FR2856468B1 - Chambre de combustion annulaire de turbomachine - Google Patents

Chambre de combustion annulaire de turbomachine

Info

Publication number
FR2856468B1
FR2856468B1 FR0350226A FR0350226A FR2856468B1 FR 2856468 B1 FR2856468 B1 FR 2856468B1 FR 0350226 A FR0350226 A FR 0350226A FR 0350226 A FR0350226 A FR 0350226A FR 2856468 B1 FR2856468 B1 FR 2856468B1
Authority
FR
France
Prior art keywords
combustion chamber
annular combustion
turbomachine annular
turbomachine
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
FR0350226A
Other languages
English (en)
Other versions
FR2856468A1 (fr
Inventor
Michel Andre Albert Desaulty
Bruno Beule
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
Priority to FR0350226A priority Critical patent/FR2856468B1/fr
Application filed by SNECMA Moteurs SA filed Critical SNECMA Moteurs SA
Priority to ES04102723T priority patent/ES2262094T3/es
Priority to DE602004000789T priority patent/DE602004000789T2/de
Priority to US10/866,695 priority patent/US7155913B2/en
Priority to CA2470928A priority patent/CA2470928C/fr
Priority to EP04102723A priority patent/EP1489359B1/fr
Priority to RU2004118309/06A priority patent/RU2342602C2/ru
Publication of FR2856468A1 publication Critical patent/FR2856468A1/fr
Application granted granted Critical
Publication of FR2856468B1 publication Critical patent/FR2856468B1/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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/06—Arrangement of apertures along the flame tube
    • 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

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)
  • Gas Burners (AREA)
  • Combustion Of Fluid Fuel (AREA)
FR0350226A 2003-06-17 2003-06-17 Chambre de combustion annulaire de turbomachine Expired - Fee Related FR2856468B1 (fr)

Priority Applications (7)

Application Number Priority Date Filing Date Title
FR0350226A FR2856468B1 (fr) 2003-06-17 2003-06-17 Chambre de combustion annulaire de turbomachine
DE602004000789T DE602004000789T2 (de) 2003-06-17 2004-06-15 Ringförmige Brennkammer für eine Turbomaschine
US10/866,695 US7155913B2 (en) 2003-06-17 2004-06-15 Turbomachine annular combustion chamber
CA2470928A CA2470928C (fr) 2003-06-17 2004-06-15 Chambre de combustion annulaire de turbomachine
ES04102723T ES2262094T3 (es) 2003-06-17 2004-06-15 Camara anular de combustion anular para turbomaquina.
EP04102723A EP1489359B1 (fr) 2003-06-17 2004-06-15 Chambre de combustion annulaire de turbomachine
RU2004118309/06A RU2342602C2 (ru) 2003-06-17 2004-06-16 Кольцевая камера сгорания газотурбинного двигателя

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0350226A FR2856468B1 (fr) 2003-06-17 2003-06-17 Chambre de combustion annulaire de turbomachine

Publications (2)

Publication Number Publication Date
FR2856468A1 FR2856468A1 (fr) 2004-12-24
FR2856468B1 true FR2856468B1 (fr) 2007-11-23

Family

ID=33396880

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0350226A Expired - Fee Related FR2856468B1 (fr) 2003-06-17 2003-06-17 Chambre de combustion annulaire de turbomachine

Country Status (7)

Country Link
US (1) US7155913B2 (fr)
EP (1) EP1489359B1 (fr)
CA (1) CA2470928C (fr)
DE (1) DE602004000789T2 (fr)
ES (1) ES2262094T3 (fr)
FR (1) FR2856468B1 (fr)
RU (1) RU2342602C2 (fr)

