SE9801818D0 - Combustion chamber arrangement - Google Patents

Combustion chamber arrangement

Info

Publication number
SE9801818D0
SE9801818D0 SE9801818A SE9801818A SE9801818D0 SE 9801818 D0 SE9801818 D0 SE 9801818D0 SE 9801818 A SE9801818 A SE 9801818A SE 9801818 A SE9801818 A SE 9801818A SE 9801818 D0 SE9801818 D0 SE 9801818D0
Authority
SE
Sweden
Prior art keywords
combustion chamber
end portion
wall member
inlet end
chamber arrangement
Prior art date
Application number
SE9801818A
Other languages
Swedish (sv)
Other versions
SE9801818L (en
Inventor
Mark Inker
Leif Andersson
Torsten Strand
Svante Stenfors
Ulf Nilsson
Original Assignee
Asea Brown Boveri
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 Asea Brown Boveri filed Critical Asea Brown Boveri
Priority to SE9801818A priority Critical patent/SE9801818L/en
Publication of SE9801818D0 publication Critical patent/SE9801818D0/en
Priority to AU46620/99A priority patent/AU4662099A/en
Priority to PCT/SE1999/000862 priority patent/WO1999061840A1/en
Publication of SE9801818L publication Critical patent/SE9801818L/en

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
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/50Combustion chambers comprising an annular flame tube within an annular casing
    • 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
    • F23R3/002Wall structures
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05CINDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
    • F05C2201/00Metals
    • F05C2201/04Heavy metals
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05CINDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
    • F05C2203/00Non-metallic inorganic materials
    • F05C2203/08Ceramics; Oxides
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05CINDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
    • F05C2253/00Other material characteristics; Treatment of material
    • F05C2253/12Coating

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)

Abstract

A combustion chamber device for a gas turbine comprises a wall member (11) which defines a combustion chamber (5) having an inlet and an outlet end, wherein the wall member (11) comprises an inlet end portion (14), which has at least one opening (7) for receiving a burner member (6), comprised to generate a flame in the combustion chamber (5) and means (16, 17, 19, 39) for conveying a cooling fluid outside the combustion chamber to the inlet end portion (14) of the wall member (11) for cooling thereof. The inlet end portion (14) is substantially closed and defines a barrier against penetration of the cooling fluid into the combustion chamber (5).
SE9801818A 1998-05-25 1998-05-25 Combustion chamber arrangement SE9801818L (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
SE9801818A SE9801818L (en) 1998-05-25 1998-05-25 Combustion chamber arrangement
AU46620/99A AU4662099A (en) 1998-05-25 1999-05-20 Combustion chamber for gas turbine
PCT/SE1999/000862 WO1999061840A1 (en) 1998-05-25 1999-05-20 Combustion chamber for gas turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE9801818A SE9801818L (en) 1998-05-25 1998-05-25 Combustion chamber arrangement

Publications (2)

Publication Number Publication Date
SE9801818D0 true SE9801818D0 (en) 1998-05-25
SE9801818L SE9801818L (en) 1999-11-26

Family

ID=20411421

Family Applications (1)

Application Number Title Priority Date Filing Date
SE9801818A SE9801818L (en) 1998-05-25 1998-05-25 Combustion chamber arrangement

Country Status (3)

Country Link
AU (1) AU4662099A (en)
SE (1) SE9801818L (en)
WO (1) WO1999061840A1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7273497B2 (en) 1999-05-28 2007-09-25 Anova Corp. Methods for treating a defect in the annulus fibrosis
US20070038231A1 (en) 1999-05-28 2007-02-15 Ferree Bret A Methods and apparatus for treating disc herniation and preventing the extrusion of interbody bone graft
US20060247665A1 (en) 1999-05-28 2006-11-02 Ferree Bret A Methods and apparatus for treating disc herniation and preventing the extrusion of interbody bone graft
US9232938B2 (en) 2006-06-13 2016-01-12 Anova Corp. Method and apparatus for closing fissures in the annulus fibrosus
US8834496B2 (en) 2006-06-13 2014-09-16 Bret A. Ferree Soft tissue repair methods and apparatus
CH704185A1 (en) * 2010-12-06 2012-06-15 Alstom Technology Ltd GAS TURBINE AND METHOD FOR recondition SUCH GAS TURBINE.

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4843825A (en) * 1988-05-16 1989-07-04 United Technologies Corporation Combustor dome heat shield
FR2670869B1 (en) * 1990-12-19 1994-10-21 Snecma COMBUSTION CHAMBER COMPRISING TWO SUCCESSIVE SPEAKERS.
DE4444961A1 (en) * 1994-12-16 1996-06-20 Mtu Muenchen Gmbh Device for cooling in particular the rear wall of the flame tube of a combustion chamber for gas turbine engines
DE19547703C2 (en) * 1995-12-20 1999-02-18 Mtu Muenchen Gmbh Combustion chamber, in particular ring combustion chamber, for gas turbine engines

Also Published As

Publication number Publication date
AU4662099A (en) 1999-12-13
SE9801818L (en) 1999-11-26
WO1999061840A1 (en) 1999-12-02

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