SG10201700831PA - In situ gas turbine prevention of crack growth progression - Google Patents

In situ gas turbine prevention of crack growth progression

Info

Publication number
SG10201700831PA
SG10201700831PA SG10201700831PA SG10201700831PA SG10201700831PA SG 10201700831P A SG10201700831P A SG 10201700831PA SG 10201700831P A SG10201700831P A SG 10201700831PA SG 10201700831P A SG10201700831P A SG 10201700831PA SG 10201700831P A SG10201700831P A SG 10201700831PA
Authority
SG
Singapore
Prior art keywords
gas turbine
crack growth
situ gas
growth progression
prevention
Prior art date
Application number
SG10201700831PA
Inventor
Herbert Chidsey Roberts
David Scott Diwinsky
Wayne R Grady
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 SG10201700831PA publication Critical patent/SG10201700831PA/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/005Repairing methods or devices
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P6/00Restoring or reconditioning objects
    • B23P6/04Repairing fractures or cracked metal parts or products, e.g. castings
    • B23P6/045Repairing fractures or cracked metal parts or products, e.g. castings of turbine components, e.g. moving or stationary blades, rotors, etc.
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/32Application in turbines in gas turbines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/30Manufacture with deposition of material
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/80Repairing, retrofitting or upgrading methods

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
SG10201700831PA 2016-02-03 2017-02-02 In situ gas turbine prevention of crack growth progression SG10201700831PA (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US15/014,103 US10094221B2 (en) 2016-02-03 2016-02-03 In situ gas turbine prevention of crack growth progression

Publications (1)

Publication Number Publication Date
SG10201700831PA true SG10201700831PA (en) 2017-09-28

Family

ID=57956190

Family Applications (1)

Application Number Title Priority Date Filing Date
SG10201700831PA SG10201700831PA (en) 2016-02-03 2017-02-02 In situ gas turbine prevention of crack growth progression

Country Status (5)

Country Link
US (1) US10094221B2 (en)
EP (1) EP3203019B1 (en)
CN (2) CN107060887B (en)
CA (1) CA2956905C (en)
SG (1) SG10201700831PA (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10544676B2 (en) * 2016-02-03 2020-01-28 General Electric Company Situ gas turbine prevention of crack growth progression
US10247002B2 (en) * 2016-02-03 2019-04-02 General Electric Company In situ gas turbine prevention of crack growth progression
US10443385B2 (en) * 2016-02-03 2019-10-15 General Electric Company In situ gas turbine prevention of crack growth progression via laser welding
US11702955B2 (en) * 2019-01-14 2023-07-18 General Electric Company Component repair system and method
US11530621B2 (en) * 2019-10-16 2022-12-20 General Electric Company Systems and method for use in servicing a machine

Family Cites Families (69)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2011484A (en) 1934-09-04 1935-08-13 Hal W Harman Method for repairing castings
US2252986A (en) 1939-03-03 1941-08-19 Lawrence B Scott Method of repairing cracked or fractured metal walls
US2361106A (en) 1940-11-04 1944-10-24 Charles A Jensen Method of repairing and for preventing cracks in metal castings
US4611744A (en) 1982-06-23 1986-09-16 Refurbished Turbine Components Ltd. Turbine blade repair
US4743733A (en) 1984-10-01 1988-05-10 General Electric Company Method and apparatus for repairing metal in an article
DE3813157A1 (en) 1987-05-27 1988-12-15 Bbc Brown Boveri & Cie Method for bonding and/or repairing component parts made of an oxide dispersion-hardened nickel-based superalloy in the zone-annealed state of coarse-grained, longitudinally oriented column crystals
US5076660A (en) 1990-01-26 1991-12-31 Olympus Corporation Light source receptacle for fiberoptic illumination
US6270603B1 (en) 1991-04-09 2001-08-07 The Boeing Company Repair method for uniformly heating composite structure
US5741965A (en) 1996-11-29 1998-04-21 Hernandez; Carlos M. Aircraft jet engine testing tool
FR2763882B1 (en) 1997-05-29 1999-08-20 Aerospatiale ON-SITE REPAIR TOOLS OF A COMPOSITE STRUCTURE HAVING A DAMAGED AREA AND CORRESPONDING METHOD
GB9816421D0 (en) 1998-07-28 1998-09-23 Keymed Medicals & Ind Equip Apparatus for delivering laser energy to a remote location
US6269540B1 (en) 1998-10-05 2001-08-07 National Research Council Of Canada Process for manufacturing or repairing turbine engine or compressor components
US6302625B1 (en) 1999-10-15 2001-10-16 United Technologies Corporation Method and apparatus for refurbishing a gas turbine airfoil
GB0020461D0 (en) 2000-08-18 2000-10-11 Oliver Crispin Consulting Ltd Improvements in and relating to the robotic positioning of a work tool to a sensor
US6414458B1 (en) 2000-12-19 2002-07-02 General Electric Company Apparatus for robotically inspecting gas turbine combustion components
US6620457B2 (en) 2001-07-13 2003-09-16 General Electric Company Method for thermal barrier coating and a liner made using said method
JP2003154483A (en) 2001-11-19 2003-05-27 Mitsubishi Heavy Ind Ltd Method of automatically repairing fissuring and device for the same
US6593540B1 (en) 2002-02-08 2003-07-15 Honeywell International, Inc. Hand held powder-fed laser fusion welding torch
US7392713B2 (en) 2002-09-30 2008-07-01 United Technologies Corporation Monitoring system for turbomachinery
US7174797B2 (en) 2002-10-15 2007-02-13 Florida Turbine Technologies, Inc. High temperature and pressure testing facility
US7032279B2 (en) 2002-10-18 2006-04-25 General Electric Company Apparatus and methods for repairing compressor airfoils in situ
US6912446B2 (en) 2002-10-23 2005-06-28 General Electric Company Systems and methods for automated sensing and machining for repairing airfoils of blades
US7000303B2 (en) 2002-10-24 2006-02-21 The Boeing Company Method of repairing a crack in a component utilizing friction stir welding
DE10316966A1 (en) 2003-04-12 2004-10-28 Rolls-Royce Deutschland Ltd & Co Kg Procedure for the reconstruction of flat, damaged components
FR2854198B1 (en) 2003-04-22 2005-06-24 Snecma Services PROCESS FOR REPLACING ABRADABLE ON THE BLOWER HOUSING OF A TURBOJETACTOR
US7043898B2 (en) * 2003-06-23 2006-05-16 Pratt & Whitney Canada Corp. Combined exhaust duct and mixer for a gas turbine engine
US7016035B2 (en) 2003-09-25 2006-03-21 General Electric Company Fiber optical apparatus and system for in situ laser plasma spectroscopy
US7038162B2 (en) 2003-11-13 2006-05-02 Honeywell International, Inc. Hand-held laser welding wand filler media delivery systems and methods
US7034262B2 (en) 2004-03-23 2006-04-25 General Electric Company Apparatus and methods for repairing tenons on turbine buckets
US7140240B2 (en) 2004-06-21 2006-11-28 Hamilton Sundstrand Electric engine start system with inspection mode
US20060042083A1 (en) * 2004-08-27 2006-03-02 Baker Martin C Repair of turbines on wing
US20060231535A1 (en) 2005-04-19 2006-10-19 Fuesting Timothy P Method of welding a gamma-prime precipitate strengthened material
US7458768B2 (en) 2005-06-28 2008-12-02 United Technologies Corporation Borescope inspection port device for gas turbine engine and gas turbine engine using same
US7513024B2 (en) 2005-08-24 2009-04-07 General Electric Company Method for repairing structural cracks
US7499772B2 (en) 2005-08-31 2009-03-03 Honeywell International Inc. Method and system for navigating a nondestructive evaluation device
GB0705696D0 (en) 2007-03-24 2007-05-02 Rolls Royce Plc A method of repairing a damaged abradable coating
DE102007029728A1 (en) 2007-06-27 2009-01-08 Rolls-Royce Deutschland Ltd & Co Kg Method and device for repairing blisks of gas turbines
GB0808432D0 (en) 2008-05-12 2008-06-18 Rolls Royce Plc An inspection arrangement
US8181528B2 (en) 2009-02-27 2012-05-22 General Electric Company Method and system for ultrasonic inspection of gearbox ring gear
US8677763B2 (en) * 2009-03-10 2014-03-25 General Electric Company Method and apparatus for gas turbine engine temperature management
US9046892B2 (en) 2009-06-05 2015-06-02 The Boeing Company Supervision and control of heterogeneous autonomous operations
US8946582B1 (en) * 2009-10-02 2015-02-03 William L. Bong System and method for metal powder welding
GB2474834B (en) 2009-10-28 2013-09-11 Rolls Royce Plc A method of inspecting and/or repairing component and a device for inspecting and/or repairing a component
US9643313B2 (en) 2010-01-19 2017-05-09 The Boeing Company Apparatus for automated maintenance of aircraft structural elements
US7866532B1 (en) 2010-04-06 2011-01-11 United Launch Alliance, Llc Friction stir welding apparatus, system and method
US8001792B1 (en) * 2010-04-08 2011-08-23 Opra Technologies B.V. Turbine inlet nozzle guide vane mounting structure for radial gas turbine engine
JP5618643B2 (en) 2010-06-14 2014-11-05 株式会社東芝 Gas turbine rotor blade repair method and gas turbine rotor blade
DE102010045869A1 (en) 2010-08-03 2012-02-23 Mtu Aero Engines Gmbh Cleaning a turbo machine stage
US8904635B2 (en) 2010-11-04 2014-12-09 General Electric Company Method for servicing a turbine part
US8927897B2 (en) 2010-11-17 2015-01-06 Rolls-Royce Corporation Laser maintenance tool
GB2490667B (en) * 2011-05-09 2013-10-23 Rolls Royce Plc A method of supporting a tool and an apparatus for supporting a tool in an assembled apparatus
GB201113083D0 (en) 2011-07-29 2011-09-14 Formatex Offshore S A L A method for in-situ cleaning of compressor blades in a gas turbine engine on aircraft and compositions
US8895887B2 (en) 2011-08-05 2014-11-25 General Electric Company Resistance weld repairing of casing flange holes
US9174314B2 (en) 2011-11-03 2015-11-03 Siemens Energy, Inc. Isothermal structural repair of superalloy components including turbine blades
DE102011122549A1 (en) 2011-12-28 2013-07-04 Rolls-Royce Deutschland Ltd & Co Kg Method for repairing an inlet layer of a compressor of a gas turbine
US8786300B2 (en) 2012-02-07 2014-07-22 General Electric Company Probe assembly and methods for use in inspecting a component
US8801502B2 (en) 2012-02-28 2014-08-12 General Electric Company In-situ airfoil contouring tool
US20140063228A1 (en) 2012-09-06 2014-03-06 General Electric Company Method and system for cleaning surfaces and non-destructive inspection thereof
GB201216703D0 (en) 2012-09-19 2012-10-31 Rolls Royce Plc A boroscope and a method of laser processing a component within an assembled apparatus using a boroscope
US9003880B2 (en) 2012-12-31 2015-04-14 General Electric Company Reference speed measurement for a non-destructive testing system
US9631512B2 (en) * 2013-01-31 2017-04-25 Solar Turbines Incorporated Gas turbine offline compressor wash with buffer air from combustor
GB2510816B (en) 2013-02-12 2015-04-08 Rolls Royce Plc Material removal method
US9470658B2 (en) 2013-03-12 2016-10-18 The Boeing Company Self-contained holonomic tracking method and apparatus for non-destructive inspection
US10648668B2 (en) * 2013-07-19 2020-05-12 United Technologies Corporation Gas turbine engine ceramic component assembly and bonding material
JP6180221B2 (en) 2013-08-01 2017-08-16 オリンパス株式会社 Blade inspection device
US20150034266A1 (en) 2013-08-01 2015-02-05 Siemens Energy, Inc. Building and repair of hollow components
US10022921B2 (en) 2013-12-19 2018-07-17 General Electric Company Turbine component patch delivery systems and methods
US20170218762A1 (en) * 2016-02-03 2017-08-03 General Electric Company Situ Gas Turbine Prevention of Crack Growth Progression
US10247002B2 (en) * 2016-02-03 2019-04-02 General Electric Company In situ gas turbine prevention of crack growth progression

