BE514534A - - Google Patents
Info
- Publication number
- BE514534A BE514534A BE514534DA BE514534A BE 514534 A BE514534 A BE 514534A BE 514534D A BE514534D A BE 514534DA BE 514534 A BE514534 A BE 514534A
- Authority
- BE
- Belgium
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
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US229071A US2742762A (en) | 1951-05-31 | 1951-05-31 | Combustion chamber for axial flow gas turbines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE514534A true BE514534A (es) |
Family
ID=22859732
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE514534D BE514534A (es) | 1951-05-31 |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US2742762A (es) |
| BE (1) | BE514534A (es) |
| CH (1) | CH317633A (es) |
| DE (1) | DE935287C (es) |
| FR (1) | FR1065482A (es) |
| GB (1) | GB731054A (es) |
| NL (1) | NL79375C (es) |
Families Citing this family (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2890569A (en) * | 1954-05-03 | 1959-06-16 | Phillips Petroleum Co | Removal of carbon deposits in jet engines |
| US2902823A (en) * | 1956-11-21 | 1959-09-08 | Clarence E Wagner | Design for a stainless steel or aluminum gas generator wall spraying system for combustion chamber |
| US3210935A (en) * | 1959-09-23 | 1965-10-12 | Lyman C Fisher | Jetevator for missile control |
| FR1421372A (fr) * | 1964-09-16 | 1965-12-17 | Perfectionnement apporté aux chambres de combustion | |
| US3874169A (en) * | 1971-01-14 | 1975-04-01 | Stal Laval Turbin Ab | Combustion chamber for gas turbines |
| US3981142A (en) * | 1974-04-01 | 1976-09-21 | General Motors Corporation | Ceramic combustion liner |
| US4298338A (en) * | 1976-12-30 | 1981-11-03 | Owens-Illinois, Inc. | Liquid fuel burners |
| JPS5966619A (ja) * | 1982-10-06 | 1984-04-16 | Hitachi Ltd | ガスタ−ビン燃焼器 |
| US5323605A (en) * | 1990-10-01 | 1994-06-28 | General Electric Company | Double dome arched combustor |
| FR2668246B1 (fr) * | 1990-10-17 | 1994-12-09 | Snecma | Chambre de combustion munie d'un dispositif de refroidissement de sa paroi. |
| CA2089272C (en) * | 1992-03-23 | 2002-09-03 | James Norman Reinhold, Jr. | Impact resistant combustor |
| US5755093A (en) * | 1995-05-01 | 1998-05-26 | United Technologies Corporation | Forced air cooled gas turbine exhaust liner |
| DE10214573A1 (de) * | 2002-04-02 | 2003-10-16 | Rolls Royce Deutschland | Brennkammer einer Gasturbine mit Starterfilmkühlung |
| US20050241316A1 (en) * | 2004-04-28 | 2005-11-03 | Honeywell International Inc. | Uniform effusion cooling method for a can combustion chamber |
| US8281600B2 (en) * | 2007-01-09 | 2012-10-09 | General Electric Company | Thimble, sleeve, and method for cooling a combustor assembly |
| US20100037622A1 (en) * | 2008-08-18 | 2010-02-18 | General Electric Company | Contoured Impingement Sleeve Holes |
| US8161752B2 (en) * | 2008-11-20 | 2012-04-24 | Honeywell International Inc. | Combustors with inserts between dual wall liners |
| GB201116608D0 (en) * | 2011-09-27 | 2011-11-09 | Rolls Royce Plc | A method of operating a combustion chamber |
| US9328923B2 (en) * | 2012-10-10 | 2016-05-03 | General Electric Company | System and method for separating fluids |
| EP3039340B1 (en) * | 2013-08-30 | 2018-11-28 | United Technologies Corporation | Vena contracta swirling dilution passages for gas turbine engine combustor |
| EP2927595B1 (en) * | 2014-04-02 | 2019-11-13 | United Technologies Corporation | Grommet assembly and method of design |
| US20160047549A1 (en) * | 2014-08-15 | 2016-02-18 | Rolls-Royce Corporation | Ceramic matrix composite components with inserts |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE709065C (de) * | 1935-07-17 | 1941-08-07 | Rene Alexandre Arthur Couzinet | Speiseeinrichtung fuer Gasturbinen |
| US2227666A (en) * | 1936-12-10 | 1941-01-07 | Bbc Brown Boveri & Cie | Starting up system for heat producing and consuming plants |
| US2471101A (en) * | 1945-03-31 | 1949-05-24 | Charles E Feinberg | Secondary combustion air distribution control for bridge wall furnaces |
| GB603485A (en) * | 1946-02-23 | 1948-06-16 | Armstrong Siddeley Motors Ltd | Liquid fuel combustion chamber |
| FR962862A (es) * | 1946-10-26 | 1950-06-22 | ||
| US2601390A (en) * | 1946-11-07 | 1952-06-24 | Westinghouse Electric Corp | Combustion chamber for gas turbines with circumferentially arranged pulverized solidfuel and air nozzles |
| DE804982C (de) * | 1947-06-23 | 1951-05-04 | Armstrong Siddeley Motors Ltd | Brennkammer fuer Brennkraftturbeinen |
| NL80817C (es) * | 1947-11-03 | |||
| BE485523A (es) * | 1947-11-03 | |||
| US2631429A (en) * | 1948-06-08 | 1953-03-17 | Jr Harold M Jacklin | Cooling arrangement for radial flow gas turbines having coaxial combustors |
| US2547619A (en) * | 1948-11-27 | 1951-04-03 | Gen Electric | Combustor with sectional housing and liner |
-
0
- BE BE514534D patent/BE514534A/xx unknown
- NL NL79375D patent/NL79375C/xx active
-
1951
- 1951-05-31 US US229071A patent/US2742762A/en not_active Expired - Lifetime
-
1952
- 1952-05-13 GB GB12152/52A patent/GB731054A/en not_active Expired
- 1952-05-20 DE DEN5542A patent/DE935287C/de not_active Expired
- 1952-05-26 FR FR1065482D patent/FR1065482A/fr not_active Expired
- 1952-05-29 CH CH317633D patent/CH317633A/fr unknown
Also Published As
| Publication number | Publication date |
|---|---|
| NL79375C (es) | |
| DE935287C (de) | 1955-11-17 |
| FR1065482A (fr) | 1954-05-26 |
| GB731054A (en) | 1955-06-01 |
| CH317633A (fr) | 1956-11-30 |
| US2742762A (en) | 1956-04-24 |