KR950011818A - 가스 터빈 연소기 - Google Patents
가스 터빈 연소기 Download PDFInfo
- Publication number
- KR950011818A KR950011818A KR1019940027387A KR19940027387A KR950011818A KR 950011818 A KR950011818 A KR 950011818A KR 1019940027387 A KR1019940027387 A KR 1019940027387A KR 19940027387 A KR19940027387 A KR 19940027387A KR 950011818 A KR950011818 A KR 950011818A
- Authority
- KR
- South Korea
- Prior art keywords
- swirl
- gas turbine
- vanes
- swirl vanes
- angle
- Prior art date
- Legal status (The legal status 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 status listed.)
- Abandoned
Links
- 239000000446 fuel Substances 0.000 claims abstract 5
- 230000001939 inductive effect Effects 0.000 claims 1
- 238000002347 injection Methods 0.000 claims 1
- 239000007924 injection Substances 0.000 claims 1
- 238000000034 method Methods 0.000 claims 1
- 238000001816 cooling Methods 0.000 abstract 2
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
Classifications
-
- 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
- F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C7/00—Combustion apparatus characterised by arrangements for air supply
- F23C7/002—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
- F23C7/004—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion using vanes
- F23C7/006—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion using vanes adjustable
-
- 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
- F23R3/04—Air inlet arrangements
- F23R3/10—Air inlet arrangements for primary air
- F23R3/12—Air inlet arrangements for primary air inducing a vortex
- F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US08/141,757 US5394688A (en) | 1993-10-27 | 1993-10-27 | Gas turbine combustor swirl vane arrangement |
| US08/141,757 | 1993-10-27 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| KR950011818A true KR950011818A (ko) | 1995-05-16 |
Family
ID=22497096
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| KR1019940027387A Abandoned KR950011818A (ko) | 1993-10-27 | 1994-10-26 | 가스 터빈 연소기 |
Country Status (10)
| Country | Link |
|---|---|
| US (2) | US5394688A (enExample) |
| EP (1) | EP0654639B1 (enExample) |
| JP (1) | JPH07180835A (enExample) |
| KR (1) | KR950011818A (enExample) |
| CN (1) | CN1107933A (enExample) |
| AU (1) | AU7575694A (enExample) |
| CA (1) | CA2134419A1 (enExample) |
| DE (1) | DE69413352T2 (enExample) |
| ES (1) | ES2123102T3 (enExample) |
| TW (1) | TW248585B (enExample) |
Families Citing this family (183)
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| JP2858104B2 (ja) * | 1996-02-05 | 1999-02-17 | 三菱重工業株式会社 | ガスタービン燃焼器 |
| GB2311596B (en) * | 1996-03-29 | 2000-07-12 | Europ Gas Turbines Ltd | Combustor for gas - or liquid - fuelled turbine |
| US6047550A (en) * | 1996-05-02 | 2000-04-11 | General Electric Co. | Premixing dry low NOx emissions combustor with lean direct injection of gas fuel |
| WO1998049496A1 (en) | 1997-04-30 | 1998-11-05 | Siemens Westinghouse Power Corporation | An apparatus for cooling a combuster, and a method of same |
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| TW362128B (en) | 1997-09-30 | 1999-06-21 | Westinghouse Electric Corp | Ultra-low NOx combustor |
| US5983642A (en) | 1997-10-13 | 1999-11-16 | Siemens Westinghouse Power Corporation | Combustor with two stage primary fuel tube with concentric members and flow regulating |
| US6109038A (en) * | 1998-01-21 | 2000-08-29 | Siemens Westinghouse Power Corporation | Combustor with two stage primary fuel assembly |
| US8135413B2 (en) * | 1998-11-24 | 2012-03-13 | Tracbeam Llc | Platform and applications for wireless location and other complex services |
| US6460344B1 (en) | 1999-05-07 | 2002-10-08 | Parker-Hannifin Corporation | Fuel atomization method for turbine combustion engines having aerodynamic turning vanes |
| US6883332B2 (en) * | 1999-05-07 | 2005-04-26 | Parker-Hannifin Corporation | Fuel nozzle for turbine combustion engines having aerodynamic turning vanes |
| ITMI991204A1 (it) * | 1999-05-31 | 2000-12-01 | Nuovo Pignone Spa | Iniettore di combustibile liquido per bruciatori in turbine a gas |
| RU2160416C2 (ru) * | 1999-12-01 | 2000-12-10 | ООО "Самаратрансгаз" АО "ГАЗПРОМ" | Камера сгорания газотурбинного двигателя |
| US6405536B1 (en) * | 2000-03-27 | 2002-06-18 | Wu-Chi Ho | Gas turbine combustor burning LBTU fuel gas |
| RU2189532C2 (ru) * | 2000-06-20 | 2002-09-20 | Открытое акционерное общество "Авиадвигатель" | Горелка камеры сгорания газотурбинного двигателя |
| DE10051221A1 (de) * | 2000-10-16 | 2002-07-11 | Alstom Switzerland Ltd | Brenner mit gestufter Brennstoff-Eindüsung |
| JP2003028425A (ja) * | 2001-07-17 | 2003-01-29 | Mitsubishi Heavy Ind Ltd | 予混合燃焼器のパイロットバーナー、予混合燃焼器、およびガスタービン |
| RU2224954C2 (ru) * | 2001-08-29 | 2004-02-27 | Открытое акционерное общество "Авиадвигатель" | Топливовоздушная горелка камеры сгорания газотурбинного двигателя |