Also Published As

Publication number Publication date
CA2956905C (en) 2020-02-18
CN110925025B (en) 2022-08-09
EP3203019B1 (en) 2020-04-01
CA2956905A1 (en) 2017-08-03
EP3203019A1 (en) 2017-08-09
CN107060887B (en) 2019-11-26
US10094221B2 (en) 2018-10-09
CN110925025A (en) 2020-03-27
CN107060887A (en) 2017-08-18
US20170218764A1 (en) 2017-08-03

Similar Documents

Publication Publication Date Title
SG10201701642PA (en) In situ gas turbine prevention of crack growth progression
GB201406386D0 (en) Gas turbine engine
GB2530628B (en) Gas Turbine Engine and Method of operation
SG10201700347XA (en) In situ gas turbine prevention of crack growth progression via laser welding
SG10201700831PA (en) In situ gas turbine prevention of crack growth progression
GB201512900D0 (en) Gas turbine engine
GB201520623D0 (en) Gas turbine engine
GB201405704D0 (en) Gas turbine engine
GB201420175D0 (en) Gas turbine engine
GB201617374D0 (en) Gas turbine engine
GB2524320B (en) Gas turbine engine
GB2544554B (en) Gas turbine engine
GB2544553B (en) Gas Turbine Engine
GB201418396D0 (en) Gas turbine engine support structures
GB2524229B (en) Gas turbine engine
SG10201700345UA (en) In situ gas turbine prevention of crack growth progression
GB201401767D0 (en) Gas turbine engine
GB201416764D0 (en) Gas turbine engine
GB201416505D0 (en) Gas turbine engine
GB201810685D0 (en) Gas turbine engine
GB201521941D0 (en) Oil/gas burners and method
GB201512494D0 (en) Gas turbine engine
AP2016009155A0 (en) Gas liquefaction plant
GB201414071D0 (en) Gas turbine engine
SG10201700346TA (en) In situ gas turbine prevention of crack growth progression