용 없음
Description
본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음
제1도, 제7도는 각기 본원 발명의 실시예를 나타낸 가스터어빈용 연소기의 개략도.
제2도는 제1도의 A부확대도.
제3도는 본원 발명에 있어서의 예혼합(豫混合) 공기과잉율의 NOx 저감효과를 나타낸 특성도.
제4도는 본원 발명에 있어서의 연료제어를 나타낸 설명도.
제5도는 본원 발명과 종래형과의 NOx 저감효과를 비교하는 것으로서 연소비와 NOx 농도와의 관계를 나타낸 특성도.
제6도는 종래형의 연소기의 개략도.
제8도는 제7도의 B부확대도.
Claims (5)
- 도면에 표시하고 본문에 상술한 바와 같이 압축공기와 기체연료를 미리 혼합한 후에 이 혼합유체를 연소실의 최상류측에서 유입시켜 파일럿화염을 형성하고, 이 화염의 선단근방에 주연소용의 기체연료를 공기와 함께 공급하여 저온도 희박연소(稀薄煙燒)를 하도록 한 것을 특징으로 하는 가스터어빈용 연소방법.
- 특허청구의 범위 1기재의 가스터어빈용연소방법에 있어서, 정격(定格)운전시에 있어서의 상기 예혼합용(豫混合用)압축공기는 예혼합용기체연료와의 관계가 공기과잉을 1.2이상으로 되도록 공급하는 것을 특징으로 하는 가스터어빈용 연소방법.
- 특허청구의 범위 2기재의 가스터어빈용연소방법에 있어서 상기 정격운전시에 있어서의 상기 주연소가 행해지는 영역은 공기과잉율 1.3이상이 되도록 각 연료 및 공기를 공급하는 것을 특징으로 하는 가스터어빈 연소방법.
- 연소실을 형성하는 내통과, 이 내통과의 간극이 연소 및 희석용의 공기의 유로가 되도록 이 내통을 덮는 외통과, 이 외통의 일단을 닫는 엔드커버와, 이 엔드커버를 관통해서 상기 내통으로 개구하는 연료 공급용의 노즐과, 상기 내통의 원주방향으로 배치된 연소용공기공급용의 팽윤부로 이루어진 가스터어빈용 연소기에 있어서, 상기 노즐의 상류측에 기체연료와 압축공기와의 예혼합을 하는 예혼합실을 배치하고, 이 예혼합실의 토출부를 이 노즐과 연통(連通)시켜, 상기 스와라에는기체연료가 공기와 함께 내통내에 토출되도록 이 기체연료의 공급관을 접속한 것을 특징으로 하는 가스터어빈용 연소기.
- 특허청구의 범위 4 기재의 가스터어빈용 연소기에 있어서 상기 평윤기보다도 상류측의 내통경(內筒徑)을 그 하류측의 내통경보다도 작게하여, 예혼합유체의 연소에 의한 화염을 지속형성하는 두부연소실을 형성한 것을 특징으로 하는 가스터어빈용 연소기.※ 참고사항 : 최초출원 내용에 의하여 공개하는 것임.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP80-115991 | 1980-08-25 | ||
JP55115991A JPS5741524A (en) | 1980-08-25 | 1980-08-25 | Combustion method of gas turbine and combustor for gas turbine |
Publications (2)
Publication Number | Publication Date |
---|---|
KR830006575A true KR830006575A (ko) | 1983-09-28 |
KR850001188B1 KR850001188B1 (ko) | 1985-08-19 |
Family
ID=14676148
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
KR1019810003038A KR850001188B1 (ko) | 1980-08-25 | 1981-08-20 | 가스터어빈용 연소기 |
Country Status (5)
Country | Link |
---|---|
US (1) | US4671069A (ko) |
JP (1) | JPS5741524A (ko) |
KR (1) | KR850001188B1 (ko) |
FR (1) | FR2488942B1 (ko) |
GB (1) | GB2082756B (ko) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR100483774B1 (ko) * | 1996-05-02 | 2005-06-16 | 제너럴 일렉트릭 캄파니 | 가스터빈용연소기와,가스터빈 |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS58122871U (ja) * | 1982-02-13 | 1983-08-20 | ヤンマーディーゼル株式会社 | ガスタ−ビン機関用エア−アシストノズルの空気供給装置 |
JPS61258929A (ja) * | 1985-05-10 | 1986-11-17 | Hitachi Ltd | ガスタ−ビンの燃料制御装置 |
US4735052A (en) * | 1985-09-30 | 1988-04-05 | Kabushiki Kaisha Toshiba | Gas turbine apparatus |
US4881373A (en) * | 1988-04-25 | 1989-11-21 | Paloma Kogyo Kabushiki Kaisha | Pulse combustion device |
US4910957A (en) * | 1988-07-13 | 1990-03-27 | Prutech Ii | Staged lean premix low nox hot wall gas turbine combustor with improved turndown capability |
JP2618448B2 (ja) * | 1988-08-09 | 1997-06-11 | 株式会社日立製作所 | ガスタービン燃焼器状態監視装置及び監視方法及び制御方法 |
US5013236A (en) * | 1989-05-22 | 1991-05-07 | Institute Of Gas Technology | Ultra-low pollutant emission combustion process and apparatus |
US5158445A (en) * | 1989-05-22 | 1992-10-27 | Institute Of Gas Technology | Ultra-low pollutant emission combustion method and apparatus |
US5099644A (en) * | 1990-04-04 | 1992-03-31 | General Electric Company | Lean staged combustion assembly |
JP2758301B2 (ja) * | 1991-11-29 | 1998-05-28 | 株式会社東芝 | ガスタービン燃焼器 |
US5638674A (en) * | 1993-07-07 | 1997-06-17 | Mowill; R. Jan | Convectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admission |
US5628182A (en) * | 1993-07-07 | 1997-05-13 | Mowill; R. Jan | Star combustor with dilution ports in can portions |
US5572862A (en) * | 1993-07-07 | 1996-11-12 | Mowill Rolf Jan | Convectively cooled, single stage, fully premixed fuel/air combustor for gas turbine engine modules |
US5377483A (en) * | 1993-07-07 | 1995-01-03 | Mowill; R. Jan | Process for single stage premixed constant fuel/air ratio combustion |
US6220034B1 (en) | 1993-07-07 | 2001-04-24 | R. Jan Mowill | Convectively cooled, single stage, fully premixed controllable fuel/air combustor |
US5613357A (en) * | 1993-07-07 | 1997-03-25 | Mowill; R. Jan | Star-shaped single stage low emission combustor system |
US5450724A (en) * | 1993-08-27 | 1995-09-19 | Northern Research & Engineering Corporation | Gas turbine apparatus including fuel and air mixer |
DE4408256A1 (de) * | 1994-03-11 | 1995-09-14 | Abb Management Ag | Verfahren und Vorrichtung zur Flammenstabilisation von Vormischbrennern |
US5813232A (en) * | 1995-06-05 | 1998-09-29 | Allison Engine Company, Inc. | Dry low emission combustor for gas turbine engines |
JPH09119641A (ja) * | 1995-06-05 | 1997-05-06 | Allison Engine Co Inc | ガスタービンエンジン用低窒素酸化物希薄予混合モジュール |
US5924276A (en) * | 1996-07-17 | 1999-07-20 | Mowill; R. Jan | Premixer with dilution air bypass valve assembly |
WO1998025084A1 (en) | 1996-12-04 | 1998-06-11 | Siemens Westinghouse Power Corporation | DIFFUSION AND PREMIX PILOT BURNER FOR LOW NOx COMBUSTOR |
US5987875A (en) * | 1997-07-14 | 1999-11-23 | Siemens Westinghouse Power Corporation | Pilot nozzle steam injection for reduced NOx emissions, and method |
US6192689B1 (en) | 1998-03-18 | 2001-02-27 | General Electric Company | Reduced emissions gas turbine combustor |
JP2003194338A (ja) | 2001-12-14 | 2003-07-09 | R Jan Mowill | 可変出口形状を有するガスタービンエンジン用燃料/空気プレミキサ及び出口速度の制御方法 |
AU2003289368A1 (en) | 2003-12-16 | 2005-07-05 | Hitachi, Ltd. | Combustor for gas turbine |
US20100018211A1 (en) * | 2008-07-23 | 2010-01-28 | General Electric Company | Gas turbine transition piece having dilution holes |
US8919132B2 (en) | 2011-05-18 | 2014-12-30 | Solar Turbines Inc. | Method of operating a gas turbine engine |
US8893500B2 (en) | 2011-05-18 | 2014-11-25 | Solar Turbines Inc. | Lean direct fuel injector |
US9182124B2 (en) | 2011-12-15 | 2015-11-10 | Solar Turbines Incorporated | Gas turbine and fuel injector for the same |
Family Cites Families (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB659859A (en) * | 1944-09-14 | 1951-10-31 | Power Jets Res & Dev Ltd | Improvements in combustion systems for burning fuel in a fast moving gas stream |
US2635426A (en) * | 1949-06-29 | 1953-04-21 | A V Roe Canada Ltd | Annular vaporizer |
US2969643A (en) * | 1949-10-13 | 1961-01-31 | Ii James W Mullen | Screened igniter for ramjet burners |
US2679295A (en) * | 1949-12-30 | 1954-05-25 | Gen Electric | Helicopter blade jet combustion chamber |
US2828609A (en) * | 1950-04-03 | 1958-04-01 | Bristol Aero Engines Ltd | Combustion chambers including suddenly enlarged chamber portions |
US2812637A (en) * | 1951-12-21 | 1957-11-12 | Phillips Petroleum Co | Fuel air ratio regulation for combustion systems |
