WO2013028167A3 - Chambre de combustion annulaire en forme de boîte présentant des buses de carburant-air étagées et tangentielles, en vue d'une utilisation sur des moteurs à turbine à gaz - Google Patents
Chambre de combustion annulaire en forme de boîte présentant des buses de carburant-air étagées et tangentielles, en vue d'une utilisation sur des moteurs à turbine à gaz Download PDFInfo
- Publication number
- WO2013028167A3 WO2013028167A3 PCT/US2011/048612 US2011048612W WO2013028167A3 WO 2013028167 A3 WO2013028167 A3 WO 2013028167A3 US 2011048612 W US2011048612 W US 2011048612W WO 2013028167 A3 WO2013028167 A3 WO 2013028167A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- fuel
- air
- gas turbine
- reduces
- turbine engines
- 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.)
- Ceased
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
- F23R3/34—Feeding into different combustion zones
- F23R3/346—Feeding into different combustion zones for staged combustion
-
- 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
- F23R3/44—Combustion chambers comprising a single tubular flame tube within a tubular 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
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Priority Applications (7)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PL11871243T PL2748444T3 (pl) | 2011-08-22 | 2011-08-22 | Komora spalania cylindryczno-pierścieniowa z rozstawionymi, stycznymi dyszami paliwowo-powietrznymi do zastosowania w silnikach turbinowych |
| PCT/US2011/048612 WO2013028167A2 (fr) | 2011-08-22 | 2011-08-22 | Chambre de combustion annulaire en forme de boîte présentant des buses de carburant-air étagées et tangentielles, en vue d'une utilisation sur des moteurs à turbine à gaz |
| RU2014110628A RU2611217C2 (ru) | 2011-08-22 | 2011-08-22 | Трубчато-кольцевая камера сгорания со ступенчатыми и тангенциальными топливовоздушными форсунками для использования в газотурбинных двигателях |
| KR1020147007518A KR101774093B1 (ko) | 2011-08-22 | 2011-08-22 | 가스 터빈 엔진에서 사용되는 스테이지가 형성되고 접선방향으로 형성된 연료-공기 노즐을 가진 캔-애뉼러형 연소실 |
| JP2014527126A JP6086391B2 (ja) | 2011-08-22 | 2011-08-22 | ガス・タービン・エンジンで使用するための段階的で接線方向の燃料空気ノズルを備えた環状筒型燃焼器 |
| EP11871243.9A EP2748444B1 (fr) | 2011-08-22 | 2011-08-22 | Chambre de combustion annulaire en forme de boîte présentant des buses de carburant-air étagées et tangentielles, en vue d'une utilisation sur des moteurs à turbine à gaz |
| CN201180073013.6A CN103998745B (zh) | 2011-08-22 | 2011-08-22 | 在燃气轮机上使用的具有分级切向燃料‑空气喷嘴的筒状环形燃烧室 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/US2011/048612 WO2013028167A2 (fr) | 2011-08-22 | 2011-08-22 | Chambre de combustion annulaire en forme de boîte présentant des buses de carburant-air étagées et tangentielles, en vue d'une utilisation sur des moteurs à turbine à gaz |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| WO2013028167A2 WO2013028167A2 (fr) | 2013-02-28 |
| WO2013028167A3 true WO2013028167A3 (fr) | 2014-03-20 |
Family
ID=47747020
