SG66497A1 - Method for applying material to a face of a flow directing assembly for a gas turbine engine - Google Patents

Method for applying material to a face of a flow directing assembly for a gas turbine engine

Info

Publication number
SG66497A1
SG66497A1 SG1998004209A SG1998004209A SG66497A1 SG 66497 A1 SG66497 A1 SG 66497A1 SG 1998004209 A SG1998004209 A SG 1998004209A SG 1998004209 A SG1998004209 A SG 1998004209A SG 66497 A1 SG66497 A1 SG 66497A1
Authority
SG
Singapore
Prior art keywords
face
gas turbine
turbine engine
flow directing
directing assembly
Prior art date
Application number
SG1998004209A
Other languages
English (en)
Inventor
Alan J Ittleson
Bryan P Dube
Jeffrey B Johnson
Jeffrey J Bayer
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of SG66497A1 publication Critical patent/SG66497A1/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K9/00—Arc welding or cutting
    • B23K9/16—Arc welding or cutting making use of shielding gas
    • B23K9/173—Arc welding or cutting making use of shielding gas and of a consumable electrode
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K9/00—Arc welding or cutting
    • B23K9/04—Welding for other purposes than joining, e.g. built-up welding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2101/00—Articles made by soldering, welding or cutting
    • B23K2101/001—Turbines
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Mechanical Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
SG1998004209A 1997-12-19 1998-10-14 Method for applying material to a face of a flow directing assembly for a gas turbine engine SG66497A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/994,678 US6034344A (en) 1997-12-19 1997-12-19 Method for applying material to a face of a flow directing assembly for a gas turbine engine

Publications (1)

Publication Number Publication Date
SG66497A1 true SG66497A1 (en) 1999-07-20

Family

ID=25540926

Family Applications (1)

Application Number Title Priority Date Filing Date
SG1998004209A SG66497A1 (en) 1997-12-19 1998-10-14 Method for applying material to a face of a flow directing assembly for a gas turbine engine

Country Status (3)

Country Link
US (1) US6034344A (enExample)
JP (1) JPH11218001A (enExample)
SG (1) SG66497A1 (enExample)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6269540B1 (en) * 1998-10-05 2001-08-07 National Research Council Of Canada Process for manufacturing or repairing turbine engine or compressor components
US6412149B1 (en) * 1999-08-25 2002-07-02 General Electric Company C-clip for shroud assembly
US6820468B2 (en) 2001-03-26 2004-11-23 General Electric Company Fixture for holding a gas turbine engine blade
GB0112876D0 (en) * 2001-05-26 2001-07-18 Rolls Royce Plc A method of manufacturing an article
JP4229734B2 (ja) * 2003-03-20 2009-02-25 株式会社Ｉｈｉ 薄肉部分の肉盛溶接方法
US7196017B2 (en) * 2003-10-24 2007-03-27 Avago Technologies Fiber Ip (Singapore) Pte. Ltd. Method for etching smooth sidewalls in III-V based compounds for electro-optical devices
JP4822924B2 (ja) * 2006-04-28 2011-11-24 株式会社東芝 タービン翼およびこれを備える蒸気タービン
US8708655B2 (en) 2010-09-24 2014-04-29 United Technologies Corporation Blade for a gas turbine engine
US9976664B2 (en) 2010-11-05 2018-05-22 Hamilton Sundtrand Corporation Furnace braze deposition of hardface coating on wear surface
US9816619B2 (en) 2011-01-17 2017-11-14 Hamilton Sundstrand Corporation Thrust plate for butterfly valve
US8602845B2 (en) 2011-09-23 2013-12-10 United Technologies Corporation Strengthening by machining
US9145792B2 (en) * 2012-01-31 2015-09-29 General Electric Company Fixture assembly for repairing a shroud tile of a gas turbine
US9206702B2 (en) 2012-01-31 2015-12-08 General Electric Company Method for repairing a shroud tile of a gas turbine
US20140053403A1 (en) * 2012-08-22 2014-02-27 General Electric Company Method for extending an original service life of gas turbine components
FR3063031B1 (fr) * 2017-02-21 2019-03-22 Safran Aircraft Engines Dispositif de support d'une piece metallique en vue de son soudage ou brasage

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4155152A (en) * 1977-12-12 1979-05-22 Matthew Bernardo Method of restoring the shrouds of turbine blades
US4170473A (en) * 1978-01-13 1979-10-09 Trw Inc. Method of making and using a welding chill
US5690469A (en) * 1996-06-06 1997-11-25 United Technologies Corporation Method and apparatus for replacing a vane assembly in a turbine engine

Also Published As

Publication number Publication date
JPH11218001A (ja) 1999-08-10
US6034344A (en) 2000-03-07

Similar Documents

Publication Publication Date Title
SG66497A1 (en) Method for applying material to a face of a flow directing assembly for a gas turbine engine
PL340922A1 (en) Sealing assembly for a gas turbine engine
EP0751104A3 (en) Abrasive composition, method of manufacturing an abrasive composition, and gas turbine engine having an abrasive seal
GB2307520B (en) A gas turbine engine
PL320693A1 (en) Fastening assembly of a gas turbine blade
GB9305012D0 (en) Sealing structures for gas turbine engines
GB2166805B (en) Coolable seal assembly for a gas turbine engine
GB9415436D0 (en) Auxiliary gas turbine engines
GB2071777B (en) Method and replacement member for repairing a gas turbine engine vane assembly
GB2291130B (en) A gas turbine engine
SG71850A1 (en) Method for applying a coating to the tip of a flow directing assembly
GB9911871D0 (en) A gas turbine engine and a method of controlling a gas turbine engine
GB9611235D0 (en) A gas turbine engine combustion chamber and a method of operation thereof
GB9523223D0 (en) A gas turbine engine
GB9608196D0 (en) Gas turbine engine
GB2299834B (en) Gas turbine engine rotary disc
DE69840572D1 (de) Gasturbine mit einem druckwellenrotor sowie betriebsverfahren
PL319809A1 (en) Exhaust gas driven turbine for a turbo-charger
GB2288640B (en) A gas turbine engine
GB9505452D0 (en) Gas turbine engine
BR8906606A (pt) Revestimento preliminar de vedacao abrasivel para turbina a gas
SG71916A1 (en) Assembly for brazing a stator component of a gas turbine engine and method for brazing articles such as an abradable material to a stator of a gas turbine engine
GB2286600B (en) Coating scheme to contain molten material during gas turbine engine fires
GB9206404D0 (en) Bladed rotor for a gas turbine engine
EP0805263A4 (en) DAWN FOR GAS TURBINE