DE69918352D1 - Gasabscheider für eine Brennkammer mit zwei Brennerköpfen - Google Patents

Gasabscheider für eine Brennkammer mit zwei Brennerköpfen

Info

Publication number
DE69918352D1
DE69918352D1 DE69918352T DE69918352T DE69918352D1 DE 69918352 D1 DE69918352 D1 DE 69918352D1 DE 69918352 T DE69918352 T DE 69918352T DE 69918352 T DE69918352 T DE 69918352T DE 69918352 D1 DE69918352 D1 DE 69918352D1
Authority
DE
Germany
Prior art keywords
combustion chamber
gas separator
burner heads
burner
heads
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
DE69918352T
Other languages
English (en)
Other versions
DE69918352T2 (de
Inventor
Alexandre Forestier
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
Application filed by SNECMA Moteurs SA filed Critical SNECMA Moteurs SA
Application granted granted Critical
Publication of DE69918352D1 publication Critical patent/DE69918352D1/de
Publication of DE69918352T2 publication Critical patent/DE69918352T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34Feeding into different combustion zones

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE69918352T 1998-04-16 1999-04-15 Gasabscheider für eine Brennkammer mit zwei Brennerköpfen Expired - Fee Related DE69918352T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9804704A FR2777634B1 (fr) 1998-04-16 1998-04-16 Separateur pour chambre de combustion a deux tetes
FR9804704 1998-04-16

Publications (2)

Publication Number Publication Date
DE69918352D1 true DE69918352D1 (de) 2004-08-05
DE69918352T2 DE69918352T2 (de) 2005-08-25

Family

ID=9525276

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69918352T Expired - Fee Related DE69918352T2 (de) 1998-04-16 1999-04-15 Gasabscheider für eine Brennkammer mit zwei Brennerköpfen

Country Status (5)

Country Link
US (1) US6155055A (de)
EP (1) EP0950859B1 (de)
JP (1) JPH11324712A (de)
DE (1) DE69918352T2 (de)
FR (1) FR2777634B1 (de)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2856468B1 (fr) * 2003-06-17 2007-11-23 Snecma Moteurs Chambre de combustion annulaire de turbomachine
GB2420614B (en) * 2004-11-30 2009-06-03 Alstom Technology Ltd Tile and exo-skeleton tile structure
DE102007062699A1 (de) * 2007-12-27 2009-07-02 Rolls-Royce Deutschland Ltd & Co Kg Brennkammerauskleidung
US8015817B2 (en) * 2009-06-10 2011-09-13 Siemens Energy, Inc. Cooling structure for gas turbine transition duct
US10101029B2 (en) * 2015-03-30 2018-10-16 United Technologies Corporation Combustor panels and configurations for a gas turbine engine

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5220795A (en) * 1991-04-16 1993-06-22 General Electric Company Method and apparatus for injecting dilution air
CA2089285C (en) * 1992-03-30 2002-06-25 Stephen Winthrop Falls Segmented centerbody for a double annular combustor
US5285632A (en) * 1993-02-08 1994-02-15 General Electric Company Low NOx combustor
FR2706021B1 (fr) * 1993-06-03 1995-07-07 Snecma Chambre de combustion comprenant un ensemble séparateur de gaz.
US5421158A (en) * 1994-10-21 1995-06-06 General Electric Company Segmented centerbody for a double annular combustor
GB2297830B (en) * 1995-02-07 1998-04-29 Rolls Royce Radially staged annular combustor
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

Also Published As

Publication number Publication date
FR2777634B1 (fr) 2000-05-19
JPH11324712A (ja) 1999-11-26
US6155055A (en) 2000-12-05
EP0950859B1 (de) 2004-06-30
FR2777634A1 (fr) 1999-10-22
EP0950859A1 (de) 1999-10-20
DE69918352T2 (de) 2005-08-25

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee