MX155871A - IMPROVEMENTS IN COMBUSTION CHAMBER FOR A GAS TURBINE - Google Patents
IMPROVEMENTS IN COMBUSTION CHAMBER FOR A GAS TURBINEInfo
- Publication number
- MX155871A MX155871A MX191352A MX19135282A MX155871A MX 155871 A MX155871 A MX 155871A MX 191352 A MX191352 A MX 191352A MX 19135282 A MX19135282 A MX 19135282A MX 155871 A MX155871 A MX 155871A
- Authority
- MX
- Mexico
- Prior art keywords
- combustion chamber
- gas turbine
- turbine
- gas
- combustion
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C6/00—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion
- F23C6/04—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection
- F23C6/045—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection with staged combustion in a single enclosure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C7/00—Combustion apparatus characterised by arrangements for air supply
- F23C7/002—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
- F23C7/004—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion using vanes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C9/00—Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber
- F23C9/006—Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber the recirculation taking place in the combustion chamber
-
- 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
-
- 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
-
- 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 |
|---|---|---|---|
| US23866881A | 1981-02-27 | 1981-02-27 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| MX155871A true MX155871A (en) | 1988-05-16 |
Family
ID=22898839
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| MX191352A MX155871A (en) | 1981-02-27 | 1982-02-11 | IMPROVEMENTS IN COMBUSTION CHAMBER FOR A GAS TURBINE |
Country Status (13)
| Country | Link |
|---|---|
| JP (2) | JPS57157935A (en) |
| AR (1) | AR227092A1 (en) |
| AU (1) | AU546612B2 (en) |
| BE (1) | BE892290A (en) |
| BR (1) | BR8201026A (en) |
| CA (1) | CA1179156A (en) |
| CH (1) | CH661974A5 (en) |
| GB (1) | GB2094464B (en) |
| IN (1) | IN155686B (en) |
| IT (1) | IT1149777B (en) |
| MX (1) | MX155871A (en) |
| NL (1) | NL8200333A (en) |
| ZA (1) | ZA82831B (en) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4702073A (en) * | 1986-03-10 | 1987-10-27 | Melconian Jerry O | Variable residence time vortex combustor |
| US5361586A (en) * | 1993-04-15 | 1994-11-08 | Westinghouse Electric Corporation | Gas turbine ultra low NOx combustor |
| US5454712A (en) * | 1993-09-15 | 1995-10-03 | The Boc Group, Inc. | Air-oxy-fuel burner method and apparatus |
| DE19627760C2 (en) | 1996-07-10 | 2001-05-03 | Mtu Aero Engines Gmbh | Burner with atomizer nozzle |
| US6240731B1 (en) * | 1997-12-31 | 2001-06-05 | United Technologies Corporation | Low NOx combustor for gas turbine engine |
| US6354072B1 (en) * | 1999-12-10 | 2002-03-12 | General Electric Company | Methods and apparatus for decreasing combustor emissions |
| US7175423B1 (en) * | 2000-10-26 | 2007-02-13 | Bloom Engineering Company, Inc. | Air staged low-NOx burner |
| DE10140422C1 (en) * | 2001-08-17 | 2002-11-28 | Eisenmann Kg Maschbau | Thermal post-combustion device for cleaning waste gases comprises a burner having a second flame tube surrounding the end of a first flame tube with a greater radius to form an annular gap |
| WO2009062473A2 (en) * | 2007-11-12 | 2009-05-22 | Ulrich Rohs | Axial piston engine and method for operating an axial piston engine |
| US8783585B2 (en) | 2009-05-20 | 2014-07-22 | General Electric Company | Methods and systems for mixing reactor feed |
| WO2019088107A1 (en) * | 2017-10-31 | 2019-05-09 | 国立研究開発法人産業技術総合研究所 | Combustor and combustion method |
-
1982
- 1982-01-29 AU AU79980/82A patent/AU546612B2/en not_active Ceased
- 1982-01-29 IN IN113/CAL/82A patent/IN155686B/en unknown
- 1982-01-29 NL NL8200333A patent/NL8200333A/en not_active Application Discontinuation
- 1982-02-09 ZA ZA82831A patent/ZA82831B/en unknown
- 1982-02-11 MX MX191352A patent/MX155871A/en unknown
- 1982-02-12 GB GB8204144A patent/GB2094464B/en not_active Expired
- 1982-02-22 CA CA000396692A patent/CA1179156A/en not_active Expired
- 1982-02-23 AR AR828528A patent/AR227092A1/en active
- 1982-02-25 JP JP57028242A patent/JPS57157935A/en active Pending
- 1982-02-25 IT IT19859/82A patent/IT1149777B/en active
- 1982-02-25 BE BE0/207422A patent/BE892290A/en not_active IP Right Cessation
- 1982-02-25 CH CH1159/82A patent/CH661974A5/en not_active IP Right Cessation
- 1982-02-26 BR BR8201026A patent/BR8201026A/en unknown
-
1984
- 1984-05-29 JP JP1984078122U patent/JPS6016866U/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| BE892290A (en) | 1982-08-25 |
| GB2094464B (en) | 1984-08-30 |
| IT1149777B (en) | 1986-12-10 |
| JPS6126774Y2 (en) | 1986-08-11 |
| AU546612B2 (en) | 1985-09-12 |
| AU7998082A (en) | 1982-09-02 |
| AR227092A1 (en) | 1982-09-15 |
| CA1179156A (en) | 1984-12-11 |
| BR8201026A (en) | 1983-01-04 |
| IN155686B (en) | 1985-02-23 |
| GB2094464A (en) | 1982-09-15 |
| JPS6016866U (en) | 1985-02-05 |
| CH661974A5 (en) | 1987-08-31 |
| JPS57157935A (en) | 1982-09-29 |
| IT8219859A0 (en) | 1982-02-25 |
| NL8200333A (en) | 1982-09-16 |
| ZA82831B (en) | 1983-03-30 |
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