SG91931A1 - Method of repairing combustion chamber liners - Google Patents

Method of repairing combustion chamber liners

Info

Publication number
SG91931A1
SG91931A1 SG200104070A SG200104070A SG91931A1 SG 91931 A1 SG91931 A1 SG 91931A1 SG 200104070 A SG200104070 A SG 200104070A SG 200104070 A SG200104070 A SG 200104070A SG 91931 A1 SG91931 A1 SG 91931A1
Authority
SG
Singapore
Prior art keywords
repairing
combustion chamber
chamber liners
liners
combustion
Prior art date
Application number
SG200104070A
Other languages
English (en)
Inventor
Farmer Gilbert
Michael Caldwell James
Allen Stiverson Steven
Bruce Patterson David
John Emilianowicz Edward
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of SG91931A1 publication Critical patent/SG91931A1/en

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
    • F23R3/002—Wall structures
    • 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
    • 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
    • F23R2900/00019—Repairing or maintaining combustion chamber liners or subparts
    • 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
    • Y10T29/49316—Impeller making
    • Y10T29/49318—Repairing or disassembling
    • 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
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine 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
    • Y10T29/49732—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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Laser Beam Processing (AREA)
  • Welding Or Cutting Using Electron Beams (AREA)
SG200104070A 2000-07-18 2001-07-09 Method of repairing combustion chamber liners SG91931A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/618,379 US6345441B1 (en) 2000-07-18 2000-07-18 Method of repairing combustion chamber liners

Publications (1)

Publication Number Publication Date
SG91931A1 true SG91931A1 (en) 2002-10-15

Family

ID=24477451

Family Applications (1)

Application Number Title Priority Date Filing Date
SG200104070A SG91931A1 (en) 2000-07-18 2001-07-09 Method of repairing combustion chamber liners

Country Status (5)

Country Link
US (1) US6345441B1 (de)
EP (1) EP1174209B1 (de)
JP (1) JP4600905B2 (de)
DE (1) DE60102628T2 (de)
SG (1) SG91931A1 (de)

