DE68903138T2 - Gasturbinenbrennkammer. - Google Patents

Gasturbinenbrennkammer.

Info

Publication number
DE68903138T2
DE68903138T2 DE8989306046T DE68903138T DE68903138T2 DE 68903138 T2 DE68903138 T2 DE 68903138T2 DE 8989306046 T DE8989306046 T DE 8989306046T DE 68903138 T DE68903138 T DE 68903138T DE 68903138 T2 DE68903138 T2 DE 68903138T2
Authority
DE
Germany
Prior art keywords
combustion chamber
gas turbine
turbine combustion
gas
chamber
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 - Lifetime
Application number
DE8989306046T
Other languages
English (en)
Other versions
DE68903138D1 (de
Inventor
Stanley James Stevens
Jonathon Frederick Carrotte
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.)
Qinetiq Ltd
Original Assignee
UK Secretary of State for Defence
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 UK Secretary of State for Defence filed Critical UK Secretary of State for Defence
Publication of DE68903138D1 publication Critical patent/DE68903138D1/de
Application granted granted Critical
Publication of DE68903138T2 publication Critical patent/DE68903138T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F23R3/06Arrangement of apertures along the flame tube
    • 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
    • F23R3/045Air inlet arrangements using pipes
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
DE8989306046T 1988-06-22 1989-06-15 Gasturbinenbrennkammer. Expired - Lifetime DE68903138T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/GB1988/000476 WO1989012788A1 (en) 1988-06-22 1988-06-22 Gas turbine engine combustors

Publications (2)

Publication Number Publication Date
DE68903138D1 DE68903138D1 (de) 1992-11-12
DE68903138T2 true DE68903138T2 (de) 1993-04-29

Family

ID=10629742

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8989306046T Expired - Lifetime DE68903138T2 (de) 1988-06-22 1989-06-15 Gasturbinenbrennkammer.

Country Status (6)

Country Link
US (1) US5187937A (de)
EP (1) EP0348097B1 (de)
CA (1) CA1334893C (de)
DE (1) DE68903138T2 (de)
GB (1) GB2238864B (de)
WO (1) WO1989012788A1 (de)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6564555B2 (en) 2001-05-24 2003-05-20 Allison Advanced Development Company Apparatus for forming a combustion mixture in a gas turbine engine
US6655027B2 (en) * 2002-01-15 2003-12-02 General Electric Company Methods for assembling gas turbine engine combustors
EP1495290A4 (de) * 2002-03-25 2006-07-12 Fleming And Associates Inc Strömungsstabilisierer für eine strömungswerkbank
AU2003218373A1 (en) * 2002-03-26 2003-10-13 Fleming And Associates, Inc. Flow vector analyzer for flow bench
EP1482246A1 (de) * 2003-05-30 2004-12-01 Siemens Aktiengesellschaft Brennkammer
US7040096B2 (en) * 2003-09-08 2006-05-09 General Electric Company Methods and apparatus for supplying feed air to turbine combustors
US20070095071A1 (en) * 2003-09-29 2007-05-03 Kastrup David A Apparatus for assembling gas turbine engine combustors
US7950233B2 (en) * 2006-03-31 2011-05-31 Pratt & Whitney Canada Corp. Combustor
US20100037622A1 (en) * 2008-08-18 2010-02-18 General Electric Company Contoured Impingement Sleeve Holes
US8387397B2 (en) * 2009-01-27 2013-03-05 General Electric Company Flow conditioner for use in gas turbine component in which combustion occurs
WO2010096817A2 (en) 2009-02-23 2010-08-26 Williams International Co., L.L.C. Combustion system
US8141365B2 (en) * 2009-02-27 2012-03-27 Honeywell International Inc. Plunged hole arrangement for annular rich-quench-lean gas turbine combustors
US8171740B2 (en) * 2009-02-27 2012-05-08 Honeywell International Inc. Annular rich-quench-lean gas turbine combustors with plunged holes
US9010121B2 (en) * 2010-12-10 2015-04-21 Rolls-Royce Plc Combustion chamber
US9360215B2 (en) * 2012-04-02 2016-06-07 United Technologies Corporation Combustor having a beveled grommet
WO2015030927A1 (en) * 2013-08-30 2015-03-05 United Technologies Corporation Contoured dilution passages for a gas turbine engine combustor
EP3039340B1 (de) * 2013-08-30 2018-11-28 United Technologies Corporation Vena-contracta-verwirbelungs-verdünnungspassagen für eine gasturbinenmotor-brennkammer
US10386070B2 (en) * 2013-12-23 2019-08-20 United Technologies Corporation Multi-streamed dilution hole configuration for a gas turbine engine
CN110489863B (zh) * 2019-08-20 2023-05-26 成立航空技术(成都)有限公司 航空发动机主燃烧室出口温度场指标的确定方法

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE479471A (de) * 1947-01-09
BE501690A (de) * 1950-03-07
GB819065A (en) * 1955-11-16 1959-08-26 Rolls Royce Improvements in or relating to combustion equipment for example of gas turbine engines
US2916878A (en) * 1958-04-03 1959-12-15 Gen Electric Air-directing vane structure for fluid fuel combustor
GB943250A (en) * 1962-02-01 1963-12-04 Rolls Royce Improvements in or relating to gas turbine combustion chambers
FR1331084A (fr) * 1962-08-10 1963-06-28 Prvni Brnenska Strojirna Zd Y Mélangeur d'air et de gaz de chambre de combustion
US3919840A (en) * 1973-04-18 1975-11-18 United Technologies Corp Combustion chamber for dissimilar fluids in swirling flow relationship
DE2636520A1 (de) * 1976-08-13 1978-02-16 Daimler Benz Ag Brennkammer, insbesondere fuer gasturbinen
GB2017827B (en) * 1978-04-04 1983-02-02 Gen Electric Combustor liner cooling
GB2113377B (en) * 1982-01-15 1985-02-06 Rolls Royce Improvements in or relating to flame tubes
US4529358A (en) * 1984-02-15 1985-07-16 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Vortex generating flow passage design for increased film cooling effectiveness
US4653279A (en) * 1985-01-07 1987-03-31 United Technologies Corporation Integral refilmer lip for floatwall panels
US4875339A (en) * 1987-11-27 1989-10-24 General Electric Company Combustion chamber liner insert

Also Published As

Publication number Publication date
GB2238864A (en) 1991-06-12
GB9028048D0 (en) 1991-02-27
WO1989012788A1 (en) 1989-12-28
GB2238864B (en) 1992-04-22
DE68903138D1 (de) 1992-11-12
EP0348097B1 (de) 1992-10-07
CA1334893C (en) 1995-03-28
EP0348097A1 (de) 1989-12-27
US5187937A (en) 1993-02-23

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: QINETIQ LTD., LONDON, GB

8328 Change in the person/name/address of the agent

Representative=s name: BEETZ & PARTNER PATENTANWAELTE, 80538 MUENCHEN