DK0776444T3 - Lavemissionsforbrændingskammer beregnet for gasturbinemotorer - Google Patents

Lavemissionsforbrændingskammer beregnet for gasturbinemotorer

Info

Publication number
DK0776444T3
DK0776444T3 DK94925056T DK94925056T DK0776444T3 DK 0776444 T3 DK0776444 T3 DK 0776444T3 DK 94925056 T DK94925056 T DK 94925056T DK 94925056 T DK94925056 T DK 94925056T DK 0776444 T3 DK0776444 T3 DK 0776444T3
Authority
DK
Denmark
Prior art keywords
pct
swirler
gas turbine
combustion chamber
turbine engines
Prior art date
Application number
DK94925056T
Other languages
Danish (da)
English (en)
Inventor
Anders Sjunnesson
Patrik Johansson
Alf Andersson
Sonny Lundgren
Rolf Gabrielsson
Original Assignee
Volvo Aero Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Volvo Aero Corp filed Critical Volvo Aero Corp
Application granted granted Critical
Publication of DK0776444T3 publication Critical patent/DK0776444T3/da

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/10Air inlet arrangements for primary air
    • F23R3/12Air inlet arrangements for primary air inducing a vortex
    • F23R3/14Air inlet arrangements for primary air inducing a vortex by using swirl vanes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
DK94925056T 1994-07-13 1994-07-13 Lavemissionsforbrændingskammer beregnet for gasturbinemotorer DK0776444T3 (da)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/SE1994/000689 WO1996002796A1 (fr) 1994-07-13 1994-07-13 Chambre de combustion a faibles emissions destinee a des moteurs a turbine a gaz

Publications (1)

Publication Number Publication Date
DK0776444T3 true DK0776444T3 (da) 2001-11-26

Family

ID=20393116

Family Applications (1)

Application Number Title Priority Date Filing Date
DK94925056T DK0776444T3 (da) 1994-07-13 1994-07-13 Lavemissionsforbrændingskammer beregnet for gasturbinemotorer

Country Status (9)

Country Link
US (1) US5816050A (fr)
EP (1) EP0776444B1 (fr)
JP (1) JP3464487B2 (fr)
AT (1) ATE206513T1 (fr)
CA (1) CA2194911C (fr)
DE (2) DE69428549T2 (fr)
DK (1) DK0776444T3 (fr)
ES (1) ES2101663T3 (fr)
WO (1) WO1996002796A1 (fr)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2332509B (en) * 1997-12-19 2002-06-19 Europ Gas Turbines Ltd Fuel/air mixing arrangement for combustion apparatus
US6272840B1 (en) 2000-01-13 2001-08-14 Cfd Research Corporation Piloted airblast lean direct fuel injector
US6374615B1 (en) 2000-01-28 2002-04-23 Alliedsignal, Inc Low cost, low emissions natural gas combustor
DE60112383T2 (de) * 2000-06-21 2006-04-06 Samsung Electronics Co., Ltd., Suwon Vorrichtung und verfahren zur schaltung der übertragung eines datenratenkontrollkanals in einem mobilen kommunikationssystem hoher datenrate
US6408611B1 (en) 2000-08-10 2002-06-25 Honeywell International, Inc. Fuel control method for gas turbine
US6367262B1 (en) * 2000-09-29 2002-04-09 General Electric Company Multiple annular swirler
US6543235B1 (en) 2001-08-08 2003-04-08 Cfd Research Corporation Single-circuit fuel injector for gas turbine combustors
US6691515B2 (en) 2002-03-12 2004-02-17 Rolls-Royce Corporation Dry low combustion system with means for eliminating combustion noise
WO2007033306A2 (fr) * 2005-09-13 2007-03-22 Rolls-Royce Corporation, Ltd. Systemes de combustion pour turbine a gaz
GB2432655A (en) * 2005-11-26 2007-05-30 Siemens Ag Combustion apparatus
US7716931B2 (en) * 2006-03-01 2010-05-18 General Electric Company Method and apparatus for assembling gas turbine engine
EP1835229A1 (fr) * 2006-03-13 2007-09-19 Siemens Aktiengesellschaft Chambre de combustion et procédé pour son fonctionnement
EP1944547A1 (fr) 2007-01-15 2008-07-16 Siemens Aktiengesellschaft Procédé de contrôle d'une fuite de carburant
US9194586B2 (en) 2011-12-07 2015-11-24 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
US9243802B2 (en) 2011-12-07 2016-01-26 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
US9416972B2 (en) 2011-12-07 2016-08-16 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
DE102012216080A1 (de) * 2012-08-17 2014-02-20 Dürr Systems GmbH Brenner
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
US9958161B2 (en) 2013-03-12 2018-05-01 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
US9228747B2 (en) * 2013-03-12 2016-01-05 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
US10508811B2 (en) 2016-10-03 2019-12-17 United Technologies Corporation Circumferential fuel shifting and biasing in an axial staged combustor for a gas turbine engine
US10739003B2 (en) 2016-10-03 2020-08-11 United Technologies Corporation Radial fuel shifting and biasing in an axial staged combustor for a gas turbine engine
CN108167860B (zh) * 2017-11-28 2019-05-21 天津水泥工业设计研究院有限公司 一种烧成系统梯度燃烧自脱硝工艺方法
CN109611890A (zh) * 2018-12-14 2019-04-12 中国航发沈阳发动机研究所 一种三级的旋流装置
CN115711176B (zh) * 2021-08-23 2025-09-05 通用电气公司 具有集成喇叭形旋流器的圆顶

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3972182A (en) * 1973-09-10 1976-08-03 General Electric Company Fuel injection apparatus
US3937123A (en) * 1974-04-08 1976-02-10 Textron Inc. Blind fastener with shear washer
US4069029A (en) * 1976-09-27 1978-01-17 United States Steel Corporation Process and apparatus for producing and using cold ammonia
US4301657A (en) * 1978-05-04 1981-11-24 Caterpillar Tractor Co. Gas turbine combustion chamber
US4260367A (en) * 1978-12-11 1981-04-07 United Technologies Corporation Fuel nozzle for burner construction
JP2644745B2 (ja) * 1987-03-06 1997-08-25 株式会社日立製作所 ガスタービン用燃焼器
DE3819898A1 (de) * 1988-06-11 1989-12-14 Daimler Benz Ag Brennkammer fuer eine thermische stroemungsmaschine
JP3077939B2 (ja) * 1990-10-23 2000-08-21 ロールス−ロイス・ピーエルシー ガスタービン燃焼室及びその操作方法
GB9023004D0 (en) * 1990-10-23 1990-12-05 Rolls Royce Plc A gas turbine engine combustion chamber and a method of operating a gas turbine engine combustion chamber
FR2673705A1 (fr) * 1991-03-06 1992-09-11 Snecma Chambre de combustion de turbomachine munie d'un dispositif anti-cokefaction du fond de ladite chambre.
US5406799A (en) * 1992-06-12 1995-04-18 United Technologies Corporation Combustion chamber

Also Published As

Publication number Publication date
ES2101663T1 (es) 1997-07-16
JPH10502727A (ja) 1998-03-10
DE776444T1 (de) 1997-12-18
US5816050A (en) 1998-10-06
EP0776444B1 (fr) 2001-10-04
CA2194911C (fr) 2004-11-16
JP3464487B2 (ja) 2003-11-10
DE69428549T2 (de) 2002-05-08
CA2194911A1 (fr) 1996-02-01
ATE206513T1 (de) 2001-10-15
DE69428549D1 (de) 2001-11-08
EP0776444A1 (fr) 1997-06-04
WO1996002796A1 (fr) 1996-02-01
ES2101663T3 (es) 2001-12-16

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