GB685068A - Combustion chamber for gas turbines - Google Patents

Combustion chamber for gas turbines

Info

Publication number
GB685068A
GB685068A GB7072/50A GB707250A GB685068A GB 685068 A GB685068 A GB 685068A GB 7072/50 A GB7072/50 A GB 7072/50A GB 707250 A GB707250 A GB 707250A GB 685068 A GB685068 A GB 685068A
Authority
GB
United Kingdom
Prior art keywords
air
orifices
burner
upstream
shroud
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
Application number
GB7072/50A
Other languages
English (en)
Inventor
Isaac Lubbock
Roy Michael Palmer
Harold Rowling
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shell Refining and Marketing Co Ltd
Original Assignee
Shell Refining and Marketing Co Ltd
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
Priority to BE502037D priority Critical patent/BE502037A/xx
Application filed by Shell Refining and Marketing Co Ltd filed Critical Shell Refining and Marketing Co Ltd
Priority to GB7072/50A priority patent/GB685068A/en
Priority to FR1037635D priority patent/FR1037635A/fr
Priority to DES22437A priority patent/DE876495C/de
Publication of GB685068A publication Critical patent/GB685068A/en
Expired legal-status Critical Current

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
    • F23R3/02—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
    • 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
    • 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)
  • Gas Burners (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
GB7072/50A 1950-03-21 1950-03-21 Combustion chamber for gas turbines Expired GB685068A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
BE502037D BE502037A (nl) 1950-03-21
GB7072/50A GB685068A (en) 1950-03-21 1950-03-21 Combustion chamber for gas turbines
FR1037635D FR1037635A (fr) 1950-03-21 1951-03-21 Chambre de combustion pour turbines à gaz
DES22437A DE876495C (de) 1950-03-21 1951-03-21 Brennkammer fuer Gasturbinen

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB7072/50A GB685068A (en) 1950-03-21 1950-03-21 Combustion chamber for gas turbines

Publications (1)

Publication Number Publication Date
GB685068A true GB685068A (en) 1952-12-31

Family

ID=9826082

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7072/50A Expired GB685068A (en) 1950-03-21 1950-03-21 Combustion chamber for gas turbines

Country Status (4)

Country Link
BE (1) BE502037A (nl)
DE (1) DE876495C (nl)
FR (1) FR1037635A (nl)
GB (1) GB685068A (nl)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3092964A (en) * 1954-03-30 1963-06-11 Martin Peter Method of relighting in combustion chambers
DE1211863B (de) * 1962-02-01 1966-03-03 Rolls Royce Brennkammer fuer Gasturbinentriebwerke
US3788065A (en) * 1970-10-26 1974-01-29 United Aircraft Corp Annular combustion chamber for dissimilar fluids in swirling flow relationship
US5050385A (en) * 1982-10-06 1991-09-24 Hitachi, Ltd. Inner cylinder for a gas turbine combustor reinforced by built up welding
EP0676590A1 (en) * 1994-04-08 1995-10-11 ROLLS-ROYCE plc Gas turbine engine combustion apparatus
JP2002155759A (ja) * 2000-11-20 2002-05-31 General Electric Co <Ge> 衝突冷却遷移ダクトの側板冷却を強化する空力装置及び関連方法
GB2461542A (en) * 2008-07-03 2010-01-06 Rolls Royce Plc Combustion Arrangement with Dilution Ports and Associated Cooling Air Trim Ports
FR2948987A1 (fr) * 2009-08-04 2011-02-11 Snecma Chambre de combustion de turbomachine comportant des orifices d'entree d'air ameliores
FR2958012A1 (fr) * 2010-03-23 2011-09-30 Snecma Chambre de combustion de turbomachine
CN102472492A (zh) * 2009-08-04 2012-05-23 斯奈克玛 带有改进的进气道的涡轮机燃烧室
CN103562500A (zh) * 2011-03-29 2014-02-05 西门子能量股份有限公司 涡轮燃烧系统冷却罩
CN106969381A (zh) * 2017-03-27 2017-07-21 南京航空航天大学 可调式气旋耦合喷嘴
EP3258066A1 (en) * 2016-06-16 2017-12-20 Doosan Heavy Industries & Construction Co., Ltd. Air flow guide cap and combustion duct having the same
CN109737450A (zh) * 2018-12-11 2019-05-10 北京航空航天大学 燃烧室燃烧振荡控制装置及燃烧室燃烧振荡控制方法

