BE745343A - Appareils de combustion - Google Patents
Appareils de combustionInfo
- Publication number
- BE745343A BE745343A BE745343DA BE745343A BE 745343 A BE745343 A BE 745343A BE 745343D A BE745343D A BE 745343DA BE 745343 A BE745343 A BE 745343A
- Authority
- BE
- Belgium
- Prior art keywords
- combustion appliances
- appliances
- combustion
- 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
- F23R3/10—Air inlet arrangements for primary air
- F23R3/12—Air inlet arrangements for primary air inducing a vortex
- F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C7/00—Combustion apparatus characterised by arrangements for air supply
- F23C7/002—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
- F23C7/004—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion using vanes
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Nozzles For Spraying Of Liquid Fuel (AREA)
- Fuel-Injection Apparatus (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US79639169A | 1969-02-04 | 1969-02-04 |
Publications (1)
Publication Number | Publication Date |
---|---|
BE745343A true BE745343A (fr) | 1970-07-16 |
Family
ID=25168090
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE745343D BE745343A (fr) | 1969-02-04 | 1970-02-02 | Appareils de combustion |
Country Status (11)
Families Citing this family (53)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3899884A (en) * | 1970-12-02 | 1975-08-19 | Gen Electric | Combustor systems |
BE795867A (fr) * | 1972-03-01 | 1973-06-18 | Gen Electric | Dispositif pour uniformiser l'ecoulement de l'air dans une turbine a gaz |
CA980584A (en) * | 1972-11-10 | 1975-12-30 | Edward E. Ekstedt | Double walled impingement cooled combustor |
US3845620A (en) * | 1973-02-12 | 1974-11-05 | Gen Electric | Cooling film promoter for combustion chambers |
US3826082A (en) * | 1973-03-30 | 1974-07-30 | Gen Electric | Combustion liner cooling slot stabilizing dimple |
US3877221A (en) * | 1973-08-27 | 1975-04-15 | Gen Motors Corp | Combustion apparatus air supply |
US3972182A (en) * | 1973-09-10 | 1976-08-03 | General Electric Company | Fuel injection apparatus |
US3853273A (en) * | 1973-10-01 | 1974-12-10 | Gen Electric | Axial swirler central injection carburetor |
FR2253389A5 (enrdf_load_stackoverflow) * | 1973-12-04 | 1975-06-27 | France Etat | |
US3901446A (en) * | 1974-05-09 | 1975-08-26 | Us Air Force | Induced vortex swirler |
JPS5129726A (enrdf_load_stackoverflow) * | 1974-09-06 | 1976-03-13 | Mitsubishi Heavy Ind Ltd | |
US4058977A (en) * | 1974-12-18 | 1977-11-22 | United Technologies Corporation | Low emission combustion chamber |
US3973395A (en) * | 1974-12-18 | 1976-08-10 | United Technologies Corporation | Low emission combustion chamber |
US4045956A (en) * | 1974-12-18 | 1977-09-06 | United Technologies Corporation | Low emission combustion chamber |
US4052844A (en) * | 1975-06-02 | 1977-10-11 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation | Gas turbine combustion chambers |
DE2528671C2 (de) * | 1975-06-27 | 1985-12-19 | Klöckner-Humboldt-Deutz AG, 5000 Köln | Brennkammer für Flüssig- und Gastreibstoffe |
US4030875A (en) * | 1975-12-22 | 1977-06-21 | General Electric Company | Integrated ceramic-metal combustor |
US4198815A (en) * | 1975-12-24 | 1980-04-22 | General Electric Company | Central injection fuel carburetor |