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US7506511B2 (en) * 2003-12-23 2009-03-24 Honeywell International Inc. Reduced exhaust emissions gas turbine engine combustor
US7954326B2 (en) * 2007-11-28 2011-06-07 Honeywell International Inc. Systems and methods for cooling gas turbine engine transition liners
GB2460403B (en) * 2008-05-28 2010-11-17 Rolls Royce Plc Combustor Wall with Improved Cooling
US7874157B2 (en) * 2008-06-05 2011-01-25 General Electric Company Coanda pilot nozzle for low emission combustors
US8220269B2 (en) * 2008-09-30 2012-07-17 Alstom Technology Ltd. Combustor for a gas turbine engine with effusion cooled baffle
FR2974162B1 (fr) * 2011-04-14 2018-04-13 Safran Aircraft Engines Virole de tube a flamme dans une chambre de combustion de turbomachine
FR2979416B1 (fr) * 2011-08-26 2013-09-20 Turbomeca Paroi de chambre de combustion
US10260748B2 (en) 2012-12-21 2019-04-16 United Technologies Corporation Gas turbine engine combustor with tailored temperature profile
EP2984317B1 (fr) * 2013-04-12 2019-03-13 United Technologies Corporation Refroidissement de jonction en t de panneau de chambre de combustion
EP3044444B1 (fr) 2013-09-13 2019-11-06 United Technologies Corporation Chambre de combustion pour une turbine à gaz avec un panneau de chemisage hermétiquement scellé
FR3011620B1 (fr) * 2013-10-04 2018-03-09 Snecma Chambre de combustion de turbomachine pourvue d'un passage d'entree d'air ameliore en aval d'un orifice de passage de bougie
EP3060852B1 (fr) 2013-10-24 2023-07-05 Raytheon Technologies Corporation Chambre de combustion pour moteur de turbine à gaz avec agencement de jet de trempe
RU2581267C2 (ru) * 2013-11-12 2016-04-20 Федеральное государственное бюджетное научное учреждение "Всероссийский научно-исследовательский институт электрификации сельского хозяйства" (ФГБНУ ВИЭСХ) Устройство камеры сгорания с регулируемым завихрителем для микро газотурбинного двигателя, где турбиной и компрессором является турбокомпрессор от двс
EP3077728B8 (fr) 2013-12-06 2021-03-31 Raytheon Technologies Corporation Chambre de combustion de moteur à turbine à gaz ayant des passages d'effusion avec orientation de co-tourbillonnement, et procédé
US10344979B2 (en) 2014-01-30 2019-07-09 United Technologies Corporation Cooling flow for leading panel in a gas turbine engine combustor
CN109578141B (zh) * 2019-01-23 2023-10-20 中国船舶重工集团公司第七0三研究所 一种可倒车燃气轮机动力涡轮的排气涡壳
CN115183273A (zh) * 2022-07-21 2022-10-14 中国航发沈阳发动机研究所 一种加力发动机燃烧室

