GB2261281B - A combustion-chamber casting for a gas turbine - Google Patents
A combustion-chamber casting for a gas turbineInfo
- Publication number
- GB2261281B GB2261281B GB9123777A GB9123777A GB2261281B GB 2261281 B GB2261281 B GB 2261281B GB 9123777 A GB9123777 A GB 9123777A GB 9123777 A GB9123777 A GB 9123777A GB 2261281 B GB2261281 B GB 2261281B
- Authority
- GB
- United Kingdom
- Prior art keywords
- combustion
- gas turbine
- chamber casting
- casting
- 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.)
- Expired - Fee Related
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
- F23R3/08—Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections
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 (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9123777A GB2261281B (en) | 1991-11-08 | 1991-11-08 | A combustion-chamber casting for a gas turbine |
DE19914142413 DE4142413C2 (en) | 1991-11-08 | 1991-12-20 | Combustion chamber housing of a gas turbine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9123777A GB2261281B (en) | 1991-11-08 | 1991-11-08 | A combustion-chamber casting for a gas turbine |
Publications (3)
Publication Number | Publication Date |
---|---|
GB9123777D0 GB9123777D0 (en) | 1992-01-02 |
GB2261281A GB2261281A (en) | 1993-05-12 |
GB2261281B true GB2261281B (en) | 1995-01-18 |
Family
ID=10704317
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9123777A Expired - Fee Related GB2261281B (en) | 1991-11-08 | 1991-11-08 | A combustion-chamber casting for a gas turbine |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE4142413C2 (en) |
GB (1) | GB2261281B (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19528406A1 (en) * | 1995-08-02 | 1997-02-06 | Bmw Rolls Royce Gmbh | Gas turbine combustion chamber with air transfer ports - has shot blasted, rolled raster or fluting design upstream of ports to specified raster dimension |
DE19856458B4 (en) * | 1998-12-03 | 2017-08-10 | General Electric Technology Gmbh | Cooling device for targeted exposure to a surface to be cooled with a gaseous cooling medium and method for this purpose |
US6468669B1 (en) * | 1999-05-03 | 2002-10-22 | General Electric Company | Article having turbulation and method of providing turbulation on an article |
US6399217B1 (en) * | 1999-12-20 | 2002-06-04 | General Electric Company | Article surface with metal wires and method for making |
DE10159668A1 (en) * | 2001-12-05 | 2003-06-18 | Rolls Royce Deutschland | Combustion chamber head has at least one turbulence-creating element on flow surface of cover |
DE10239534A1 (en) * | 2002-08-23 | 2004-04-22 | Man Turbomaschinen Ag | Hot gas leading gas manifold |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2093177A (en) * | 1981-01-22 | 1982-08-25 | United Technologies Corp | Combustion liner cooling scheme |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DD18719A (en) * | ||||
US3826082A (en) * | 1973-03-30 | 1974-07-30 | Gen Electric | Combustion liner cooling slot stabilizing dimple |
DE3942271A1 (en) * | 1989-12-21 | 1991-07-04 | Mtu Maintenance Gmbh | Repair method for gas turbine flame tubes - involves cutting away damaged part and welding on new ring |
-
1991
- 1991-11-08 GB GB9123777A patent/GB2261281B/en not_active Expired - Fee Related
- 1991-12-20 DE DE19914142413 patent/DE4142413C2/en not_active Expired - Fee Related
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2093177A (en) * | 1981-01-22 | 1982-08-25 | United Technologies Corp | Combustion liner cooling scheme |
Also Published As
Publication number | Publication date |
---|---|
DE4142413A1 (en) | 1993-05-19 |
GB9123777D0 (en) | 1992-01-02 |
GB2261281A (en) | 1993-05-12 |
DE4142413C2 (en) | 1993-12-09 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20051108 |