DE602004004319D1 - Belüftungskanäle im Konfluenz-Blech einer Nachverbrennungskammer - Google Patents

Belüftungskanäle im Konfluenz-Blech einer Nachverbrennungskammer

Info

Publication number
DE602004004319D1
DE602004004319D1 DE602004004319T DE602004004319T DE602004004319D1 DE 602004004319 D1 DE602004004319 D1 DE 602004004319D1 DE 602004004319 T DE602004004319 T DE 602004004319T DE 602004004319 T DE602004004319 T DE 602004004319T DE 602004004319 D1 DE602004004319 D1 DE 602004004319D1
Authority
DE
Germany
Prior art keywords
post
combustion chamber
confluence plate
aeration channels
aeration
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
DE602004004319T
Other languages
English (en)
Other versions
DE602004004319T2 (de
Inventor
Thierry Cortes
Alain Page
Sebastien Baboeuf
Jacques Roche
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
Publication of DE602004004319D1 publication Critical patent/DE602004004319D1/de
Application granted granted Critical
Publication of DE602004004319T2 publication Critical patent/DE602004004319T2/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/38—Introducing air inside the jet
    • F02K1/386—Introducing air inside the jet mixing devices in the jet pipe, e.g. for mixing primary and secondary flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

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)
  • Spray-Type Burners (AREA)
  • Jet Pumps And Other Pumps (AREA)
DE602004004319T 2003-06-25 2004-06-22 Belüftungskanäle im Konfluenz-Blech einer Nachverbrennungskammer Active DE602004004319T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0307657A FR2856744B1 (fr) 2003-06-25 2003-06-25 Canaux de ventilation sur tole de confluence d'une chambre de post-combustion
FR0307657 2003-06-25

Publications (2)

Publication Number Publication Date
DE602004004319D1 true DE602004004319D1 (de) 2007-03-08
DE602004004319T2 DE602004004319T2 (de) 2007-08-30

Family

ID=33396844

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602004004319T Active DE602004004319T2 (de) 2003-06-25 2004-06-22 Belüftungskanäle im Konfluenz-Blech einer Nachverbrennungskammer

Country Status (9)

Country Link
US (1) US6976361B1 (de)
EP (1) EP1491752B1 (de)
JP (1) JP4150360B2 (de)
CA (1) CA2470268A1 (de)
DE (1) DE602004004319T2 (de)
ES (1) ES2280914T3 (de)
FR (1) FR2856744B1 (de)
RU (1) RU2347930C2 (de)
UA (1) UA84262C2 (de)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2899280B1 (fr) * 2006-03-30 2012-08-31 Snecma Dispositif de montage d'une paroi de separation de flux dans une chambre de post-combustion d'un turboreacteur
FR2902150B1 (fr) * 2006-06-09 2011-10-14 Snecma Dispositif injecteur de carburant, systeme de post-combustion et turboreacteur a double flux
US8726670B2 (en) * 2010-06-24 2014-05-20 General Electric Company Ejector purge of cavity adjacent exhaust flowpath
JP6229590B2 (ja) * 2014-04-30 2017-11-15 株式会社Ihi アフタバーナ及び航空機エンジン
CN105465831A (zh) * 2016-01-12 2016-04-06 西北工业大学 带有双火焰筒及稳焰器的燃气轮机燃烧室
CN114738795B (zh) * 2022-04-14 2023-06-09 西北工业大学 具有混气功能的支板稳定器和一体化加力燃烧室
CN115200042B (zh) * 2022-07-21 2023-08-22 中国航发沈阳发动机研究所 一种采用气冷串列和分流支板整流的加力燃烧室

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1923150A1 (de) * 1968-05-08 1970-01-15 Man Turbo Gmbh Zweistromturbinenstrahltriebwerk
FR1588974A (de) * 1968-10-02 1970-03-16
US5483793A (en) * 1970-09-02 1996-01-16 General Electric Company Infrared radiation suppression device
US3747345A (en) * 1972-07-24 1973-07-24 United Aircraft Corp Shortened afterburner construction for turbine engine
US3826088A (en) * 1973-02-01 1974-07-30 Gen Electric Gas turbine engine augmenter cooling liner stabilizers and supports
US5694767A (en) * 1981-11-02 1997-12-09 General Electric Company Variable slot bypass injector system
FR2696502B1 (fr) * 1992-10-07 1994-11-04 Snecma Dispositif de post-combustion pour turbo réacteur double flux.
US4958489A (en) * 1985-03-04 1990-09-25 General Electric Company Means for controlling augmentor liner coolant flow pressure in a mixed flow, variable cycle gas turbine engine
FR2626044A1 (fr) * 1988-01-14 1989-07-21 Snecma Melangeur de flux a section variable avec stabilisateur de rechauffe integre pour turboreacteur double flux

Also Published As

Publication number Publication date
US20050274114A1 (en) 2005-12-15
FR2856744A1 (fr) 2004-12-31
JP4150360B2 (ja) 2008-09-17
DE602004004319T2 (de) 2007-08-30
EP1491752A1 (de) 2004-12-29
US6976361B1 (en) 2005-12-20
FR2856744B1 (fr) 2007-05-25
UA84262C2 (ru) 2008-10-10
JP2005016521A (ja) 2005-01-20
EP1491752B1 (de) 2007-01-17
ES2280914T3 (es) 2007-09-16
RU2347930C2 (ru) 2009-02-27
CA2470268A1 (fr) 2004-12-25
RU2004119361A (ru) 2005-12-10

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition