FR2897922B1 - Agencement pour une chambre de combustion de turboreacteur - Google Patents

Agencement pour une chambre de combustion de turboreacteur

Info

Publication number
FR2897922B1
FR2897922B1 FR0601695A FR0601695A FR2897922B1 FR 2897922 B1 FR2897922 B1 FR 2897922B1 FR 0601695 A FR0601695 A FR 0601695A FR 0601695 A FR0601695 A FR 0601695A FR 2897922 B1 FR2897922 B1 FR 2897922B1
Authority
FR
France
Prior art keywords
turboreactor
arrangement
combustion chamber
combustion
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.)
Active
Application number
FR0601695A
Other languages
English (en)
Other versions
FR2897922A1 (fr
Inventor
Didier Hippolyte Hernandez
Thomas Olivier Marie Noel
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 FR0601695A priority Critical patent/FR2897922B1/fr
Priority to EP07102863.3A priority patent/EP1826492B1/fr
Priority to JP2007043682A priority patent/JP2007232359A/ja
Priority to RU2007107030/06A priority patent/RU2007107030A/ru
Priority to CA2578711A priority patent/CA2578711C/fr
Priority to US11/678,896 priority patent/US7775051B2/en
Priority to CNA2007100799508A priority patent/CN101029743A/zh
Publication of FR2897922A1 publication Critical patent/FR2897922A1/fr
Application granted granted Critical
Publication of FR2897922B1 publication Critical patent/FR2897922B1/fr
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
    • F23R3/28—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
    • F23R3/42—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)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
FR0601695A 2006-02-27 2006-02-27 Agencement pour une chambre de combustion de turboreacteur Active FR2897922B1 (fr)

Priority Applications (7)

Application Number Priority Date Filing Date Title
FR0601695A FR2897922B1 (fr) 2006-02-27 2006-02-27 Agencement pour une chambre de combustion de turboreacteur
EP07102863.3A EP1826492B1 (fr) 2006-02-27 2007-02-22 Agencement pour une chambre de combustion de turboréacteur
JP2007043682A JP2007232359A (ja) 2006-02-27 2007-02-23 ジェットエンジンの燃焼チャンバの装置
CA2578711A CA2578711C (fr) 2006-02-27 2007-02-26 Agencement pour une chambre de combustion de turboreacteur
RU2007107030/06A RU2007107030A (ru) 2006-02-27 2007-02-26 Оборудование для камеры сгорания турбореактивного двигателя
US11/678,896 US7775051B2 (en) 2006-02-27 2007-02-26 Arrangement for a jet engine combustion chamber
CNA2007100799508A CN101029743A (zh) 2006-02-27 2007-02-27 一种喷气发动机燃烧室的装置

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0601695A FR2897922B1 (fr) 2006-02-27 2006-02-27 Agencement pour une chambre de combustion de turboreacteur

Publications (2)

Publication Number Publication Date
FR2897922A1 FR2897922A1 (fr) 2007-08-31
FR2897922B1 true FR2897922B1 (fr) 2008-10-10

Family

ID=37101916

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0601695A Active FR2897922B1 (fr) 2006-02-27 2006-02-27 Agencement pour une chambre de combustion de turboreacteur

Country Status (7)

Country Link
US (1) US7775051B2 (fr)
EP (1) EP1826492B1 (fr)
JP (1) JP2007232359A (fr)
CN (1) CN101029743A (fr)
CA (1) CA2578711C (fr)
FR (1) FR2897922B1 (fr)
RU (1) RU2007107030A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102057224B (zh) * 2008-06-10 2013-04-24 斯奈克玛 包括cmc偏转部的气体涡轮机燃烧室

