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FR2686683B1 - Turbomachine a chambre de combustion demontable. - Google Patents

Turbomachine a chambre de combustion demontable.

Info

Publication number
FR2686683B1
FR2686683B1 FR9200853A FR9200853A FR2686683B1 FR 2686683 B1 FR2686683 B1 FR 2686683B1 FR 9200853 A FR9200853 A FR 9200853A FR 9200853 A FR9200853 A FR 9200853A FR 2686683 B1 FR2686683 B1 FR 2686683B1
Authority
FR
France
Prior art keywords
turbomachine
combustion chamber
removable combustion
removable
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
FR9200853A
Other languages
English (en)
Other versions
FR2686683A1 (fr
Inventor
Georges Mazeaud
Christophe Pieussergues
Jean Maurice Sandelis Denis
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
Priority to FR9200853A priority Critical patent/FR2686683B1/fr
Priority to US08/004,606 priority patent/US5524430A/en
Priority to GB9301292A priority patent/GB2263733B/en
Publication of FR2686683A1 publication Critical patent/FR2686683A1/fr
Application granted granted Critical
Publication of FR2686683B1 publication Critical patent/FR2686683B1/fr
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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
FR9200853A 1992-01-28 1992-01-28 Turbomachine a chambre de combustion demontable. Expired - Lifetime FR2686683B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR9200853A FR2686683B1 (fr) 1992-01-28 1992-01-28 Turbomachine a chambre de combustion demontable.
US08/004,606 US5524430A (en) 1992-01-28 1993-01-14 Gas-turbine engine with detachable combustion chamber
GB9301292A GB2263733B (en) 1992-01-28 1993-01-22 Turbomachine with removable combustion chamber

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9200853A FR2686683B1 (fr) 1992-01-28 1992-01-28 Turbomachine a chambre de combustion demontable.

Publications (2)

Publication Number Publication Date
FR2686683A1 FR2686683A1 (fr) 1993-07-30
FR2686683B1 true FR2686683B1 (fr) 1994-04-01

Family

ID=9426019

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9200853A Expired - Lifetime FR2686683B1 (fr) 1992-01-28 1992-01-28 Turbomachine a chambre de combustion demontable.

Country Status (3)

Country Link
US (1) US5524430A (fr)
FR (1) FR2686683B1 (fr)
GB (1) GB2263733B (fr)