Family Cites Families (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2974485A (en) * 1958-06-02 1961-03-14 Gen Electric Combustor for fluid fuels
DE2018641C2 (de) * 1970-04-18 1972-05-10 Motoren Turbinen Union Umkehrbrennkammer fuer gasturbinentriebwerke
GB1492049A (en) * 1974-12-07 1977-11-16 Rolls Royce Combustion equipment for gas turbine engines
FR2402068A1 (fr) * 1977-09-02 1979-03-30 Snecma Chambre de combustion anti-pollution
US4194358A (en) * 1977-12-15 1980-03-25 General Electric Company Double annular combustor configuration
US4244178A (en) * 1978-03-20 1981-01-13 General Motors Corporation Porous laminated combustor structure
GB2021204B (en) * 1978-05-20 1982-10-13 Rolls Royce Gas turbinr combustion chamber
GB2073396B (en) * 1980-03-29 1984-02-22 Rolls Royce Gas turbine combustion chambers
GB2099978A (en) * 1981-05-11 1982-12-15 Rolls Royce Gas turbine engine combustor
US4896510A (en) * 1987-02-06 1990-01-30 General Electric Company Combustor liner cooling arrangement
US5197289A (en) * 1990-11-26 1993-03-30 General Electric Company Double dome combustor
US5197278A (en) * 1990-12-17 1993-03-30 General Electric Company Double dome combustor and method of operation
US5142871A (en) * 1991-01-22 1992-09-01 General Electric Company Combustor dome plate support having uniform thickness arcuate apex with circumferentially spaced coolant apertures
US5220795A (en) * 1991-04-16 1993-06-22 General Electric Company Method and apparatus for injecting dilution air
CA2070518C (fr) * 1991-07-01 2001-10-02 Adrian Mark Ablett Ensemble dome pour chambre de combustion
US5154060A (en) * 1991-08-12 1992-10-13 General Electric Company Stiffened double dome combustor
US5289687A (en) * 1992-03-30 1994-03-01 General Electric Company One-piece cowl for a double annular combustor
CA2089285C (fr) * 1992-03-30 2002-06-25 Stephen Winthrop Falls Noyau central segmente pour chambre de combustion annulaire double
US5321951A (en) * 1992-03-30 1994-06-21 General Electric Company Integral combustor splash plate and sleeve
CA2089302C (fr) * 1992-03-30 2004-07-06 Joseph Frank Savelli Chambre de combustion annulaire double
JP2597800B2 (ja) * 1992-06-12 1997-04-09 ゼネラル・エレクトリック・カンパニイ ガスタービンエンジン用燃焼器
US5331805A (en) * 1993-04-22 1994-07-26 Alliedsignal Inc. Reduced diameter annular combustor
FR2706021B1 (fr) * 1993-06-03 1995-07-07 Snecma Chambre de combustion comprenant un ensemble séparateur de gaz.
FR2712379B1 (fr) * 1993-11-10 1995-12-29 Snecma Chambre de combustion pour turbomachine munie d'un séparateur des gaz.
US5421158A (en) * 1994-10-21 1995-06-06 General Electric Company Segmented centerbody for a double annular combustor
US5623827A (en) * 1995-01-26 1997-04-29 General Electric Company Regenerative cooled dome assembly for a gas turbine engine combustor
WO1996027766A1 (fr) * 1995-03-08 1996-09-12 Bmw Rolls-Royce Gmbh Chambre de combustion a anneau double et etagement axial pour une turbine a gaz
FR2733582B1 (fr) * 1995-04-26 1997-06-06 Snecma Chambre de combustion comportant une multiperforation d'inclinaison axiale et tangentielle variable
US5970716A (en) * 1997-10-02 1999-10-26 General Electric Company Apparatus for retaining centerbody between adjacent domes of multiple annular combustor employing interference and clamping fits
US5974805A (en) * 1997-10-28 1999-11-02 Rolls-Royce Plc Heat shielding for a turbine combustor
FR2777634B1 (fr) * 1998-04-16 2000-05-19 Snecma Separateur pour chambre de combustion a deux tetes
US6079199A (en) * 1998-06-03 2000-06-27 Pratt & Whitney Canada Inc. Double pass air impingement and air film cooling for gas turbine combustor walls
US6155056A (en) * 1998-06-04 2000-12-05 Pratt & Whitney Canada Corp. Cooling louver for annular gas turbine engine combustion chamber
US6474070B1 (en) * 1998-06-10 2002-11-05 General Electric Company Rich double dome combustor
US6145319A (en) * 1998-07-16 2000-11-14 General Electric Company Transitional multihole combustion liner
US6286317B1 (en) * 1998-12-18 2001-09-11 General Electric Company Cooling nugget for a liner of a gas turbine engine combustor having trapped vortex cavity
US6260359B1 (en) * 1999-11-01 2001-07-17 General Electric Company Offset dilution combustor liner
US6279323B1 (en) * 1999-11-01 2001-08-28 General Electric Company Low emissions combustor
US6655146B2 (en) * 2001-07-31 2003-12-02 General Electric Company Hybrid film cooled combustor liner
US6513331B1 (en) * 2001-08-21 2003-02-04 General Electric Company Preferential multihole combustor liner

Also Published As

Publication number Publication date
ES2262094T3 (es) 2006-11-16
DE602004000789D1 (de) 2006-06-08
US20050042076A1 (en) 2005-02-24
FR2856468A1 (fr) 2004-12-24
US7155913B2 (en) 2007-01-02
RU2342602C2 (ru) 2008-12-27
CA2470928A1 (fr) 2004-12-17
EP1489359A1 (fr) 2004-12-22
DE602004000789T2 (de) 2007-05-31
CA2470928C (fr) 2011-11-15
EP1489359B1 (fr) 2006-05-03
RU2004118309A (ru) 2006-01-10

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Legal Events

Date Code Title Description
CD Change of name or company name
ST Notification of lapse

Effective date: 20080229