ATE528589T1 - Swirler - Google Patents
SwirlerInfo
- Publication number
- ATE528589T1 ATE528589T1 AT08013950T AT08013950T ATE528589T1 AT E528589 T1 ATE528589 T1 AT E528589T1 AT 08013950 T AT08013950 T AT 08013950T AT 08013950 T AT08013950 T AT 08013950T AT E528589 T1 ATE528589 T1 AT E528589T1
- Authority
- AT
- Austria
- Prior art keywords
- hub
- limiting wall
- axle
- swirlers
- swirler
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 abstract 1
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
- F23R3/02—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
- F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl 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
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP08013950A EP2151630B1 (de) | 2008-08-04 | 2008-08-04 | Swirler |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE528589T1 true ATE528589T1 (de) | 2011-10-15 |
Family
ID=40351605
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT08013950T ATE528589T1 (de) | 2008-08-04 | 2008-08-04 | Swirler |
Country Status (3)
| Country | Link |
|---|---|
| EP (1) | EP2151630B1 (enExample) |
| JP (1) | JP5574635B2 (enExample) |
| AT (1) | ATE528589T1 (enExample) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102012002465A1 (de) | 2012-02-08 | 2013-08-08 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinenbrennkammer mit unsymmetrischen Kraftstoffdüsen |
| US20180335214A1 (en) * | 2017-05-18 | 2018-11-22 | United Technologies Corporation | Fuel air mixer assembly for a gas turbine engine combustor |
| CN114413284A (zh) * | 2021-12-28 | 2022-04-29 | 北京动力机械研究所 | 一种与环形燃烧室头部匹配的异形旋流器 |
Family Cites Families (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6122127A (ja) * | 1984-07-10 | 1986-01-30 | Hitachi Ltd | ガスタ−ビン燃焼器 |
| JPH02267419A (ja) * | 1989-04-10 | 1990-11-01 | Hitachi Ltd | ガスタービン燃焼器 |
| US5359847B1 (en) * | 1993-06-01 | 1996-04-09 | Westinghouse Electric Corp | Dual fuel ultra-flow nox combustor |
| FR2751054B1 (fr) * | 1996-07-11 | 1998-09-18 | Snecma | Chambre de combustion anti-nox a injection de carburant de type annulaire |
| US6038861A (en) * | 1998-06-10 | 2000-03-21 | Siemens Westinghouse Power Corporation | Main stage fuel mixer with premixing transition for dry low Nox (DLN) combustors |
| US6119459A (en) * | 1998-08-18 | 2000-09-19 | Alliedsignal Inc. | Elliptical axial combustor swirler |
| JP2002031343A (ja) * | 2000-07-13 | 2002-01-31 | Mitsubishi Heavy Ind Ltd | 燃料噴出部材、バーナ、燃焼器の予混合ノズル、燃焼器、ガスタービン及びジェットエンジン |
| JP2002213746A (ja) * | 2001-01-19 | 2002-07-31 | Mitsubishi Heavy Ind Ltd | バーナ、燃焼器の予混合ノズル及び燃焼器 |
| JP4610796B2 (ja) * | 2001-06-13 | 2011-01-12 | 三菱重工業株式会社 | ガスタービン燃焼器 |
| JP3986348B2 (ja) * | 2001-06-29 | 2007-10-03 | 三菱重工業株式会社 | ガスタービン燃焼器の燃料供給ノズルおよびガスタービン燃焼器並びにガスタービン |
| JP4610800B2 (ja) * | 2001-06-29 | 2011-01-12 | 三菱重工業株式会社 | ガスタービン燃焼器 |
| JP2003130351A (ja) * | 2001-10-18 | 2003-05-08 | Mitsubishi Heavy Ind Ltd | 燃焼器、ガスタービン及びジェットエンジン |
| JP4070758B2 (ja) * | 2004-09-10 | 2008-04-02 | 三菱重工業株式会社 | ガスタービン燃焼器 |
| JP4476177B2 (ja) * | 2005-06-06 | 2010-06-09 | 三菱重工業株式会社 | ガスタービンの燃焼バーナー |
| JP4486549B2 (ja) * | 2005-06-06 | 2010-06-23 | 三菱重工業株式会社 | ガスタービンの燃焼器 |
-
2008
- 2008-08-04 AT AT08013950T patent/ATE528589T1/de active
- 2008-08-04 EP EP08013950A patent/EP2151630B1/de not_active Not-in-force
-
2009
- 2009-07-31 JP JP2009179079A patent/JP5574635B2/ja not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| EP2151630B1 (de) | 2011-10-12 |
| JP2010038538A (ja) | 2010-02-18 |
| EP2151630A1 (de) | 2010-02-10 |
| JP5574635B2 (ja) | 2014-08-20 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| WO2015076883A3 (en) | Dual fuel nozzle with swirling axial gas injection for a gas turbine engine | |
| GB2471231B (en) | Unitary swirlers and method of manufacturing the same | |
| GB201020230D0 (en) | Nose cone assembly | |
| EP2481985A3 (en) | Fuel injector assembly | |
| EP2771618B8 (fr) | Paroi annulaire de chambre de combustion à refroidissement amélioré au niveau des trous primaires et/ou de dilution | |
| EP2626635A3 (en) | Combustor assembly with trapped vortex cavity | |
| MX2011006702A (es) | Difusor de aire y sistema de circulacion de aire. | |
| UA114369C2 (uk) | Твердопаливний пальник та твердопаливний котел | |
| MX2014008144A (es) | Quemador de gas con llama de remolino interior. | |
| EP2855875A4 (en) | TRANSMISSION TOWER WITH THREE TURBINES WITH HIGH-SPEED FAN DRIVER TURBINE | |
| MX2015003099A (es) | Mecanismo divisor de flujo variable para una cámara de combustión de etapas múltiples. | |
| WO2015050592A3 (en) | Gas turbine engine combustor liner panel | |
| BRPI0907645A2 (pt) | Difusor para uma turbomáquina e turbomáquina, como um turborreator ou um turbopropulsor de avião | |
| WO2009007283A3 (de) | Gasturbinenbrenner | |
| BR112014013182A2 (pt) | Queimador, e método de combustão | |
| EP2977680A3 (en) | Dilution hole assembly | |
| WO2015002686A3 (en) | Gas turbine engine combustor liner panel | |
| ATE528589T1 (de) | Swirler | |
| GB201120105D0 (en) | A turbomachine casing assembly | |
| JP2013522551A5 (enExample) | ||
| Li et al. | Extinction in periodic competitive stage-structured Lotka–Volterra model with the effects of toxic substances | |
| JP2014149127A5 (enExample) | ||
| WO2014099076A3 (en) | Gas turbine engine combustor with integrated combustor vane | |
| MX2015014400A (es) | Montaje de generador de vortices removible para una camisa de la camara de combustion. | |
| WO2012144766A3 (ko) | 연소실 냉각장치 및 연소실 냉각 구조를 갖는 연소장치 |