GB8305112D0 - Low-no x' rich-lean combustor - Google Patents
Low-no x' rich-lean combustorInfo
- Publication number
- GB8305112D0 GB8305112D0 GB838305112A GB8305112A GB8305112D0 GB 8305112 D0 GB8305112 D0 GB 8305112D0 GB 838305112 A GB838305112 A GB 838305112A GB 8305112 A GB8305112 A GB 8305112A GB 8305112 D0 GB8305112 D0 GB 8305112D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- rich
- low
- lean combustor
- combustor
- lean
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
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
- F23C13/00—Apparatus in which combustion takes place in the presence of catalytic material
-
- 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
- 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
- F23R3/40—Continuous combustion chambers using liquid or gaseous fuel characterised by the use of catalytic means
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US35606882A | 1982-03-08 | 1982-03-08 |
Publications (3)
Publication Number | Publication Date |
---|---|
GB8305112D0 true GB8305112D0 (en) | 1983-03-30 |
GB2116308A GB2116308A (en) | 1983-09-21 |
GB2116308B GB2116308B (en) | 1985-11-13 |
Family
ID=23399972
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08305112A Expired GB2116308B (en) | 1982-03-08 | 1983-02-24 | Improved low-nox, rich-lean combustor |
Country Status (7)
Country | Link |
---|---|
JP (1) | JPS58164929A (en) |
BE (1) | BE896105A (en) |
BR (1) | BR8301099A (en) |
CA (1) | CA1206764A (en) |
GB (1) | GB2116308B (en) |
IT (1) | IT1170117B (en) |
MX (1) | MX158476A (en) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA1285207C (en) * | 1985-09-30 | 1991-06-25 | Yoshinori Idota | Fuel spray combustion device |
DE3545524C2 (en) * | 1985-12-20 | 1996-02-29 | Siemens Ag | Multi-stage combustion chamber for the combustion of nitrogenous gas with reduced NO¶x¶ emission and method for its operation |
AT391185B (en) * | 1988-02-08 | 1990-08-27 | Vaillant Gmbh | DEVICE FOR STAGE COMBUSTION OF A FUEL-AIR MIXTURE |
US5117636A (en) * | 1990-02-05 | 1992-06-02 | General Electric Company | Low nox emission in gas turbine system |
DE4422535A1 (en) * | 1994-06-28 | 1996-01-04 | Abb Research Ltd | Process for operating a furnace |
DE19612507C2 (en) * | 1996-03-29 | 2002-06-27 | Kunkel Klaus | Method for driving a shaft and drive therefor |
US5996351A (en) * | 1997-07-07 | 1999-12-07 | General Electric Company | Rapid-quench axially staged combustor |
DE10112864A1 (en) * | 2001-03-16 | 2002-09-19 | Alstom Switzerland Ltd | Process for igniting a thermal turbomachine |
US7093441B2 (en) * | 2003-10-09 | 2006-08-22 | United Technologies Corporation | Gas turbine annular combustor having a first converging volume and a second converging volume, converging less gradually than the first converging volume |
US8430665B2 (en) * | 2008-02-25 | 2013-04-30 | General Electric Company | Combustion systems and processes for burning fossil fuel with reduced nitrogen oxide emissions |
-
1983
- 1983-02-24 GB GB08305112A patent/GB2116308B/en not_active Expired
- 1983-02-28 CA CA000422504A patent/CA1206764A/en not_active Expired
- 1983-03-01 MX MX196427A patent/MX158476A/en unknown
- 1983-03-04 IT IT19895/83A patent/IT1170117B/en active
- 1983-03-07 BR BR8301099A patent/BR8301099A/en not_active IP Right Cessation
- 1983-03-08 JP JP58036795A patent/JPS58164929A/en active Granted
- 1983-03-08 BE BE0/210276A patent/BE896105A/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
BE896105A (en) | 1983-09-08 |
GB2116308A (en) | 1983-09-21 |
MX158476A (en) | 1989-02-03 |
JPH0210348B2 (en) | 1990-03-07 |
IT8319895A0 (en) | 1983-03-04 |
IT1170117B (en) | 1987-06-03 |
CA1206764A (en) | 1986-07-02 |
GB2116308B (en) | 1985-11-13 |
BR8301099A (en) | 1983-11-22 |
JPS58164929A (en) | 1983-09-29 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19950224 |