IL37737A - Annular slot combustor - Google Patents
Annular slot combustorInfo
- Publication number
- IL37737A IL37737A IL37737A IL3773771A IL37737A IL 37737 A IL37737 A IL 37737A IL 37737 A IL37737 A IL 37737A IL 3773771 A IL3773771 A IL 3773771A IL 37737 A IL37737 A IL 37737A
- Authority
- IL
- Israel
- Prior art keywords
- fuel
- air
- combustion zone
- annular
- carbureting device
- Prior art date
Links
- 239000000446 fuel Substances 0.000 claims description 75
- 238000002485 combustion reaction Methods 0.000 claims description 57
- 239000000203 mixture Substances 0.000 claims description 28
- 238000011144 upstream manufacturing Methods 0.000 claims description 13
- 238000002347 injection Methods 0.000 claims description 3
- 239000007924 injection Substances 0.000 claims description 3
- 239000003795 chemical substances by application Substances 0.000 claims 1
- 239000007789 gas Substances 0.000 description 21
- 238000001816 cooling Methods 0.000 description 5
- 238000009826 distribution Methods 0.000 description 5
- 238000002156 mixing Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000009467 reduction Effects 0.000 description 3
- 230000006641 stabilisation Effects 0.000 description 3
- 238000011105 stabilization Methods 0.000 description 3
- 238000013459 approach Methods 0.000 description 2
- 239000000779 smoke Substances 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 230000009429 distress Effects 0.000 description 1
- 239000003344 environmental pollutant Substances 0.000 description 1
- 239000000284 extract Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 231100000719 pollutant Toxicity 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000007921 spray Substances 0.000 description 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
-
- 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)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10360471A | 1971-01-04 | 1971-01-04 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| IL37737A0 IL37737A0 (en) | 1971-11-29 |
| IL37737A true IL37737A (en) | 1973-05-31 |
Family
ID=22296052
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IL37737A IL37737A (en) | 1971-01-04 | 1971-09-16 | Annular slot combustor |
Country Status (10)
| Country | Link |
|---|---|
| US (1) | US3722216A (OSRAM) |
| BE (1) | BE773357A (OSRAM) |
| CA (1) | CA938115A (OSRAM) |
| CH (1) | CH533234A (OSRAM) |
| DE (1) | DE2148826A1 (OSRAM) |
| FR (1) | FR2121496B1 (OSRAM) |
| GB (1) | GB1352369A (OSRAM) |
| IL (1) | IL37737A (OSRAM) |
| IT (1) | IT938896B (OSRAM) |
| NL (1) | NL7113604A (OSRAM) |
Families Citing this family (25)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3914348A (en) * | 1974-02-25 | 1975-10-21 | Aerojet General Co | Platelet-venturi carburetor for combustion engine |
| GB1600130A (en) * | 1977-05-21 | 1981-10-14 | Rolls Royce | Combustion systems |
| US4215535A (en) * | 1978-01-19 | 1980-08-05 | United Technologies Corporation | Method and apparatus for reducing nitrous oxide emissions from combustors |
| US4226083A (en) * | 1978-01-19 | 1980-10-07 | United Technologies Corporation | Method and apparatus for reducing nitrous oxide emissions from combustors |
| US4543781A (en) * | 1981-06-17 | 1985-10-01 | Rice Ivan G | Annular combustor for gas turbine |
| US4565490A (en) * | 1981-06-17 | 1986-01-21 | Rice Ivan G | Integrated gas/steam nozzle |
| US4471890A (en) * | 1982-04-29 | 1984-09-18 | St. Luke's Hospital | Eye drop dispenser |
| GB9023004D0 (en) * | 1990-10-23 | 1990-12-05 | Rolls Royce Plc | A gas turbine engine combustion chamber and a method of operating a gas turbine engine combustion chamber |
| EP0554325B1 (en) * | 1990-10-23 | 1995-07-26 | ROLLS-ROYCE plc | Gasturbine combustion chamber and method of operation thereof |
| US5450724A (en) * | 1993-08-27 | 1995-09-19 | Northern Research & Engineering Corporation | Gas turbine apparatus including fuel and air mixer |
| DE59710046D1 (de) * | 1997-03-20 | 2003-06-12 | Alstom Switzerland Ltd | Gasturbine mit toroidaler Brennkammer |
| DE19721936A1 (de) * | 1997-05-26 | 1998-12-03 | Abb Research Ltd | Brenner zum Betrieb eines Aggregates zur Erzeugung eines Heissgases |
