[go: up one dir, main page]

FR2917487B1 - Chambre de combustion de turbomachine a circulation helicoidale de l'air - Google Patents

Chambre de combustion de turbomachine a circulation helicoidale de l'air

Info

Publication number
FR2917487B1
FR2917487B1 FR0755761A FR0755761A FR2917487B1 FR 2917487 B1 FR2917487 B1 FR 2917487B1 FR 0755761 A FR0755761 A FR 0755761A FR 0755761 A FR0755761 A FR 0755761A FR 2917487 B1 FR2917487 B1 FR 2917487B1
Authority
FR
France
Prior art keywords
helicoidal
circulation
air
combustion chamber
turbomachine combustion
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
FR0755761A
Other languages
English (en)
Other versions
FR2917487A1 (fr
Inventor
Laurent Bernard Cameriano
Michel Pierre Cazalens
Sylvain Duval
Romain Nicolas Lunel
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
Priority to FR0755761A priority Critical patent/FR2917487B1/fr
Application filed by SNECMA SAS filed Critical SNECMA SAS
Priority to EP08158059.9A priority patent/EP2003399B1/fr
Priority to RU2008124152/06A priority patent/RU2478880C2/ru
Priority to IL192052A priority patent/IL192052A/en
Priority to CA2634615A priority patent/CA2634615C/fr
Priority to US12/137,863 priority patent/US7673456B2/en
Priority to JP2008153791A priority patent/JP5084626B2/ja
Priority to CN2008101252146A priority patent/CN101324344B/zh
Publication of FR2917487A1 publication Critical patent/FR2917487A1/fr
Application granted granted Critical
Publication of FR2917487B1 publication Critical patent/FR2917487B1/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
    • F23R3/42—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)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Supercharger (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Fuel-Injection Apparatus (AREA)
FR0755761A 2007-06-14 2007-06-14 Chambre de combustion de turbomachine a circulation helicoidale de l'air Expired - Fee Related FR2917487B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR0755761A FR2917487B1 (fr) 2007-06-14 2007-06-14 Chambre de combustion de turbomachine a circulation helicoidale de l'air
RU2008124152/06A RU2478880C2 (ru) 2007-06-14 2008-06-11 Камера сгорания газотурбинного двигателя со спиралеобразной циркуляцией воздуха
IL192052A IL192052A (en) 2007-06-14 2008-06-11 Combustion chamber with coil air flow for turbocharged devices
CA2634615A CA2634615C (fr) 2007-06-14 2008-06-11 Chambre de combustion de turbomachine a circulation helicoidale de l'air
EP08158059.9A EP2003399B1 (fr) 2007-06-14 2008-06-11 Chambre de combustion de turbomachine à circulation hélicoïdale de l'air
US12/137,863 US7673456B2 (en) 2007-06-14 2008-06-12 Turbomachine combustion chamber with helical air flow
JP2008153791A JP5084626B2 (ja) 2007-06-14 2008-06-12 螺旋空気流を用いるターボ機械燃焼チャンバ
CN2008101252146A CN101324344B (zh) 2007-06-14 2008-06-16 一种采用螺线气流的涡轮机燃烧室

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0755761A FR2917487B1 (fr) 2007-06-14 2007-06-14 Chambre de combustion de turbomachine a circulation helicoidale de l'air

Publications (2)

Publication Number Publication Date
FR2917487A1 FR2917487A1 (fr) 2008-12-19
FR2917487B1 true FR2917487B1 (fr) 2009-10-02

Family

ID=39004879

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0755761A Expired - Fee Related FR2917487B1 (fr) 2007-06-14 2007-06-14 Chambre de combustion de turbomachine a circulation helicoidale de l'air

Country Status (8)

Country Link
US (1) US7673456B2 (fr)
EP (1) EP2003399B1 (fr)
JP (1) JP5084626B2 (fr)
CN (1) CN101324344B (fr)
CA (1) CA2634615C (fr)
FR (1) FR2917487B1 (fr)
IL (1) IL192052A (fr)
RU (1) RU2478880C2 (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103930723A (zh) * 2011-08-22 2014-07-16 马吉德·托甘 在燃气涡轮机上使用的、具有预混合的燃料和空气的切向环形燃烧器
CN103470376A (zh) * 2013-09-23 2013-12-25 蔡肃民 红外线发生器
RU182644U1 (ru) * 2018-03-28 2018-08-24 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" Кольцевая камера сгорания малоразмерного газотурбинного двигателя
US11378277B2 (en) 2018-04-06 2022-07-05 General Electric Company Gas turbine engine and combustor having air inlets and pilot burner
FR3081494B1 (fr) 2018-05-28 2020-12-25 Safran Aircraft Engines Module de combustion de turbomachine a gaz avec butee de fond de chambre
US11181269B2 (en) * 2018-11-15 2021-11-23 General Electric Company Involute trapped vortex combustor assembly
CN112577069B (zh) * 2020-12-17 2022-03-29 中国科学院工程热物理研究所 一种适用于小头部倾斜角下的斜流燃烧室侧壁面结构
CN113154456B (zh) * 2021-04-15 2022-06-21 中国航发湖南动力机械研究所 回流燃烧室机匣头部结构及其制造方法和发动机燃烧室
CN113739207B (zh) * 2021-09-22 2022-04-29 西北工业大学 一种采用气动内柱的旋转爆震燃烧室
CN113803744B (zh) * 2021-09-27 2023-03-10 中国联合重型燃气轮机技术有限公司 燃烧室入料装置及入料系统

