BR0202273B1 - mÉtodo para substituir painÉis de revestimento, parte de um revestimento, e painÉis de revestimento deteriorados de combustor de motor de turbina a gÁs. - Google Patents

mÉtodo para substituir painÉis de revestimento, parte de um revestimento, e painÉis de revestimento deteriorados de combustor de motor de turbina a gÁs.

Info

Publication number
BR0202273B1
BR0202273B1 BRPI0202273-7A BR0202273A BR0202273B1 BR 0202273 B1 BR0202273 B1 BR 0202273B1 BR 0202273 A BR0202273 A BR 0202273A BR 0202273 B1 BR0202273 B1 BR 0202273B1
Authority
BR
Brazil
Prior art keywords
casing
panels
gas turbine
replacing
turbine engine
Prior art date
Application number
BRPI0202273-7A
Other languages
English (en)
Other versions
BR0202273A (pt
Inventor
Edward John Emilianowicz
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 BR0202273A publication Critical patent/BR0202273A/pt
Publication of BR0202273B1 publication Critical patent/BR0202273B1/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P6/00—Restoring or reconditioning objects
    • B23P6/002—Repairing turbine components, e.g. moving or stationary blades, rotors
    • B23P6/005—Repairing turbine components, e.g. moving or stationary blades, rotors using only replacement pieces of a particular form
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P2700/00—Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
    • B23P2700/13—Parts of turbine combustion chambers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C2900/00—Special features of, or arrangements for combustion apparatus using fluid fuels or solid fuels suspended in air; Combustion processes therefor
    • F23C2900/03001—Miniaturized combustion devices using fluid fuels
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00016—Retrofitting in general, e.g. to respect new regulations on pollution
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49346—Rocket or jet device making
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49718—Repairing
    • Y10T29/49721—Repairing with disassembling
    • Y10T29/4973—Replacing of defective part
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49718—Repairing
    • Y10T29/49732—Repairing by attaching repair preform, e.g., remaking, restoring, or patching
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49718—Repairing
    • Y10T29/49732—Repairing by attaching repair preform, e.g., remaking, restoring, or patching
    • Y10T29/49734—Repairing by attaching repair preform, e.g., remaking, restoring, or patching and removing damaged material
    • Y10T29/49737—Metallurgically attaching preform
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49718—Repairing
    • Y10T29/49732—Repairing by attaching repair preform, e.g., remaking, restoring, or patching
    • Y10T29/49742—Metallurgically attaching preform

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
BRPI0202273-7A 2001-06-11 2002-06-07 mÉtodo para substituir painÉis de revestimento, parte de um revestimento, e painÉis de revestimento deteriorados de combustor de motor de turbina a gÁs. BR0202273B1 (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/878,849 US6581285B2 (en) 2001-06-11 2001-06-11 Methods for replacing nuggeted combustor liner panels

Publications (2)

Publication Number Publication Date
BR0202273A BR0202273A (pt) 2003-04-01
BR0202273B1 true BR0202273B1 (pt) 2011-06-14

Family

ID=25372971

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0202273-7A BR0202273B1 (pt) 2001-06-11 2002-06-07 mÉtodo para substituir painÉis de revestimento, parte de um revestimento, e painÉis de revestimento deteriorados de combustor de motor de turbina a gÁs.

Country Status (6)

