CN1441198B - 用于燃气涡轮发动机燃烧器的波纹式壳体及其成形方法 - Google Patents

用于燃气涡轮发动机燃烧器的波纹式壳体及其成形方法 Download PDF

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Publication number
CN1441198B
CN1441198B CN03106639.9A CN03106639A CN1441198B CN 1441198 B CN1441198 B CN 1441198B CN 03106639 A CN03106639 A CN 03106639A CN 1441198 B CN1441198 B CN 1441198B
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China
Prior art keywords
housing
burner
inch
annular corrugated
shell body
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Expired - Fee Related
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CN03106639.9A
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English (en)
Chinese (zh)
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CN1441198A (zh
Inventor
G·法默
R·D·雷登
B·B·肖特
J·A·格勒申
M·M·德代
D·L·杜尔斯托克
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General Electric Co
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General Electric Co
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Publication of CN1441198A publication Critical patent/CN1441198A/zh
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    • 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

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CN03106639.9A 2002-02-27 2003-02-27 用于燃气涡轮发动机燃烧器的波纹式壳体及其成形方法 Expired - Fee Related CN1441198B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/085,767 US6672067B2 (en) 2002-02-27 2002-02-27 Corrugated cowl for combustor of a gas turbine engine and method for configuring same
US10/085767 2002-02-27

Publications (2)

Publication Number Publication Date
CN1441198A CN1441198A (zh) 2003-09-10
CN1441198B true CN1441198B (zh) 2010-05-26

Family

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Family Applications (1)

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CN03106639.9A Expired - Fee Related CN1441198B (zh) 2002-02-27 2003-02-27 用于燃气涡轮发动机燃烧器的波纹式壳体及其成形方法

Country Status (5)

Country Link
US (1) US6672067B2 (enExample)
EP (1) EP1340941B1 (enExample)
JP (1) JP4245936B2 (enExample)
CN (1) CN1441198B (enExample)
DE (1) DE60316487T2 (enExample)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007041621A2 (en) * 2005-10-03 2007-04-12 Xingsheng Sean Ling Hybridization assisted nanopore sequencing
FR2897144B1 (fr) * 2006-02-08 2008-05-02 Snecma Sa Chambre de combustion de turbomachine a fentes tangentielles
FR2897145B1 (fr) * 2006-02-08 2013-01-18 Snecma Chambre de combustion annulaire de turbomachine a fixations alternees.
FR2906350B1 (fr) * 2006-09-22 2009-03-20 Snecma Sa Chambre de combustion annulaire d'une turbomachine
US7765809B2 (en) * 2006-11-10 2010-08-03 General Electric Company Combustor dome and methods of assembling such
US7856826B2 (en) * 2006-11-10 2010-12-28 General Electric Company Combustor dome mixer retaining means
WO2009046094A1 (en) 2007-10-01 2009-04-09 Nabsys, Inc. Biopolymer sequencing by hybridization of probes to form ternary complexes and variable range alignment
US8013738B2 (en) 2007-10-04 2011-09-06 Kd Secure, Llc Hierarchical storage manager (HSM) for intelligent storage of large volumes of data
WO2009045218A1 (en) 2007-10-04 2009-04-09 Donovan John J A video surveillance, storage, and alerting system having network management, hierarchical data storage, video tip processing, and vehicle plate analysis
US8262879B2 (en) 2008-09-03 2012-09-11 Nabsys, Inc. Devices and methods for determining the length of biopolymers and distances between probes bound thereto
US9650668B2 (en) 2008-09-03 2017-05-16 Nabsys 2.0 Llc Use of longitudinally displaced nanoscale electrodes for voltage sensing of biomolecules and other analytes in fluidic channels
EP2342362B1 (en) * 2008-09-03 2017-03-01 Nabsys 2.0 LLC Use of longitudinally displaced nanoscale electrodes for voltage sensing of biomolecules and other analytes in fluidic channels
WO2010111605A2 (en) * 2009-03-27 2010-09-30 Nabsys, Inc. Devices and methods for analyzing biomolecules and probes bound thereto
US8455260B2 (en) * 2009-03-27 2013-06-04 Massachusetts Institute Of Technology Tagged-fragment map assembly
US8246799B2 (en) * 2009-05-28 2012-08-21 Nabsys, Inc. Devices and methods for analyzing biomolecules and probes bound thereto
US8715933B2 (en) 2010-09-27 2014-05-06 Nabsys, Inc. Assay methods using nicking endonucleases
EP2640849B1 (en) 2010-11-16 2016-04-06 Nabsys 2.0 LLC Methods for sequencing a biomolecule by detecting relative positions of hybridized probes
WO2012109574A2 (en) 2011-02-11 2012-08-16 Nabsys, Inc. Assay methods using dna binding proteins
WO2014024942A1 (ja) 2012-08-07 2014-02-13 日野自動車 株式会社 バーナー
WO2014024944A1 (ja) 2012-08-07 2014-02-13 日野自動車 株式会社 排気浄化装置用バーナー
EP2843306A4 (en) 2012-08-07 2015-12-02 Hino Motors Ltd BURNER FOR EXHAUST GAS CLEANING DEVICES
CN104603539B (zh) 2012-08-13 2017-06-23 日野自动车株式会社 燃烧器
US9914966B1 (en) 2012-12-20 2018-03-13 Nabsys 2.0 Llc Apparatus and methods for analysis of biomolecules using high frequency alternating current excitation
EP2956550B1 (en) 2013-01-18 2020-04-08 Nabsys 2.0 LLC Enhanced probe binding
DE102014213302A1 (de) 2014-07-09 2016-01-14 Rolls-Royce Deutschland Ltd & Co Kg Brennkammer einer Gasturbine mit verschraubtem Brennkammerkopf
US10094332B2 (en) 2014-09-03 2018-10-09 The Boeing Company Core cowl for a turbofan engine
EP3051206B1 (en) * 2015-01-28 2019-10-30 Ansaldo Energia Switzerland AG Sequential gas turbine combustor arrangement with a mixer and a damper
DE102015213629A1 (de) 2015-07-20 2017-01-26 Rolls-Royce Deutschland Ltd & Co Kg Abdeckteil und Brennkammerbaugruppe für eine Gasturbine
US10228136B2 (en) * 2016-02-25 2019-03-12 General Electric Company Combustor assembly
US10982852B2 (en) 2018-11-05 2021-04-20 Rolls-Royce Corporation Cowl integration to combustor wall

