EP2742292A4 - Chambre de combustion - Google Patents
Chambre de combustionInfo
- Publication number
- EP2742292A4 EP2742292A4 EP12822757.6A EP12822757A EP2742292A4 EP 2742292 A4 EP2742292 A4 EP 2742292A4 EP 12822757 A EP12822757 A EP 12822757A EP 2742292 A4 EP2742292 A4 EP 2742292A4
- Authority
- EP
- European Patent Office
- Prior art keywords
- combustor
- 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.)
- Withdrawn
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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
-
- 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
- F23R3/06—Arrangement of apertures along the flame tube
-
- 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
-
- 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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/38—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means
-
- 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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
-
- 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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/58—Cyclone or vortex type combustion chambers
-
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US201161522412P | 2011-08-11 | 2011-08-11 | |
| PCT/US2012/050349 WO2013023147A1 (fr) | 2011-08-11 | 2012-08-10 | Chambre de combustion |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP2742292A1 EP2742292A1 (fr) | 2014-06-18 |
| EP2742292A4 true EP2742292A4 (fr) | 2015-08-12 |
Family
ID=47668992
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP12822757.6A Withdrawn EP2742292A4 (fr) | 2011-08-11 | 2012-08-10 | Chambre de combustion |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US20140190178A1 (fr) |
| EP (1) | EP2742292A4 (fr) |
| CN (1) | CN103998867A (fr) |
| CA (1) | CA2844693A1 (fr) |
| WO (1) | WO2013023147A1 (fr) |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10634354B2 (en) | 2011-08-11 | 2020-04-28 | Beckett Gas, Inc. | Combustor |
| US9228747B2 (en) | 2013-03-12 | 2016-01-05 | Pratt & Whitney Canada Corp. | Combustor for gas turbine engine |
| US9541292B2 (en) | 2013-03-12 | 2017-01-10 | Pratt & Whitney Canada Corp. | Combustor for gas turbine engine |
| US9127843B2 (en) * | 2013-03-12 | 2015-09-08 | Pratt & Whitney Canada Corp. | Combustor for gas turbine engine |
| US9366187B2 (en) | 2013-03-12 | 2016-06-14 | Pratt & Whitney Canada Corp. | Slinger combustor |
| US9958161B2 (en) | 2013-03-12 | 2018-05-01 | Pratt & Whitney Canada Corp. | Combustor for gas turbine engine |
| CN104373962B (zh) * | 2014-10-28 | 2016-08-24 | 北京华清燃气轮机与煤气化联合循环工程技术有限公司 | 一种燃气轮机燃烧室叶片进气旋流喷嘴 |
| EP3545236B1 (fr) * | 2016-11-22 | 2024-01-24 | Beckett Thermal Solutions | Chambre de combustion |
| CN110440290B (zh) * | 2018-05-02 | 2024-03-29 | 中国联合重型燃气轮机技术有限公司 | 用于燃气轮机的微混合喷嘴 |
| KR102583222B1 (ko) | 2022-01-06 | 2023-09-25 | 두산에너빌리티 주식회사 | 연소기용 노즐, 연소기 및 이를 포함하는 가스 터빈 |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2718757A (en) * | 1951-01-17 | 1955-09-27 | Lummus Co | Aircraft gas turbine and jet |
| US4996838A (en) * | 1988-10-27 | 1991-03-05 | Sol-3 Resources, Inc. | Annular vortex slinger combustor |
| US6623267B1 (en) * | 2002-12-31 | 2003-09-23 | Tibbs M. Golladay, Jr. | Industrial burner |
| US20090056338A1 (en) * | 2007-09-05 | 2009-03-05 | Snecma | Turbomachine combustion chamber with helical air flow |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2785878A (en) * | 1953-09-16 | 1957-03-19 | Earl W Conrad | Porous walled conduit for fluid cooling |
| US3788065A (en) * | 1970-10-26 | 1974-01-29 | United Aircraft Corp | Annular combustion chamber for dissimilar fluids in swirling flow relationship |
| US4058977A (en) * | 1974-12-18 | 1977-11-22 | United Technologies Corporation | Low emission combustion chamber |
| US4642993A (en) * | 1985-04-29 | 1987-02-17 | Avco Corporation | Combustor liner wall |
| KR20000069289A (ko) * | 1996-12-03 | 2000-11-25 | 번함.더글라스 알. | 환형연소기를 갖는 발전시스템 |
| EP1710505A2 (fr) * | 1999-12-15 | 2006-10-11 | Osaka Gas Co., Ltd. | Brûleur, moteur de turbine à gaz et système de cogénération |
| JP3600911B2 (ja) * | 2001-01-25 | 2004-12-15 | 川崎重工業株式会社 | 環状燃焼器のライナ支持構造 |
| US7581396B2 (en) * | 2005-07-25 | 2009-09-01 | General Electric Company | Mixer assembly for combustor of a gas turbine engine having a plurality of counter-rotating swirlers |
| US20110097189A1 (en) * | 2007-12-31 | 2011-04-28 | Aaron Sandoval | Boundary layer effect turbine |
-
2012
- 2012-08-10 US US14/238,067 patent/US20140190178A1/en not_active Abandoned
- 2012-08-10 EP EP12822757.6A patent/EP2742292A4/fr not_active Withdrawn
- 2012-08-10 WO PCT/US2012/050349 patent/WO2013023147A1/fr not_active Ceased
- 2012-08-10 CN CN201280050137.7A patent/CN103998867A/zh active Pending
- 2012-08-10 CA CA2844693A patent/CA2844693A1/fr not_active Abandoned
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2718757A (en) * | 1951-01-17 | 1955-09-27 | Lummus Co | Aircraft gas turbine and jet |
| US4996838A (en) * | 1988-10-27 | 1991-03-05 | Sol-3 Resources, Inc. | Annular vortex slinger combustor |
| US6623267B1 (en) * | 2002-12-31 | 2003-09-23 | Tibbs M. Golladay, Jr. | Industrial burner |
| US20090056338A1 (en) * | 2007-09-05 | 2009-03-05 | Snecma | Turbomachine combustion chamber with helical air flow |
Non-Patent Citations (1)
| Title |
|---|
| See also references of WO2013023147A1 * |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2013023147A1 (fr) | 2013-02-14 |
| US20140190178A1 (en) | 2014-07-10 |
| CN103998867A (zh) | 2014-08-20 |
| EP2742292A1 (fr) | 2014-06-18 |
| CA2844693A1 (fr) | 2013-02-14 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
| 17P | Request for examination filed |
Effective date: 20140211 |
|
| AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
| DAX | Request for extension of the european patent (deleted) | ||
| RA4 | Supplementary search report drawn up and despatched (corrected) |
Effective date: 20150713 |
|
| RIC1 | Information provided on ipc code assigned before grant |
Ipc: F23R 3/58 20060101ALI20150707BHEP Ipc: F23R 3/06 20060101AFI20150707BHEP |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN |
|
| 18D | Application deemed to be withdrawn |
Effective date: 20160210 |