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2906350B1 (fr) * 2006-09-22 2009-03-20 Snecma Sa Chambre de combustion annulaire d'une turbomachine
FR2910115B1 (fr) * 2006-12-19 2012-11-16 Snecma Deflecteur pour fond de chambre de combustion, chambre de combustion en etant equipee et turboreacteur les comportant
FR2918443B1 (fr) * 2007-07-04 2009-10-30 Snecma Sa Chambre de combustion comportant des deflecteurs de protection thermique de fond de chambre et moteur a turbine a gaz en etant equipe
FR2921462B1 (fr) * 2007-09-21 2012-08-24 Snecma Chambre de combustion annulaire de moteur a turbine a gaz
EP2039999A1 (fr) * 2007-09-24 2009-03-25 Siemens Aktiengesellschaft Chambre de combustion
FR2921464B1 (fr) * 2007-09-24 2014-03-28 Snecma Agencement de systemes d'injection dans un fond de chambre de combustion d'un moteur d'aeronef
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
FR2929689B1 (fr) * 2008-04-03 2013-04-12 Snecma Propulsion Solide Chambre de combustion de turbine a gaz a parois interne et externe sectorisees
FR2935465B1 (fr) * 2008-08-29 2013-09-20 Snecma Fixation d'un deflecteur en cmc sur un fond de chambre par pincage a l'aide d'un support metallique.
US8266912B2 (en) * 2008-09-16 2012-09-18 General Electric Company Reusable weld joint for syngas fuel nozzles
US8943835B2 (en) * 2010-05-10 2015-02-03 General Electric Company Gas turbine engine combustor with CMC heat shield and methods therefor
FR2976346B1 (fr) * 2011-06-08 2013-07-05 Turbomeca Chambre de combustion annulaire de turbomachine
DE102013007443A1 (de) * 2013-04-30 2014-10-30 Rolls-Royce Deutschland Ltd & Co Kg Brennerdichtung für Gasturbinen-Brennkammerkopf und Hitzeschild
US9829198B2 (en) 2013-08-12 2017-11-28 Pratt & Whitney Canada Corp. Combustor floating collar assembly
US9625152B2 (en) 2014-06-03 2017-04-18 Pratt & Whitney Canada Corp. Combustor heat shield for a gas turbine engine
EP3002518B1 (fr) 2014-09-30 2019-01-30 Ansaldo Energia Switzerland AG Panneau avant de chambre de combustion
FR3026827B1 (fr) * 2014-10-01 2019-06-07 Safran Aircraft Engines Chambre de combustion de turbomachine
US10041679B2 (en) * 2015-06-24 2018-08-07 Delavan Inc Combustion systems
GB2543803B (en) * 2015-10-29 2019-10-30 Rolls Royce Plc A combustion chamber assembly
US10317085B2 (en) * 2016-02-25 2019-06-11 General Electric Company Combustor assembly
GB2548585B (en) * 2016-03-22 2020-05-27 Rolls Royce Plc A combustion chamber assembly
US10215419B2 (en) 2016-07-08 2019-02-26 Pratt & Whitney Canada Corp. Particulate buildup prevention in ignitor and fuel nozzle bosses
FR3061761B1 (fr) * 2017-01-10 2021-01-01 Safran Aircraft Engines Chambre de combustion pour turbomachine
US10690347B2 (en) 2017-02-01 2020-06-23 General Electric Company CMC combustor deflector
FR3084731B1 (fr) * 2019-02-19 2020-07-03 Safran Aircraft Engines Chambre de combustion pour une turbomachine
CN109967871B (zh) * 2019-03-29 2020-09-18 北京航空航天大学 微型燃气轮机燃烧室的加工工装
US11428410B2 (en) 2019-10-08 2022-08-30 Rolls-Royce Corporation Combustor for a gas turbine engine with ceramic matrix composite heat shield and seal retainer
US11466858B2 (en) 2019-10-11 2022-10-11 Rolls-Royce Corporation Combustor for a gas turbine engine with ceramic matrix composite sealing element
US11486581B2 (en) * 2020-09-29 2022-11-01 Pratt & Whitney Canada Corp. Fuel nozzle and associated method of assembly
US20230112757A1 (en) * 2021-10-12 2023-04-13 General Electric Company Combustor swirler to dome attachment

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3742704A (en) * 1971-07-13 1973-07-03 Westinghouse Electric Corp Combustion chamber support structure
FR2639095B1 (fr) * 1988-11-17 1990-12-21 Snecma Chambre de combustion de turbomachine a bols de prevaporisation montes flottants
US5117624A (en) * 1990-09-17 1992-06-02 General Electric Company Fuel injector nozzle support
US6502400B1 (en) 2000-05-20 2003-01-07 General Electric Company Combustor dome assembly and method of assembling the same
FR2903171B1 (fr) * 2006-06-29 2008-10-17 Snecma Sa Agencement a liaison par crabot pour chambre de combustion de turbomachine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102057224B (zh) * 2008-06-10 2013-04-24 斯奈克玛 包括cmc偏转部的气体涡轮机燃烧室

Also Published As

Publication number Publication date
CA2578711C (fr) 2015-04-21
CN101029743A (zh) 2007-09-05
US7775051B2 (en) 2010-08-17
CA2578711A1 (fr) 2007-08-27
EP1826492B1 (fr) 2014-09-17
US20070199329A1 (en) 2007-08-30
JP2007232359A (ja) 2007-09-13
RU2007107030A (ru) 2008-09-10
EP1826492A1 (fr) 2007-08-29
FR2897922A1 (fr) 2007-08-31

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