FR2817016B1 - Procede d'assemblage d'un injecteur de combustible pour chambre de combustion de turbomachine - Google Patents
Procede d'assemblage d'un injecteur de combustible pour chambre de combustion de turbomachineInfo
- Publication number
- FR2817016B1 FR2817016B1 FR0015003A FR0015003A FR2817016B1 FR 2817016 B1 FR2817016 B1 FR 2817016B1 FR 0015003 A FR0015003 A FR 0015003A FR 0015003 A FR0015003 A FR 0015003A FR 2817016 B1 FR2817016 B1 FR 2817016B1
- Authority
- FR
- France
- Prior art keywords
- assembling
- combustion chamber
- fuel injector
- turbomachine combustion
- turbomachine
- 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
- 238000002485 combustion reaction Methods 0.000 title 1
- 239000000446 fuel Substances 0.000 title 1
- 238000000034 method Methods 0.000 title 1
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
- F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
-
- 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
- F23D2214/00—Cooling
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49405—Valve or choke making
- Y10T29/49412—Valve or choke making with assembly, disassembly or composite article making
- Y10T29/49425—Valve or choke making with assembly, disassembly or composite article making including metallurgical bonding
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0015003A FR2817016B1 (fr) | 2000-11-21 | 2000-11-21 | Procede d'assemblage d'un injecteur de combustible pour chambre de combustion de turbomachine |
CA2363305A CA2363305C (fr) | 2000-11-21 | 2001-11-19 | Procede d'assemblage d'un injecteur de combustible pour chambre de combustion de turbomachine |
GB0127823A GB2372474B (en) | 2000-11-21 | 2001-11-20 | A method of assembling a fuel injector for the combustion chamber of a turbomachine |
RU2001131073/06A RU2278331C2 (ru) | 2000-11-21 | 2001-11-20 | Способ сборки топливной форсунки для камеры сгорания и распылитель топливной форсунки |
US09/988,526 US6595000B2 (en) | 2000-11-21 | 2001-11-20 | Method of assembling a fuel injector for the combustion chamber of a turbomachine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0015003A FR2817016B1 (fr) | 2000-11-21 | 2000-11-21 | Procede d'assemblage d'un injecteur de combustible pour chambre de combustion de turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2817016A1 FR2817016A1 (fr) | 2002-05-24 |
FR2817016B1 true FR2817016B1 (fr) | 2003-02-21 |
Family
ID=8856701
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0015003A Expired - Lifetime FR2817016B1 (fr) | 2000-11-21 | 2000-11-21 | Procede d'assemblage d'un injecteur de combustible pour chambre de combustion de turbomachine |
Country Status (5)
Country | Link |
---|---|
US (1) | US6595000B2 (fr) |
CA (1) | CA2363305C (fr) |
FR (1) | FR2817016B1 (fr) |
GB (1) | GB2372474B (fr) |
RU (1) | RU2278331C2 (fr) |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6698207B1 (en) * | 2002-09-11 | 2004-03-02 | Siemens Westinghouse Power Corporation | Flame-holding, single-mode nozzle assembly with tip cooling |
US7117675B2 (en) * | 2002-12-03 | 2006-10-10 | General Electric Company | Cooling of liquid fuel components to eliminate coking |
US6918255B2 (en) * | 2002-12-03 | 2005-07-19 | General Electric Company | Cooling of liquid fuel components to eliminate coking |
US7325402B2 (en) * | 2004-08-04 | 2008-02-05 | Siemens Power Generation, Inc. | Pilot nozzle heat shield having connected tangs |
KR100611060B1 (ko) * | 2004-12-07 | 2006-08-09 | 삼성전자주식회사 | 기판 상으로 용액을 공급하기 위한 장치 |
FR2891314B1 (fr) * | 2005-09-28 | 2015-04-24 | Snecma | Bras d'injecteur anti-cokefaction. |
US8166763B2 (en) * | 2006-09-14 | 2012-05-01 | Solar Turbines Inc. | Gas turbine fuel injector with a removable pilot assembly |
US8286433B2 (en) * | 2007-10-26 | 2012-10-16 | Solar Turbines Inc. | Gas turbine fuel injector with removable pilot liquid tube |
US8393155B2 (en) * | 2007-11-28 | 2013-03-12 | Solar Turbines Incorporated | Gas turbine fuel injector with insulating air shroud |
US8443608B2 (en) * | 2008-02-26 | 2013-05-21 | Delavan Inc | Feed arm for a multiple circuit fuel injector |
EP2196734A1 (fr) * | 2008-12-12 | 2010-06-16 | Siemens Aktiengesellschaft | Lance de combustible pour un brûleur |