| US6666029B2 (en) | 2001-12-06 | 2003-12-23 | Siemens Westinghouse Power Corporation | Gas turbine pilot burner and method |
| RU2210026C1 (ru) * | 2001-12-27 | 2003-08-10 | Государственное унитарное предприятие Тушинское машиностроительное конструкторское бюро "Союз" - дочернее предприятие Федерального государственного унитарного предприятия Российской самолётостроительной корпорации "МиГ" | Акустическая топливная форсунка |
| US6691515B2 (en) | 2002-03-12 | 2004-02-17 | Rolls-Royce Corporation | Dry low combustion system with means for eliminating combustion noise |
| RU2217663C1 (ru) * | 2002-11-25 | 2003-11-27 | Открытое акционерное общество "Научно-производственное объединение "Сатурн" | Кольцевая камера сгорания газотурбинного двигателя |
| DE10257704A1 (de) * | 2002-12-11 | 2004-07-15 | Alstom Technology Ltd | Verfahren zur Verbrennung eines Brennstoffs |
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| US7308794B2 (en) | 2004-08-27 | 2007-12-18 | Pratt & Whitney Canada Corp. | Combustor and method of improving manufacturing accuracy thereof |
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| US7360364B2 (en) * | 2004-12-17 | 2008-04-22 | General Electric Company | Method and apparatus for assembling gas turbine engine combustors |
| US7421843B2 (en) * | 2005-01-15 | 2008-09-09 | Siemens Power Generation, Inc. | Catalytic combustor having fuel flow control responsive to measured combustion parameters |
| US7137256B1 (en) * | 2005-02-28 | 2006-11-21 | Peter Stuttaford | Method of operating a combustion system for increased turndown capability |
| GB2429516B (en) * | 2005-08-27 | 2010-12-29 | Siemens Ind Turbomachinery Ltd | An apparatus for modifying the content of a gaseous fuel |
| RU2300052C1 (ru) * | 2005-11-01 | 2007-05-27 | Сергей Александрович Маяцкий | Форсунка с кислородной подпиткой |
| CN100483029C (zh) * | 2006-01-12 | 2009-04-29 | 中国科学院工程热物理研究所 | 燃用天然气的双预混通道微型燃气轮机燃烧室 |
| US20070220898A1 (en) * | 2006-03-22 | 2007-09-27 | General Electric Company | Secondary fuel nozzle with improved fuel pegs and fuel dispersion method |
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| US7631500B2 (en) * | 2006-09-29 | 2009-12-15 | General Electric Company | Methods and apparatus to facilitate decreasing combustor acoustics |
| US8171736B2 (en) * | 2007-01-30 | 2012-05-08 | Pratt & Whitney Canada Corp. | Combustor with chamfered dome |
| ITTO20070193A1 (it) * | 2007-03-14 | 2008-09-15 | Ansaldo Ricerche S P A | Bruciatore premix di una turbina a gas, in particolare per una microturbina |
| EP1985924A1 (en) * | 2007-04-23 | 2008-10-29 | Siemens Aktiengesellschaft | Swirler |
| US20090019854A1 (en) * | 2007-07-16 | 2009-01-22 | General Electric Company | APPARATUS/METHOD FOR COOLING COMBUSTION CHAMBER/VENTURI IN A LOW NOx COMBUSTOR |
| US7665309B2 (en) | 2007-09-14 | 2010-02-23 | Siemens Energy, Inc. | Secondary fuel delivery system |
| US8387398B2 (en) * | 2007-09-14 | 2013-03-05 | Siemens Energy, Inc. | Apparatus and method for controlling the secondary injection of fuel |
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| EP2107311A1 (en) * | 2008-04-01 | 2009-10-07 | Siemens Aktiengesellschaft | Size scaling of a burner |
| EP2107301B1 (en) * | 2008-04-01 | 2016-01-06 | Siemens Aktiengesellschaft | Gas injection in a burner |
| EP2107300A1 (en) * | 2008-04-01 | 2009-10-07 | Siemens Aktiengesellschaft | Swirler with gas injectors |
| JP5172468B2 (ja) * | 2008-05-23 | 2013-03-27 | 川崎重工業株式会社 | 燃焼装置および燃焼装置の制御方法 |
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-
1993
- 1993-10-27 US US08/141,757 patent/US5394688A/en not_active Expired - Lifetime
-
1994
- 1994-10-06 TW TW083109273A patent/TW248585B/zh active
- 1994-10-07 US US08/319,686 patent/US5479782A/en not_active Expired - Fee Related
- 1994-10-12 AU AU75756/94A patent/AU7575694A/en not_active Abandoned
- 1994-10-25 DE DE69413352T patent/DE69413352T2/de not_active Expired - Fee Related
- 1994-10-25 ES ES94307823T patent/ES2123102T3/es not_active Expired - Lifetime
- 1994-10-25 EP EP94307823A patent/EP0654639B1/en not_active Expired - Lifetime
- 1994-10-26 CA CA002134419A patent/CA2134419A1/en not_active Abandoned
- 1994-10-26 KR KR1019940027387A patent/KR950011818A/ko not_active Abandoned
- 1994-10-27 CN CN94117610A patent/CN1107933A/zh active Pending
- 1994-10-27 JP JP6289135A patent/JPH07180835A/ja not_active Withdrawn
Also Published As
| Publication number | Publication date |
|---|---|
| EP0654639A1 (en) | 1995-05-24 |
| TW248585B (enExample) | 1995-06-01 |
| CN1107933A (zh) | 1995-09-06 |
| DE69413352D1 (de) | 1998-10-22 |
| EP0654639B1 (en) | 1998-09-16 |
| CA2134419A1 (en) | 1995-04-28 |
| AU7575694A (en) | 1995-05-18 |
| JPH07180835A (ja) | 1995-07-18 |
| US5479782A (en) | 1996-01-02 |
| US5394688A (en) | 1995-03-07 |
| ES2123102T3 (es) | 1999-01-01 |
| DE69413352T2 (de) | 1999-05-12 |
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