BR0106654B1 - conjunto de cúpula de combustor e método para a sua fabricação. - Google Patents

conjunto de cúpula de combustor e método para a sua fabricação.

Info

Publication number
BR0106654B1
BR0106654B1 BRPI0106654-4A BR0106654A BR0106654B1 BR 0106654 B1 BR0106654 B1 BR 0106654B1 BR 0106654 A BR0106654 A BR 0106654A BR 0106654 B1 BR0106654 B1 BR 0106654B1
Authority
BR
Brazil
Prior art keywords
manufacture
combustor dome
dome assembly
assembly
combustor
Prior art date
Application number
BRPI0106654-4A
Other languages
English (en)
Other versions
BR0106654A (pt
Inventor
Max Joseph Friedhauer
Michael Philip Hagle
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 filed Critical
Publication of BR0106654A publication Critical patent/BR0106654A/pt
Publication of BR0106654B1 publication Critical patent/BR0106654B1/pt

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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • 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
    • 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)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Gas Burners (AREA)
  • Combustion Of Fluid Fuel (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
BRPI0106654-4A 2000-05-20 2001-03-23 conjunto de cúpula de combustor e método para a sua fabricação. BR0106654B1 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/575,416 US6502400B1 (en) 2000-05-20 2000-05-20 Combustor dome assembly and method of assembling the same
PCT/US2001/009320 WO2001090652A1 (en) 2000-05-20 2001-03-23 Combustor dome assembly and method of assembling the same

Publications (2)

Publication Number Publication Date
BR0106654A BR0106654A (pt) 2002-04-02
BR0106654B1 true BR0106654B1 (pt) 2010-10-19

Family

ID=24300236

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0106654-4A BR0106654B1 (pt) 2000-05-20 2001-03-23 conjunto de cúpula de combustor e método para a sua fabricação.

Country Status (7)

Country Link
US (1) US6502400B1 (pt)
EP (1) EP1290378B1 (pt)
JP (1) JP4553093B2 (pt)
BR (1) BR0106654B1 (pt)
CA (1) CA2379110C (pt)
DE (1) DE60112754T2 (pt)
WO (1) WO2001090652A1 (pt)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6655027B2 (en) * 2002-01-15 2003-12-02 General Electric Company Methods for assembling gas turbine engine combustors
US6725667B2 (en) * 2002-08-22 2004-04-27 General Electric Company Combustor dome for gas turbine engine
US6931728B2 (en) * 2002-12-19 2005-08-23 General Electric Company Test model for a gas turbine combustor dome and method of fabricating
US6782620B2 (en) * 2003-01-28 2004-08-31 General Electric Company Methods for replacing a portion of a combustor dome assembly
US7094450B2 (en) * 2003-04-30 2006-08-22 General Electric Company Method for applying or repairing thermal barrier coatings
US6968693B2 (en) * 2003-09-22 2005-11-29 General Electric Company Method and apparatus for reducing gas turbine engine emissions
US20070095071A1 (en) * 2003-09-29 2007-05-03 Kastrup David A Apparatus for assembling gas turbine engine combustors
US7690207B2 (en) * 2004-08-24 2010-04-06 Pratt & Whitney Canada Corp. Gas turbine floating collar arrangement
US7134286B2 (en) * 2004-08-24 2006-11-14 Pratt & Whitney Canada Corp. Gas turbine floating collar arrangement
US7628019B2 (en) * 2005-03-21 2009-12-08 United Technologies Corporation Fuel injector bearing plate assembly and swirler assembly
US20080016876A1 (en) * 2005-06-02 2008-01-24 General Electric Company Method and apparatus for reducing gas turbine engine emissions
US7673460B2 (en) * 2005-06-07 2010-03-09 Snecma System of attaching an injection system to a turbojet combustion chamber base
FR2886714B1 (fr) * 2005-06-07 2007-09-07 Snecma Moteurs Sa Systeme d'injection anti-rotatif pour turbo-reacteur
US20070119052A1 (en) * 2005-11-28 2007-05-31 General Electric Company Combustor dome repair method
FR2897922B1 (fr) 2006-02-27 2008-10-10 Snecma Sa Agencement pour une chambre de combustion de turboreacteur
US7845549B2 (en) * 2006-05-31 2010-12-07 General Electric Company MIM braze preforms
US7856826B2 (en) * 2006-11-10 2010-12-28 General Electric Company Combustor dome mixer retaining means
US7765809B2 (en) * 2006-11-10 2010-08-03 General Electric Company Combustor dome and methods of assembling such
US7841509B2 (en) * 2007-10-23 2010-11-30 Gm Global Technology Operations, Inc. Method of brazing with two different braze compositions
US10317081B2 (en) * 2011-01-26 2019-06-11 United Technologies Corporation Fuel injector assembly
EP2716976B1 (en) * 2011-06-02 2018-10-31 Kawasaki Jukogyo Kabushiki Kaisha Gas turbine combustor
US8726669B2 (en) 2011-06-30 2014-05-20 General Electric Company Combustor dome with combined deflector/mixer retainer
US10041676B2 (en) 2015-07-08 2018-08-07 General Electric Company Sealed conical-flat dome for flight engine combustors
US10125634B2 (en) * 2015-12-10 2018-11-13 General Electric Company Combustor assembly alignment and securement systems
US10837640B2 (en) 2017-03-06 2020-11-17 General Electric Company Combustion section of a gas turbine engine
US12072099B2 (en) * 2021-12-21 2024-08-27 General Electric Company Gas turbine fuel nozzle having a lip extending from the vanes of a swirler

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2800768A (en) 1954-08-19 1957-07-30 United Aircraft Corp Burner construction
US3853273A (en) * 1973-10-01 1974-12-10 Gen Electric Axial swirler central injection carburetor
US3930369A (en) 1974-02-04 1976-01-06 General Motors Corporation Lean prechamber outflow combustor with two sets of primary air entrances
GB2135440B (en) 1983-02-19 1986-06-25 Rolls Royce Mounting combustion chambers
US4787209A (en) * 1987-04-29 1988-11-29 Avco Corporation Stacked ring combustor assembly
US5154060A (en) 1991-08-12 1992-10-13 General Electric Company Stiffened double dome combustor
US5289687A (en) * 1992-03-30 1994-03-01 General Electric Company One-piece cowl for a double annular combustor
CA2089302C (en) * 1992-03-30 2004-07-06 Joseph Frank Savelli Double annular combustor
US5916142A (en) 1996-10-21 1999-06-29 General Electric Company Self-aligning swirler with ball joint
US6212870B1 (en) * 1998-09-22 2001-04-10 General Electric Company Self fixturing combustor dome assembly

Also Published As

Publication number Publication date
BR0106654A (pt) 2002-04-02
WO2001090652A1 (en) 2001-11-29
JP4553093B2 (ja) 2010-09-29
CA2379110C (en) 2009-02-17
EP1290378A1 (en) 2003-03-12
DE60112754D1 (de) 2005-09-22
DE60112754T2 (de) 2006-06-01
US6502400B1 (en) 2003-01-07
JP2003534516A (ja) 2003-11-18
EP1290378B1 (en) 2005-08-17
CA2379110A1 (en) 2001-11-29

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Legal Events

Date Code Title Description
B06A Patent application procedure suspended [chapter 6.1 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 23/03/2001, OBSERVADAS AS CONDICOES LEGAIS.

B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time
B24J Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12)