| US6694743B2 (en) | 2001-07-23 | 2004-02-24 | Ramgen Power Systems, Inc. | Rotary ramjet engine with flameholder extending to running clearance at engine casing interior wall |
| US7603841B2 (en) * | 2001-07-23 | 2009-10-20 | Ramgen Power Systems, Llc | Vortex combustor for low NOx emissions when burning lean premixed high hydrogen content fuel |
| US7003961B2 (en) * | 2001-07-23 | 2006-02-28 | Ramgen Power Systems, Inc. | Trapped vortex combustor |
| DE102006004840A1 (de) * | 2006-02-02 | 2007-08-23 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinenbrennkammer mit Kraftstoffeinspritzung über den gesamten Brennkammerring |
| US20130067932A1 (en) * | 2011-09-20 | 2013-03-21 | Honeywell International Inc. | Combustion sections of gas turbine engines with convection shield assemblies |
| WO2014055122A1 (en) * | 2012-10-01 | 2014-04-10 | United Technologies Corporation | Geared turbofan high gearbox power density |
| US20140144141A1 (en) * | 2012-11-26 | 2014-05-29 | General Electric Company | Premixer with diluent fluid and fuel tubes having chevron outlets |
| US20150323185A1 (en) * | 2014-05-07 | 2015-11-12 | General Electric Compamy | Turbine engine and method of assembling thereof |
| US9810434B2 (en) * | 2016-01-21 | 2017-11-07 | Siemens Energy, Inc. | Transition duct system with arcuate ceramic liner for delivering hot-temperature gases in a combustion turbine engine |
| US10823418B2 (en) | 2017-03-02 | 2020-11-03 | General Electric Company | Gas turbine engine combustor comprising air inlet tubes arranged around the combustor |
| US10823422B2 (en) * | 2017-10-17 | 2020-11-03 | General Electric Company | Tangential bulk swirl air in a trapped vortex combustor for a gas turbine engine |
| US12392290B2 (en) | 2022-11-01 | 2025-08-19 | General Electric Company | Gas turbine engine |
| US12291979B1 (en) | 2023-10-26 | 2025-05-06 | General Electric Company | Turbine engine and turbine nozzle |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2647369A (en) * | 1946-09-06 | 1953-08-04 | Leduc Rene | Combustion chamber for fluid fuel burning in an air stream of high velocity |
| US2646664A (en) * | 1949-02-24 | 1953-07-28 | A V Roe Canada Ltd | Annular fuel vaporizer for gas turbine engines |
| US2698050A (en) * | 1949-06-10 | 1954-12-28 | Lummus Co | Combustion for liquid fuels |
| US2773350A (en) * | 1950-01-31 | 1956-12-11 | Hillard E Barrett | Combustion chamber assembly for ram jet fuel burner |
| FR1149404A (fr) * | 1955-05-25 | 1957-12-26 | Daimler Benz Ag | Chambre de combustion pour turbines à combustion, générateurs à gaz moteurs, appareils moteurs à jets d'air chaud et analogues |
| GB1136543A (en) * | 1966-02-21 | 1968-12-11 | Rolls Royce | Liquid fuel combustion apparatus for gas turbine engines |
| US3605405A (en) * | 1970-04-09 | 1971-09-20 | Gen Electric | Carbon elimination and cooling improvement to scroll type combustors |
| US3570242A (en) * | 1970-04-20 | 1971-03-16 | United Aircraft Corp | Fuel premixing for smokeless jet engine main burner |
-
1971
- 1971-01-04 US US00103604A patent/US3722216A/en not_active Expired - Lifetime
- 1971-08-24 CA CA121169A patent/CA938115A/en not_active Expired
- 1971-09-16 IL IL37737A patent/IL37737A/en unknown
- 1971-09-29 GB GB4530071A patent/GB1352369A/en not_active Expired
- 1971-09-30 IT IT29357/71A patent/IT938896B/it active
- 1971-09-30 BE BE773357A patent/BE773357A/xx unknown
- 1971-09-30 DE DE19712148826 patent/DE2148826A1/de active Pending
- 1971-10-04 FR FR7135687A patent/FR2121496B1/fr not_active Expired
- 1971-10-04 NL NL7113604A patent/NL7113604A/xx unknown
- 1971-10-04 CH CH1441771A patent/CH533234A/de not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| IL37737A0 (en) | 1971-11-29 |
| NL7113604A (OSRAM) | 1972-07-06 |
| IT938896B (it) | 1973-02-10 |
| FR2121496B1 (OSRAM) | 1974-10-11 |
| CA938115A (en) | 1973-12-11 |
| US3722216A (en) | 1973-03-27 |
| BE773357A (fr) | 1972-01-17 |
| GB1352369A (en) | 1974-05-08 |
| FR2121496A1 (OSRAM) | 1972-08-25 |
| CH533234A (de) | 1973-01-31 |
| DE2148826A1 (de) | 1972-07-27 |
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