US4098074A (en) * | 1976-06-01 | 1978-07-04 | United Technologies Corporation | Combustor diffuser for turbine type power plant and construction thereof |
GB1592858A (en) * | 1977-01-21 | 1981-07-08 | Rolls Royce | Combustion equipment for gas turbine engines |
US4246757A (en) * | 1979-03-27 | 1981-01-27 | General Electric Company | Combustor including a cyclone prechamber and combustion process for gas turbines fired with liquid fuel |
US4276018A (en) * | 1979-05-30 | 1981-06-30 | Davey Compressor Co. | Mobile heater |
US4356693A (en) * | 1980-04-22 | 1982-11-02 | Rolls-Royce Limited | Gas turbine engine combustion chambers |
US4584834A (en) * | 1982-07-06 | 1986-04-29 | General Electric Company | Gas turbine engine carburetor |
GB2150277B (en) * | 1983-11-26 | 1987-01-28 | Rolls Royce | Combustion apparatus for a gas turbine engine |
US4638636A (en) * | 1984-06-28 | 1987-01-27 | General Electric Company | Fuel nozzle |
US4763482A (en) * | 1987-01-02 | 1988-08-16 | General Electric Company | Swirler arrangement for combustor of gas turbine engine |
FR2639095B1 (fr) * | 1988-11-17 | 1990-12-21 | Snecma | Chambre de combustion de turbomachine a bols de prevaporisation montes flottants |
US5117637A (en) * | 1990-08-02 | 1992-06-02 | General Electric Company | Combustor dome assembly |
US5154060A (en) * | 1991-08-12 | 1992-10-13 | General Electric Company | Stiffened double dome combustor |
US5463864A (en) * | 1993-12-27 | 1995-11-07 | United Technologies Corporation | Fuel nozzle guide for a gas turbine engine combustor |
WO1997011311A2 (de) * | 1995-09-22 | 1997-03-27 | Siemens Aktiengesellschaft | Brenner, insbesondere für eine gasturbine |
US6032457A (en) * | 1996-06-27 | 2000-03-07 | United Technologies Corporation | Fuel nozzle guide |
US6550251B1 (en) | 1997-12-18 | 2003-04-22 | General Electric Company | Venturiless swirl cup |
US5996352A (en) * | 1997-12-22 | 1999-12-07 | United Technologies Corporation | Thermally decoupled swirler for a gas turbine combustor |
US6453671B1 (en) * | 2000-01-13 | 2002-09-24 | General Electric Company | Combustor swirler assembly |
US6286300B1 (en) | 2000-01-27 | 2001-09-11 | Honeywell International Inc. | Combustor with fuel preparation chambers |
US6536201B2 (en) * | 2000-12-11 | 2003-03-25 | Pratt & Whitney Canada Corp. | Combustor turbine successive dual cooling |
US6487861B1 (en) * | 2001-06-05 | 2002-12-03 | General Electric Company | Combustor for gas turbine engines with low air flow swirlers |
US20040007056A1 (en) * | 2001-08-06 | 2004-01-15 | Webb Cynthia C. | Method for testing catalytic converter durability |
US6983645B2 (en) * | 2002-08-06 | 2006-01-10 | Southwest Research Institute | Method for accelerated aging of catalytic converters incorporating engine cold start simulation |
GB2390890B (en) * | 2002-07-17 | 2005-07-06 | Rolls Royce Plc | Diffuser for gas turbine engine |
US7412335B2 (en) | 2002-08-06 | 2008-08-12 | Southwest Research Institute | Component evaluations using non-engine based test system |
FR2881813B1 (fr) * | 2005-02-09 | 2011-04-08 | Snecma Moteurs | Carenage de chambre de combustion de turbomachine |
WO2006101991A2 (en) | 2005-03-17 | 2006-09-28 | Southwest Research Institute | Mass air flow compensation for burner-based exhaust gas generation system |
