DE60216023D1 - Gasturbinenbrennkammer - Google Patents

Gasturbinenbrennkammer

Info

Publication number
DE60216023D1
DE60216023D1 DE60216023T DE60216023T DE60216023D1 DE 60216023 D1 DE60216023 D1 DE 60216023D1 DE 60216023 T DE60216023 T DE 60216023T DE 60216023 T DE60216023 T DE 60216023T DE 60216023 D1 DE60216023 D1 DE 60216023D1
Authority
DE
Germany
Prior art keywords
gas turbine
turbine combustor
combustor
gas
turbine
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
DE60216023T
Other languages
English (en)
Other versions
DE60216023T2 (de
Inventor
David James Sherwood
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 claimed from GB0121916A external-priority patent/GB0121916D0/en
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of DE60216023D1 publication Critical patent/DE60216023D1/de
Publication of DE60216023T2 publication Critical patent/DE60216023T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • 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
DE60216023T 2001-09-11 2002-08-23 Gasturbinenbrennkammer Expired - Lifetime DE60216023T2 (de)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
GB0121916 2001-09-11
GB0121916A GB0121916D0 (en) 2001-09-11 2001-09-11 Gas turbine engine combustor
GB0215146A GB2379499B (en) 2001-09-11 2002-07-01 Gas turbine engine combustor
GB0215146 2002-07-01

Publications (2)

Publication Number Publication Date
DE60216023D1 true DE60216023D1 (de) 2006-12-28
DE60216023T2 DE60216023T2 (de) 2007-06-28

Family

ID=26246530

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60216023T Expired - Lifetime DE60216023T2 (de) 2001-09-11 2002-08-23 Gasturbinenbrennkammer

Country Status (4)

Country Link
US (1) US7395669B2 (de)
EP (1) EP1291581B1 (de)
DE (1) DE60216023T2 (de)
GB (1) GB2379499B (de)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
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GB2399408B (en) 2003-03-14 2006-02-22 Rolls Royce Plc Gas turbine engine combustor
US8973374B2 (en) * 2007-09-06 2015-03-10 United Technologies Corporation Blades in a turbine section of a gas turbine engine
US7984607B2 (en) * 2007-09-06 2011-07-26 United Technologies Corp. Gas turbine engine systems and related methods involving vane-blade count ratios greater than unity
US8468797B2 (en) * 2007-09-06 2013-06-25 United Technologies Corporation Gas turbine engine systems and related methods involving vane-blade count ratios greater than unity
US8205457B2 (en) 2007-12-27 2012-06-26 General Electric Company Gas turbine engine combustor and method for delivering purge gas into a combustion chamber of the combustor
US8128366B2 (en) * 2008-06-06 2012-03-06 United Technologies Corporation Counter-vortex film cooling hole design
US20090304494A1 (en) * 2008-06-06 2009-12-10 United Technologies Corporation Counter-vortex paired film cooling hole design
US8806747B2 (en) 2008-08-08 2014-08-19 Alliant Techsystems Inc. Method of manufacturing heat exchanger cooling passages in aero propulsion structure
US20100269513A1 (en) * 2009-04-23 2010-10-28 General Electric Company Thimble Fan for a Combustion System
US8863527B2 (en) * 2009-04-30 2014-10-21 Rolls-Royce Corporation Combustor liner
US20120036859A1 (en) * 2010-08-12 2012-02-16 General Electric Company Combustor transition piece with dilution sleeves and related method
US9062884B2 (en) 2011-05-26 2015-06-23 Honeywell International Inc. Combustors with quench inserts
US9631517B2 (en) 2012-12-29 2017-04-25 United Technologies Corporation Multi-piece fairing for monolithic turbine exhaust case
US11112115B2 (en) * 2013-08-30 2021-09-07 Raytheon Technologies Corporation Contoured dilution passages for gas turbine engine combustor
US20160201908A1 (en) * 2013-08-30 2016-07-14 United Technologies Corporation Vena contracta swirling dilution passages for gas turbine engine combustor
EP2957833B1 (de) 2014-06-17 2018-10-24 Rolls-Royce Corporation Brennkammeranordnung mit rinnen
US10309655B2 (en) * 2014-08-26 2019-06-04 Siemens Energy, Inc. Cooling system for fuel nozzles within combustor in a turbine engine
DE102016203012A1 (de) 2016-02-25 2017-06-01 Deutsches Zentrum für Luft- und Raumfahrt e.V. Brennkammer
US11262142B2 (en) 2016-04-26 2022-03-01 Northrop Grumman Systems Corporation Heat exchangers, weld configurations for heat exchangers and related systems and methods
US20200041127A1 (en) * 2018-08-01 2020-02-06 General Electric Company Dilution Structure for Gas Turbine Engine Combustor
US11255543B2 (en) * 2018-08-07 2022-02-22 General Electric Company Dilution structure for gas turbine engine combustor
US11085639B2 (en) * 2018-12-27 2021-08-10 Rolls-Royce North American Technologies Inc. Gas turbine combustor liner with integral chute made by additive manufacturing process
KR102164620B1 (ko) * 2019-06-19 2020-10-12 두산중공업 주식회사 연소기 및 이를 포함하는 가스터빈
US20220364729A1 (en) * 2021-05-14 2022-11-17 General Electric Company Combustor dilution with vortex generating turbulators
CN116658932A (zh) * 2022-02-18 2023-08-29 通用电气公司 具有带旋流轮叶的稀释开口的燃烧器衬套

