GB2107448B - Gas turbine engine combustion chambers - Google Patents
Gas turbine engine combustion chambersInfo
- Publication number
- GB2107448B GB2107448B GB08033850A GB8033850A GB2107448B GB 2107448 B GB2107448 B GB 2107448B GB 08033850 A GB08033850 A GB 08033850A GB 8033850 A GB8033850 A GB 8033850A GB 2107448 B GB2107448 B GB 2107448B
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas turbine
- turbine engine
- combustion chambers
- engine combustion
- chambers
- 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
Links
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
-
- 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
- F23R3/02—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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB08033850A GB2107448B (en) | 1980-10-21 | 1980-10-21 | Gas turbine engine combustion chambers |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB08033850A GB2107448B (en) | 1980-10-21 | 1980-10-21 | Gas turbine engine combustion chambers |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2107448A GB2107448A (en) | 1983-04-27 |
GB2107448B true GB2107448B (en) | 1984-06-06 |
Family
ID=10516795
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08033850A Expired GB2107448B (en) | 1980-10-21 | 1980-10-21 | Gas turbine engine combustion chambers |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2107448B (en) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2221291A (en) * | 1988-07-27 | 1990-01-31 | Rolls Royce Plc | Improvements in or relating to combustion chambers chambers for gas turbines engines |
US5220795A (en) * | 1991-04-16 | 1993-06-22 | General Electric Company | Method and apparatus for injecting dilution air |
US5235814A (en) * | 1991-08-01 | 1993-08-17 | General Electric Company | Flashback resistant fuel staged premixed combustor |
JPH05196232A (en) * | 1991-08-01 | 1993-08-06 | General Electric Co <Ge> | Back fire-resistant fuel staging type premixed combustion apparatus |
US5524438A (en) * | 1994-12-15 | 1996-06-11 | United Technologies Corporation | Segmented bulkhead liner for a gas turbine combustor |
US5581999A (en) * | 1994-12-15 | 1996-12-10 | United Technologies Corporation | Bulkhead liner with raised lip |
DE4444961A1 (en) * | 1994-12-16 | 1996-06-20 | Mtu Muenchen Gmbh | Device for cooling in particular the rear wall of the flame tube of a combustion chamber for gas turbine engines |
DE10048864A1 (en) * | 2000-10-02 | 2002-04-11 | Rolls Royce Deutschland | Combustion chamber head for a gas turbine |
US6751961B2 (en) | 2002-05-14 | 2004-06-22 | United Technologies Corporation | Bulkhead panel for use in a combustion chamber of a gas turbine engine |
US6976363B2 (en) | 2003-08-11 | 2005-12-20 | General Electric Company | Combustor dome assembly of a gas turbine engine having a contoured swirler |
EP2182285A1 (en) | 2008-10-29 | 2010-05-05 | Siemens Aktiengesellschaft | Burner insert for a gas turbine combustion chamber and gas turbine |
DE102011014670A1 (en) | 2011-03-22 | 2012-09-27 | Rolls-Royce Deutschland Ltd & Co Kg | Segmented combustion chamber head |
-
1980
- 1980-10-21 GB GB08033850A patent/GB2107448B/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB2107448A (en) | 1983-04-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |