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FR2825783B1 - Accrochage de chambre de combustion cmc de turbomachine par pattes brasees - Google Patents

Accrochage de chambre de combustion cmc de turbomachine par pattes brasees

Info

Publication number
FR2825783B1
FR2825783B1 FR0107363A FR0107363A FR2825783B1 FR 2825783 B1 FR2825783 B1 FR 2825783B1 FR 0107363 A FR0107363 A FR 0107363A FR 0107363 A FR0107363 A FR 0107363A FR 2825783 B1 FR2825783 B1 FR 2825783B1
Authority
FR
France
Prior art keywords
turbomachine
brazed
hanging
legs
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.)
Expired - Fee Related
Application number
FR0107363A
Other languages
English (en)
Other versions
FR2825783A1 (fr
Inventor
Gwenaelle Calvez
Didier Hernandez
Alexandre Forestier
Eric Conete
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 Moteurs SA
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 Moteurs SA filed Critical SNECMA Moteurs SA
Priority to FR0107363A priority Critical patent/FR2825783B1/fr
Priority to JP2002161064A priority patent/JP3907529B2/ja
Priority to EP02291363A priority patent/EP1265034B1/fr
Priority to DE60229465T priority patent/DE60229465D1/de
Priority to US10/162,385 priority patent/US6708495B2/en
Publication of FR2825783A1 publication Critical patent/FR2825783A1/fr
Application granted granted Critical
Publication of FR2825783B1 publication Critical patent/FR2825783B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F23R3/60—Support structures; Attaching or mounting means
    • 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
    • F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2230/00—Manufacture
    • F05B2230/60—Assembly methods
    • F05B2230/604—Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins
    • F05B2230/606—Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins using maintaining alignment while permitting differential dilatation

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR0107363A 2001-06-06 2001-06-06 Accrochage de chambre de combustion cmc de turbomachine par pattes brasees Expired - Fee Related FR2825783B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR0107363A FR2825783B1 (fr) 2001-06-06 2001-06-06 Accrochage de chambre de combustion cmc de turbomachine par pattes brasees
JP2002161064A JP3907529B2 (ja) 2001-06-06 2002-06-03 ろう付けされたタブを用いたターボマシンにおけるｃｍｃ燃焼室の取り付け
EP02291363A EP1265034B1 (fr) 2001-06-06 2002-06-04 Accrochage de chambre de combustion CMC de turbomachine par pattes brasées
DE60229465T DE60229465D1 (de) 2001-06-06 2002-06-04 Befestigung einer Turbinenbrennkammer aus keramischem Matrix-Verbundswerkstoff mit gelöteten Befestigungsfüssen
US10/162,385 US6708495B2 (en) 2001-06-06 2002-06-05 Fastening a CMC combustion chamber in a turbomachine using brazed tabs

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0107363A FR2825783B1 (fr) 2001-06-06 2001-06-06 Accrochage de chambre de combustion cmc de turbomachine par pattes brasees

Publications (2)

Publication Number Publication Date
FR2825783A1 FR2825783A1 (fr) 2002-12-13
FR2825783B1 true FR2825783B1 (fr) 2003-11-07

Family

ID=8863987

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0107363A Expired - Fee Related FR2825783B1 (fr) 2001-06-06 2001-06-06 Accrochage de chambre de combustion cmc de turbomachine par pattes brasees

Country Status (5)

Country Link
US (1) US6708495B2 (fr)
EP (1) EP1265034B1 (fr)
JP (1) JP3907529B2 (fr)
DE (1) DE60229465D1 (fr)
FR (1) FR2825783B1 (fr)

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FR2929689B1 (fr) * 2008-04-03 2013-04-12 Snecma Propulsion Solide Chambre de combustion de turbine a gaz a parois interne et externe sectorisees
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Also Published As

Publication number Publication date
US6708495B2 (en) 2004-03-23
DE60229465D1 (de) 2008-12-04
EP1265034A1 (fr) 2002-12-11
FR2825783A1 (fr) 2002-12-13
US20020184892A1 (en) 2002-12-12
EP1265034B1 (fr) 2008-10-22
JP2003014234A (ja) 2003-01-15
JP3907529B2 (ja) 2007-04-18

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Effective date: 20110228