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1108517B (de) * 1957-09-27 1961-06-08 Rolls Royce Gasturbinenbrennkammer
DE1123868B (de) * 1958-08-26 1962-02-15 Schweizerische Lokomotiv Brennkammer, insbesondere fuer Gasturbinen
DE1284157B (de) * 1963-12-04 1968-11-28 Rolls Royce Verbrennungseinrichtung fuer Gasturbinentriebwerke
DE2808874C2 (de) * 1978-03-02 1985-01-24 Smit Ovens Nijmegen B.V., Nijmegen Vorrichtung zur Verbrennung von in einem Gasstrom mitgeführten brennbaren Stoffen bzw. zur Erwärmung von Luft
US4702073A (en) * 1986-03-10 1987-10-27 Melconian Jerry O Variable residence time vortex combustor
US5289686A (en) * 1992-11-12 1994-03-01 General Motors Corporation Low nox gas turbine combustor liner with elliptical apertures for air swirling

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3092964A (en) * 1954-03-30 1963-06-11 Martin Peter Method of relighting in combustion chambers
DE1211863B (de) * 1962-02-01 1966-03-03 Rolls Royce Brennkammer fuer Gasturbinentriebwerke
US3788065A (en) * 1970-10-26 1974-01-29 United Aircraft Corp Annular combustion chamber for dissimilar fluids in swirling flow relationship
US5050385A (en) * 1982-10-06 1991-09-24 Hitachi, Ltd. Inner cylinder for a gas turbine combustor reinforced by built up welding
EP0676590A1 (en) * 1994-04-08 1995-10-11 ROLLS-ROYCE plc Gas turbine engine combustion apparatus
US5590530A (en) * 1994-04-08 1997-01-07 Rolls-Royce Plc Fuel and air mixing parts for a turbine combustion chamber
JP2002155759A (ja) * 2000-11-20 2002-05-31 General Electric Co <Ge> 衝突冷却遷移ダクトの側板冷却を強化する空力装置及び関連方法
EP1207273A3 (en) * 2000-11-20 2002-11-20 General Electric Company Aerodynamic devices for enhancing sidepanel cooling on an impingement cooled transition duct and related method
EP2813761A3 (en) * 2000-11-20 2015-01-07 General Electric Company Aerodynamic devices for enhancing sidepanel cooling on an impingement cooled transition duct
GB2461542A (en) * 2008-07-03 2010-01-06 Rolls Royce Plc Combustion Arrangement with Dilution Ports and Associated Cooling Air Trim Ports
GB2461542B (en) * 2008-07-03 2010-10-13 Rolls Royce Plc Combustion Arrangement with Dilution and Trim Ports
CN102472492A (zh) * 2009-08-04 2012-05-23 斯奈克玛 带有改进的进气道的涡轮机燃烧室
FR2948987A1 (fr) * 2009-08-04 2011-02-11 Snecma Chambre de combustion de turbomachine comportant des orifices d'entree d'air ameliores
CN102472492B (zh) * 2009-08-04 2015-05-06 斯奈克玛 带有改进的进气道的涡轮机燃烧室
US9175856B2 (en) 2009-08-04 2015-11-03 Snecma Combustion chamber for a turbomachine including improved air inlets
FR2958012A1 (fr) * 2010-03-23 2011-09-30 Snecma Chambre de combustion de turbomachine
CN103562500A (zh) * 2011-03-29 2014-02-05 西门子能量股份有限公司 涡轮燃烧系统冷却罩
CN103562500B (zh) * 2011-03-29 2016-08-24 西门子能量股份有限公司 涡轮燃烧系统冷却罩
US10520192B2 (en) 2016-06-16 2019-12-31 DOOSAN Heavy Industries Construction Co., LTD Air flow guide cap and combustion duct having the same
EP3258066A1 (en) * 2016-06-16 2017-12-20 Doosan Heavy Industries & Construction Co., Ltd. Air flow guide cap and combustion duct having the same
JP2017223214A (ja) * 2016-06-16 2017-12-21 ドゥサン ヘヴィー インダストリーズ アンド コンストラクション カンパニー リミテッド 空気誘導キャップ及びこれを備える燃焼ダクト
CN106969381A (zh) * 2017-03-27 2017-07-21 南京航空航天大学 可调式气旋耦合喷嘴
CN106969381B (zh) * 2017-03-27 2023-09-26 南京航空航天大学 可调式气旋耦合喷嘴
CN109737450B (zh) * 2018-12-11 2019-12-03 北京航空航天大学 燃烧室燃烧振荡控制装置及燃烧室燃烧振荡控制方法
CN109737450A (zh) * 2018-12-11 2019-05-10 北京航空航天大学 燃烧室燃烧振荡控制装置及燃烧室燃烧振荡控制方法

Also Published As

Publication number Publication date
DE876495C (de) 1953-05-15
FR1037635A (fr) 1953-09-22
BE502037A (nl)

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