DE602006001806D1 - Brennkammer einer Gasturbine - Google Patents

Brennkammer einer Gasturbine

Info

Publication number
DE602006001806D1
DE602006001806D1 DE602006001806T DE602006001806T DE602006001806D1 DE 602006001806 D1 DE602006001806 D1 DE 602006001806D1 DE 602006001806 T DE602006001806 T DE 602006001806T DE 602006001806 T DE602006001806 T DE 602006001806T DE 602006001806 D1 DE602006001806 D1 DE 602006001806D1
Authority
DE
Germany
Prior art keywords
combustion chamber
gas turbine
turbine
gas
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.)
Active
Application number
DE602006001806T
Other languages
English (en)
Inventor
Olivier Kreder
Delphine Parent
Guillaume Sevi
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 DE602006001806D1 publication Critical patent/DE602006001806D1/de
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
    • F23R3/60—Support structures; Attaching or mounting means
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DE602006001806T 2005-08-31 2006-08-22 Brennkammer einer Gasturbine Active DE602006001806D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0508891A FR2890156A1 (fr) 2005-08-31 2005-08-31 Chambre de combustion d'une turbomachine

Publications (1)

Publication Number Publication Date
DE602006001806D1 true DE602006001806D1 (de) 2008-08-28

Family

ID=36061594

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006001806T Active DE602006001806D1 (de) 2005-08-31 2006-08-22 Brennkammer einer Gasturbine

Country Status (6)

Country Link
US (1) US7568350B2 (de)
EP (1) EP1760404B1 (de)
CA (1) CA2557944C (de)
DE (1) DE602006001806D1 (de)
FR (1) FR2890156A1 (de)
RU (1) RU2382279C2 (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2892181B1 (fr) * 2005-10-18 2008-02-01 Snecma Sa Fixation d'une chambre de combustion a l'interieur de son carter
US7578134B2 (en) * 2006-01-11 2009-08-25 General Electric Company Methods and apparatus for assembling gas turbine engines
FR2906350B1 (fr) * 2006-09-22 2009-03-20 Snecma Sa Chambre de combustion annulaire d'une turbomachine
US9335049B2 (en) 2012-06-07 2016-05-10 United Technologies Corporation Combustor liner with reduced cooling dilution openings
GB2512642A (en) * 2013-04-05 2014-10-08 Rolls Royce Plc A combustion chamber
FR3047544B1 (fr) * 2016-02-10 2018-03-02 Safran Aircraft Engines Chambre de combustion de turbomachine
FR3085743B1 (fr) 2018-09-12 2021-06-25 Safran Aircraft Engines Chambre annulaire de combustion pour une turbomachine
US20210003284A1 (en) * 2019-07-03 2021-01-07 United Technologies Corporation Combustor mounting structures for gas turbine engines
CN115560356B (zh) * 2022-12-07 2023-05-05 成都中科翼能科技有限公司 一种燃气轮机扩压进气结构及分流环结构

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1578474A (en) * 1976-06-21 1980-11-05 Gen Electric Combustor mounting arrangement
GB2221979B (en) * 1988-08-17 1992-03-25 Rolls Royce Plc A combustion chamber for a gas turbine engine
DE19745683A1 (de) * 1997-10-16 1999-04-22 Bmw Rolls Royce Gmbh Aufhängung einer ringförmigen Gasturbinen-Brennkammer
FR2825784B1 (fr) * 2001-06-06 2003-08-29 Snecma Moteurs Accrochage de chambre de combustion cmc de turbomachine utilisant les trous de dilution
FR2869094B1 (fr) * 2004-04-15 2006-07-21 Snecma Moteurs Sa Chambre de combustion annulaire de turbomachine a bride interne de fixation amelioree
FR2871847B1 (fr) * 2004-06-17 2006-09-29 Snecma Moteurs Sa Montage d'un distributeur de turbine sur une chambre de combustion a parois en cmc dans une turbine a gaz

Also Published As

Publication number Publication date
FR2890156A1 (fr) 2007-03-02
EP1760404A1 (de) 2007-03-07
EP1760404B1 (de) 2008-07-16
RU2006131300A (ru) 2008-03-10
CA2557944C (fr) 2015-02-10
US20070044474A1 (en) 2007-03-01
US7568350B2 (en) 2009-08-04
RU2382279C2 (ru) 2010-02-20
CA2557944A1 (fr) 2007-02-28

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition