DE69204453D1 - Brennkammeranordnung. - Google Patents
Brennkammeranordnung.Info
- Publication number
- DE69204453D1 DE69204453D1 DE69204453T DE69204453T DE69204453D1 DE 69204453 D1 DE69204453 D1 DE 69204453D1 DE 69204453 T DE69204453 T DE 69204453T DE 69204453 T DE69204453 T DE 69204453T DE 69204453 D1 DE69204453 D1 DE 69204453D1
- Authority
- DE
- Germany
- Prior art keywords
- combustion chamber
- chamber arrangement
- arrangement
- 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.)
- Expired - Lifetime
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
-
- 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
- F23R3/60—Support structures; Attaching or mounting means
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)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB919108235A GB9108235D0 (en) | 1991-04-17 | 1991-04-17 | A combustion chamber assembly |
PCT/GB1992/000017 WO1992018760A1 (en) | 1991-04-17 | 1992-01-06 | A combustion chamber assembly |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69204453D1 true DE69204453D1 (de) | 1995-10-05 |
DE69204453T2 DE69204453T2 (de) | 1996-02-22 |
Family
ID=10693465
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69204453T Expired - Lifetime DE69204453T2 (de) | 1991-04-17 | 1992-01-06 | Brennkammeranordnung. |
Country Status (6)
Country | Link |
---|---|
US (1) | US5353586A (de) |
EP (1) | EP0580583B1 (de) |
JP (1) | JP3142563B2 (de) |
DE (1) | DE69204453T2 (de) |
GB (1) | GB9108235D0 (de) |
WO (1) | WO1992018760A1 (de) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2293232B (en) * | 1994-09-15 | 1998-05-20 | Rolls Royce Plc | A combustion chamber assembly |
GB9813972D0 (en) * | 1998-06-30 | 1998-08-26 | Rolls Royce Plc | A combustion chamber |
JP3951909B2 (ja) * | 2002-12-12 | 2007-08-01 | 株式会社日立製作所 | ガスタービン燃焼器 |
US7647779B2 (en) * | 2005-04-27 | 2010-01-19 | United Technologies Corporation | Compliant metal support for ceramic combustor liner in a gas turbine engine |
US7559203B2 (en) * | 2005-09-16 | 2009-07-14 | Pratt & Whitney Canada Corp. | Cooled support boss for a combustor in a gas turbine engine |
US7600370B2 (en) | 2006-05-25 | 2009-10-13 | Siemens Energy, Inc. | Fluid flow distributor apparatus for gas turbine engine mid-frame section |
US8863528B2 (en) * | 2006-07-27 | 2014-10-21 | United Technologies Corporation | Ceramic combustor can for a gas turbine engine |
GB2445565A (en) * | 2006-09-26 | 2008-07-16 | Siemens Ag | Gas turbine engine having a plurality of modules comprising a combustor and transition duct |
US7870738B2 (en) | 2006-09-29 | 2011-01-18 | Siemens Energy, Inc. | Gas turbine: seal between adjacent can annular combustors |
US9388738B2 (en) * | 2011-10-04 | 2016-07-12 | Siemens Energy, Inc. | Casing for a gas turbine engine |
US20130232949A1 (en) * | 2012-03-09 | 2013-09-12 | Gary J. Dillard | Pressure balanced area control of high aspect ratio nozzle |
US9551238B2 (en) | 2012-09-28 | 2017-01-24 | United Technologies Corporation | Pin connector for ceramic matrix composite turbine frame |
US9617917B2 (en) | 2013-07-31 | 2017-04-11 | General Electric Company | Flow control assembly and methods of assembling the same |
US11732892B2 (en) | 2013-08-14 | 2023-08-22 | General Electric Company | Gas turbomachine diffuser assembly with radial flow splitters |
Family Cites Families (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2489692A (en) * | 1942-04-07 | 1949-11-29 | Power Jets Res Dev Ltd | Compressor |
US2410450A (en) * | 1943-01-30 | 1946-11-05 | Westinghouse Electric Corp | Turbine apparatus |
GB710862A (en) * | 1951-02-09 | 1954-06-23 | Rolls Royce | Improvements in or relating to gas-turbine plant |
US2711072A (en) * | 1951-06-14 | 1955-06-21 | Gen Motors Corp | Combustion chamber fairing |
GB743633A (en) * | 1952-12-31 | 1956-01-18 | Gen Motors Corp | Improvements in or relating to gas turbine engines |
DE1218800B (de) * | 1961-04-25 | 1966-06-08 | M A N Turbo Ges Mit Beschraenk | Gasturbine, insbesondere Kleingasturbine |
US3116604A (en) * | 1962-05-17 | 1964-01-07 | Gen Electric | Engine exhaust system |
US3327473A (en) * | 1966-01-11 | 1967-06-27 | Gen Motors Corp | Engine support structure |
US3372542A (en) * | 1966-11-25 | 1968-03-12 | United Aircraft Corp | Annular burner for a gas turbine |
AT279483B (de) * | 1968-10-18 | 1970-03-10 | Flensburger Maschinenbau Ansta | Beschickungswagen, insbesondere zum transport von heiszem schwarzdeckenmischgut |
US3756020A (en) * | 1972-06-26 | 1973-09-04 | Curtiss Wright Corp | Gas turbine engine and cooling system therefor |
US4009569A (en) * | 1975-07-21 | 1977-03-01 | United Technologies Corporation | Diffuser-burner casing for a gas turbine engine |
GB1585157A (en) * | 1976-07-17 | 1981-02-25 | Stone Platt Fluid Fire Ltd | Gas turbine engine |
US4435958A (en) * | 1981-09-29 | 1984-03-13 | The Boeing Company | Turbine bypass turbofan with mid-turbine reingestion and method of operating the same |
GB2149491B (en) * | 1983-07-30 | 1988-06-08 | John Hunter | Heat storage regenerator for gas turbines etc |
US4987736A (en) * | 1988-12-14 | 1991-01-29 | General Electric Company | Lightweight gas turbine engine frame with free-floating heat shield |
US5048288A (en) * | 1988-12-20 | 1991-09-17 | United Technologies Corporation | Combined turbine stator cooling and turbine tip clearance control |
GB8914825D0 (en) * | 1989-06-28 | 1989-08-16 | Rolls Royce Plc | Gas turbine engine power unit |
GB8928378D0 (en) * | 1989-12-15 | 1990-02-21 | Rolls Royce Plc | A diffuser |
GB2247521A (en) * | 1990-09-01 | 1992-03-04 | Rolls Royce Plc | A combustion chamber assembly |
-
1991
- 1991-04-17 GB GB919108235A patent/GB9108235D0/en active Pending
-
1992
- 1992-01-06 JP JP04502550A patent/JP3142563B2/ja not_active Expired - Lifetime
- 1992-01-06 US US08/122,595 patent/US5353586A/en not_active Expired - Lifetime
- 1992-01-06 DE DE69204453T patent/DE69204453T2/de not_active Expired - Lifetime
- 1992-01-06 EP EP92902366A patent/EP0580583B1/de not_active Expired - Lifetime
- 1992-01-06 WO PCT/GB1992/000017 patent/WO1992018760A1/en active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
EP0580583B1 (de) | 1995-08-30 |
US5353586A (en) | 1994-10-11 |
EP0580583A1 (de) | 1994-02-02 |
JP3142563B2 (ja) | 2001-03-07 |
DE69204453T2 (de) | 1996-02-22 |
JPH06506746A (ja) | 1994-07-28 |
GB9108235D0 (en) | 1991-06-05 |
WO1992018760A1 (en) | 1992-10-29 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |