DE60319168D1 - Vorrichtung zur Positionierung eines Zünders an einer Gasturbinenbrennkammerwand - Google Patents

Vorrichtung zur Positionierung eines Zünders an einer Gasturbinenbrennkammerwand

Info

Publication number
DE60319168D1
DE60319168D1 DE60319168T DE60319168T DE60319168D1 DE 60319168 D1 DE60319168 D1 DE 60319168D1 DE 60319168 T DE60319168 T DE 60319168T DE 60319168 T DE60319168 T DE 60319168T DE 60319168 D1 DE60319168 D1 DE 60319168D1
Authority
DE
Germany
Prior art keywords
fuze
positioning
gas turbine
turbine combustor
combustor wall
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
DE60319168T
Other languages
English (en)
Other versions
DE60319168T2 (de
Inventor
Tracy Lowell White
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of DE60319168D1 publication Critical patent/DE60319168D1/de
Publication of DE60319168T2 publication Critical patent/DE60319168T2/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
    • F23R3/002—Wall structures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2207/00—Ignition devices associated with burner
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00012—Details of sealing devices

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gasket Seals (AREA)
  • Spark Plugs (AREA)
DE60319168T 2002-03-04 2003-03-04 Vorrichtung zur Positionierung eines Zünders an einer Gasturbinenbrennkammerwand Expired - Lifetime DE60319168T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US90192 2002-03-04
US10/090,192 US6715279B2 (en) 2002-03-04 2002-03-04 Apparatus for positioning an igniter within a liner port of a gas turbine engine

Publications (2)

Publication Number Publication Date
DE60319168D1 true DE60319168D1 (de) 2008-04-03
DE60319168T2 DE60319168T2 (de) 2009-03-19

Family

ID=27753978

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60319168T Expired - Lifetime DE60319168T2 (de) 2002-03-04 2003-03-04 Vorrichtung zur Positionierung eines Zünders an einer Gasturbinenbrennkammerwand

Country Status (5)

Country Link
US (1) US6715279B2 (de)
EP (1) EP1342954B1 (de)
JP (1) JP4272451B2 (de)
CN (1) CN100529545C (de)
DE (1) DE60319168T2 (de)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1312865A1 (de) * 2001-11-15 2003-05-21 Siemens Aktiengesellschaft Ringbrennkammer für eine Gasturbine
GB0227842D0 (en) * 2002-11-29 2003-01-08 Rolls Royce Plc Sealing Arrangement
US7007480B2 (en) * 2003-04-09 2006-03-07 Honeywell International, Inc. Multi-axial pivoting combustor liner in gas turbine engine
FR2856466B1 (fr) * 2003-06-20 2005-08-26 Snecma Moteurs Dispositif d'etancheite de bougie non soude sur la paroi de chambre
US20080229749A1 (en) * 2005-03-04 2008-09-25 Michel Gamil Rabbat Plug in rabbat engine
US20060196189A1 (en) * 2005-03-04 2006-09-07 Rabbat Michel G Rabbat engine
US7546739B2 (en) * 2005-07-05 2009-06-16 General Electric Company Igniter tube and method of assembling same
US8479490B2 (en) * 2007-03-30 2013-07-09 Honeywell International Inc. Combustors with impingement cooled igniters and igniter tubes for improved cooling of igniters
US20090293486A1 (en) * 2007-10-26 2009-12-03 Honeywell International, Inc. Combustors with igniters having protrusions
FR2925147B1 (fr) * 2007-12-14 2012-07-13 Snecma Dispositif de guidage d'un element dans un orifice d'une paroi de chambre de combustion de turbomachine
US8046987B2 (en) * 2008-09-03 2011-11-01 Woodard, Inc. Air cooled core mounted ignition system
FR2952702B1 (fr) * 2009-11-19 2013-05-10 Snecma Guidage d'une bougie d'allumage dans une chambre de combustion
US8726631B2 (en) * 2009-11-23 2014-05-20 Honeywell International Inc. Dual walled combustors with impingement cooled igniters
FR2953908A1 (fr) * 2009-12-16 2011-06-17 Snecma Guidage d'une bougie dans une chambre de combustion de turbomachine
FR2957975B1 (fr) * 2010-03-24 2013-06-28 Snecma Dispositif de positionnement d'une bougie d'allumage
US8973365B2 (en) * 2010-10-29 2015-03-10 Solar Turbines Incorporated Gas turbine combustor with mounting for Helmholtz resonators
US9157638B2 (en) 2012-01-31 2015-10-13 General Electric Company Adaptor assembly for removable components
WO2014137409A1 (en) 2013-03-07 2014-09-12 Rolls-Royce Corporation Flexible bellows igniter seal for a gas turbine with a ceramic combustion liner
EP2971967B1 (de) 2013-03-14 2018-03-21 Rolls-Royce Corporation Zündrohr mit umgekehrter kappe
DE102013222932A1 (de) * 2013-11-11 2015-05-28 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenbrennkammer mit Schindel zur Durchführung einer Zündkerze
FR3015642B1 (fr) * 2013-12-23 2018-03-02 Safran Aircraft Engines Bougie de turbomachine et son dispositif de fixation radiale
EP2927595B1 (de) * 2014-04-02 2019-11-13 United Technologies Corporation Schutzmanschettenanordnung und verfahren zum entwurf
US9651261B2 (en) * 2014-06-25 2017-05-16 Siemens Energy, Inc. Combustion turbine engine combustor basket igniter port alignment verification tool and method for validating igniter alignment
DE102014214775A1 (de) 2014-07-28 2016-01-28 Rolls-Royce Deutschland Ltd & Co Kg Fluggasturbine mit einer Dichtung zur Abdichtung einer Zündkerze an der Brennkammerwand einer Gasturbine
US9803863B2 (en) * 2015-05-13 2017-10-31 Solar Turbines Incorporated Controlled-leak combustor grommet
US10041413B2 (en) * 2015-06-05 2018-08-07 General Electric Company Igniter assembly for a gas turbine engine
US10145559B2 (en) 2015-12-15 2018-12-04 General Electric Company Gas turbine engine with igniter stack or borescope mount having noncollinear cooling passages
GB201804656D0 (en) 2018-03-23 2018-05-09 Rolls Royce Plc An igniter seal arrangement for a combustion chamber
FR3081211B1 (fr) * 2018-05-16 2021-02-26 Safran Aircraft Engines Ensemble pour une chambre de combustion de turbomachine
CN111502861B (zh) * 2020-04-23 2021-05-04 中国航发湖南动力机械研究所 一种发动机燃烧室

