BR6913369D0 - COMBUSTION CAMERA AND PROCESS TO REDUCE SMOKE AND MAINTAIN THE TOTALITY OF YIELD PARAMETERS IN THE SAME - Google Patents
COMBUSTION CAMERA AND PROCESS TO REDUCE SMOKE AND MAINTAIN THE TOTALITY OF YIELD PARAMETERS IN THE SAMEInfo
- Publication number
- BR6913369D0 BR6913369D0 BR213369/69A BR21336969A BR6913369D0 BR 6913369 D0 BR6913369 D0 BR 6913369D0 BR 213369/69 A BR213369/69 A BR 213369/69A BR 21336969 A BR21336969 A BR 21336969A BR 6913369 D0 BR6913369 D0 BR 6913369D0
- Authority
- BR
- Brazil
- Prior art keywords
- totality
- maintain
- same
- reduce smoke
- yield parameters
- Prior art date
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 |
---|---|
BR6913369D0 true BR6913369D0 (en) | 1973-06-26 |
Family
ID=25081076
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR213369/69A BR6913369D0 (en) | 1968-10-16 | 1969-10-16 | COMBUSTION CAMERA AND PROCESS TO REDUCE SMOKE AND MAINTAIN THE TOTALITY OF YIELD PARAMETERS IN THE SAME |
Country Status (9)
Country | Link |
---|---|
US (1) | US3498055A (en) |
BE (1) | BE740301A (en) |
BR (1) | BR6913369D0 (en) |
CH (1) | CH500438A (en) |
DE (1) | DE1951198C3 (en) |
FR (1) | FR2020807A1 (en) |
GB (1) | GB1252194A (en) |
IL (1) | IL33166A (en) |
NL (1) | NL6915585A (en) |
Families Citing this family (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1934700B2 (en) * | 1969-07-09 | 1972-01-05 | Mtu Muenchen Gmbh | FUEL NOZZLE FOR GAS TURBINE ENGINES |
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 (en) * | 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 (en) * | 1978-05-20 | 1985-07-26 | Rolls Royce | COMBUSTION CHAMBER OF GAS TURBINE ENGINE WITH ANNULAR REFRIGERANT AIR INTAKE |
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 (en) * | 1991-03-06 | 1992-09-11 | Snecma | Combustion chamber of a turbine engine equipped with an anti-coking device for the bottom of said chamber |
AU2001232583A1 (en) | 2000-02-14 | 2001-07-24 | Potencia Medical Ag | Hydraulic urinary incontinence treatment apparatus |
DE102006041955A1 (en) * | 2006-08-30 | 2008-03-20 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Method for controlling combustion in a combustion chamber and combustion chamber device |
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/en not_active Expired
- 1969-10-12 IL IL33166A patent/IL33166A/en unknown
- 1969-10-13 FR FR6935057A patent/FR2020807A1/fr not_active Withdrawn
- 1969-10-13 CH CH1530369A patent/CH500438A/en not_active IP Right Cessation
- 1969-10-15 NL NL6915585A patent/NL6915585A/xx unknown
- 1969-10-15 BE BE740301D patent/BE740301A/xx unknown
- 1969-10-16 BR BR213369/69A patent/BR6913369D0/en unknown
Also Published As
Publication number | Publication date |
---|---|
IL33166A (en) | 1973-08-29 |
FR2020807A1 (en) | 1970-07-17 |
DE1951198A1 (en) | 1970-05-14 |
GB1252194A (en) | 1971-11-03 |
CH500438A (en) | 1970-12-15 |
IL33166A0 (en) | 1970-03-22 |
NL6915585A (en) | 1970-04-20 |
DE1951198C3 (en) | 1973-12-06 |
US3498055A (en) | 1970-03-03 |
DE1951198B2 (en) | 1973-05-17 |
BE740301A (en) | 1970-03-16 |
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