GB201306124D0 - A combustion chamber - Google Patents
A combustion chamberInfo
- Publication number
- GB201306124D0 GB201306124D0 GB201306124A GB201306124A GB201306124D0 GB 201306124 D0 GB201306124 D0 GB 201306124D0 GB 201306124 A GB201306124 A GB 201306124A GB 201306124 A GB201306124 A GB 201306124A GB 201306124 D0 GB201306124 D0 GB 201306124D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- combustion chamber
- combustion
- chamber
- 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.)
- Withdrawn
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
- F23R3/06—Arrangement of apertures along the flame tube
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB201306124A GB2512642A (en) | 2013-04-05 | 2013-04-05 | A combustion chamber |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB201306124A GB2512642A (en) | 2013-04-05 | 2013-04-05 | A combustion chamber |
Publications (2)
Publication Number | Publication Date |
---|---|
GB201306124D0 true GB201306124D0 (en) | 2013-05-22 |
GB2512642A GB2512642A (en) | 2014-10-08 |
Family
ID=48483352
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB201306124A Withdrawn GB2512642A (en) | 2013-04-05 | 2013-04-05 | A combustion chamber |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2512642A (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11686473B2 (en) | 2021-11-11 | 2023-06-27 | General Electric Company | Combustion liner |
US11808454B2 (en) | 2021-11-11 | 2023-11-07 | General Electric Company | Combustion liner |
US11754284B2 (en) | 2021-11-11 | 2023-09-12 | General Electric Company | Combustion liner |
CN116221774A (en) | 2021-12-06 | 2023-06-06 | 通用电气公司 | Variable dilution hole design for combustor liner |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2890156A1 (en) * | 2005-08-31 | 2007-03-02 | Snecma | Turbomachine e.g. aircraft turbojet, combustion chamber, has internal and external flanges with orifices of triangular shape, where successive triangular orifices are arranged in staggered and head-to-tail configuration |
-
2013
- 2013-04-05 GB GB201306124A patent/GB2512642A/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
GB2512642A (en) | 2014-10-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |