FR2921462B1 - Chambre de combustion annulaire de moteur a turbine a gaz - Google Patents

Chambre de combustion annulaire de moteur a turbine a gaz

Info

Publication number
FR2921462B1
FR2921462B1 FR0706644A FR0706644A FR2921462B1 FR 2921462 B1 FR2921462 B1 FR 2921462B1 FR 0706644 A FR0706644 A FR 0706644A FR 0706644 A FR0706644 A FR 0706644A FR 2921462 B1 FR2921462 B1 FR 2921462B1
Authority
FR
France
Prior art keywords
combustion chamber
gas turbine
turbine engine
annular combustion
annular
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
FR0706644A
Other languages
English (en)
Other versions
FR2921462A1 (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 FR0706644A priority Critical patent/FR2921462B1/fr
Priority to CA2639588A priority patent/CA2639588C/fr
Priority to RU2008137660/06A priority patent/RU2485405C2/ru
Priority to US12/233,943 priority patent/US8156744B2/en
Priority to EP08164751.3A priority patent/EP2040001B1/fr
Publication of FR2921462A1 publication Critical patent/FR2921462A1/fr
Application granted granted Critical
Publication of FR2921462B1 publication Critical patent/FR2921462B1/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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
    • 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
    • F23R3/002—Wall structures
    • 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)
FR0706644A 2007-09-21 2007-09-21 Chambre de combustion annulaire de moteur a turbine a gaz Active FR2921462B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR0706644A FR2921462B1 (fr) 2007-09-21 2007-09-21 Chambre de combustion annulaire de moteur a turbine a gaz
CA2639588A CA2639588C (fr) 2007-09-21 2008-09-18 Chambre de combustion annulaire de moteur a turbine a gaz
RU2008137660/06A RU2485405C2 (ru) 2007-09-21 2008-09-19 Кольцевая камера сгорания газотурбинного двигателя
US12/233,943 US8156744B2 (en) 2007-09-21 2008-09-19 Annular combustion chamber for a gas turbine engine
EP08164751.3A EP2040001B1 (fr) 2007-09-21 2008-09-19 Chambre de combustion annulaire de moteur à turbine à gaz

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0706644A FR2921462B1 (fr) 2007-09-21 2007-09-21 Chambre de combustion annulaire de moteur a turbine a gaz

Publications (2)

Publication Number Publication Date
FR2921462A1 FR2921462A1 (fr) 2009-03-27
FR2921462B1 true FR2921462B1 (fr) 2012-08-24

Family

ID=39327017

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0706644A Active FR2921462B1 (fr) 2007-09-21 2007-09-21 Chambre de combustion annulaire de moteur a turbine a gaz

Country Status (5)

Country Link
US (1) US8156744B2 (fr)
EP (1) EP2040001B1 (fr)
CA (1) CA2639588C (fr)
FR (1) FR2921462B1 (fr)
RU (1) RU2485405C2 (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH704185A1 (de) * 2010-12-06 2012-06-15 Alstom Technology Ltd Gasturbine sowie verfahren zum rekonditionieren einer solchen gasturbine.
FR2970666B1 (fr) * 2011-01-24 2013-01-18 Snecma Procede de perforation d'au moins une paroi d'une chambre de combustion
GB2491580A (en) * 2011-06-06 2012-12-12 Rolls Royce Plc A method of manufacturing a sheet metal annular combustion chamber
US10260748B2 (en) 2012-12-21 2019-04-16 United Technologies Corporation Gas turbine engine combustor with tailored temperature profile
US10816201B2 (en) 2013-09-13 2020-10-27 Raytheon Technologies Corporation Sealed combustor liner panel for a gas turbine engine
DE102015202570A1 (de) * 2015-02-12 2016-08-18 Rolls-Royce Deutschland Ltd & Co Kg Abdichtung eines Randspalts zwischen Effusionsschindeln einer Gasturbinenbrennkammer
US10816213B2 (en) 2018-03-01 2020-10-27 General Electric Company Combustor assembly with structural cowl and decoupled chamber

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4222230A (en) * 1978-08-14 1980-09-16 General Electric Company Combustor dome assembly
US4843825A (en) * 1988-05-16 1989-07-04 United Technologies Corporation Combustor dome heat shield
FR2673454B1 (fr) * 1991-02-28 1995-01-13 Snecma Chambre de combustion comportant une paroi de fond comprenant une pluralite de troncs de cones partiels.
US5463864A (en) * 1993-12-27 1995-11-07 United Technologies Corporation Fuel nozzle guide for a 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
US5974805A (en) * 1997-10-28 1999-11-02 Rolls-Royce Plc Heat shielding for a turbine combustor
US6164074A (en) * 1997-12-12 2000-12-26 United Technologies Corporation Combustor bulkhead with improved cooling and air recirculation zone
US6550251B1 (en) * 1997-12-18 2003-04-22 General Electric Company Venturiless swirl cup
US6212870B1 (en) * 1998-09-22 2001-04-10 General Electric Company Self fixturing combustor dome assembly
US6279323B1 (en) * 1999-11-01 2001-08-28 General Electric Company Low emissions combustor
RU2225575C2 (ru) * 2001-12-06 2004-03-10 Межрегиональная общественная организация "Поволжское отделение Российской инженерной академии" Устройство для подвода топлива в камеру сгорания
RU2223488C1 (ru) * 2002-10-25 2004-02-10 Красноярский государственный университет Индикаторный состав для определения меди (ii) в водных растворах
US7121095B2 (en) * 2003-08-11 2006-10-17 General Electric Company Combustor dome assembly of a gas turbine engine having improved deflector plates
US7673460B2 (en) 2005-06-07 2010-03-09 Snecma System of attaching an injection system to a turbojet combustion chamber base
US7415826B2 (en) * 2005-07-25 2008-08-26 General Electric Company Free floating mixer assembly for combustor of a gas turbine engine
FR2897417A1 (fr) 2006-02-10 2007-08-17 Snecma Sa Chambre de combustion annulaire d'une turbomachine
FR2897922B1 (fr) * 2006-02-27 2008-10-10 Snecma Sa Agencement pour une chambre de combustion de turboreacteur
FR2903171B1 (fr) * 2006-06-29 2008-10-17 Snecma Sa Agencement a liaison par crabot pour chambre de combustion de turbomachine
FR2909748B1 (fr) * 2006-12-07 2009-07-10 Snecma Sa Fond de chambre, procede de realisation de celui-ci, chambre de combustion le comportant et turboreacteur en etant equipe
FR2914399B1 (fr) * 2007-03-27 2009-10-02 Snecma Sa Carenage pour fond de chambre de combustion.

Also Published As

Publication number Publication date
US8156744B2 (en) 2012-04-17
CA2639588C (fr) 2016-03-29
CA2639588A1 (fr) 2009-03-21
EP2040001A3 (fr) 2010-02-17
EP2040001B1 (fr) 2018-04-18
EP2040001A2 (fr) 2009-03-25
RU2008137660A (ru) 2010-03-27
FR2921462A1 (fr) 2009-03-27
US20090077976A1 (en) 2009-03-26
RU2485405C2 (ru) 2013-06-20

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