Country Link
US (1) US6581285B2 (pt)
EP (1) EP1266718B1 (pt)
BR (1) BR0202273B1 (pt)
CA (1) CA2388281C (pt)
DE (1) DE60237060D1 (pt)
SG (1) SG104312A1 (pt)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6986201B2 (en) * 2002-12-04 2006-01-17 General Electric Company Methods for replacing combustor liners
US6904676B2 (en) * 2002-12-04 2005-06-14 General Electric Company Methods for replacing a portion of a combustor liner
US6912782B2 (en) * 2003-04-09 2005-07-05 Honeywell International Inc. Forming and assembly method for multi-axial pivoting combustor liner in gas turbine engine
US6868675B1 (en) * 2004-01-09 2005-03-22 Honeywell International Inc. Apparatus and method for controlling combustor liner carbon formation
US7546684B2 (en) * 2004-07-27 2009-06-16 General Electric Company Method for repair and replacement of combustor liner panel
US7546743B2 (en) * 2005-10-12 2009-06-16 General Electric Company Bolting configuration for joining ceramic combustor liner to metal mounting attachments
US8312627B2 (en) * 2006-12-22 2012-11-20 General Electric Company Methods for repairing combustor liners
US20080148565A1 (en) * 2006-12-22 2008-06-26 Edward John Emilianowicz Methods for making combustor liner replacement panels
US8910378B2 (en) 2012-05-01 2014-12-16 United Technologies Corporation Method for working of combustor float wall panels
US9249976B2 (en) * 2012-06-28 2016-02-02 General Electric Company Method for servicing a combustor cap assembly for a turbine
US10107497B2 (en) 2012-10-04 2018-10-23 United Technologies Corporation Gas turbine engine combustor liner
WO2015074052A1 (en) 2013-11-18 2015-05-21 United Technologies Corporation Swept combustor liner panels for gas turbine engine combustor
JP6470135B2 (ja) 2014-07-14 2019-02-13 ユナイテッド テクノロジーズ コーポレイションＵｎｉｔｅｄ Ｔｅｃｈｎｏｌｏｇｉｅｓ Ｃｏｒｐｏｒａｔｉｏｎ 付加製造された表面仕上げ
US10830433B2 (en) 2016-11-10 2020-11-10 Raytheon Technologies Corporation Axial non-linear interface for combustor liner panels in a gas turbine combustor
US10655853B2 (en) 2016-11-10 2020-05-19 United Technologies Corporation Combustor liner panel with non-linear circumferential edge for a gas turbine engine combustor
US10935235B2 (en) 2016-11-10 2021-03-02 Raytheon Technologies Corporation Non-planar combustor liner panel for a gas turbine engine combustor
US10935236B2 (en) 2016-11-10 2021-03-02 Raytheon Technologies Corporation Non-planar combustor liner panel for a gas turbine engine combustor
US11092076B2 (en) 2017-11-28 2021-08-17 General Electric Company Turbine engine with combustor
CN117359271B (zh) * 2023-10-10 2024-04-26 唐山信恒元机械设备有限公司 基于棒磨机更换衬板用辅助设备

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4912922A (en) * 1972-12-19 1990-04-03 General Electric Company Combustion chamber construction
US4614082A (en) * 1972-12-19 1986-09-30 General Electric Company Combustion chamber construction
US4361010A (en) * 1980-04-02 1982-11-30 United Technologies Corporation Combustor liner construction
US4773227A (en) * 1982-04-07 1988-09-27 United Technologies Corporation Combustion chamber with improved liner construction
US4485630A (en) 1982-12-08 1984-12-04 General Electric Company Combustor liner
US4622821A (en) 1985-01-07 1986-11-18 United Technologies Corporation Combustion liner for a gas turbine engine
DE3942271A1 (de) 1989-12-21 1991-07-04 Mtu Maintenance Gmbh Verfahren zur reparatur eines flammrohres
US5181379A (en) 1990-11-15 1993-01-26 General Electric Company Gas turbine engine multi-hole film cooled combustor liner and method of manufacture
CA2056592A1 (en) 1990-12-21 1992-06-22 Phillip D. Napoli Multi-hole film cooled combustor liner with slotted film starter
US5142871A (en) 1991-01-22 1992-09-01 General Electric Company Combustor dome plate support having uniform thickness arcuate apex with circumferentially spaced coolant apertures
US5241827A (en) 1991-05-03 1993-09-07 General Electric Company Multi-hole film cooled combuster linear with differential cooling
CA2070518C (en) 1991-07-01 2001-10-02 Adrian Mark Ablett Combustor dome assembly
US5154060A (en) 1991-08-12 1992-10-13 General Electric Company Stiffened double dome combustor
US5307637A (en) 1992-07-09 1994-05-03 General Electric Company Angled multi-hole film cooled single wall combustor dome plate
US5261223A (en) 1992-10-07 1993-11-16 General Electric Company Multi-hole film cooled combustor liner with rectangular film restarting holes
US5323604A (en) 1992-11-16 1994-06-28 General Electric Company Triple annular combustor for gas turbine engine
US5430935A (en) * 1993-07-14 1995-07-11 Yaworsky; Chester E. Method for repairing a combustion chamber assembly
JPH08278029A (ja) * 1995-02-06 1996-10-22 Toshiba Corp 燃焼器用ライナー及びその製造方法
GB2306155B (en) * 1995-10-11 1997-11-19 Toshiba Kk Apparatus and method for disassembling and assembling gas turbine combuster
US6079199A (en) * 1998-06-03 2000-06-27 Pratt & Whitney Canada Inc. Double pass air impingement and air film cooling for gas turbine combustor walls
US6286317B1 (en) * 1998-12-18 2001-09-11 General Electric Company Cooling nugget for a liner of a gas turbine engine combustor having trapped vortex cavity
US6434821B1 (en) * 1999-12-06 2002-08-20 General Electric Company Method of making a combustion chamber liner
US6345441B1 (en) * 2000-07-18 2002-02-12 General Electric Company Method of repairing combustion chamber liners

