FR1037635A - Chambre de combustion pour turbines à gaz - Google Patents

Chambre de combustion pour turbines à gaz

Info

Publication number
FR1037635A
FR1037635A FR1037635DA FR1037635A FR 1037635 A FR1037635 A FR 1037635A FR 1037635D A FR1037635D A FR 1037635DA FR 1037635 A FR1037635 A FR 1037635A
Authority
FR
France
Prior art keywords
combustion chamber
gas turbines
turbines
gas
combustion
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
Other languages
English (en)
French (fr)
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
Application filed by Shell Refining and Marketing Co Ltd filed Critical Shell Refining and Marketing Co Ltd
Application granted granted Critical
Publication of FR1037635A publication Critical patent/FR1037635A/fr
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)
FR1037635D 1950-03-21 1951-03-21 Chambre de combustion pour turbines à gaz Expired FR1037635A (fr)

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
FR1037635A true FR1037635A (fr) 1953-09-22

Family

ID=9826082

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1037635D Expired FR1037635A (fr) 1950-03-21 1951-03-21 Chambre de combustion pour turbines à gaz

Country Status (4)

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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011015543A1 (fr) * 2009-08-04 2011-02-10 Snecma Chambre de combustion de turbomachine comprenant des orifices d'entree d'air ameliores

Families Citing this family (19)

* 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
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
GB943250A (en) * 1962-02-01 1963-12-04 Rolls Royce Improvements in or relating to gas turbine combustion chambers
DE1284157B (de) * 1963-12-04 1968-11-28 Rolls Royce Verbrennungseinrichtung fuer Gasturbinentriebwerke
US3788065A (en) * 1970-10-26 1974-01-29 United Aircraft Corp Annular combustion chamber for dissimilar fluids in swirling flow relationship
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
JPS5966619A (ja) * 1982-10-06 1984-04-16 Hitachi Ltd ガスタ−ビン燃焼器
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
GB9407029D0 (en) * 1994-04-08 1994-06-08 Rolls Royce Plc Gas turbine engine combustion apparatus
US6494044B1 (en) * 1999-11-19 2002-12-17 General Electric Company Aerodynamic devices for enhancing sidepanel cooling on an impingement cooled transition duct and related method
GB2461542B (en) * 2008-07-03 2010-10-13 Rolls Royce Plc Combustion Arrangement with Dilution and Trim Ports
FR2948987B1 (fr) * 2009-08-04 2011-12-09 Snecma Chambre de combustion de turbomachine comportant des orifices d'entree d'air ameliores
FR2958012B1 (fr) * 2010-03-23 2013-12-13 Snecma Chambre de combustion de turbomachine
US9127551B2 (en) * 2011-03-29 2015-09-08 Siemens Energy, Inc. Turbine combustion system cooling scoop
KR101766449B1 (ko) 2016-06-16 2017-08-08 두산중공업 주식회사 공기유도 캡 및 이를 구비하는 연소 덕트
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

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011015543A1 (fr) * 2009-08-04 2011-02-10 Snecma Chambre de combustion de turbomachine comprenant des orifices d'entree d'air ameliores
FR2948988A1 (fr) * 2009-08-04 2011-02-11 Snecma Chambre de combustion de turbomachine comprenant des orifices d'entree d'air ameliores
US9175856B2 (en) 2009-08-04 2015-11-03 Snecma Combustion chamber for a turbomachine including improved air inlets

Also Published As

Publication number Publication date
GB685068A (en) 1952-12-31
DE876495C (de) 1953-05-15
BE502037A (enrdf_load_stackoverflow)

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