FR2885201B1 - Chambre de combustion aisement demontable a performance aerodynamique amelioree - Google Patents
Chambre de combustion aisement demontable a performance aerodynamique amelioreeInfo
- Publication number
- FR2885201B1 FR2885201B1 FR0504283A FR0504283A FR2885201B1 FR 2885201 B1 FR2885201 B1 FR 2885201B1 FR 0504283 A FR0504283 A FR 0504283A FR 0504283 A FR0504283 A FR 0504283A FR 2885201 B1 FR2885201 B1 FR 2885201B1
- Authority
- FR
- France
- Prior art keywords
- combustion chamber
- aerodynamic performance
- improved aerodynamic
- easily dismantling
- dismantling
- 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.)
- Active
Links
- 238000002485 combustion reaction 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
- F23R3/02—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
-
- 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
- F23R3/002—Wall structures
-
- 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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
-
- 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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/60—Support structures; Attaching or mounting 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
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00017—Assembling combustion chamber liners or subparts
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
- Fuel-Injection Apparatus (AREA)
- Portable Nailing Machines And Staplers (AREA)
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0504283A FR2885201B1 (fr) | 2005-04-28 | 2005-04-28 | Chambre de combustion aisement demontable a performance aerodynamique amelioree |
EP06112766.8A EP1717516B1 (fr) | 2005-04-28 | 2006-04-19 | Chambre de combustion aisément démontable à performance aérodynamique améliorée |
US11/410,068 US7637111B2 (en) | 2005-04-28 | 2006-04-25 | Easily demountable combustion chamber with improved aerodynamic performance |
JP2006120123A JP2006307854A (ja) | 2005-04-28 | 2006-04-25 | 改善された空力性能を備えた、容易に取り外しできる燃焼チャンバ |
CA2544957A CA2544957C (fr) | 2005-04-28 | 2006-04-26 | Chambre de combustion aisement demontable a performance aerodynamique amelioree |
RU2006114416/06A RU2411412C2 (ru) | 2005-04-28 | 2006-04-27 | Демонтируемая камера сгорания с улучшенными аэродинамическими характеристиками |
CNA2006100781482A CN1854610A (zh) | 2005-04-28 | 2006-04-28 | 空气动力性能提高且易于拆卸的燃烧室 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0504283A FR2885201B1 (fr) | 2005-04-28 | 2005-04-28 | Chambre de combustion aisement demontable a performance aerodynamique amelioree |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2885201A1 FR2885201A1 (fr) | 2006-11-03 |
FR2885201B1 true FR2885201B1 (fr) | 2010-09-17 |
Family
ID=35500968
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0504283A Active FR2885201B1 (fr) | 2005-04-28 | 2005-04-28 | Chambre de combustion aisement demontable a performance aerodynamique amelioree |
Country Status (7)
Country | Link |
---|---|
US (1) | US7637111B2 (fr) |
EP (1) | EP1717516B1 (fr) |
JP (1) | JP2006307854A (fr) |
CN (1) | CN1854610A (fr) |
CA (1) | CA2544957C (fr) |
FR (1) | FR2885201B1 (fr) |
RU (1) | RU2411412C2 (fr) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8109098B2 (en) * | 2006-05-04 | 2012-02-07 | Siemens Energy, Inc. | Combustor liner for gas turbine engine |
FR2911668B1 (fr) * | 2007-01-18 | 2009-03-20 | Snecma Sa | Chambre de combustion d'une turbomachine |
FR2911669B1 (fr) * | 2007-01-23 | 2011-09-16 | Snecma | Carenage pour chambre de combustion, chambre de combustion en etant equipee et turboreacteur les comportant. |
FR2920525B1 (fr) * | 2007-08-31 | 2014-06-13 | Snecma | Separateur pour alimentation de l'air de refroidissement d'une turbine |
FR2964725B1 (fr) * | 2010-09-14 | 2012-10-12 | Snecma | Carenage aerodynamique pour fond de chambre de combustion |
