FR2901314B1 - Appareil et procede de compensation de la dilatation thermique differentielle de composants d'injecteur - Google Patents
Appareil et procede de compensation de la dilatation thermique differentielle de composants d'injecteurInfo
- Publication number
- FR2901314B1 FR2901314B1 FR0703515A FR0703515A FR2901314B1 FR 2901314 B1 FR2901314 B1 FR 2901314B1 FR 0703515 A FR0703515 A FR 0703515A FR 0703515 A FR0703515 A FR 0703515A FR 2901314 B1 FR2901314 B1 FR 2901314B1
- Authority
- FR
- France
- Prior art keywords
- thermal expansion
- differential thermal
- injector components
- compensating differential
- compensating
- 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 - Fee Related
Links
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
- F23D11/10—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
- F23D11/106—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting at the burner outlet
- F23D11/107—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting at the burner outlet at least one of both being subjected to a swirling motion
-
- 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
-
- 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
- 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
- F23D2206/00—Burners for specific applications
- F23D2206/10—Turbines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2211/00—Thermal dilatation prevention or compensation
-
- 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
- F23R2900/00005—Preventing fatigue failures or reducing mechanical stress in gas turbine components
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US80186406P | 2006-05-19 | 2006-05-19 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2901314A1 FR2901314A1 (fr) | 2007-11-23 |
FR2901314B1 true FR2901314B1 (fr) | 2011-11-25 |
Family
ID=38234666
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0703515A Expired - Fee Related FR2901314B1 (fr) | 2006-05-19 | 2007-05-16 | Appareil et procede de compensation de la dilatation thermique differentielle de composants d'injecteur |
Country Status (5)
Country | Link |
---|---|
US (1) | US7900456B2 (fr) |
JP (1) | JP2007309641A (fr) |
DE (1) | DE102007023266B4 (fr) |
FR (1) | FR2901314B1 (fr) |
GB (1) | GB2438316B (fr) |
Families Citing this family (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7966819B2 (en) * | 2006-09-26 | 2011-06-28 | Parker-Hannifin Corporation | Vibration damper for fuel injector |
US20090218421A1 (en) * | 2008-02-28 | 2009-09-03 | General Electric Company | Combustor fuel nozzle construction |
US8091362B2 (en) * | 2008-08-20 | 2012-01-10 | Woodward, Inc. | Fuel injector sans support/stem |
US7827795B2 (en) * | 2008-09-19 | 2010-11-09 | Woodward Governor Company | Active thermal protection for fuel injectors |
US7832377B2 (en) * | 2008-09-19 | 2010-11-16 | Woodward Governor Company | Thermal protection for fuel injectors |
US8205643B2 (en) * | 2008-10-16 | 2012-06-26 | Woodward, Inc. | Multi-tubular fluid transfer conduit |
US20100205970A1 (en) * | 2009-02-19 | 2010-08-19 | General Electric Company | Systems, Methods, and Apparatus Providing a Secondary Fuel Nozzle Assembly |
US9010119B2 (en) * | 2010-11-03 | 2015-04-21 | General Electric Company | Premixing nozzle |
US20120137691A1 (en) * | 2010-12-01 | 2012-06-07 | Bottcher Andreas | Gas turbine assembly and method therefor |
CN102434880A (zh) * | 2011-11-30 | 2012-05-02 | 中国船舶重工集团公司第七�三研究所 | 一种增压锅炉燃烧器 |
US9032735B2 (en) * | 2012-04-26 | 2015-05-19 | General Electric Company | Combustor and a method for assembling the combustor |
US9534787B2 (en) | 2013-03-12 | 2017-01-03 | General Electric Company | Micromixing cap assembly |
US9651259B2 (en) | 2013-03-12 | 2017-05-16 | General Electric Company | Multi-injector micromixing system |
US9528444B2 (en) * | 2013-03-12 | 2016-12-27 | General Electric Company | System having multi-tube fuel nozzle with floating arrangement of mixing tubes |
US9765973B2 (en) | 2013-03-12 | 2017-09-19 | General Electric Company | System and method for tube level air flow conditioning |
US9671112B2 (en) | 2013-03-12 | 2017-06-06 | General Electric Company | Air diffuser for a head end of a combustor |
US9759425B2 (en) | 2013-03-12 | 2017-09-12 | General Electric Company | System and method having multi-tube fuel nozzle with multiple fuel injectors |
US9650959B2 (en) | 2013-03-12 | 2017-05-16 | General Electric Company | Fuel-air mixing system with mixing chambers of various lengths for gas turbine system |