GB726491A (en) * | 1952-07-16 | 1955-03-16 | Onera (Off Nat Aerospatiale) | Improvements in internal combustion engines through which a continuous gaseous stream is flowing and in particular in turbo-jet and turbo-prop engines |
US2999359A (en) * | 1956-04-25 | 1961-09-12 | Rolls Royce | Combustion equipment of gas-turbine engines |
FR1206830A (fr) * | 1958-05-19 | 1960-02-11 | Rolls Royce | Perfectionnements aux appareillages de combustion des moteurs à turbine à gaz |
DE1932881C3 (de) * | 1969-06-28 | 1978-06-29 | Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen | Brennkammer für Gasturbinentriebwerke |
GB1284440A (en) * | 1969-12-09 | 1972-08-09 | Rolls Royce | Improvements in or relating to gas turbine engines |
US3581493A (en) * | 1969-12-12 | 1971-06-01 | Avco Corp | Air assist for fuel injector |
JPS4724483Y1 (ko) * | 1970-12-22 | 1972-08-02 | ||
US3958413A (en) * | 1974-09-03 | 1976-05-25 | General Motors Corporation | Combustion method and apparatus |
US3973390A (en) * | 1974-12-18 | 1976-08-10 | United Technologies Corporation | Combustor employing serially staged pilot combustion, fuel vaporization, and primary combustion zones |
US4006589A (en) * | 1975-04-14 | 1977-02-08 | Phillips Petroleum Company | Low emission combustor with fuel flow controlled primary air flow and circumferentially directed secondary air flows |
DE2524036C2 (de) * | 1975-05-30 | 1983-05-11 | Caloric Gesellschaft für Apparatebau mbH, 8032 Gräfelfing | Brenner für fließfähige Brennstoffe |
US4052844A (en) * | 1975-06-02 | 1977-10-11 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation | Gas turbine combustion chambers |
US4012904A (en) * | 1975-07-17 | 1977-03-22 | Chrysler Corporation | Gas turbine burner |
US4015954A (en) * | 1975-12-29 | 1977-04-05 | John Zink Company | Laminar flow flame arrestor |
DE2629761A1 (de) * | 1976-07-02 | 1978-01-05 | Volkswagenwerk Ag | Brennkammer fuer gasturbinen |
US4112676A (en) * | 1977-04-05 | 1978-09-12 | Westinghouse Electric Corp. | Hybrid combustor with staged injection of pre-mixed fuel |
US4253301A (en) * | 1978-10-13 | 1981-03-03 | General Electric Company | Fuel injection staged sectoral combustor for burning low-BTU fuel gas |
DE2937631A1 (de) * | 1979-09-18 | 1981-04-02 | Daimler-Benz Ag, 7000 Stuttgart | Brennkammer fuer gasturbinen |
-
1980
- 1980-08-25 JP JP55115991A patent/JPS5741524A/ja active Granted
-
1981
- 1981-08-20 KR KR1019810003038A patent/KR850001188B1/ko active
- 1981-08-24 GB GB8125785A patent/GB2082756B/en not_active Expired
- 1981-08-25 FR FR8116250A patent/FR2488942B1/fr not_active Expired
-
1985
- 1985-12-16 US US06/809,200 patent/US4671069A/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR100483774B1 (ko) * | 1996-05-02 | 2005-06-16 | 제너럴 일렉트릭 캄파니 | 가스터빈용연소기와,가스터빈 |
Also Published As
Publication number | Publication date |
---|---|
US4671069A (en) | 1987-06-09 |
GB2082756B (en) | 1984-06-27 |
JPS5741524A (en) | 1982-03-08 |
FR2488942A1 (fr) | 1982-02-26 |
KR850001188B1 (ko) | 1985-08-19 |
GB2082756A (en) | 1982-03-10 |
FR2488942B1 (fr) | 1986-08-08 |
JPS6233490B2 (ko) | 1987-07-21 |
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