DE602009000109D1 - Montageanordnung einer Zündkerze in einer Brennkammer eines Gasturbinenmotors - Google Patents

Montageanordnung einer Zündkerze in einer Brennkammer eines Gasturbinenmotors

Info

Publication number
DE602009000109D1
DE602009000109D1 DE602009000109T DE602009000109T DE602009000109D1 DE 602009000109 D1 DE602009000109 D1 DE 602009000109D1 DE 602009000109 T DE602009000109 T DE 602009000109T DE 602009000109 T DE602009000109 T DE 602009000109T DE 602009000109 D1 DE602009000109 D1 DE 602009000109D1
Authority
DE
Germany
Prior art keywords
combustion chamber
gas turbine
turbine engine
spark plug
mounting arrangement
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.)
Active
Application number
DE602009000109T
Other languages
English (en)
Inventor
Christophe Pieussergues
Denis Jean Maurice Sandelis
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Publication of DE602009000109D1 publication Critical patent/DE602009000109D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • F02C7/264—Ignition
    • F02C7/266—Electric
    • 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
    • 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
    • F23D—BURNERS
    • F23D2211/00—Thermal dilatation prevention or compensation
    • 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)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Ignition Installations For Internal Combustion Engines (AREA)
  • Spark Plugs (AREA)
DE602009000109T 2008-02-11 2009-02-11 Montageanordnung einer Zündkerze in einer Brennkammer eines Gasturbinenmotors Active DE602009000109D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0800712A FR2927367B1 (fr) 2008-02-11 2008-02-11 Dispositif de montage d'une bougie d'allumage dans une chambre de combustion de moteur a turbine a gaz

Publications (1)

Publication Number Publication Date
DE602009000109D1 true DE602009000109D1 (de) 2010-09-30

Family

ID=39800459

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602009000109T Active DE602009000109D1 (de) 2008-02-11 2009-02-11 Montageanordnung einer Zündkerze in einer Brennkammer eines Gasturbinenmotors

Country Status (7)

Country Link
US (1) US8099963B2 (de)
EP (1) EP2088374B1 (de)
JP (1) JP5441424B2 (de)
CA (1) CA2652798C (de)
DE (1) DE602009000109D1 (de)
FR (1) FR2927367B1 (de)
RU (1) RU2488044C2 (de)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2952703B1 (fr) * 2009-11-19 2011-10-28 Snecma Guide d'une bougie d'allumage dans une chambre de combustion d'une turbomachine
FR2952704B1 (fr) * 2009-11-19 2015-08-07 Snecma Guidage rotulant d'une bougie d'allumage dans une chambre de combustion d'une turbomachine
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
FR2975172B1 (fr) * 2011-05-10 2013-05-31 Snecma Dispositif pour le montage d'une bougie d'allumage dans une chambre de combustion de moteur a turbine a gaz
US8997453B2 (en) * 2012-06-29 2015-04-07 United Technologies Corporation Igniter for a turbomachine and mounting assembly therefor
US9249978B2 (en) * 2012-07-03 2016-02-02 Alstom Technology Ltd Retaining collar for a gas turbine combustion liner
US9097130B2 (en) * 2012-09-13 2015-08-04 General Electric Company Seal for use between injector and combustion chamber in gas turbine
FR3001283A1 (fr) * 2013-01-18 2014-07-25 Snecma Traversee coulissante d'axe d'inclinaison variable relativement a l'axe d'un bol melangeur
WO2014168654A1 (en) 2013-03-14 2014-10-16 Rolls-Royce Corporation Inverted cap igniter tube
US9989254B2 (en) * 2013-06-03 2018-06-05 General Electric Company Combustor leakage control system
FR3015642B1 (fr) * 2013-12-23 2018-03-02 Safran Aircraft Engines Bougie de turbomachine et son dispositif de fixation radiale
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
US9897319B2 (en) * 2015-02-25 2018-02-20 United Technologies Corporation Igniter position for a combustor of a gas turbine engine
FR3033028B1 (fr) * 2015-02-25 2019-12-27 Safran Helicopter Engines Chambre de combustion de turbomachine comportant une piece penetrante avec ouverture
US10041413B2 (en) 2015-06-05 2018-08-07 General Electric Company Igniter assembly for a gas turbine engine
US11242804B2 (en) 2017-06-14 2022-02-08 General Electric Company Inleakage management apparatus

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3879940A (en) * 1973-07-30 1975-04-29 Gen Electric Gas turbine engine fuel delivery tube assembly
JPS5257106U (de) * 1975-10-23 1977-04-25
GB2097112B (en) * 1981-04-16 1984-12-12 Rolls Royce Fuel burners and combustion equipment for use in gas turbine engines
RU2111592C1 (ru) * 1994-07-04 1998-05-20 Акционерное общество "Авиадвигатель" Свеча зажигания камеры сгорания газотурбинного двигателя
US6557350B2 (en) * 2001-05-17 2003-05-06 General Electric Company Method and apparatus for cooling gas turbine engine igniter tubes
RU2215348C2 (ru) * 2001-12-06 2003-10-27 Открытое акционерное общество "Авиадвигатель" Свеча зажигания газотурбинного двигателя
US6920762B2 (en) * 2003-01-14 2005-07-26 General Electric Company Mounting assembly for igniter in a gas turbine engine combustor having a ceramic matrix composite liner
FR2856466B1 (fr) 2003-06-20 2005-08-26 Snecma Moteurs Dispositif d'etancheite de bougie non soude sur la paroi de chambre
US7628019B2 (en) * 2005-03-21 2009-12-08 United Technologies Corporation Fuel injector bearing plate assembly and swirler assembly
FR2891350A1 (fr) * 2005-09-29 2007-03-30 Snecma Sa Dispositif de guidage d'un element dans un orifice d'une paroi de chambre de combustion de turbomachine
RU52529U1 (ru) * 2005-10-24 2006-03-27 Федеральное государственное унитарное предприятие Уфимское научно-производственное предприятие "Молния" Свеча зажигания для газотурбинного двигателя
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

Also Published As

Publication number Publication date
RU2009104549A (ru) 2010-08-20
FR2927367A1 (fr) 2009-08-14
JP5441424B2 (ja) 2014-03-12
EP2088374B1 (de) 2010-08-18
CA2652798C (fr) 2015-11-24
RU2488044C2 (ru) 2013-07-20
FR2927367B1 (fr) 2010-05-28
CA2652798A1 (fr) 2009-08-11
US8099963B2 (en) 2012-01-24
EP2088374A1 (de) 2009-08-12
JP2009185821A (ja) 2009-08-20
US20090199564A1 (en) 2009-08-13

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