BE551418A - - Google Patents
Info
- Publication number
- BE551418A BE551418A BE551418DA BE551418A BE 551418 A BE551418 A BE 551418A BE 551418D A BE551418D A BE 551418DA BE 551418 A BE551418 A BE 551418A
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Testing Of Engines (AREA)
- Measuring Fluid Pressure (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1135017T | 1955-10-28 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE551418A true BE551418A (en:Method) |
Family
ID=9639615
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE551418D BE551418A (en:Method) | 1955-10-28 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US3082603A (en:Method) |
| BE (1) | BE551418A (en:Method) |
| FR (1) | FR1135017A (en:Method) |
| GB (1) | GB812201A (en:Method) |
Families Citing this family (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS548890B1 (en:Method) * | 1971-04-01 | 1979-04-19 | ||
| FR2406075A1 (fr) * | 1977-10-11 | 1979-05-11 | Snecma | Appareil de combustion et son procede de realisation |
| US4265615A (en) * | 1978-12-11 | 1981-05-05 | United Technologies Corporation | Fuel injection system for low emission burners |
| US5323605A (en) * | 1990-10-01 | 1994-06-28 | General Electric Company | Double dome arched combustor |
| JPH094825A (ja) * | 1995-06-21 | 1997-01-10 | Mitsubishi Heavy Ind Ltd | 燃焼器 |
| DE19649486A1 (de) * | 1996-11-29 | 1998-06-04 | Abb Research Ltd | Brennkammer |
| US6021570A (en) * | 1997-11-20 | 2000-02-08 | Caterpillar Inc. | Annular one piece combustor liner |
| US6729141B2 (en) * | 2002-07-03 | 2004-05-04 | Elliot Energy Systems, Inc. | Microturbine with auxiliary air tubes for NOx emission reduction |
| GB2441342B (en) * | 2006-09-01 | 2009-03-18 | Rolls Royce Plc | Wall elements with apertures for gas turbine engine components |
| JP2011102669A (ja) * | 2009-11-10 | 2011-05-26 | Mitsubishi Heavy Ind Ltd | ガスタービン燃焼器及びガスタービン |
| US8707708B2 (en) | 2010-02-22 | 2014-04-29 | United Technologies Corporation | 3D non-axisymmetric combustor liner |
| EP2420730B1 (en) * | 2010-08-16 | 2018-03-07 | Ansaldo Energia IP UK Limited | Reheat burner |
| US11747019B1 (en) * | 2022-09-02 | 2023-09-05 | General Electric Company | Aerodynamic combustor liner design for emissions reductions |
Family Cites Families (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR962581A (en:Method) * | 1950-06-16 | |||
| US945967A (en) * | 1909-07-14 | 1910-01-11 | Julius A Mahr | Oil-burner. |
| US2546432A (en) * | 1944-03-20 | 1951-03-27 | Power Jets Res & Dev Ltd | Apparatus for deflecting a fuel jet towards a region of turbulence in a propulsive gaseous stream |
| BE466639A (en:Method) * | 1944-12-13 | |||
| NL72524C (en:Method) * | 1947-11-03 | |||
| US2644512A (en) * | 1949-06-13 | 1953-07-07 | Heizmotoren Ges Uberlingen Am | Burner device having heat exchange and gas flow control means for maintaining pyrophoric ignition therein |
| US2828609A (en) * | 1950-04-03 | 1958-04-01 | Bristol Aero Engines Ltd | Combustion chambers including suddenly enlarged chamber portions |
| GB687667A (en) * | 1950-04-03 | 1953-02-18 | Bristol Aeroplane Co Ltd | Improvements in or relating to combustion systems |
| US2825202A (en) * | 1950-06-19 | 1958-03-04 | Snecma | Pipes traversed by pulsating flow gases |
| US2699648A (en) * | 1950-10-03 | 1955-01-18 | Gen Electric | Combustor sectional liner structure with annular inlet nozzles |
| GB726491A (en) * | 1952-07-16 | 1955-03-16 | Onera (Off Nat Aerospatiale) | Improvements in internal combustion engines through which a continuous gaseous stream is flowing and in particular in turbo-jet and turbo-prop engines |
| US2907171A (en) * | 1954-02-15 | 1959-10-06 | Lysholm Alf | Combustion chamber inlet for thermal power plants |
| FR998079A (fr) * | 1958-08-22 | 1952-01-14 | Snecma | Dispositif pour l'entrée de l'air dans la zone primaire d'une chambre de combustion de turbo-machine |
-
0
- BE BE551418D patent/BE551418A/xx unknown
-
1955
- 1955-10-28 FR FR1135017D patent/FR1135017A/fr not_active Expired
-
1956
- 1956-10-02 US US613497A patent/US3082603A/en not_active Expired - Lifetime
- 1956-10-03 GB GB30168/56A patent/GB812201A/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| US3082603A (en) | 1963-03-26 |
| FR1135017A (fr) | 1957-04-23 |
| GB812201A (en) | 1959-04-22 |