DE69306290T2 - Geteilter Mittelkörper für eine Ringbrennkammer - Google Patents
Geteilter Mittelkörper für eine RingbrennkammerInfo
- Publication number
- DE69306290T2 DE69306290T2 DE69306290T DE69306290T DE69306290T2 DE 69306290 T2 DE69306290 T2 DE 69306290T2 DE 69306290 T DE69306290 T DE 69306290T DE 69306290 T DE69306290 T DE 69306290T DE 69306290 T2 DE69306290 T2 DE 69306290T2
- Authority
- DE
- Germany
- Prior art keywords
- combustion chamber
- middle body
- annular combustion
- split middle
- split
- 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
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
- F23R3/42—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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/34—Feeding into different combustion zones
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Spray-Type Burners (AREA)
- Gas Burners (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US85976092A | 1992-03-30 | 1992-03-30 |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69306290D1 DE69306290D1 (de) | 1997-01-16 |
DE69306290T2 true DE69306290T2 (de) | 1997-06-26 |
Family
ID=25331637
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69306290T Expired - Lifetime DE69306290T2 (de) | 1992-03-30 | 1993-03-25 | Geteilter Mittelkörper für eine Ringbrennkammer |
Country Status (5)
Country | Link |
---|---|
US (1) | US5375420A (de) |
EP (1) | EP0564170B1 (de) |
JP (1) | JP2599883B2 (de) |
CA (1) | CA2089285C (de) |
DE (1) | DE69306290T2 (de) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2706021B1 (fr) * | 1993-06-03 | 1995-07-07 | Snecma | Chambre de combustion comprenant un ensemble séparateur de gaz. |
FR2712379B1 (fr) * | 1993-11-10 | 1995-12-29 | Snecma | Chambre de combustion pour turbomachine munie d'un séparateur des gaz. |
US5421158A (en) * | 1994-10-21 | 1995-06-06 | General Electric Company | Segmented centerbody for a double annular combustor |
US5657633A (en) * | 1995-12-29 | 1997-08-19 | General Electric Company | Centerbody for a multiple annular combustor |
US5682747A (en) * | 1996-04-10 | 1997-11-04 | General Electric Company | Gas turbine combustor heat shield of casted super alloy |
US5970716A (en) * | 1997-10-02 | 1999-10-26 | General Electric Company | Apparatus for retaining centerbody between adjacent domes of multiple annular combustor employing interference and clamping fits |
FR2777634B1 (fr) * | 1998-04-16 | 2000-05-19 | Snecma | Separateur pour chambre de combustion a deux tetes |
US6286302B1 (en) * | 1999-04-01 | 2001-09-11 | General Electric Company | Venturi for use in the swirl cup package of a gas turbine combustor having water injected therein |
GB2373319B (en) * | 2001-03-12 | 2005-03-30 | Rolls Royce Plc | Combustion apparatus |
US6553767B2 (en) * | 2001-06-11 | 2003-04-29 | General Electric Company | Gas turbine combustor liner with asymmetric dilution holes machined from a single piece form |
US6651437B2 (en) * | 2001-12-21 | 2003-11-25 | General Electric Company | Combustor liner and method for making thereof |
US7003959B2 (en) * | 2002-12-31 | 2006-02-28 | General Electric Company | High temperature splash plate for temperature reduction by optical reflection and process for manufacturing |
US6782620B2 (en) * | 2003-01-28 | 2004-08-31 | General Electric Company | Methods for replacing a portion of a combustor dome assembly |
FR2856468B1 (fr) * | 2003-06-17 | 2007-11-23 | Snecma Moteurs | Chambre de combustion annulaire de turbomachine |
US6868675B1 (en) * | 2004-01-09 | 2005-03-22 | Honeywell International Inc. | Apparatus and method for controlling combustor liner carbon formation |
FR2958372B1 (fr) * | 2010-03-30 | 2013-05-17 | Snecma | Chambre de combustion de turbomachine. |
US9494081B2 (en) | 2013-05-09 | 2016-11-15 | Siemens Aktiengesellschaft | Turbine engine shutdown temperature control system with an elongated ejector |
US10119424B2 (en) | 2015-05-08 | 2018-11-06 | General Electric Company | Attachment assembly and gas turbine engine with attachment assembly |
US20230408098A1 (en) * | 2022-05-25 | 2023-12-21 | General Electric Company | Combustor with secondary fuel nozzle in dilution fence |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL69245C (de) * | 1946-01-09 | |||
GB758213A (en) * | 1954-03-03 | 1956-10-03 | Parsons & Marine Eng Turbine | Improvements in and relating to cylindrical combustion chambers or furnaces |
US4555901A (en) * | 1972-12-19 | 1985-12-03 | General Electric Company | Combustion chamber construction |
US3952504A (en) * | 1973-12-14 | 1976-04-27 | Joseph Lucas (Industries) Limited | Flame tubes |
US4194358A (en) * | 1977-12-15 | 1980-03-25 | General Electric Company | Double annular combustor configuration |
US4414816A (en) * | 1980-04-02 | 1983-11-15 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Combustor liner construction |
JPS5914693A (ja) * | 1982-07-16 | 1984-01-25 | 松下電器産業株式会社 | プリント基板装置の製造方法 |
US4567730A (en) * | 1983-10-03 | 1986-02-04 | General Electric Company | Shielded combustor |
JPS6120770A (ja) * | 1984-07-10 | 1986-01-29 | Matsushita Electric Ind Co Ltd | プラテン駆動装置 |
DE3519938A1 (de) * | 1985-06-04 | 1986-12-04 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Brennkammereinrichtung |
JPH0195224A (ja) * | 1987-10-08 | 1989-04-13 | Tokyo Electric Power Co Inc:The | セラミック燃焼器 |
FR2644209B1 (fr) * | 1989-03-08 | 1991-05-03 | Snecma | Chemise de protection thermique pour canal chaud de turboreacteur |
US5197289A (en) * | 1990-11-26 | 1993-03-30 | General Electric Company | Double dome combustor |
-
1993
- 1993-02-11 CA CA002089285A patent/CA2089285C/en not_active Expired - Fee Related
- 1993-03-25 EP EP93302309A patent/EP0564170B1/de not_active Expired - Lifetime
- 1993-03-25 DE DE69306290T patent/DE69306290T2/de not_active Expired - Lifetime
- 1993-03-29 JP JP5068998A patent/JP2599883B2/ja not_active Expired - Fee Related
- 1993-08-12 US US08/105,772 patent/US5375420A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
CA2089285A1 (en) | 1993-10-01 |
US5375420A (en) | 1994-12-27 |
EP0564170A1 (de) | 1993-10-06 |
JPH0618043A (ja) | 1994-01-25 |
DE69306290D1 (de) | 1997-01-16 |
CA2089285C (en) | 2002-06-25 |
JP2599883B2 (ja) | 1997-04-16 |
EP0564170B1 (de) | 1996-12-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8328 | Change in the person/name/address of the agent |
Representative=s name: ROEGER UND KOLLEGEN, 73728 ESSLINGEN |