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/US2011/048612 Ceased WO2013028167A2 (fr) | 2011-08-22 | 2011-08-22 | Chambre de combustion annulaire en forme de boîte présentant des buses de carburant-air étagées et tangentielles, en vue d'une utilisation sur des moteurs à turbine à gaz |
Country Status (7)
| Country | Link |
|---|---|
| EP (1) | EP2748444B1 (fr) |
| JP (1) | JP6086391B2 (fr) |
| KR (1) | KR101774093B1 (fr) |
| CN (1) | CN103998745B (fr) |
| PL (1) | PL2748444T3 (fr) |
| RU (1) | RU2611217C2 (fr) |
| WO (1) | WO2013028167A2 (fr) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10139111B2 (en) | 2014-03-28 | 2018-11-27 | Siemens Energy, Inc. | Dual outlet nozzle for a secondary fuel stage of a combustor of a gas turbine engine |
| FR3032781B1 (fr) * | 2015-02-17 | 2018-07-06 | Safran Helicopter Engines | Systeme de combustion a volume constant pour turbomachine de moteur d'aeronef |
| WO2018090384A1 (fr) * | 2016-11-21 | 2018-05-24 | 深圳智慧能源技术有限公司 | Chambre de combustion de turbine à gaz |
| CN106439914A (zh) * | 2016-11-21 | 2017-02-22 | 深圳智慧能源技术有限公司 | 燃气轮机燃烧室 |
| WO2018090383A1 (fr) * | 2016-11-21 | 2018-05-24 | 深圳智慧能源技术有限公司 | Chambre de combustion d'un moteur à turbine à gaz, et buse associée |
| US11156164B2 (en) | 2019-05-21 | 2021-10-26 | General Electric Company | System and method for high frequency accoustic dampers with caps |
| US11174792B2 (en) | 2019-05-21 | 2021-11-16 | General Electric Company | System and method for high frequency acoustic dampers with baffles |
| KR102265626B1 (ko) * | 2020-09-25 | 2021-06-16 | 박재현 | 샌드 스프레이 시험 장치 |
| CN114135901A (zh) * | 2021-11-08 | 2022-03-04 | 中国航发四川燃气涡轮研究院 | 一种防烧蚀的火焰筒大孔射流套筒 |
| CN114427689B (zh) * | 2022-01-20 | 2024-07-12 | 中国空气动力研究与发展中心空天技术研究所 | 一种可实现超声速流场观测的圆盘形旋转爆震燃烧室 |
| CN114857617B (zh) * | 2022-05-20 | 2023-07-14 | 南昌航空大学 | 一种带锯齿型凹槽涡流发生器的支板火焰稳定器 |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20040144098A1 (en) * | 2000-02-24 | 2004-07-29 | Willis Jeffrey W. | Multi-stage multi-plane combustion method for a gas turbine engine |
| US20070119183A1 (en) * | 2005-11-28 | 2007-05-31 | General Electric Company | Gas turbine engine combustor |
| US20100242484A1 (en) * | 2009-03-31 | 2010-09-30 | Baha Mahmoud Suleiman | Apparatus and method for cooling gas turbine engine combustors |
| US20110020118A1 (en) * | 2009-07-21 | 2011-01-27 | Honeywell International Inc. | Turbine nozzle assembly including radially-compliant spring member for gas turbine engine |
Family Cites Families (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4098075A (en) * | 1976-06-01 | 1978-07-04 | United Technologies Corporation | Radial inflow combustor |
| IN150349B (fr) * | 1978-12-12 | 1982-09-18 | Council Scient Ind Res | |
| US4938020A (en) * | 1987-06-22 | 1990-07-03 | Sundstrand Corporation | Low cost annular combustor |
| US4891936A (en) * | 1987-12-28 | 1990-01-09 | Sundstrand Corporation | Turbine combustor with tangential fuel injection and bender jets |
| JPH0375414A (ja) * | 1989-08-15 | 1991-03-29 | Nissan Motor Co Ltd | ガスタービン燃焼器 |
| US5113647A (en) * | 1989-12-22 | 1992-05-19 | Sundstrand Corporation | Gas turbine annular combustor |
| GB2295887A (en) * | 1994-12-08 | 1996-06-12 | Rolls Royce Plc | Combustor assembly |