US9366439B2 (en) | 2013-03-12 | 2016-06-14 | General Electric Company | Combustor end cover with fuel plenums |
US9347668B2 (en) | 2013-03-12 | 2016-05-24 | General Electric Company | End cover configuration and assembly |
GB201310429D0 (en) * | 2013-06-12 | 2013-07-24 | Rolls Royce Plc | Combustion equipment for use in a gas turbine engine |
US9625155B2 (en) | 2014-01-03 | 2017-04-18 | Delavan Inc. | Compensating for thermal expansion via controlled tube buckling |
US20140215828A1 (en) * | 2014-04-07 | 2014-08-07 | Electro-Motive Diesel, Inc. | Valve mounting fixture for an internal combustion engine |
US9739202B2 (en) | 2015-05-12 | 2017-08-22 | Rolls-Royce North American Technologies, Inc. | Thermal adjustment member for a fuel nozzle of a gas turbine engine |
US10955141B2 (en) * | 2017-06-19 | 2021-03-23 | General Electric Company | Dual-fuel fuel nozzle with gas and liquid fuel capability |
US10865714B2 (en) | 2018-03-22 | 2020-12-15 | Woodward. Inc. | Gas turbine engine fuel injector |
US11460037B2 (en) | 2019-03-29 | 2022-10-04 | Pratt & Whitney Canada Corp. | Bearing housing |
FR3105984B1 (fr) * | 2020-01-03 | 2023-07-14 | Safran Aircraft Engines | Système d’injection de carburant antirotatif |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3129891A (en) * | 1964-04-21 | Fuel nozzle | ||
US2548904A (en) * | 1949-09-07 | 1951-04-17 | Westinghouse Electric Corp | Jet engine fuel nozzle holder and mounting |
US3159971A (en) * | 1961-02-24 | 1964-12-08 | Parker Hannifin Corp | Resilient nozzle mount |
US3662959A (en) * | 1970-08-07 | 1972-05-16 | Parker Hannifin Corp | Fuel injection nozzle |
US4258544A (en) * | 1978-09-15 | 1981-03-31 | Caterpillar Tractor Co. | Dual fluid fuel nozzle |
FR2471480A1 (fr) * | 1979-12-13 | 1981-06-19 | Snecma | Dispositif d'injection pour chambre a combustion de moteur a turbine |
US4735044A (en) * | 1980-11-25 | 1988-04-05 | General Electric Company | Dual fuel path stem for a gas turbine engine |
US4649950A (en) * | 1985-11-27 | 1987-03-17 | Ex-Cell-O Corporation | Fuel nozzle assembly with integral valve assembly and inlet wash filter and primary fuel take-off |
US4850196A (en) * | 1987-10-13 | 1989-07-25 | Westinghouse Electric Corp. | Fuel nozzle assembly for a gas turbine engine |
US5105621A (en) * | 1991-08-16 | 1992-04-21 | Parker-Hannifin Corporation | Exhaust system combustor |
US5423178A (en) * | 1992-09-28 | 1995-06-13 | Parker-Hannifin Corporation | Multiple passage cooling circuit method and device for gas turbine engine fuel nozzle |
US5701732A (en) * | 1995-01-24 | 1997-12-30 | Delavan Inc. | Method and apparatus for purging of gas turbine injectors |
EP0886744B1 (fr) * | 1996-03-13 | 2001-05-23 | Parker Hannifin Corporation | Buse a bouclier thermique interieur |
FR2748553B1 (fr) * | 1996-05-09 | 1998-06-19 | Snecma | Systeme d'injection a geometrie variable adoptant un debit d'air en fonction du regime moteur |
US6321541B1 (en) * | 1999-04-01 | 2001-11-27 | Parker-Hannifin Corporation | Multi-circuit multi-injection point atomizer |
US6755024B1 (en) * | 2001-08-23 | 2004-06-29 | Delavan Inc. | Multiplex injector |
US6523350B1 (en) * | 2001-10-09 | 2003-02-25 | General Electric Company | Fuel injector fuel conduits with multiple laminated fuel strips |
US6718770B2 (en) | 2002-06-04 | 2004-04-13 | General Electric Company | Fuel injector laminated fuel strip |
-
2007
- 2007-04-09 US US11/784,658 patent/US7900456B2/en not_active Expired - Fee Related
- 2007-05-16 FR FR0703515A patent/FR2901314B1/fr not_active Expired - Fee Related
- 2007-05-18 DE DE102007023266.9A patent/DE102007023266B4/de not_active Expired - Fee Related
- 2007-05-18 JP JP2007132386A patent/JP2007309641A/ja active Pending
- 2007-05-18 GB GB0709553A patent/GB2438316B/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
GB2438316A (en) | 2007-11-21 |
US20070283931A1 (en) | 2007-12-13 |
JP2007309641A (ja) | 2007-11-29 |
GB0709553D0 (en) | 2007-06-27 |
FR2901314A1 (fr) | 2007-11-23 |
DE102007023266B4 (de) | 2018-07-05 |
US7900456B2 (en) | 2011-03-08 |
GB2438316B (en) | 2011-09-07 |
DE102007023266A1 (de) | 2007-11-22 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 10 |
|
PLFP | Fee payment |
Year of fee payment: 11 |
|
PLFP | Fee payment |
Year of fee payment: 12 |
|
PLFP | Fee payment |
Year of fee payment: 13 |
|
PLFP | Fee payment |
Year of fee payment: 14 |
|
ST | Notification of lapse |
Effective date: 20220105 |