DE69306291D1 - Einteiliger Aufsatz für eine Dualringbrennkammer - Google Patents

Einteiliger Aufsatz für eine Dualringbrennkammer

Info

Publication number
DE69306291D1
DE69306291D1 DE69306291T DE69306291T DE69306291D1 DE 69306291 D1 DE69306291 D1 DE 69306291D1 DE 69306291 T DE69306291 T DE 69306291T DE 69306291 T DE69306291 T DE 69306291T DE 69306291 D1 DE69306291 D1 DE 69306291D1
Authority
DE
Germany
Prior art keywords
combustion chamber
dual ring
piece attachment
ring combustion
attachment
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 - Lifetime
Application number
DE69306291T
Other languages
English (en)
Other versions
DE69306291T2 (de
Inventor
Eric John Kress
Joseph Frank Savelli
David Walte Parry
John Michael Koshoffer
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of DE69306291D1 publication Critical patent/DE69306291D1/de
Publication of DE69306291T2 publication Critical patent/DE69306291T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • 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
    • 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
    • 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)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
DE69306291T 1992-03-30 1993-03-25 Einteiliger Aufsatz für eine Dualringbrennkammer Expired - Lifetime DE69306291T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/860,398 US5289687A (en) 1992-03-30 1992-03-30 One-piece cowl for a double annular combustor

Publications (2)

Publication Number Publication Date
DE69306291D1 true DE69306291D1 (de) 1997-01-16
DE69306291T2 DE69306291T2 (de) 1997-06-26

Family

ID=25333150

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69306291T Expired - Lifetime DE69306291T2 (de) 1992-03-30 1993-03-25 Einteiliger Aufsatz für eine Dualringbrennkammer

Country Status (5)

Country Link
US (1) US5289687A (de)
EP (1) EP0564171B1 (de)
JP (1) JP2599882B2 (de)
CA (1) CA2089295C (de)
DE (1) DE69306291T2 (de)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US5657633A (en) * 1995-12-29 1997-08-19 General Electric Company Centerbody for a multiple 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
US6148600A (en) * 1999-02-26 2000-11-21 General Electric Company One-piece sheet metal cowl for combustor of a gas turbine engine and method of configuring same
US6502400B1 (en) * 2000-05-20 2003-01-07 General Electric Company Combustor dome assembly and method of assembling the same
DE10048864A1 (de) * 2000-10-02 2002-04-11 Rolls Royce Deutschland Brennkammerkopf für eine Gasturbine
US6449952B1 (en) 2001-04-17 2002-09-17 General Electric Company Removable cowl for gas turbine combustor
US6553767B2 (en) * 2001-06-11 2003-04-29 General Electric Company Gas turbine combustor liner with asymmetric dilution holes machined from a single piece form
US6581386B2 (en) 2001-09-29 2003-06-24 General Electric Company Threaded combustor baffle
US7222488B2 (en) 2002-09-10 2007-05-29 General Electric Company Fabricated cowl for double annular combustor of a gas turbine engine
FR2856468B1 (fr) * 2003-06-17 2007-11-23 Snecma Moteurs Chambre de combustion annulaire de turbomachine
US6901758B2 (en) * 2003-08-08 2005-06-07 General Electric Company Method for repairing an air cooled combustor liner segment edge portion and repaired segment
US6868675B1 (en) * 2004-01-09 2005-03-22 Honeywell International Inc. Apparatus and method for controlling combustor liner carbon formation
US6983599B2 (en) * 2004-02-12 2006-01-10 General Electric Company Combustor member and method for making a combustor assembly
FR2891351B1 (fr) 2005-09-23 2007-12-07 Snecma Chambre de combustion de moteur a turbine a gaz avec carenage
US7500364B2 (en) * 2005-11-22 2009-03-10 Honeywell International Inc. System for coupling flow from a centrifugal compressor to an axial combustor for gas turbines
FR2899314B1 (fr) * 2006-03-30 2008-05-09 Snecma Sa Dispositif d'injection d'un melange d'air et de carburant, chambre de combustion et turbomachine munies d'un tel dispositif
FR2909163B1 (fr) * 2006-11-28 2011-02-25 Snecma Carenage de chambre de combustion de turbomachine.
FR2909748B1 (fr) 2006-12-07 2009-07-10 Snecma Sa Fond de chambre, procede de realisation de celui-ci, chambre de combustion le comportant et turboreacteur en etant equipe
US9194586B2 (en) 2011-12-07 2015-11-24 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
US9416972B2 (en) 2011-12-07 2016-08-16 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
US9243802B2 (en) 2011-12-07 2016-01-26 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
FR3011317B1 (fr) * 2013-10-01 2018-02-23 Safran Aircraft Engines Chambre de combustion pour turbomachine a admission d'air homogene au travers de systemes d'injection
US11333360B2 (en) * 2020-09-25 2022-05-17 General Electric Company Fuel injector for a turbomachine
US11859819B2 (en) 2021-10-15 2024-01-02 General Electric Company Ceramic composite combustor dome and liners

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2686401A (en) * 1950-08-02 1954-08-17 United Aircraft Corp Fuel manifold for gas turbine power plants
US2930193A (en) * 1955-08-29 1960-03-29 Gen Electric Cowled dome liner for combustors
US2973624A (en) * 1955-10-26 1961-03-07 Gen Electric Cowled dome liners
US2996884A (en) * 1959-03-11 1961-08-22 Rolls Royce Combustion chamber
US3132483A (en) * 1960-04-25 1964-05-12 Rolls Royce Gas turbine engine combustion chamber
GB903834A (en) * 1960-05-18 1962-08-22 Rolls Royce Combustion chamber
DE1297937B (de) * 1965-03-23 1969-06-19 Prvni Brnenska Strojirna Brennkammer fuer Gasturbinen
BE795867A (fr) * 1972-03-01 1973-06-18 Gen Electric Dispositif pour uniformiser l'ecoulement de l'air dans une turbine a gaz
DE2728399C2 (de) * 1977-06-24 1982-04-22 Brown, Boveri & Cie Ag, 6800 Mannheim Brennkammer für eine Gasturbine
JPS5914693A (ja) * 1982-07-16 1984-01-25 松下電器産業株式会社 プリント基板装置の製造方法
JPS6120770A (ja) * 1984-07-10 1986-01-29 Matsushita Electric Ind Co Ltd プラテン駆動装置
FR2616889B1 (fr) * 1987-06-18 1992-07-31 Snecma Carter de chambre de combustion de turboreacteur comportant des orifices de prelevement d'air
US5197289A (en) * 1990-11-26 1993-03-30 General Electric Company Double dome combustor

Also Published As

Publication number Publication date
CA2089295A1 (en) 1993-10-01
EP0564171B1 (de) 1996-12-04
US5289687A (en) 1994-03-01
JPH0618042A (ja) 1994-01-25
DE69306291T2 (de) 1997-06-26
CA2089295C (en) 2002-12-24
JP2599882B2 (ja) 1997-04-16
EP0564171A1 (de) 1993-10-06

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8328 Change in the person/name/address of the agent

Representative=s name: ROEGER UND KOLLEGEN, 73728 ESSLINGEN