ES409277A1 - Method of introducing three streams of air into a combustor with selective heating - Google Patents
Method of introducing three streams of air into a combustor with selective heatingInfo
- Publication number
- ES409277A1 ES409277A1 ES409277A ES409277A ES409277A1 ES 409277 A1 ES409277 A1 ES 409277A1 ES 409277 A ES409277 A ES 409277A ES 409277 A ES409277 A ES 409277A ES 409277 A1 ES409277 A1 ES 409277A1
- Authority
- ES
- Spain
- Prior art keywords
- combustor
- air
- streams
- introducing
- primary
- 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.)
- Expired
Links
- 238000000034 method Methods 0.000 title abstract 3
- 238000010438 heat treatment Methods 0.000 title 1
- 238000002485 combustion reaction Methods 0.000 abstract 3
- MWUXSHHQAYIFBG-UHFFFAOYSA-N nitrogen oxide Inorganic materials O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 abstract 3
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
- F23R3/005—Combined with pressure or heat exchangers
-
- 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
-
- 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)
- Combustion Of Fluid Fuel (AREA)
Abstract
New combustors, and methods of operating same, which produce lower emissions, particularly lower emissions of nitrogen oxides. Methods and means are provided for supplying separate streams of air to primary and secondary combustion zones of a combustor, for removing heat from said primary combustion zone, and reintroducing said heat into the combustor at a region spaced apart and downstream from said primary and secondary combustion zones.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US20810271A | 1971-12-15 | 1971-12-15 | |
| US00238317A US3826077A (en) | 1971-12-15 | 1972-03-27 | Method of introducing three streams of air into a combustor with selective heating |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES409277A1 true ES409277A1 (en) | 1976-03-16 |
Family
ID=26902905
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES409277A Expired ES409277A1 (en) | 1971-12-15 | 1972-12-04 | Method of introducing three streams of air into a combustor with selective heating |
Country Status (10)
| Country | Link |
|---|---|
| US (1) | US3826077A (en) |
| JP (1) | JPS512563B2 (en) |
| CA (1) | CA964072A (en) |
| CH (1) | CH564733A5 (en) |
| DE (1) | DE2261596B2 (en) |
| ES (1) | ES409277A1 (en) |
| FR (1) | FR2197449A5 (en) |
| GB (1) | GB1410990A (en) |
| IT (1) | IT971654B (en) |
| SE (1) | SE409360B (en) |
Families Citing this family (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3939653A (en) * | 1974-03-29 | 1976-02-24 | Phillips Petroleum Company | Gas turbine combustors and method of operation |
| US4012902A (en) * | 1974-03-29 | 1977-03-22 | Phillips Petroleum Company | Method of operating a gas turbine combustor having an independent airstream to remove heat from the primary combustion zone |
| US4021186A (en) * | 1974-06-19 | 1977-05-03 | Exxon Research And Engineering Company | Method and apparatus for reducing NOx from furnaces |
| GB1490145A (en) * | 1974-09-11 | 1977-10-26 | Mtu Muenchen Gmbh | Gas turbine engine |
| US4067681A (en) * | 1975-03-10 | 1978-01-10 | Columbia Gas System Service Corporation | Gas-fired smooth top range |
| US4138842A (en) * | 1975-11-05 | 1979-02-13 | Zwick Eugene B | Low emission combustion apparatus |
| EP0007424B1 (en) * | 1978-06-28 | 1982-11-24 | Smit Ovens Nijmegen B.V. | Burner device for combustion of liquid fuel |
| US4427362A (en) * | 1980-08-14 | 1984-01-24 | Rockwell International Corporation | Combustion method |
| JPS5829234U (en) * | 1981-08-24 | 1983-02-25 | 株式会社クボタ | Structure of handling torso |
| US4720970A (en) * | 1982-11-05 | 1988-01-26 | The United States Of America As Represented By The Secretary Of The Air Force | Sector airflow variable geometry combustor |
| JPS60131136U (en) * | 1984-02-10 | 1985-09-02 | 三菱農機株式会社 | Threshing machine handling barrel |
| US4958488A (en) * | 1989-04-17 | 1990-09-25 | General Motors Corporation | Combustion system |
| US6071115A (en) * | 1994-03-11 | 2000-06-06 | Gas Research Institute | Apparatus for low NOx, rapid mix combustion |