| JP4608154B2 (ja) * | 2001-09-27 | 2011-01-05 | 大阪瓦斯株式会社 | ガスタービン用燃焼装置及びそれを備えたガスタービン |
| US6751961B2 (en) * | 2002-05-14 | 2004-06-22 | United Technologies Corporation | Bulkhead panel for use in a combustion chamber of a gas turbine engine |
| JP3959632B2 (ja) * | 2002-09-04 | 2007-08-15 | 石川島播磨重工業株式会社 | 拡散燃焼方式低NOx燃焼器 |
| JP3901629B2 (ja) * | 2002-11-11 | 2007-04-04 | 石川島播磨重工業株式会社 | アニュラ型渦巻き拡散火炎燃焼器 |
| US7052231B2 (en) * | 2003-04-28 | 2006-05-30 | General Electric Company | Methods and apparatus for injecting fluids in gas turbine engines |
| US20070107437A1 (en) * | 2005-11-15 | 2007-05-17 | Evulet Andrei T | Low emission combustion and method of operation |
| GB0610578D0 (en) * | 2006-05-27 | 2006-07-05 | Rolls Royce Plc | Method of removing deposits |
| US8863528B2 (en) * | 2006-07-27 | 2014-10-21 | United Technologies Corporation | Ceramic combustor can for a gas turbine engine |
| EP2075508B1 (fr) * | 2006-10-20 | 2018-05-23 | IHI Corporation | Chambre de combustion de turbine à gaz |
| US8015814B2 (en) * | 2006-10-24 | 2011-09-13 | Caterpillar Inc. | Turbine engine having folded annular jet combustor |
| US8176739B2 (en) * | 2008-07-17 | 2012-05-15 | General Electric Company | Coanda injection system for axially staged low emission combustors |
| JP2010243009A (ja) * | 2009-04-02 | 2010-10-28 | Ihi Corp | ガスタービンの燃焼器 |
| US8904799B2 (en) * | 2009-05-25 | 2014-12-09 | Majed Toqan | Tangential combustor with vaneless turbine for use on gas turbine engines |
-
2011
- 2011-08-22 CN CN201180073013.6A patent/CN103998745B/zh not_active Expired - Fee Related
- 2011-08-22 EP EP11871243.9A patent/EP2748444B1/fr active Active
- 2011-08-22 PL PL11871243T patent/PL2748444T3/pl unknown
- 2011-08-22 RU RU2014110628A patent/RU2611217C2/ru active
- 2011-08-22 WO PCT/US2011/048612 patent/WO2013028167A2/fr not_active Ceased
- 2011-08-22 JP JP2014527126A patent/JP6086391B2/ja active Active
- 2011-08-22 KR KR1020147007518A patent/KR101774093B1/ko not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20040144098A1 (en) * | 2000-02-24 | 2004-07-29 | Willis Jeffrey W. | Multi-stage multi-plane combustion method for a gas turbine engine |
| US20070119183A1 (en) * | 2005-11-28 | 2007-05-31 | General Electric Company | Gas turbine engine combustor |
| US20100242484A1 (en) * | 2009-03-31 | 2010-09-30 | Baha Mahmoud Suleiman | Apparatus and method for cooling gas turbine engine combustors |
| US20110020118A1 (en) * | 2009-07-21 | 2011-01-27 | Honeywell International Inc. | Turbine nozzle assembly including radially-compliant spring member for gas turbine engine |
Also Published As
| Publication number | Publication date |
|---|---|
| EP2748444A2 (fr) | 2014-07-02 |
| PL2748444T3 (pl) | 2019-11-29 |
| EP2748444A4 (fr) | 2015-05-27 |
| RU2611217C2 (ru) | 2017-02-21 |
| CN103998745B (zh) | 2017-02-15 |
| EP2748444B1 (fr) | 2019-02-13 |
| KR20140082658A (ko) | 2014-07-02 |
| WO2013028167A2 (fr) | 2013-02-28 |
| CN103998745A (zh) | 2014-08-20 |
| JP6086391B2 (ja) | 2017-03-01 |
| RU2014110628A (ru) | 2015-09-27 |
| KR101774093B1 (ko) | 2017-09-12 |
| JP2014526029A (ja) | 2014-10-02 |
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