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FR2758384B1 (fr) * 1997-01-16 1999-02-12 Snecma Controle des debits de refroidissement pour des chambres de combustion a haute temperature
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FR2770283B1 (fr) * 1997-10-29 1999-11-19 Snecma Chambre de combustion pour turbomachine
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US6334298B1 (en) * 2000-07-14 2002-01-01 General Electric Company Gas turbine combustor having dome-to-liner joint
DE10048864A1 (de) 2000-10-02 2002-04-11 Rolls Royce Deutschland Brennkammerkopf für eine Gasturbine
JP3600911B2 (ja) * 2001-01-25 2004-12-15 川崎重工業株式会社 環状燃焼器のライナ支持構造
US6449952B1 (en) * 2001-04-17 2002-09-17 General Electric Company Removable cowl for gas turbine combustor
FR2825785B1 (fr) * 2001-06-06 2004-08-27 Snecma Moteurs Liaison de chambre de combustion cmc de turbomachine en deux parties
FR2825787B1 (fr) * 2001-06-06 2004-08-27 Snecma Moteurs Montage de chambre de combustion cmc de turbomachine par viroles de liaison souples
FR2825784B1 (fr) * 2001-06-06 2003-08-29 Snecma Moteurs Accrochage de chambre de combustion cmc de turbomachine utilisant les trous de dilution
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US20070095071A1 (en) * 2003-09-29 2007-05-03 Kastrup David A Apparatus for assembling gas turbine engine combustors
FR2881813B1 (fr) * 2005-02-09 2011-04-08 Snecma Moteurs Carenage de chambre de combustion de turbomachine
FR2885201B1 (fr) * 2005-04-28 2010-09-17 Snecma Moteurs Chambre de combustion aisement demontable a performance aerodynamique amelioree
US8327538B2 (en) * 2005-10-17 2012-12-11 General Electric Company Methods to facilitate extending gas turbine engine useful life
US7637110B2 (en) * 2005-11-30 2009-12-29 General Electric Company Methods and apparatuses for assembling a gas turbine engine
US7523616B2 (en) 2005-11-30 2009-04-28 General Electric Company Methods and apparatuses for assembling a gas turbine engine
DE102006004785A1 (de) * 2006-02-02 2007-08-30 Alstom Technology Ltd. Strömungsmaschine
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.
US7765809B2 (en) * 2006-11-10 2010-08-03 General Electric Company Combustor dome and methods of assembling such
FR2911668B1 (fr) * 2007-01-18 2009-03-20 Snecma Sa Chambre de combustion d'une turbomachine
FR2914399B1 (fr) * 2007-03-27 2009-10-02 Snecma Sa Carenage pour fond de chambre de combustion.
FR2919380B1 (fr) 2007-07-26 2013-10-25 Snecma Chambre de combustion d'une turbomachine.
FR2920524B1 (fr) * 2007-08-30 2013-11-01 Snecma Turbomachine a chambre annulaire de combustion
JP5276345B2 (ja) * 2008-03-28 2013-08-28 三菱重工業株式会社 ガスタービン及びガスタービンの燃焼器挿入孔形成方法
FR2930628B1 (fr) * 2008-04-24 2010-04-30 Snecma Chambre annulaire de combustion pour turbomachine
US8590313B2 (en) * 2008-07-30 2013-11-26 Rolls-Royce Corporation Precision counter-swirl combustor
US8161752B2 (en) * 2008-11-20 2012-04-24 Honeywell International Inc. Combustors with inserts between dual wall liners
US9046272B2 (en) * 2008-12-31 2015-06-02 Rolls-Royce Corporation Combustion liner assembly having a mount stake coupled to an upstream support
GB0920371D0 (en) * 2009-11-23 2010-01-06 Rolls Royce Plc Combustor system
GB201009548D0 (en) * 2010-06-08 2010-07-21 Rolls Royce Plc A mounting assembly
US20120047909A1 (en) * 2010-08-24 2012-03-01 Nuovo Pignone S.P.A. Combustor liner concentric support and method
FR2964725B1 (fr) * 2010-09-14 2012-10-12 Snecma Carenage aerodynamique pour fond de chambre de combustion
US8899051B2 (en) 2010-12-30 2014-12-02 Rolls-Royce Corporation Gas turbine engine flange assembly including flow circuit
US8893382B2 (en) * 2011-09-30 2014-11-25 General Electric Company Combustion system and method of assembling the same
KR101614636B1 (ko) * 2011-11-16 2016-04-21 미츠비시 히타치 파워 시스템즈 가부시키가이샤 가스 터빈 연소기
US9435535B2 (en) * 2012-02-20 2016-09-06 General Electric Company Combustion liner guide stop and method for assembling a combustor
EP2735796B1 (fr) * 2012-11-23 2020-01-01 Ansaldo Energia IP UK Limited Paroi située sur la trajectoire des gaz chauds d'une turbine à gaz et procédé pour améliorer le comportement de fonctionnment d'une turbine à gaz
US10036317B2 (en) 2013-03-05 2018-07-31 Industrial Turbine Company (Uk) Limited Capacity control of turbine by the use of a reheat combustor in multi shaft engine
US9624829B2 (en) 2013-03-05 2017-04-18 Industrial Turbine Company (Uk) Limited Cogen heat load matching through reheat and capacity match
US9546789B2 (en) * 2013-03-15 2017-01-17 General Electric Company System having a multi-tube fuel nozzle
EP3052862A4 (fr) * 2013-10-04 2016-11-02 United Technologies Corp Panneau de chambre de combustion doté de plusieurs fixations
DE102014204466A1 (de) 2014-03-11 2015-10-01 Rolls-Royce Deutschland Ltd & Co Kg Brennkammer einer Gasturbine
FR3020865B1 (fr) 2014-05-12 2016-05-20 Snecma Chambre annulaire de combustion
GB201408690D0 (en) * 2014-05-16 2014-07-02 Rolls Royce Plc A combustion chamber arrangement
US10041679B2 (en) * 2015-06-24 2018-08-07 Delavan Inc Combustion systems
US10578021B2 (en) * 2015-06-26 2020-03-03 Delavan Inc Combustion systems
US10801729B2 (en) * 2015-07-06 2020-10-13 General Electric Company Thermally coupled CMC combustor liner
DE102015224990A1 (de) 2015-12-11 2017-06-14 Rolls-Royce Deutschland Ltd & Co Kg Verfahren zur Montage einer Brennkammer eines Gasturbinentriebwerks
GB201613110D0 (en) 2016-07-29 2016-09-14 Rolls Royce Plc A combustion chamber
US10859269B2 (en) * 2017-03-31 2020-12-08 Delavan Inc. Fuel injectors for multipoint arrays
US10816213B2 (en) 2018-03-01 2020-10-27 General Electric Company Combustor assembly with structural cowl and decoupled chamber
RU186956U1 (ru) * 2018-07-16 2019-02-11 Публичное Акционерное Общество "Одк-Сатурн" Жаровая труба камеры сгорания газотурбинного двигателя
FR3096115B1 (fr) * 2019-05-14 2022-12-09 Safran Aircraft Engines Fixation de chambre de combustion de turbomachine
CN113431703B (zh) * 2021-06-30 2022-07-12 中国航发动力股份有限公司 一种多层装配结构的复合装配方法
CN114165816B (zh) * 2022-02-09 2022-06-03 中国航发四川燃气涡轮研究院 一种发动机液压作动筒安装装置

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Also Published As

Publication number Publication date
US5524430A (en) 1996-06-11
GB9301292D0 (en) 1993-03-17
GB2263733A (en) 1993-08-04
GB2263733B (en) 1995-01-18
FR2686683A1 (fr) 1993-07-30

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TP Transmission of property
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