| US5681159A (en) * | 1994-03-11 | 1997-10-28 | Gas Research Institute | Process and apparatus for low NOx staged-air combustion |
| DE102006011727B3 (en) * | 2006-03-14 | 2007-11-22 | Webasto Ag | Combined heating / hot water system for mobile applications |
| US9239165B2 (en) * | 2012-06-07 | 2016-01-19 | United Technologies Corporation | Combustor liner with convergent cooling channel |
| KR102377720B1 (en) * | 2019-04-10 | 2022-03-23 | 두산중공업 주식회사 | Liner cooling structure with improved pressure losses and combustor for gas turbine having the same |
| ES2998182A1 (en) * | 2023-08-16 | 2025-02-19 | New Technology Transf | COMBUSTION CHAMBER (Machine-translation by Google Translate, not legally binding) |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CH417906A (en) * | 1963-02-28 | 1966-07-31 | Ghelfi Salvatore | Hot gas generator that can be operated with injectable fuel |
| US3360929A (en) * | 1966-03-10 | 1968-01-02 | Montrose K. Drewry | Gas turbine combustors |
| US3705492A (en) * | 1971-01-11 | 1972-12-12 | Gen Motors Corp | Regenerative gas turbine system |
-
1972
- 1972-03-27 US US00238317A patent/US3826077A/en not_active Expired - Lifetime
- 1972-11-21 CA CA157,092A patent/CA964072A/en not_active Expired
- 1972-12-04 ES ES409277A patent/ES409277A1/en not_active Expired
- 1972-12-06 IT IT32634/72A patent/IT971654B/en active
- 1972-12-14 SE SE7216323A patent/SE409360B/en unknown
- 1972-12-14 CH CH1821772A patent/CH564733A5/xx not_active IP Right Cessation
- 1972-12-15 JP JP47126065A patent/JPS512563B2/ja not_active Expired
- 1972-12-15 FR FR7244858A patent/FR2197449A5/fr not_active Expired
- 1972-12-15 GB GB5813872A patent/GB1410990A/en not_active Expired
- 1972-12-15 DE DE2261596A patent/DE2261596B2/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| US3826077A (en) | 1974-07-30 |
| IT971654B (en) | 1974-05-10 |
| CA964072A (en) | 1975-03-11 |
| DE2261596B2 (en) | 1979-07-19 |
| JPS512563B2 (en) | 1976-01-27 |
| GB1410990A (en) | 1975-10-22 |
| DE2261596A1 (en) | 1973-06-28 |
| DE2261596C3 (en) | 1980-03-13 |
| CH564733A5 (en) | 1975-07-31 |
| FR2197449A5 (en) | 1974-03-22 |
| JPS4865314A (en) | 1973-09-08 |
| SE409360B (en) | 1979-08-13 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| ES409277A1 (en) | Method of introducing three streams of air into a combustor with selective heating | |
| ES409276A1 (en) | Combustion process with selective heating of combustion and quench air | |
| GB1118601A (en) | Apparatus for the elimination of odors from noxious gases | |
| CA2054014A1 (en) | Low nox burner | |
| GB986849A (en) | Improvements in or relating to shaft furnaces | |
| ES337987A1 (en) | Method and Apparatus for Minimizing Air Pollution | |
| SE7408286L (en) | ||
| JPS5257551A (en) | Recuperator for use of radiation pipe | |
| GB1151486A (en) | Burner | |
| JPS52138728A (en) | Range nox combusting method of self-recirculation system radiant tube burner and its apparatus | |
| GB1276398A (en) | Apparatus for treating or mixing gases | |
| JPS529672A (en) | A fluid passage apparatus passing into high-temperature gas | |
| JPS5260442A (en) | Preliminary mixing type gas burner | |
| JPS5259335A (en) | Infrared generator | |
| FR2406725A1 (en) | Combustion method for gas turbines - has flame-holder dividing chamber and split airstream swirling in opposite directions | |
| JPS51128032A (en) | Process of combustion | |
| GB1208033A (en) | A method of and apparatus for mixing a high temperature gas stream containing products of combustion with a low temperature gas or air stream containing solid particles | |
| JPS5236335A (en) | Gas burner for decreasing nox | |
| JPS5238669A (en) | Pre-heating method of air for combustion of direct-flame single-disc d ryer | |
| JPS5243131A (en) | Supression of generation of nitrogen oxides in a heating furnace | |
| JPS529671A (en) | A fluid passage apparatus passing into high-temperature gas | |
| JPS5260323A (en) | Gas-turbine combustor | |
| JPS5228729A (en) | Combustion process with decreasing nitrogen oxidization | |
| JPS5317507A (en) | Preheating apparatus for jet stream in heating furnace | |
| JPS56100211A (en) | Denitrification in combustion |