WO2006101987A2 (en) * | 2005-03-17 | 2006-09-28 | Southwest Research Institute | Use of recirculated exhaust gas in a burner-based exhaust generation system for reduced fuel consumption and for cooling |
WO2007019329A2 (en) * | 2005-08-05 | 2007-02-15 | Southwest Research Institute | Secondary air injector for use with exhaust gas simulation system |
FR2921464B1 (fr) * | 2007-09-24 | 2014-03-28 | Snecma | Agencement de systemes d'injection dans un fond de chambre de combustion d'un moteur d'aeronef |
US8327648B2 (en) * | 2008-12-09 | 2012-12-11 | Pratt & Whitney Canada Corp. | Combustor liner with integrated anti-rotation and removal feature |
US8689563B2 (en) * | 2009-07-13 | 2014-04-08 | United Technologies Corporation | Fuel nozzle guide plate mistake proofing |
US10156189B2 (en) | 2014-01-28 | 2018-12-18 | Pratt & Whitney Canada Corp. | Combustor igniter assembly |
DE102021110617A1 (de) | 2021-04-26 | 2022-10-27 | Rolls-Royce Deutschland Ltd & Co Kg | Brennkammerbaugruppe für ein Triebwerk mit einer Brennkammerwand verbundenem Pre-Diffusor |
US11578869B2 (en) * | 2021-05-20 | 2023-02-14 | General Electric Company | Active boundary layer control in diffuser |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE464055C (de) * | 1926-07-29 | 1928-08-07 | Maschb Akt Ges Balcke | Einrichtung zur Einfuehrung der Verbrennungsluft fuer OElfeuerungen mit mehreren Feuerstellen |
US2398654A (en) * | 1940-01-24 | 1946-04-16 | Anglo Saxon Petroleum Co | Combustion burner |
US2560223A (en) * | 1948-02-04 | 1951-07-10 | Wright Aeronautical Corp | Double air-swirl baffle construction for fuel burners |
US3031012A (en) * | 1957-12-27 | 1962-04-24 | Gen Thermique Procedes Brola S | Combustion apparatus |
US3064424A (en) * | 1959-09-30 | 1962-11-20 | Gen Motors Corp | Flame tube |
GB1031184A (en) * | 1964-02-26 | 1966-06-02 | Arthur Henry Lefebvre | An improved fuel injection system for gas turbine engines |
GB1135670A (en) * | 1966-04-20 | 1968-12-04 | Rolls Royce | Combustion chamber for a gas turbine engine |
-
1969
- 1969-02-04 US US796391A patent/US3589127A/en not_active Expired - Lifetime
-
1970
- 1970-01-20 SE SE00645/70A patent/SE356554B/xx unknown
- 1970-01-20 GB GB1297244D patent/GB1297244A/en not_active Expired
- 1970-01-23 NL NL7000956A patent/NL7000956A/xx unknown
- 1970-01-29 ES ES376005A patent/ES376005A1/es not_active Expired
- 1970-02-02 BE BE745343D patent/BE745343A/xx unknown
- 1970-02-02 DK DK48970AA patent/DK126704B/da unknown
- 1970-02-03 CH CH150170A patent/CH523471A/de not_active IP Right Cessation
- 1970-02-03 DE DE19702004702 patent/DE2004702A1/de not_active Withdrawn
- 1970-02-03 NO NO00384/70*[A patent/NO129541B/no unknown
- 1970-02-03 FR FR7003796A patent/FR2033912A5/fr not_active Expired
Also Published As
Publication number | Publication date |
---|---|
CH523471A (de) | 1972-05-31 |
DK126704B (da) | 1973-08-13 |
US3589127A (en) | 1971-06-29 |
DE2004702A1 (de) | 1970-09-10 |
SE356554B (enrdf_load_stackoverflow) | 1973-05-28 |
NL7000956A (enrdf_load_stackoverflow) | 1970-08-06 |
FR2033912A5 (enrdf_load_stackoverflow) | 1970-12-04 |
GB1297244A (enrdf_load_stackoverflow) | 1972-11-22 |
ES376005A1 (es) | 1972-03-16 |
NO129541B (enrdf_load_stackoverflow) | 1974-04-22 |
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