CH380444A - Flame tube for combustion chambers - Google Patents
Flame tube for combustion chambersInfo
- Publication number
- CH380444A CH380444A CH1120260A CH1120260A CH380444A CH 380444 A CH380444 A CH 380444A CH 1120260 A CH1120260 A CH 1120260A CH 1120260 A CH1120260 A CH 1120260A CH 380444 A CH380444 A CH 380444A
- Authority
- CH
- Switzerland
- Prior art keywords
- combustion chambers
- flame tube
- flame
- tube
- chambers
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title 1
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)
- Spray-Type Burners (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US844279A US3064425A (en) | 1959-10-05 | 1959-10-05 | Combustion liner |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CH380444A true CH380444A (en) | 1964-07-31 |
Family
ID=25292282
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CH1120260A CH380444A (en) | 1959-10-05 | 1960-10-05 | Flame tube for combustion chambers |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US3064425A (en) |
| CH (1) | CH380444A (en) |
| GB (1) | GB891836A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2354504A1 (en) * | 1972-11-02 | 1974-05-16 | Gen Electric | REINFORCEMENT FOR BURNER LINING |
Families Citing this family (32)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3485043A (en) * | 1968-02-01 | 1969-12-23 | Gen Electric | Shingled combustion liner |
| US3589128A (en) * | 1970-02-02 | 1971-06-29 | Avco Corp | Cooling arrangement for a reverse flow gas turbine combustor |
| US3705492A (en) * | 1971-01-11 | 1972-12-12 | Gen Motors Corp | Regenerative gas turbine system |
| US3742702A (en) * | 1971-01-22 | 1973-07-03 | Gen Motors Corp | Regenerative gas turbine system |
| US3751910A (en) * | 1972-02-25 | 1973-08-14 | Gen Motors Corp | Combustion liner |
| US3854285A (en) * | 1973-02-26 | 1974-12-17 | Gen Electric | Combustor dome assembly |
| GB1552132A (en) * | 1975-11-29 | 1979-09-12 | Rolls Royce | Combustion chambers for gas turbine engines |
| US4050241A (en) * | 1975-12-22 | 1977-09-27 | General Electric Company | Stabilizing dimple for combustion liner cooling slot |
| US4008568A (en) * | 1976-03-01 | 1977-02-22 | General Motors Corporation | Combustor support |
| US4132066A (en) * | 1977-09-23 | 1979-01-02 | United Technologies Corporation | Combustor liner for gas turbine engine |
| US4244178A (en) * | 1978-03-20 | 1981-01-13 | General Motors Corporation | Porous laminated combustor structure |
| US4180972A (en) * | 1978-06-08 | 1980-01-01 | General Motors Corporation | Combustor support structure |
| GB2049152B (en) * | 1979-05-01 | 1983-05-18 | Rolls Royce | Perforate laminated material |
| US4312186A (en) * | 1979-10-17 | 1982-01-26 | General Motors Corporation | Shingled laminated porous material |
| US4413477A (en) * | 1980-12-29 | 1983-11-08 | General Electric Company | Liner assembly for gas turbine combustor |
| US4928479A (en) * | 1987-12-28 | 1990-05-29 | Sundstrand Corporation | Annular combustor with tangential cooling air injection |
| US4887663A (en) * | 1988-05-31 | 1989-12-19 | United Technologies Corporation | Hot gas duct liner |
| US5181377A (en) * | 1991-04-16 | 1993-01-26 | General Electric Company | Damped combustor cowl structure |
| US6823677B2 (en) * | 2002-09-03 | 2004-11-30 | Pratt & Whitney Canada Corp. | Stress relief feature for aerated gas turbine fuel injector |
| US7043921B2 (en) * | 2003-08-26 | 2006-05-16 | Honeywell International, Inc. | Tube cooled combustor |
| US7464537B2 (en) * | 2005-04-04 | 2008-12-16 | United Technologies Corporation | Heat transfer enhancement features for a tubular wall combustion chamber |
| FR2887615B1 (en) * | 2005-06-22 | 2007-08-31 | Snecma Moteurs Sa | CIRCULAR FITTING OF TURBOMACHINE COMBUSTION CHAMBER |
| FR2896575B1 (en) * | 2006-01-26 | 2013-01-18 | Snecma | ANNULAR COMBUSTION CHAMBER OF A TURBOMACHINE |
| US7827801B2 (en) * | 2006-02-09 | 2010-11-09 | Siemens Energy, Inc. | Gas turbine engine transitions comprising closed cooled transition cooling channels |
| RU2319075C9 (en) * | 2006-05-10 | 2008-05-27 | Открытое акционерное общество "Климов" | Heating tube of a combustion chamber |
| FR2905166B1 (en) * | 2006-08-28 | 2008-11-14 | Snecma Sa | ANNULAR COMBUSTION CHAMBER OF A TURBOMACHINE. |
| RU2343355C2 (en) * | 2006-11-30 | 2009-01-10 | Открытое акционерное общество "Климов" | Combustion liner of gas-turbine engine |
| FR2910597B1 (en) * | 2006-12-22 | 2009-03-20 | Snecma Sa | FURNITURE FOR BOTTOM OF COMBUSTION CHAMBER |
| DE102007050664A1 (en) * | 2007-10-24 | 2009-04-30 | Man Turbo Ag | Burner for a turbomachine, baffle for such a burner and a turbomachine with such a burner |
| KR102071168B1 (en) * | 2016-05-23 | 2020-01-29 | 미츠비시 히타치 파워 시스템즈 가부시키가이샤 | Combustor, gas turbine |
| RU205407U1 (en) * | 2020-12-08 | 2021-07-13 | Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") | Combustion tube with expansion slots |
| CN117469698A (en) | 2022-07-21 | 2024-01-30 | 通用电气公司 | Combustion Liner Performance Factor |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2645081A (en) * | 1949-08-19 | 1953-07-14 | A V Roe Canada Ltd | Spacing means for the wall sections of flame tubes |
| US2670601A (en) * | 1950-10-17 | 1954-03-02 | A V Roe Canada Ltd | Spacing means for wall sections of flame tubes |
| US2884759A (en) * | 1956-04-25 | 1959-05-05 | Curtiss Wright Corp | Combustion chamber construction |
-
1959
- 1959-10-05 US US844279A patent/US3064425A/en not_active Expired - Lifetime
-
1960
- 1960-09-16 GB GB31939/60A patent/GB891836A/en not_active Expired
- 1960-10-05 CH CH1120260A patent/CH380444A/en unknown
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2354504A1 (en) * | 1972-11-02 | 1974-05-16 | Gen Electric | REINFORCEMENT FOR BURNER LINING |
Also Published As
| Publication number | Publication date |
|---|---|
| GB891836A (en) | 1962-03-21 |
| US3064425A (en) | 1962-11-20 |
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