Families Citing this family (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6581285B2 (en) * 2001-06-11 2003-06-24 General Electric Co. Methods for replacing nuggeted combustor liner panels
US6568079B2 (en) * 2001-06-11 2003-05-27 General Electric Company Methods for replacing combustor liner panels
US6571472B2 (en) * 2001-08-14 2003-06-03 General Electric Company Restoration of thickness to load-bearing gas turbine engine components
US6925810B2 (en) 2002-11-08 2005-08-09 Honeywell International, Inc. Gas turbine engine transition liner assembly and repair
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
US6892931B2 (en) * 2002-12-27 2005-05-17 General Electric Company Methods for replacing portions of turbine shroud supports
US6782620B2 (en) 2003-01-28 2004-08-31 General Electric Company Methods for replacing a portion of a combustor dome assembly
US6779268B1 (en) 2003-05-13 2004-08-24 General Electric Company Outer and inner cowl-wire wrap to one piece cowl conversion
US7065955B2 (en) * 2003-06-18 2006-06-27 General Electric Company Methods and apparatus for injecting cleaning fluids into combustors
US6868675B1 (en) * 2004-01-09 2005-03-22 Honeywell International Inc. Apparatus and method for controlling combustor liner carbon formation
US6969826B2 (en) * 2004-04-08 2005-11-29 General Electric Company Welding process
US7546684B2 (en) * 2004-07-27 2009-06-16 General Electric Company Method for repair and replacement of combustor liner panel
US7448133B2 (en) * 2004-09-23 2008-11-11 Honeywell International Inc. Procedure for replacement of acoustic liner in integrated exhaust duct muffler for use with airborne auxiliary power units
KR100687872B1 (ko) * 2005-05-18 2007-02-27 주식회사 하이닉스반도체 반도체소자 제조를 위한 이온주입방법 및 이를 이용한경사형 접합 형성방법
US8327538B2 (en) * 2005-10-17 2012-12-11 General Electric Company Methods to facilitate extending gas turbine engine useful life
US20080148565A1 (en) * 2006-12-22 2008-06-26 Edward John Emilianowicz Methods for making combustor liner replacement panels
US8312627B2 (en) * 2006-12-22 2012-11-20 General Electric Company Methods for repairing combustor liners
US8001793B2 (en) * 2008-08-29 2011-08-23 Pratt & Whitney Canada Corp. Gas turbine engine reverse-flow combustor
US20100095525A1 (en) * 2008-10-22 2010-04-22 Shaw Alan Terence Gas turbine combustor repair using a make-up ring
US8281487B2 (en) * 2009-01-20 2012-10-09 United Technologies Corporation Control of case wall growth during repair and method
US8276253B2 (en) * 2009-06-03 2012-10-02 General Electric Company Method and apparatus to remove or install combustion liners
US8713776B2 (en) 2010-04-07 2014-05-06 General Electric Company System and tool for installing combustion liners
US8910378B2 (en) * 2012-05-01 2014-12-16 United Technologies Corporation Method for working of combustor float wall panels
FR2996154B1 (fr) * 2012-10-02 2015-04-03 Snecma Outillage pour l'assemblage de deux pieces annulaires de carter
EP3096920A4 (de) * 2014-01-24 2017-03-01 United Technologies Corporation Additivreparatur für brennkammerwandabschnitte
US10088167B2 (en) 2015-06-15 2018-10-02 General Electric Company Combustion flow sleeve lifting tool
EP3519681A4 (de) * 2016-09-29 2020-12-02 GKN Aerospace Newington LLC Herstellungsverfahren für zylindrische teile
CN107363480A (zh) * 2017-07-20 2017-11-21 江苏省常熟环通实业有限公司 一种汽车前防撞梁用钢材及其异形化成型方法
US11614002B2 (en) * 2020-10-30 2023-03-28 Raytheon Technologies Corporation Split case structure for a gas turbine engine
US11846249B1 (en) 2022-09-02 2023-12-19 Rtx Corporation Gas turbine engine with integral bypass duct

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5430935A (en) * 1993-07-14 1995-07-11 Yaworsky; Chester E. Method for repairing a combustion chamber assembly
US5839643A (en) * 1996-06-17 1998-11-24 Kabushiki Kaisha Yutaka Giken Method of weld-recoulping front cover and pump shell of torque converter
US6049978A (en) * 1996-12-23 2000-04-18 Recast Airfoil Group Methods for repairing and reclassifying gas turbine engine airfoil parts

Family Cites Families (7)

* 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
US4361010A (en) * 1980-04-02 1982-11-30 United Technologies Corporation Combustor liner construction
JPH0648092B2 (ja) * 1985-04-04 1994-06-22 ゼネラル・エレクトリツク・カンパニイ 燃焼室構造
JPS6434591A (en) * 1987-07-30 1989-02-06 Toshiba Corp Method for joining ring of gas turbine combustor liner
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
FR2777318B1 (fr) * 1998-04-09 2000-05-12 Snecma Procede de reduction du jeu existant entre une chemise et un distributeur de turbine d'un turboreacteur

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5430935A (en) * 1993-07-14 1995-07-11 Yaworsky; Chester E. Method for repairing a combustion chamber assembly
US5839643A (en) * 1996-06-17 1998-11-24 Kabushiki Kaisha Yutaka Giken Method of weld-recoulping front cover and pump shell of torque converter
US6049978A (en) * 1996-12-23 2000-04-18 Recast Airfoil Group Methods for repairing and reclassifying gas turbine engine airfoil parts

Also Published As

Publication number Publication date
EP1174209A1 (de) 2002-01-23
DE60102628D1 (de) 2004-05-13
JP4600905B2 (ja) 2010-12-22
US6345441B1 (en) 2002-02-12
JP2002138853A (ja) 2002-05-17
EP1174209B1 (de) 2004-04-07
DE60102628T2 (de) 2005-07-07

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