SG139615A1 - Pre-coating burnishing of erosion coated parts - Google Patents

Pre-coating burnishing of erosion coated parts

Info

Publication number
SG139615A1
SG139615A1 SG200702556-2A SG2007025562A SG139615A1 SG 139615 A1 SG139615 A1 SG 139615A1 SG 2007025562 A SG2007025562 A SG 2007025562A SG 139615 A1 SG139615 A1 SG 139615A1
Authority
SG
Singapore
Prior art keywords
platform
coating
airfoil
coated parts
burnishing
Prior art date
Application number
SG200702556-2A
Other languages
English (en)
Inventor
David A Rutz
Monika D Kinstler
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 SG139615A1 publication Critical patent/SG139615A1/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P9/00Treating or finishing surfaces mechanically, with or without calibrating, primarily to resist wear or impact, e.g. smoothing or roughening turbine blades or bearings; Features of such surfaces not otherwise provided for, their treatment being unspecified
    • B23P9/02Treating or finishing by applying pressure, e.g. knurling
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/02Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from one piece
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/04Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from several pieces
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D7/00Modifying the physical properties of iron or steel by deformation
    • C21D7/02Modifying the physical properties of iron or steel by deformation by cold working
    • C21D7/04Modifying the physical properties of iron or steel by deformation by cold working of the surface
    • C21D7/08Modifying the physical properties of iron or steel by deformation by cold working of the surface by burnishing or the like
    • 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
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/286Particular treatment of blades, e.g. to increase durability or resistance against corrosion or erosion
    • 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
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288Protective coatings for blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/02Selection of particular materials
    • F04D29/023Selection of particular materials especially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • F04D29/324Blades
    • 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
    • F05D2230/90Coating; Surface treatment
    • 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
    • F05D2240/00Components
    • F05D2240/10Stators
    • F05D2240/12Fluid guiding means, e.g. vanes
    • F05D2240/121Fluid guiding means, e.g. vanes related to the leading edge of a stator vane
    • 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
    • F05D2240/00Components
    • F05D2240/20Rotors
    • F05D2240/30Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/303Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the leading edge of a rotor blade
    • 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
    • F05D2300/00Materials; Properties thereof
    • F05D2300/20Oxide or non-oxide ceramics
    • F05D2300/22Non-oxide ceramics
    • F05D2300/226Carbides
    • 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
    • F05D2300/00Materials; Properties thereof
    • F05D2300/60Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/611Coating
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Physical Vapour Deposition (AREA)
  • Coating By Spraying Or Casting (AREA)
SG200702556-2A 2006-08-03 2007-04-05 Pre-coating burnishing of erosion coated parts SG139615A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US49916306A 2006-08-03 2006-08-03

Publications (1)

Publication Number Publication Date
SG139615A1 true SG139615A1 (en) 2008-02-29

Family

ID=39030947

Family Applications (1)

Application Number Title Priority Date Filing Date
SG200702556-2A SG139615A1 (en) 2006-08-03 2007-04-05 Pre-coating burnishing of erosion coated parts

Country Status (8)

Country Link
US (1) US8221841B2 (ru)
EP (1) EP1862643B1 (ru)
JP (1) JP2008038896A (ru)
KR (1) KR20080012744A (ru)
CN (1) CN101117898A (ru)
CA (1) CA2590496A1 (ru)
RU (1) RU2007120712A (ru)
SG (1) SG139615A1 (ru)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8065898B2 (en) 2008-07-29 2011-11-29 Hamilton Sundstrand Corporation Method and article for improved adhesion of fatigue-prone components
DE102011007224A1 (de) * 2011-04-12 2012-10-18 Rolls-Royce Deutschland Ltd & Co Kg Verfahren und Herstellung eines einstückigen Rotorbereiches und einstückiger Rotorbereich
US8906181B2 (en) * 2011-06-30 2014-12-09 United Technologies Corporation Fan blade finishing
US9404172B2 (en) 2012-02-22 2016-08-02 Sikorsky Aircraft Corporation Erosion and fatigue resistant blade and blade coating
DE102012018604A1 (de) 2012-09-20 2014-03-20 Rolls-Royce Deutschland Ltd & Co Kg Walzwerkzeugvorrichtung
DE102012018605A1 (de) 2012-09-20 2014-03-20 Rolls-Royce Deutschland Ltd & Co Kg Walzwerkzeugvorrichtung
US20150107072A1 (en) * 2013-10-22 2015-04-23 Kazim Ozbaysal Fatigue resistant turbine through bolt
JP6246666B2 (ja) 2014-06-11 2017-12-13 日本発條株式会社 積層体の製造方法

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3689311A (en) 1970-11-06 1972-09-05 Ler Son Co Inc Method for external coating of cylindrical objects
US4585395A (en) 1983-12-12 1986-04-29 General Electric Company Gas turbine engine blade
EP0188057A1 (en) * 1984-11-19 1986-07-23 Avco Corporation Erosion resistant coatings
US4904528A (en) * 1987-12-24 1990-02-27 United Technologies Corporation Coated gas turbine engine compressor components
US5476363A (en) 1993-10-15 1995-12-19 Charles E. Sohl Method and apparatus for reducing stress on the tips of turbine or compressor blades
US6095755A (en) * 1996-11-26 2000-08-01 United Technologies Corporation Gas turbine engine airfoils having increased fatigue strength
US5826453A (en) 1996-12-05 1998-10-27 Lambda Research, Inc. Burnishing method and apparatus for providing a layer of compressive residual stress in the surface of a workpiece
CN2371342Y (zh) 1999-06-04 2000-03-29 中国科学院金属研究所 一种抗腐蚀疲劳汽轮机叶轮
US6415486B1 (en) * 2000-03-01 2002-07-09 Surface Technology Holdings, Ltd. Method and apparatus for providing a residual stress distribution in the surface of a part
US6672838B1 (en) * 2000-07-27 2004-01-06 General Electric Company Method for making a metallic article with integral end band under compression
US6465040B2 (en) * 2001-02-06 2002-10-15 General Electric Company Method for refurbishing a coating including a thermally grown oxide
US7188398B2 (en) * 2004-01-17 2007-03-13 Surface Technology Holdings, Ltd. Method for improving the magnitude of compressive stress developed in the surface of a part
US20050158460A1 (en) * 2004-01-21 2005-07-21 Williams Christopher C. Method for protecting new/used engine parts
US7229253B2 (en) * 2004-11-30 2007-06-12 General Electric Company Fatigue-resistant components and method therefor

Also Published As

Publication number Publication date
KR20080012744A (ko) 2008-02-12
EP1862643A2 (en) 2007-12-05
US20100119375A1 (en) 2010-05-13
JP2008038896A (ja) 2008-02-21
CA2590496A1 (en) 2008-02-03
CN101117898A (zh) 2008-02-06
RU2007120712A (ru) 2008-12-10
EP1862643B1 (en) 2015-07-15
US8221841B2 (en) 2012-07-17
EP1862643A3 (en) 2010-12-29

Similar Documents

Publication Publication Date Title
SG139615A1 (en) Pre-coating burnishing of erosion coated parts
DK201170633A (en) Erosion protection coating for rotor blade of wind turbine
WO2008090394A3 (en) Second stage turbine airfoil
EP1693552A3 (en) A turbine blade
EP1813776A3 (en) Microcircuits for cooling of small turbine engine blades
TW200728592A (en) Microcircuit cooling with an aspect ratio of unity
EP1645721A3 (en) Gas turbine airfoil with leading edge cooling
TW200720529A (en) Microcircuit cooling for vanes
AU2003300242A1 (en) Cambered vane for use in turbochargers
ATE441739T1 (de) Auftragen einer haftbeschichtung auf motorbauteile mittels eines kaltsprühverfahrens
JP2010038156A (ja) 圧縮機ブレード前縁シム及び関連する方法
EP2148042A3 (en) A blade for a rotor having a squealer tip with a partly inclined surface
ATE475725T1 (de) Beschichtungen für turbinenlaufschaufeln
WO2007075497A3 (en) Method and coating for protecting and repairing an airfoil surface
EP1760266A3 (en) Turbine Vane Construction
EP1507018A8 (en) Method of pre-treating the surface of a gas turbine component to be coated
WO2012112613A3 (en) Turbine blades, systems and methods
SG134183A1 (en) Turbine component trailing edge and platform restoration by laser cladding
EP4234947A3 (en) Total camber distribution for a rotor and rotor blade having camber and location of local maximum thickness distribution
WO2010121597A3 (de) Verfahren zur herstellung einer panzerung einer schaufespitze gasturbinenschaufel
EP2182092A3 (en) A method of repairing an aluminide coating on an article
US9945232B2 (en) Gas turbine blade configuration
CA3081501A1 (en) Water droplet erosion resistant coatings for turbine blades and other components
WO2005074469A3 (en) Mitigation of unsteady peak fan blade and disc stresses in turbofan engines
WO2009006871A3 (de) Turbomaschinenschaufel mit verschleissschutzschicht