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5025622A (en) * 1988-08-26 1991-06-25 Sol-3- Resources, Inc. Annular vortex combustor
CA2076102C (fr) * 1991-09-23 2001-12-18 Stephen John Howell Chambre de combustion a bague de projection
FR2695460B1 (fr) * 1992-09-09 1994-10-21 Snecma Chambre de combustion de turbomachine à plusieurs injecteurs.
US5791148A (en) * 1995-06-07 1998-08-11 General Electric Company Liner of a gas turbine engine combustor having trapped vortex cavity
DE19549143A1 (de) * 1995-12-29 1997-07-03 Abb Research Ltd Gasturbinenringbrennkammer
JPH09222228A (ja) * 1996-02-16 1997-08-26 Toshiba Corp ガスタービン燃焼器
JP3673009B2 (ja) * 1996-03-28 2005-07-20 株式会社東芝 ガスタービン燃焼器
US6530223B1 (en) * 1998-10-09 2003-03-11 General Electric Company Multi-stage radial axial gas turbine engine combustor
US6350223B1 (en) * 2000-01-11 2002-02-26 William P. Niedermeyer Rolls to fold, cut, or advance segments in folding apparatus
US6298667B1 (en) * 2000-06-22 2001-10-09 General Electric Company Modular combustor dome
US6481209B1 (en) * 2000-06-28 2002-11-19 General Electric Company Methods and apparatus for decreasing combustor emissions with swirl stabilized mixer
RU2215241C2 (ru) * 2002-01-23 2003-10-27 Открытое акционерное общество "Авиадвигатель" Камера сгорания газотурбинного двигателя
RU2219439C1 (ru) * 2002-09-03 2003-12-20 Андреев Анатолий Васильевич Камера сгорания
US7506511B2 (en) * 2003-12-23 2009-03-24 Honeywell International Inc. Reduced exhaust emissions gas turbine engine combustor
JP4670035B2 (ja) * 2004-06-25 2011-04-13 独立行政法人 宇宙航空研究開発機構 ガスタービン燃焼器
FR2920523B1 (fr) * 2007-09-05 2009-12-18 Snecma Chambre de combustion de turbomachine a circulation helicoidale de l'air.

Also Published As

Publication number Publication date
JP2008309466A (ja) 2008-12-25
EP2003399A3 (fr) 2013-07-31
IL192052A (en) 2011-07-31
JP5084626B2 (ja) 2012-11-28
CN101324344B (zh) 2011-08-17
US20080307792A1 (en) 2008-12-18
FR2917487A1 (fr) 2008-12-19
US7673456B2 (en) 2010-03-09
EP2003399B1 (fr) 2014-04-30
RU2478880C2 (ru) 2013-04-10
IL192052A0 (en) 2009-02-11
RU2008124152A (ru) 2009-12-20
CN101324344A (zh) 2008-12-17
CA2634615A1 (fr) 2008-12-14
CA2634615C (fr) 2014-08-05
EP2003399A2 (fr) 2008-12-17

Similar Documents

Publication Publication Date Title
FR2920523B1 (fr) Chambre de combustion de turbomachine a circulation helicoidale de l'air.
FR2917487B1 (fr) Chambre de combustion de turbomachine a circulation helicoidale de l'air
FR2897143B1 (fr) Chambre de combustion d'une turbomachine
FR2901349B1 (fr) Chambre de combustion d'une turbomachine
FR2953909B1 (fr) Guidage d'une bougie dans une chambre de combustion de turbomachine
FR2928994B1 (fr) Chambre de combustion de turbomachine.
FR2897144B1 (fr) Chambre de combustion de turbomachine a fentes tangentielles
FR2897418B1 (fr) Chambre de combustion annulaire d'une turbomachine
FR2897145B1 (fr) Chambre de combustion annulaire de turbomachine a fixations alternees.
GB2444736B (en) Combustion Chamber Air Inlet
EP2211433A4 (fr) Bougie d'allumage
FR2935777B1 (fr) Chambre de combustion de turbomachine
EP2187128A4 (fr) Chambre de combustion
FR2952698B1 (fr) Chambre de combustion avec bougie d'allumage ventilee
EP2221931A4 (fr) Bougie d'allumage
DE602006021127D1 (de) Turbinentriebwerk mit verbesserter Kühlung
FR2905166B1 (fr) Chambre de combustion annulaire d'une turbomachine.
FR2952701B1 (fr) Guidage d'une bougie d'allumage dans une chambre de combustion d'une turbomachine
FR2922629B1 (fr) Chambre de combustion a dilution optimisee et turbomachine en etant munie
FR2930591B1 (fr) Optimisation du positionnement angulaire d'un distributeur de turbine en sortie d'une chambre de combustion de turbomachine
BRPI0919986A2 (pt) ''queimador de combustivel compreendendo uma câmara de combustão''
FR2881813B1 (fr) Carenage de chambre de combustion de turbomachine
FR2943403B1 (fr) Chambre de combustion de turbomachine comprenant des moyens ameliores d'alimentation en air
FR2922630B1 (fr) Paroi de chambre de combustion a dilution et refroidissement optimises,chambre de combustion et turbomachine en etant munies
FR2948988B1 (fr) Chambre de combustion de turbomachine comprenant des orifices d'entree d'air ameliores

Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20160229