BE740301A - - Google Patents
Info
- Publication number
- BE740301A BE740301A BE740301DA BE740301A BE 740301 A BE740301 A BE 740301A BE 740301D A BE740301D A BE 740301DA BE 740301 A BE740301 A BE 740301A
- 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
- F23R3/10—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)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US76795368A | 1968-10-16 | 1968-10-16 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE740301A true BE740301A (enrdf_load_stackoverflow) | 1970-03-16 |
Family
ID=25081076
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE740301D BE740301A (enrdf_load_stackoverflow) | 1968-10-16 | 1969-10-15 |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US3498055A (enrdf_load_stackoverflow) |
| BE (1) | BE740301A (enrdf_load_stackoverflow) |
| BR (1) | BR6913369D0 (enrdf_load_stackoverflow) |
| CH (1) | CH500438A (enrdf_load_stackoverflow) |
| DE (1) | DE1951198C3 (enrdf_load_stackoverflow) |
| FR (1) | FR2020807A1 (enrdf_load_stackoverflow) |
| GB (1) | GB1252194A (enrdf_load_stackoverflow) |
| IL (1) | IL33166A (enrdf_load_stackoverflow) |
| NL (1) | NL6915585A (enrdf_load_stackoverflow) |
Families Citing this family (25)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1934700B2 (de) * | 1969-07-09 | 1972-01-05 | Mtu Muenchen Gmbh | Brennstoffduese fuer gasturbinentriebwerke |
| US3630024A (en) * | 1970-02-02 | 1971-12-28 | Gen Electric | Air swirler for gas turbine combustor |
| US3643430A (en) * | 1970-03-04 | 1972-02-22 | United Aircraft Corp | Smoke reduction combustion chamber |
| USRE30160E (en) * | 1970-03-04 | 1979-11-27 | United Technologies Corporation | Smoke reduction combustion chamber |
| US3656298A (en) * | 1970-11-27 | 1972-04-18 | Gen Motors Corp | Combustion apparatus |
| US3741483A (en) * | 1971-12-10 | 1973-06-26 | Mitsubishi Heavy Ind Ltd | Combustion air supply arrangement for gas turbines |
| US3916619A (en) * | 1972-10-30 | 1975-11-04 | Hitachi Ltd | Burning method for gas turbine combustor and a construction thereof |
| JPS5342897B2 (enrdf_load_stackoverflow) * | 1972-11-09 | 1978-11-15 | ||
| GB1429677A (en) * | 1973-03-20 | 1976-03-24 | Rolls Royce | Gas turbine engine combustion equipment |
| US3901446A (en) * | 1974-05-09 | 1975-08-26 | Us Air Force | Induced vortex swirler |
| US4155220A (en) * | 1977-01-21 | 1979-05-22 | Westinghouse Electric Corp. | Combustion apparatus for a gas turbine engine |
| US4151713A (en) * | 1977-03-15 | 1979-05-01 | United Technologies Corporation | Burner for gas turbine engine |
| FR2426157B1 (fr) * | 1978-05-20 | 1985-07-26 | Rolls Royce | Chambre de combustion de moteur a turbine a gaz a prise annulaire d'air refrigerant |
| GB2099978A (en) * | 1981-05-11 | 1982-12-15 | Rolls Royce | Gas turbine engine combustor |
| US5297385A (en) * | 1988-05-31 | 1994-03-29 | United Technologies Corporation | Combustor |
| FR2673705A1 (fr) * | 1991-03-06 | 1992-09-11 | Snecma | Chambre de combustion de turbomachine munie d'un dispositif anti-cokefaction du fond de ladite chambre. |
| US6953429B2 (en) | 2000-02-14 | 2005-10-11 | Obtech Medical Ag | Hydraulic urinary incontinence treatment apparatus |
| DE102006041955A1 (de) * | 2006-08-30 | 2008-03-20 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Verfahren zur Steuerung der Verbrennung in einer Brennkammer und Brennkammervorrichtung |
| US9181812B1 (en) * | 2009-05-05 | 2015-11-10 | Majed Toqan | Can-annular combustor with premixed tangential fuel-air nozzles for use on gas turbine engines |
| US9027350B2 (en) * | 2009-12-30 | 2015-05-12 | Rolls-Royce Corporation | Gas turbine engine having dome panel assembly with bifurcated swirler flow |
| US9599343B2 (en) * | 2012-11-28 | 2017-03-21 | General Electric Company | Fuel nozzle for use in a turbine engine and method of assembly |
| US9228747B2 (en) * | 2013-03-12 | 2016-01-05 | Pratt & Whitney Canada Corp. | Combustor for gas turbine engine |
| USD911402S1 (en) * | 2019-07-18 | 2021-02-23 | Illinois Tool Works Inc. | Chamber |
| US11885497B2 (en) * | 2019-07-19 | 2024-01-30 | Pratt & Whitney Canada Corp. | Fuel nozzle with slot for cooling |
| US11662097B2 (en) | 2020-10-13 | 2023-05-30 | Venture Aerospace, Llc | Jet engine with toroidal air stream combustion |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2560207A (en) * | 1948-02-04 | 1951-07-10 | Wright Aeronautical Corp | Annular combustion chamber with circumferentially spaced double air-swirl burners |
| US2700416A (en) * | 1949-06-30 | 1955-01-25 | Rolls Royce | Fuel injection means for gas-turbine engines and combustion equipment used therewith |
| US2982099A (en) * | 1956-10-09 | 1961-05-02 | Rolls Royce | Fuel injection arrangement in combustion equipment for gas turbine engines |
| US3134229A (en) * | 1961-10-02 | 1964-05-26 | Gen Electric | Combustion chamber |
-
1968
- 1968-10-16 US US767953A patent/US3498055A/en not_active Expired - Lifetime
-
1969
- 1969-10-08 GB GB1252194D patent/GB1252194A/en not_active Expired
- 1969-10-10 DE DE1951198A patent/DE1951198C3/de not_active Expired
- 1969-10-12 IL IL33166A patent/IL33166A/xx unknown
- 1969-10-13 CH CH1530369A patent/CH500438A/de not_active IP Right Cessation
- 1969-10-13 FR FR6935057A patent/FR2020807A1/fr not_active Withdrawn
- 1969-10-15 BE BE740301D patent/BE740301A/xx unknown
- 1969-10-15 NL NL6915585A patent/NL6915585A/xx unknown
- 1969-10-16 BR BR213369/69A patent/BR6913369D0/pt unknown
Also Published As
| Publication number | Publication date |
|---|---|
| FR2020807A1 (enrdf_load_stackoverflow) | 1970-07-17 |
| US3498055A (en) | 1970-03-03 |
| IL33166A (en) | 1973-08-29 |
| BR6913369D0 (pt) | 1973-06-26 |
| DE1951198A1 (de) | 1970-05-14 |
| NL6915585A (enrdf_load_stackoverflow) | 1970-04-20 |
| GB1252194A (enrdf_load_stackoverflow) | 1971-11-03 |
| IL33166A0 (en) | 1970-03-22 |
| DE1951198C3 (de) | 1973-12-06 |
| DE1951198B2 (de) | 1973-05-17 |
| CH500438A (de) | 1970-12-15 |