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3898797A (en) * 1973-08-16 1975-08-12 Rolls Royce Cooling arrangements for duct walls
US5197290A (en) * 1990-03-26 1993-03-30 Fuel Systems Textron Inc. Variable area combustor air swirler
US5279127A (en) * 1990-12-21 1994-01-18 General Electric Company Multi-hole film cooled combustor liner with slotted film starter
US5924288A (en) * 1994-12-22 1999-07-20 General Electric Company One-piece combustor cowl
US6212870B1 (en) * 1998-09-22 2001-04-10 General Electric Company Self fixturing combustor dome assembly

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3854285A (en) * 1973-02-26 1974-12-17 Gen Electric Combustor dome assembly
GB2039359A (en) * 1979-01-15 1980-08-06 United Technologies Corp Gas turbine combustion chamber
US4606190A (en) * 1982-07-22 1986-08-19 United Technologies Corporation Variable area inlet guide vanes
US5181377A (en) * 1991-04-16 1993-01-26 General Electric Company Damped combustor cowl structure
US6148600A (en) 1999-02-26 2000-11-21 General Electric Company One-piece sheet metal cowl for combustor of a gas turbine engine and method of configuring same
US6438958B1 (en) * 2000-02-28 2002-08-27 General Electric Company Apparatus for reducing heat load in combustor panels

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3898797A (en) * 1973-08-16 1975-08-12 Rolls Royce Cooling arrangements for duct walls
US5197290A (en) * 1990-03-26 1993-03-30 Fuel Systems Textron Inc. Variable area combustor air swirler
US5279127A (en) * 1990-12-21 1994-01-18 General Electric Company Multi-hole film cooled combustor liner with slotted film starter
US5924288A (en) * 1994-12-22 1999-07-20 General Electric Company One-piece combustor cowl
US6212870B1 (en) * 1998-09-22 2001-04-10 General Electric Company Self fixturing combustor dome assembly

Also Published As

Publication number Publication date
DE60316487T2 (de) 2008-05-21
JP2003279044A (ja) 2003-10-02
EP1340941A3 (en) 2004-06-09
CN1441198A (zh) 2003-09-10
JP4245936B2 (ja) 2009-04-02
EP1340941B1 (en) 2007-09-26
DE60316487D1 (de) 2007-11-08
US20030159445A1 (en) 2003-08-28
US6672067B2 (en) 2004-01-06
EP1340941A2 (en) 2003-09-03

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Granted publication date: 20100526

Termination date: 20120227