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FR2897107B1 - Paroi transversale de chambre de combustion munie de trous de multiperforation - Google Patents

Paroi transversale de chambre de combustion munie de trous de multiperforation

Info

Publication number
FR2897107B1
FR2897107B1 FR0650459A FR0650459A FR2897107B1 FR 2897107 B1 FR2897107 B1 FR 2897107B1 FR 0650459 A FR0650459 A FR 0650459A FR 0650459 A FR0650459 A FR 0650459A FR 2897107 B1 FR2897107 B1 FR 2897107B1
Authority
FR
France
Prior art keywords
cross
combustion chamber
chamber wall
sectional combustion
multiperforation
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
FR0650459A
Other languages
English (en)
Other versions
FR2897107A1 (fr
Inventor
Gerard Caboche
Claude Gautier
Denis 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
Priority to FR0650459A priority Critical patent/FR2897107B1/fr
Priority to US11/670,534 priority patent/US7992391B2/en
Priority to EP07101655A priority patent/EP1818617B1/fr
Priority to JP2007026385A priority patent/JP2007211774A/ja
Priority to CA2577595A priority patent/CA2577595C/fr
Priority to RU2007104918/06A priority patent/RU2426948C2/ru
Priority to CNA2007100050119A priority patent/CN101016999A/zh
Publication of FR2897107A1 publication Critical patent/FR2897107A1/fr
Application granted granted Critical
Publication of FR2897107B1 publication Critical patent/FR2897107B1/fr
Expired - Fee Related 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03044—Impingement cooled combustion chamber walls or subassemblies

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Fuel-Injection Apparatus (AREA)
FR0650459A 2006-02-09 2006-02-09 Paroi transversale de chambre de combustion munie de trous de multiperforation Expired - Fee Related FR2897107B1 (fr)

Priority Applications (7)

Application Number Priority Date Filing Date Title
FR0650459A FR2897107B1 (fr) 2006-02-09 2006-02-09 Paroi transversale de chambre de combustion munie de trous de multiperforation
US11/670,534 US7992391B2 (en) 2006-02-09 2007-02-02 Transverse wall of a combustion chamber provided with multi-perforation holes
EP07101655A EP1818617B1 (fr) 2006-02-09 2007-02-02 Paroi transversale de chambre de combustion munie de trous de multiperforations
JP2007026385A JP2007211774A (ja) 2006-02-09 2007-02-06 多穿孔の穴が設けられた燃焼チャンバの横断壁
CA2577595A CA2577595C (fr) 2006-02-09 2007-02-08 Paroi transversale de chambre de combustion munie de trous de multiperforation
RU2007104918/06A RU2426948C2 (ru) 2006-02-09 2007-02-08 Поперечная стенка камеры сгорания, содержащая множество перфорационных отверстий, камера сгорания газотурбинного двигателя и газотурбинный двигатель
CNA2007100050119A CN101016999A (zh) 2006-02-09 2007-02-09 具有多孔洞的燃烧室横向壁

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0650459A FR2897107B1 (fr) 2006-02-09 2006-02-09 Paroi transversale de chambre de combustion munie de trous de multiperforation

Publications (2)

Publication Number Publication Date
FR2897107A1 FR2897107A1 (fr) 2007-08-10
FR2897107B1 true FR2897107B1 (fr) 2013-01-18

Family

ID=37101624

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0650459A Expired - Fee Related FR2897107B1 (fr) 2006-02-09 2006-02-09 Paroi transversale de chambre de combustion munie de trous de multiperforation

Country Status (7)