US20100263382A1 (en) * | 2009-04-16 | 2010-10-21 | Alfred Albert Mancini | Dual orifice pilot fuel injector |
WO2012156631A1 (fr) | 2011-05-17 | 2012-11-22 | Snecma | Chambre annulaire de combustion pour une turbomachine |
US20130036740A1 (en) * | 2011-08-09 | 2013-02-14 | Ulrich Woerz | Multi-fuel injection nozzle |
US10739005B2 (en) * | 2013-08-16 | 2020-08-11 | Raytheon Technologies Corporation | Cooled fuel injector system for a gas turbine engine |
US9797313B2 (en) * | 2014-01-16 | 2017-10-24 | Pratt & Whitney Canada Corp. | Internal manifold with fuel inlet |
US10934890B2 (en) * | 2014-05-09 | 2021-03-02 | Raytheon Technologies Corporation | Shrouded conduit for arranging a fluid flowpath |
US9915480B2 (en) | 2014-07-03 | 2018-03-13 | United Technologies Corporation | Tube assembly |
US9989257B2 (en) * | 2015-06-24 | 2018-06-05 | Delavan Inc | Cooling in staged fuel systems |
US10054093B2 (en) | 2016-01-05 | 2018-08-21 | Solar Turbines Incorporated | Fuel injector with a center body assembly for liquid prefilm injection |
CA2955613A1 (fr) | 2016-01-28 | 2017-07-28 | Rolls-Royce North American Technologies, Inc. | Echangeur thermique integre comportant une buse de carburant |
US11118784B2 (en) | 2016-01-28 | 2021-09-14 | Rolls-Royce North American Technologies Inc. | Heat exchanger integrated with fuel nozzle |
US10830150B2 (en) | 2016-01-28 | 2020-11-10 | Rolls-Royce Corporation | Fuel heat exchanger with leak management |
CA3000372A1 (fr) * | 2017-05-11 | 2018-11-11 | Rolls-Royce North American Technologies, Inc. | Echangeur thermique integre comportant une buse de carburant |
CA3000460A1 (fr) * | 2017-05-23 | 2018-11-23 | Rolls-Royce Corporation | Echangeur thermique a carburant dote de gestion de fuite |
FR3088969B1 (fr) * | 2018-11-27 | 2021-02-19 | Ifp Energies Now | Injecteur de carburant avec moyens de refroidissement |
US11519332B1 (en) | 2021-05-11 | 2022-12-06 | Rolls-Royce North American Technologies Inc. | Fuel injector with integrated heat exchanger for use in gas turbine engines |
Family Cites Families (7)
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 |
FR2721693B1 (fr) * | 1994-06-22 | 1996-07-19 | Snecma | Procédé et dispositif pour alimenter en carburant et refroidir l'injecteur de décollage d'une chambre de combustion à deux têtes. |
US5988531A (en) * | 1997-11-25 | 1999-11-23 | Solar Turbines | Method of making a fuel injector |
US6098407A (en) * | 1998-06-08 | 2000-08-08 | United Technologies Corporation | Premixing fuel injector with improved secondary fuel-air injection |
US6256995B1 (en) * | 1999-11-29 | 2001-07-10 | Pratt & Whitney Canada Corp. | Simple low cost fuel nozzle support |
US6351948B1 (en) * | 1999-12-02 | 2002-03-05 | Woodward Fst, Inc. | Gas turbine engine fuel injector |
US6665726B1 (en) * | 2000-01-06 | 2003-12-16 | Akamai Technologies, Inc. | Method and system for fault tolerant media streaming over the internet |
-
2000
- 2000-11-21 FR FR0015003A patent/FR2817016B1/fr not_active Expired - Lifetime
-
2001
- 2001-11-19 CA CA2363305A patent/CA2363305C/fr not_active Expired - Lifetime
- 2001-11-20 GB GB0127823A patent/GB2372474B/en not_active Expired - Lifetime
- 2001-11-20 RU RU2001131073/06A patent/RU2278331C2/ru not_active IP Right Cessation
- 2001-11-20 US US09/988,526 patent/US6595000B2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
GB0127823D0 (en) | 2002-01-09 |
CA2363305A1 (fr) | 2002-05-21 |
US6595000B2 (en) | 2003-07-22 |
RU2278331C2 (ru) | 2006-06-20 |
GB2372474A (en) | 2002-08-28 |
GB2372474B (en) | 2004-03-31 |
FR2817016A1 (fr) | 2002-05-24 |
US20020073708A1 (en) | 2002-06-20 |
CA2363305C (fr) | 2011-02-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CL | Concession to grant licences | ||
TP | Transmission of property | ||
TP | Transmission of property | ||
PLFP | Fee payment |
Year of fee payment: 16 |
|
PLFP | Fee payment |
Year of fee payment: 17 |
|
PLFP | Fee payment |
Year of fee payment: 18 |
|
CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170719 |
|
PLFP | Fee payment |
Year of fee payment: 19 |
|
PLFP | Fee payment |
Year of fee payment: 20 |