US8938978B2 (en) * | 2011-05-03 | 2015-01-27 | General Electric Company | Gas turbine engine combustor with lobed, three dimensional contouring |
US8938976B2 (en) * | 2011-05-20 | 2015-01-27 | Siemens Energy, Inc. | Structural frame for gas turbine combustion cap assembly |
FR2976346B1 (fr) * | 2011-06-08 | 2013-07-05 | Turbomeca | Chambre de combustion annulaire de turbomachine |
FR2998038B1 (fr) * | 2012-11-09 | 2017-12-08 | Snecma | Chambre de combustion pour une turbomachine |
DE102015213629A1 (de) * | 2015-07-20 | 2017-01-26 | Rolls-Royce Deutschland Ltd & Co Kg | Abdeckteil und Brennkammerbaugruppe für eine Gasturbine |
US9995175B2 (en) * | 2016-06-29 | 2018-06-12 | General Electric Company | System and method for gas bearing support of turbine |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3422620A (en) * | 1967-05-04 | 1969-01-21 | Westinghouse Electric Corp | Combustion apparatus |
US3854285A (en) * | 1973-02-26 | 1974-12-17 | Gen Electric | Combustor dome assembly |
US4411134A (en) * | 1981-10-26 | 1983-10-25 | Moir David L | Apparatus for the repair and replacement of transition ducts on jet engines and bracket therefor |
FR2662784B1 (fr) * | 1990-06-05 | 1992-08-14 | Snecma | Ensemble d'injection pour turbomachine, comprenant un bol de prevaporisation. |
JP2597800B2 (ja) * | 1992-06-12 | 1997-04-09 | ゼネラル・エレクトリック・カンパニイ | ガスタービンエンジン用燃焼器 |
DE69930455T2 (de) * | 1998-11-12 | 2006-11-23 | Mitsubishi Heavy Industries, Ltd. | Gasturbinenbrennkammer |
FR2825779B1 (fr) * | 2001-06-06 | 2003-08-29 | Snecma Moteurs | Chambre de combustion munie d'un systeme de fixation de fond de chambre |
FR2855249B1 (fr) * | 2003-05-20 | 2005-07-08 | Snecma Moteurs | Chambre de combustion ayant une liaison souple entre un fond de chambre et une paroi de chambre |
US7415826B2 (en) * | 2005-07-25 | 2008-08-26 | General Electric Company | Free floating mixer assembly for combustor of a gas turbine engine |
-
2005
- 2005-04-28 FR FR0504283A patent/FR2885201B1/fr active Active
-
2006
- 2006-04-19 EP EP06112766.8A patent/EP1717516B1/fr active Active
- 2006-04-25 US US11/410,068 patent/US7637111B2/en active Active
- 2006-04-25 JP JP2006120123A patent/JP2006307854A/ja not_active Withdrawn
- 2006-04-26 CA CA2544957A patent/CA2544957C/fr active Active
- 2006-04-27 RU RU2006114416/06A patent/RU2411412C2/ru active
- 2006-04-28 CN CNA2006100781482A patent/CN1854610A/zh active Pending
Also Published As
Publication number | Publication date |
---|---|
US7637111B2 (en) | 2009-12-29 |
FR2885201A1 (fr) | 2006-11-03 |
JP2006307854A (ja) | 2006-11-09 |
CA2544957C (fr) | 2014-12-23 |
RU2006114416A (ru) | 2007-11-10 |
RU2411412C2 (ru) | 2011-02-10 |
EP1717516A1 (fr) | 2006-11-02 |
EP1717516B1 (fr) | 2019-04-03 |
CA2544957A1 (fr) | 2006-10-28 |
CN1854610A (zh) | 2006-11-01 |
US20060242939A1 (en) | 2006-11-02 |
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Legal Events
Date | Code | Title | Description |
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CD | Change of name or company name | ||
PLFP | Fee payment |
Year of fee payment: 12 |
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PLFP | Fee payment |
Year of fee payment: 13 |
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CD | Change of name or company name |
Owner name: SNECMA, FR Effective date: 20170713 |
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PLFP | Fee payment |
Year of fee payment: 14 |
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PLFP | Fee payment |
Year of fee payment: 16 |
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PLFP | Fee payment |
Year of fee payment: 17 |
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PLFP | Fee payment |
Year of fee payment: 18 |
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PLFP | Fee payment |
Year of fee payment: 19 |
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PLFP | Fee payment |
Year of fee payment: 20 |