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US4392355A (en) * 1969-11-13 1983-07-12 General Motors Corporation Combustion liner
US3899882A (en) * 1974-03-27 1975-08-19 Westinghouse Electric Corp Gas turbine combustor basket cooling
US3981142A (en) * 1974-04-01 1976-09-21 General Motors Corporation Ceramic combustion liner
US4315405A (en) * 1978-12-09 1982-02-16 Rolls-Royce Limited Combustion apparatus
GB2037419B (en) * 1978-12-09 1983-02-09 Rolls Royce Gas turbine
US4233123A (en) * 1978-12-18 1980-11-11 General Motors Corporation Method for making an air cooled combustor
JPS5913829A (ja) * 1982-07-15 1984-01-24 Hitachi Ltd ガスタ−ビン燃焼器
US4641240A (en) * 1984-05-18 1987-02-03 R. F. Shoup Corporation Electronic voting machine and system
US4629416A (en) * 1985-06-11 1986-12-16 Voorheis Industries, Inc. Bluff body register
US5329773A (en) * 1989-08-31 1994-07-19 Alliedsignal Inc. Turbine combustor cooling system
FR2674317B1 (fr) * 1991-03-20 1993-05-28 Snecma Chambre de combustion de turbomachine comportant un reglage du debit de comburant.
DE4239856A1 (de) * 1992-11-27 1994-06-01 Asea Brown Boveri Gasturbinenbrennkammer
US5337568A (en) * 1993-04-05 1994-08-16 General Electric Company Micro-grooved heat transfer wall
US5610383A (en) * 1996-04-26 1997-03-11 Chumbley; Gregory R. Device for collecting voting data
US6250548B1 (en) * 1997-10-16 2001-06-26 Mcclure Neil Electronic voting system
US6081793A (en) * 1997-12-30 2000-06-27 International Business Machines Corporation Method and system for secure computer moderated voting
JPH11296597A (ja) * 1998-04-06 1999-10-29 Center For Polytical Pub Relations:The 有権者登録確認方法ならびに装置及び同方法がプログラムされ記録される記録媒体
AU5805099A (en) * 1998-09-02 2000-03-21 Diversified Dynamics, Inc. Direct vote recording system
US6101814A (en) * 1999-04-15 2000-08-15 United Technologies Corporation Low emissions can combustor with dilution hole arrangement for a turbine engine
US6769613B2 (en) * 2000-12-07 2004-08-03 Anthony I. Provitola Auto-verifying voting system and voting method
US6540138B2 (en) * 2000-12-20 2003-04-01 Symbol Technologies, Inc. Voting method and system
US6968999B2 (en) * 2000-12-28 2005-11-29 Reardon David C Computer enhanced voting system including verifiable, custom printed ballots imprinted to the specifications of each voter

Also Published As

Publication number Publication date
GB2379499B (en) 2004-01-28
US7395669B2 (en) 2008-07-08
EP1291581A2 (de) 2003-03-12
DE60216023T2 (de) 2007-06-28
GB2379499A (en) 2003-03-12
US20030046934A1 (en) 2003-03-13
EP1291581B1 (de) 2006-11-15
EP1291581A3 (de) 2004-04-28
GB0215146D0 (en) 2002-08-07

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition