BE461591A - - Google Patents
Info
- Publication number
- BE461591A BE461591A BE461591DA BE461591A BE 461591 A BE461591 A BE 461591A BE 461591D A BE461591D A BE 461591DA BE 461591 A BE461591 A BE 461591A
- 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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/44—Combustion chambers comprising a single tubular flame tube within a tubular casing
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- 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
-
- 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
-
- 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
- F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
-
- 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
- F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
- F23R3/48—Flame tube interconnectors, e.g. cross-over tubes
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- 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)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4968/44A GB594285A (en) | 1944-03-16 | Improvements relating to combustion apparatus |
Publications (1)
Publication Number | Publication Date |
---|---|
BE461591A true BE461591A (da) |
Family
ID=9787280
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE461591D BE461591A (da) | 1944-03-16 |
Country Status (4)
Country | Link |
---|---|
US (1) | US2475911A (da) |
BE (1) | BE461591A (da) |
CH (1) | CH258672A (da) |
FR (1) | FR918088A (da) |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2581999A (en) * | 1946-02-01 | 1952-01-08 | Gen Electric | Hemispherical combustion chamber end dome having cooling air deflecting means |
FR962862A (da) * | 1946-10-26 | 1950-06-22 | ||
US2603064A (en) * | 1946-12-12 | 1952-07-15 | Chrysler Corp | Combustion chamber with multiple conical sections providing multiple air paths for gas turbines |
US2541171A (en) * | 1947-01-25 | 1951-02-13 | Kellogg M W Co | Air inlet structure for combustion chambers |
US2620625A (en) * | 1947-05-16 | 1952-12-09 | Edward A Phaneuf | Jet engine having an air compressor driven solely by a fuel gas turbine |
GB684669A (en) * | 1947-10-21 | 1952-12-24 | Power Jets Res & Dev Ltd | Improvements in or relating to combustion apparatus |
BE485523A (da) * | 1947-11-03 | |||
US2659201A (en) * | 1947-11-26 | 1953-11-17 | Phillips Petroleum Co | Gas turbine combustion chamber with provision for turbulent mixing of air and fuel |
US2552492A (en) * | 1948-06-07 | 1951-05-08 | Power Jets Res & Dev Ltd | Air ducting arrangement for combustion chambers |
US2553091A (en) * | 1948-09-11 | 1951-05-15 | Harold R Horning | Heater |
US2627720A (en) * | 1948-10-08 | 1953-02-10 | Packard Motor Car Co | Circumferentially arranged combustion chamber with arcuate walls defining an air flow path between chambers |
US2646664A (en) * | 1949-02-24 | 1953-07-28 | A V Roe Canada Ltd | Annular fuel vaporizer for gas turbine engines |
US2628474A (en) * | 1949-05-13 | 1953-02-17 | Floyd T Hague | Annular combustion liner having conical reentrant walls with fuel reversing elements |
US2696076A (en) * | 1949-11-28 | 1954-12-07 | Ivan F Weeks | Turbulence and combustion-promoting device for ram jet motors |
US2718757A (en) * | 1951-01-17 | 1955-09-27 | Lummus Co | Aircraft gas turbine and jet |
US2729938A (en) * | 1951-01-26 | 1956-01-10 | Gen Motors Corp | Combustion chamber crossover tube |
US2692478A (en) * | 1951-02-24 | 1954-10-26 | Boeing Co | Turbine burner incorporating removable burner liner |
US2984979A (en) * | 1951-03-27 | 1961-05-23 | Eldon R Babcock | Vortex pilot flame source for ramjet engines |
US2765620A (en) * | 1951-06-23 | 1956-10-09 | Gen Motors Corp | Flow deflector for combustion chamber apparatus |
US2780916A (en) * | 1952-08-22 | 1957-02-12 | Continental Aviat & Engineerin | Pilot burner for jet engines |
US2823628A (en) * | 1953-01-21 | 1958-02-18 | Babcock & Wilcox Co | Multi-fuel burner |
US2979899A (en) * | 1953-06-27 | 1961-04-18 | Snecma | Flame spreading device for combustion equipments |
US6231334B1 (en) * | 1998-11-24 | 2001-05-15 | John Zink Company | Biogas flaring unit |
FR2808500B1 (fr) * | 2000-05-04 | 2002-08-16 | Philippe Michel | Autorespirateur subaquatique a rechargement manuel integre |
US6840048B2 (en) * | 2002-09-26 | 2005-01-11 | General Electric Company | Dynamically uncoupled can combustor |
GB2461542B (en) * | 2008-07-03 | 2010-10-13 | Rolls Royce Plc | Combustion Arrangement with Dilution and Trim Ports |
US20110271654A1 (en) * | 2010-05-05 | 2011-11-10 | General Electric Company | Diffuser for gas turbine system |
US9476355B2 (en) * | 2012-02-29 | 2016-10-25 | Siemens Energy, Inc. | Mid-section of a can-annular gas turbine engine with a radial air flow discharged from the compressor section |
US9546601B2 (en) * | 2012-11-20 | 2017-01-17 | General Electric Company | Clocked combustor can array |
US11940151B2 (en) * | 2022-01-12 | 2024-03-26 | General Electric Company | Combustor with baffle |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US910665A (en) * | 1908-05-16 | 1909-01-26 | August W H Griepe | Gas turbine-engine. |
US990222A (en) * | 1910-09-12 | 1911-04-25 | Julius Brown | Explosive gas-turbine engine. |
US2164954A (en) * | 1936-10-06 | 1939-07-04 | Thomas J Stephens | Combustion and gas mixing assembly for gas circulating systems |
CH206286A (de) * | 1937-11-18 | 1939-07-31 | Messerschmitt Boelkow Blohm | Brennkammer für Gasströmungsmaschinen, wie z. B. Gasturbinen, insbesondere zur Verwendung bei Luftfahrzeugen. |
US2353929A (en) * | 1940-01-29 | 1944-07-18 | Allis Chalmers Mfg Co | Combustion turbine |
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0
- BE BE461591D patent/BE461591A/xx unknown
-
1945
- 1945-10-09 US US621336A patent/US2475911A/en not_active Expired - Lifetime
- 1945-11-28 FR FR918088D patent/FR918088A/fr not_active Expired
- 1945-11-30 CH CH258672D patent/CH258672A/de unknown
Also Published As
Publication number | Publication date |
---|---|
CH258672A (de) | 1948-12-15 |
FR918088A (fr) | 1947-01-29 |
US2475911A (en) | 1949-07-12 |