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2941363A (en) * 1955-04-11 1960-06-21 Bendix Aviat Corp Dual baffled igniter for combustion chamber
US3990834A (en) 1973-09-17 1976-11-09 General Electric Company Cooled igniter
GB1602836A (en) * 1977-05-11 1981-11-18 Lucas Industries Ltd Sealing arrangement for use in a combustion assembly
US4194358A (en) 1977-12-15 1980-03-25 General Electric Company Double annular combustor configuration
JPS598652B2 (ja) * 1978-03-01 1984-02-25 トヨタ自動車株式会社 ト−チ点火装置
US4584834A (en) * 1982-07-06 1986-04-29 General Electric Company Gas turbine engine carburetor
US4593340A (en) 1985-08-13 1986-06-03 Allied Corporation Igniter with improved insulator support
US4903476A (en) 1988-12-27 1990-02-27 General Electric Company Gas turbine igniter with ball-joint support
US5129231A (en) * 1990-03-12 1992-07-14 United Technologies Corporation Cooled combustor dome heatshield
US5421158A (en) 1994-10-21 1995-06-06 General Electric Company Segmented centerbody for a double annular combustor
US6286302B1 (en) * 1999-04-01 2001-09-11 General Electric Company Venturi for use in the swirl cup package of a gas turbine combustor having water injected therein
US6557350B2 (en) * 2001-05-17 2003-05-06 General Electric Company Method and apparatus for cooling gas turbine engine igniter tubes

Also Published As

Publication number Publication date
JP2003287229A (ja) 2003-10-10
US6715279B2 (en) 2004-04-06
US20030163995A1 (en) 2003-09-04
CN100529545C (zh) 2009-08-19
EP1342954A1 (de) 2003-09-10
DE60319168T2 (de) 2009-03-19
JP4272451B2 (ja) 2009-06-03
CN1490563A (zh) 2004-04-21
EP1342954B1 (de) 2008-02-20

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Legal Events

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8364 No opposition during term of opposition