Also Published As

Publication number Publication date
US20020184763A1 (en) 2002-12-12
EP1266718A3 (en) 2003-10-29
US6581285B2 (en) 2003-06-24
EP1266718A2 (en) 2002-12-18
DE60237060D1 (de) 2010-09-02
CA2388281C (en) 2009-04-14
CA2388281A1 (en) 2002-12-11
BR0202273A (pt) 2003-04-01
EP1266718B1 (en) 2010-07-21
SG104312A1 (en) 2004-06-21

Similar Documents

Publication Publication Date Title
BR0201961B1 (pt) método para operar um motor de turbina a gás, combustor para uma turbina a gás e montagem de misturador para o mesmo.
BR0202273B1 (pt) mÉtodo para substituir painÉis de revestimento, parte de um revestimento, e painÉis de revestimento deteriorados de combustor de motor de turbina a gÁs.
BR0203493B1 (pt) aerofólio de turbina para motor de turbina a gás.
BR0104648B1 (pt) método para fabricação de uma estrutura de rotor, estrutura de rotor e motor de turbina a gás.
BR0204101B1 (pt) mÉtodo de restauraÇço de lÂminas de compressor de motor de turbina a gÁs.
BR0201430B1 (pt) métodos e aparelho para resfriar combustores de motor de turbina a gás.
BR0104522B1 (pt) reparo com brasagem de um invólucro estacionário de motor de turbina a gás.
GB2382382B (en) A fan for a turbofan gas turbine engine
BR0203490B1 (pt) aerofólio de turbina para motor de turbina a gás.
BR0104191B1 (pt) montagem de rotor para um rotor de turbina a gás.
DE60227769D1 (de) Brennkammer für Gasturbine
BR0203413B1 (pt) mÉtodo e sistema de diagnàstico para motores de turbina a gÁs.
GB2402717B (en) A vane assembly for a gas turbine engine
BR0304068B1 (pt) mÉtodo para reparar um envoltàrio estacionÁrio de um motor a turbina a gÁs
IL165844A0 (en) Stator vane assembly for a gas turbine engine
BR0203418B1 (pt) motor de turbina a gÁs, mÉtodo para a fabricaÇço de um disco de rotor para o mesmo e montagem em rabo de andorinha para o mesmo.
DE60239120D1 (de) Bläserschaufelblatt für ein Gasturbinentriebwerk
AU2003236766A1 (en) Method and device for operating a burner of a heat engine, especially a gas turbine plant
DE60012289D1 (de) Brennkammer für eine Gasturbine
DE60203959D1 (de) Luftgekühltes Abgasgehäuse für eine Gasturbine
EP1291581A3 (en) Gas turbine engine combustor
DE60105531D1 (de) Gasturbinenbrennkammer, Gasturbine und Düsentriebwerk
DE60125441D1 (de) Mehrstufiges, mehrebenes Vebrennungssystem für Gasturbine
DE60122414D1 (de) Verbrennungssystem für eine Gasturbine
DE60221782D1 (de) Gasturbine mit einer Zusatzdichtung für Statorelemente

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 07/06/2002, OBSERVADAS AS CONDICOES LEGAIS.

B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time

Free format text: REFERENTE A 16A ANUIDADE.

B24J Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12)