EP0841520A3 - Gasturbinenbrennkammer - Google Patents
Gasturbinenbrennkammer Download PDFInfo
- Publication number
- EP0841520A3 EP0841520A3 EP97308248A EP97308248A EP0841520A3 EP 0841520 A3 EP0841520 A3 EP 0841520A3 EP 97308248 A EP97308248 A EP 97308248A EP 97308248 A EP97308248 A EP 97308248A EP 0841520 A3 EP0841520 A3 EP 0841520A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- gas turbine
- turbine engine
- cylinder
- engine combustor
- cooling air
- 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.)
- Granted
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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
-
- 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
- F23D—BURNERS
- F23D2214/00—Cooling
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)
- Spray-Type Burners (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB9623195.6A GB9623195D0 (en) | 1996-11-07 | 1996-11-07 | Gas turbine engine combustor |
GB9623195 | 1996-11-07 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0841520A2 EP0841520A2 (de) | 1998-05-13 |
EP0841520A3 true EP0841520A3 (de) | 1999-11-03 |
EP0841520B1 EP0841520B1 (de) | 2003-03-12 |
Family
ID=10802586
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP19970308248 Expired - Lifetime EP0841520B1 (de) | 1996-11-07 | 1997-10-17 | Gasturbinenbrennkammer |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP0841520B1 (de) |
DE (1) | DE69719671T2 (de) |
GB (1) | GB9623195D0 (de) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10048864A1 (de) * | 2000-10-02 | 2002-04-11 | Rolls Royce Deutschland | Brennkammerkopf für eine Gasturbine |
US6923002B2 (en) * | 2003-08-28 | 2005-08-02 | General Electric Company | Combustion liner cap assembly for combustion dynamics reduction |
US8312627B2 (en) * | 2006-12-22 | 2012-11-20 | General Electric Company | Methods for repairing combustor liners |
FR3033028B1 (fr) * | 2015-02-25 | 2019-12-27 | Safran Helicopter Engines | Chambre de combustion de turbomachine comportant une piece penetrante avec ouverture |
GB201701380D0 (en) | 2016-12-20 | 2017-03-15 | Rolls Royce Plc | A combustion chamber and a combustion chamber fuel injector seal |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4914918A (en) * | 1988-09-26 | 1990-04-10 | United Technologies Corporation | Combustor segmented deflector |
US4934145A (en) * | 1988-10-12 | 1990-06-19 | United Technologies Corporation | Combustor bulkhead heat shield assembly |
DE4427222A1 (de) * | 1994-08-01 | 1996-02-08 | Bmw Rolls Royce Gmbh | Hitzeschild für eine Gasturbinen-Brennkammer |
DE19508111A1 (de) * | 1995-03-08 | 1996-09-12 | Bmw Rolls Royce Gmbh | Hitzeschild-Anordnung für eine Gasturbinen-Brennkammer |
-
1996
- 1996-11-07 GB GBGB9623195.6A patent/GB9623195D0/en active Pending
-
1997
- 1997-10-17 DE DE1997619671 patent/DE69719671T2/de not_active Expired - Lifetime
- 1997-10-17 EP EP19970308248 patent/EP0841520B1/de not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4914918A (en) * | 1988-09-26 | 1990-04-10 | United Technologies Corporation | Combustor segmented deflector |
US4934145A (en) * | 1988-10-12 | 1990-06-19 | United Technologies Corporation | Combustor bulkhead heat shield assembly |
DE4427222A1 (de) * | 1994-08-01 | 1996-02-08 | Bmw Rolls Royce Gmbh | Hitzeschild für eine Gasturbinen-Brennkammer |
DE19508111A1 (de) * | 1995-03-08 | 1996-09-12 | Bmw Rolls Royce Gmbh | Hitzeschild-Anordnung für eine Gasturbinen-Brennkammer |
Also Published As
Publication number | Publication date |
---|---|
DE69719671T2 (de) | 2003-08-14 |
EP0841520A2 (de) | 1998-05-13 |
EP0841520B1 (de) | 2003-03-12 |
DE69719671D1 (de) | 2003-04-17 |
GB9623195D0 (en) | 1997-01-08 |
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