Country Link
US (1) US7992391B2 (fr)
EP (1) EP1818617B1 (fr)
JP (1) JP2007211774A (fr)
CN (1) CN101016999A (fr)
CA (1) CA2577595C (fr)
FR (1) FR2897107B1 (fr)
RU (1) RU2426948C2 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
FR2920525B1 (fr) * 2007-08-31 2014-06-13 Snecma Separateur pour alimentation de l'air de refroidissement d'une turbine
FR2932251B1 (fr) * 2008-06-10 2011-09-16 Snecma Chambre de combustion de moteur a turbine a gaz comportant des deflecteurs en cmc
US7712314B1 (en) 2009-01-21 2010-05-11 Gas Turbine Efficiency Sweden Ab Venturi cooling system
FR2958013B1 (fr) * 2010-03-26 2014-06-20 Snecma Chambre de combustion de turbomachine a compresseur centrifuge sans deflecteur
US9377198B2 (en) 2012-01-31 2016-06-28 United Technologies Corporation Heat shield for a combustor
GB2543803B (en) * 2015-10-29 2019-10-30 Rolls Royce Plc A combustion chamber assembly
US11313560B2 (en) 2018-07-18 2022-04-26 General Electric Company Combustor assembly for a heat engine
US11391461B2 (en) * 2020-01-07 2022-07-19 Raytheon Technologies Corporation Combustor bulkhead with circular impingement hole pattern

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2410138A2 (fr) * 1977-11-29 1979-06-22 Snecma Perfectionnements aux chambres de combustion pour moteur a turbine a gaz
US4934145A (en) * 1988-10-12 1990-06-19 United Technologies Corporation Combustor bulkhead heat shield assembly
GB9018014D0 (en) * 1990-08-16 1990-10-03 Rolls Royce Plc Gas turbine engine combustor
GB2247522B (en) * 1990-09-01 1993-11-10 Rolls Royce Plc Gas turbine engine combustor
US5419115A (en) * 1994-04-29 1995-05-30 United Technologies Corporation Bulkhead and fuel nozzle guide assembly for an annular combustion chamber
DE4427222A1 (de) * 1994-08-01 1996-02-08 Bmw Rolls Royce Gmbh Hitzeschild für eine Gasturbinen-Brennkammer
US5581999A (en) * 1994-12-15 1996-12-10 United Technologies Corporation Bulkhead liner with raised lip
US6164074A (en) * 1997-12-12 2000-12-26 United Technologies Corporation Combustor bulkhead with improved cooling and air recirculation zone
US6155056A (en) * 1998-06-04 2000-12-05 Pratt & Whitney Canada Corp. Cooling louver for annular gas turbine engine combustion chamber
US6557349B1 (en) * 2000-04-17 2003-05-06 General Electric Company Method and apparatus for increasing heat transfer from combustors
US6530227B1 (en) * 2001-04-27 2003-03-11 General Electric Co. Methods and apparatus for cooling gas turbine engine combustors
US6497105B1 (en) * 2001-06-04 2002-12-24 Pratt & Whitney Canada Corp. Low cost combustor burner collar
US6546733B2 (en) * 2001-06-28 2003-04-15 General Electric Company Methods and systems for cooling gas turbine engine combustors
FR2836986B1 (fr) * 2002-03-07 2004-11-19 Snecma Moteurs Systeme d'injection multi-modes d'un melange air/carburant dans une chambre de combustion
US6792757B2 (en) * 2002-11-05 2004-09-21 Honeywell International Inc. Gas turbine combustor heat shield impingement cooling baffle
US8596071B2 (en) * 2006-05-05 2013-12-03 General Electric Company Method and apparatus for assembling a gas turbine engine

Also Published As

Publication number Publication date
RU2007104918A (ru) 2008-08-20
EP1818617B1 (fr) 2012-08-29
CN101016999A (zh) 2007-08-15
US7992391B2 (en) 2011-08-09
EP1818617A1 (fr) 2007-08-15
CA2577595C (fr) 2014-12-23
RU2426948C2 (ru) 2011-08-20
JP2007211774A (ja) 2007-08-23
FR2897107A1 (fr) 2007-08-10
US20070180834A1 (en) 2007-08-09
CA2577595A1 (fr) 2007-08-09

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20141031