DE69932318D1 - FUEL INJECTION DEVICE FOR A GAS TURBINE BURNING CHAMBER - Google Patents
FUEL INJECTION DEVICE FOR A GAS TURBINE BURNING CHAMBERInfo
- Publication number
- DE69932318D1 DE69932318D1 DE69932318T DE69932318T DE69932318D1 DE 69932318 D1 DE69932318 D1 DE 69932318D1 DE 69932318 T DE69932318 T DE 69932318T DE 69932318 T DE69932318 T DE 69932318T DE 69932318 D1 DE69932318 D1 DE 69932318D1
- Authority
- DE
- Germany
- Prior art keywords
- fuel injection
- gas turbine
- injection device
- burning chamber
- turbine burning
- 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.)
- Expired - Lifetime
Links
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
- 239000000446 fuel Substances 0.000 title 1
- 238000002347 injection Methods 0.000 title 1
- 239000007924 injection Substances 0.000 title 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/36—Details, e.g. burner cooling means, noise reduction means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/36—Details, e.g. burner cooling means, noise reduction means
- F23D11/40—Mixing tubes or chambers; Burner heads
- F23D11/402—Mixing chambers downstream of the nozzle
-
- 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
- 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
- F23D—BURNERS
- F23D2206/00—Burners for specific applications
- F23D2206/10—Turbines
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
- Spray-Type Burners (AREA)
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10364998P | 1998-10-09 | 1998-10-09 | |
US103649P | 1998-10-09 | ||
US398558 | 1999-09-17 | ||
US09/398,558 US6357237B1 (en) | 1998-10-09 | 1999-09-17 | Fuel injection assembly for gas turbine engine combustor |
PCT/US1999/022661 WO2000022347A1 (en) | 1998-10-09 | 1999-09-29 | Fuel injection assembly for gas turbine engine combustor |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69932318D1 true DE69932318D1 (en) | 2006-08-24 |
DE69932318T2 DE69932318T2 (en) | 2007-07-05 |
Family
ID=26800697
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69932318T Expired - Lifetime DE69932318T2 (en) | 1998-10-09 | 1999-09-29 | FUEL INJECTION DEVICE FOR A GAS TURBINE BURNING CHAMBER |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP1046010B1 (en) |
JP (1) | JP4323723B2 (en) |
DE (1) | DE69932318T2 (en) |
WO (1) | WO2000022347A1 (en) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6298667B1 (en) * | 2000-06-22 | 2001-10-09 | General Electric Company | Modular combustor dome |
US6481209B1 (en) * | 2000-06-28 | 2002-11-19 | General Electric Company | Methods and apparatus for decreasing combustor emissions with swirl stabilized mixer |
US7654088B2 (en) * | 2004-02-27 | 2010-02-02 | Pratt & Whitney Canada Corp. | Dual conduit fuel manifold for gas turbine engine |
JP4670035B2 (en) * | 2004-06-25 | 2011-04-13 | 独立行政法人 宇宙航空研究開発機構 | Gas turbine combustor |
JP4882422B2 (en) * | 2006-02-28 | 2012-02-22 | 株式会社日立製作所 | Gas turbine combustor and combustion method of combustion apparatus |
EP1936276A1 (en) * | 2006-12-22 | 2008-06-25 | Siemens Aktiengesellschaft | Gas turbine burner |
US7891192B2 (en) * | 2007-08-28 | 2011-02-22 | General Electric Company | Gas turbine engine combustor assembly having integrated control valves |
EP2189720A1 (en) * | 2008-11-21 | 2010-05-26 | Siemens Aktiengesellschaft | Burner assembly |
ES2389482T3 (en) * | 2010-02-19 | 2012-10-26 | Siemens Aktiengesellschaft | Burner system |
EP2402652A1 (en) * | 2010-07-01 | 2012-01-04 | Siemens Aktiengesellschaft | Burner |
JP6621658B2 (en) | 2015-12-22 | 2019-12-18 | 川崎重工業株式会社 | Fuel injection device |
US11029029B2 (en) | 2019-01-03 | 2021-06-08 | General Electric Company | Fuel injector heat exchanger assembly |
US20240093869A1 (en) * | 2022-09-15 | 2024-03-21 | Pratt & Whitney Canada Corp. | Fuel nozzle |
GB2629434A (en) * | 2023-04-28 | 2024-10-30 | Siemens Energy Global Gmbh & Co Kg | Fuel lance for burner of gas turbine engine |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5423178A (en) * | 1992-09-28 | 1995-06-13 | Parker-Hannifin Corporation | Multiple passage cooling circuit method and device for gas turbine engine fuel nozzle |
FR2721694B1 (en) * | 1994-06-22 | 1996-07-19 | Snecma | Cooling of the take-off injector of a combustion chamber with two heads. |
DE19645961A1 (en) * | 1996-11-07 | 1998-05-14 | Bmw Rolls Royce Gmbh | Fuel injector for a gas turbine combustor with a liquid cooled injector |
-
1999
- 1999-09-29 DE DE69932318T patent/DE69932318T2/en not_active Expired - Lifetime
- 1999-09-29 WO PCT/US1999/022661 patent/WO2000022347A1/en active IP Right Grant
- 1999-09-29 JP JP2000576213A patent/JP4323723B2/en not_active Expired - Fee Related
- 1999-09-29 EP EP99970455A patent/EP1046010B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
WO2000022347A1 (en) | 2000-04-20 |
EP1046010A1 (en) | 2000-10-25 |
JP4323723B2 (en) | 2009-09-02 |
DE69932318T2 (en) | 2007-07-05 |
EP1046010B1 (en) | 2006-07-12 |
JP2002527708A (en) | 2002-08-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |