BRPI0701724A - dispositivo de recuperação de um aerofólio de turbina de alta pressão e método de tratamento térmico - Google Patents

dispositivo de recuperação de um aerofólio de turbina de alta pressão e método de tratamento térmico

Info

Publication number
BRPI0701724A
BRPI0701724A BRPI0701724-3A BRPI0701724A BRPI0701724A BR PI0701724 A BRPI0701724 A BR PI0701724A BR PI0701724 A BRPI0701724 A BR PI0701724A BR PI0701724 A BRPI0701724 A BR PI0701724A
Authority
BR
Brazil
Prior art keywords
article
support
heat
high pressure
recovery device
Prior art date
Application number
BRPI0701724-3A
Other languages
English (en)
Portuguese (pt)
Inventor
Thomas J Kelly
Warren D Grossklaus Jr
Brent R Tholke
Christine Govern Walston
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 BRPI0701724A publication Critical patent/BRPI0701724A/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
    • B23P6/007—Repairing turbine components, e.g. moving or stationary blades, rotors using only additive methods, e.g. build-up welding
    • C—CHEMISTRY; METALLURGY
    • C21—METALLURGY OF IRON
    • C21D—MODIFYING 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
    • C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/0068—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for particular articles not mentioned below
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/10—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of nickel or cobalt or alloys based thereon
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/005—Repairing methods or devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/40—Heat treatment
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/80—Repairing, retrofitting or upgrading methods
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Heat Treatment Of Articles (AREA)
BRPI0701724-3A 2006-05-17 2007-05-16 dispositivo de recuperação de um aerofólio de turbina de alta pressão e método de tratamento térmico BRPI0701724A (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/383,783 US20070267109A1 (en) 2006-05-17 2006-05-17 High pressure turbine airfoil recovery device and method of heat treatment

Publications (1)

Publication Number Publication Date
BRPI0701724A true BRPI0701724A (pt) 2008-01-15

Family

ID=38420608

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0701724-3A BRPI0701724A (pt) 2006-05-17 2007-05-16 dispositivo de recuperação de um aerofólio de turbina de alta pressão e método de tratamento térmico

Country Status (6)

Country Link
US (2) US20070267109A1 (enExample)
EP (1) EP1857217B1 (enExample)
JP (1) JP5350603B2 (enExample)
BR (1) BRPI0701724A (enExample)
CA (1) CA2587311C (enExample)
SG (3) SG137786A1 (enExample)

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US9797253B2 (en) * 2014-09-17 2017-10-24 General Electric Company System and method for repairing blades
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JP6754682B2 (ja) 2016-11-28 2020-09-16 三菱日立パワーシステムズ株式会社 ニッケル基合金再生部材の製造方法
US20180238173A1 (en) * 2017-02-22 2018-08-23 General Electric Company Method of manufacturing turbine airfoil and tip component thereof
US10625342B2 (en) 2017-02-22 2020-04-21 General Electric Company Method of repairing turbine component
US10717130B2 (en) 2017-02-22 2020-07-21 General Electric Company Method of manufacturing turbine airfoil and tip component thereof
US11154956B2 (en) 2017-02-22 2021-10-26 General Electric Company Method of repairing turbine component using ultra-thin plate
US10610933B2 (en) 2017-02-22 2020-04-07 General Electric Company Method of manufacturing turbine airfoil with open tip casting and tip component thereof
US10702958B2 (en) 2017-02-22 2020-07-07 General Electric Company Method of manufacturing turbine airfoil and tip component thereof using ceramic core with witness feature
US11371349B2 (en) 2019-04-05 2022-06-28 Raytheon Technologies Corporation Gas impingement in-process cooling system
US11242588B2 (en) * 2019-12-12 2022-02-08 General Electric Company System and method to apply multiple thermal treatments to workpiece and related turbomachine components
US11199101B2 (en) 2019-12-12 2021-12-14 General Electric Company System and method to apply multiple thermal treatments to workpiece and related turbomachine components
CN111575671B (zh) * 2020-06-12 2022-03-29 中国人民解放军空军工程大学 用于叶片表面选区制备涂层的夹具及涂层的制备方法
KR102252487B1 (ko) * 2020-12-07 2021-05-14 한전케이피에스 주식회사 가스터빈 회전익 코팅용 지그
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Also Published As

Publication number Publication date
US20090314393A1 (en) 2009-12-24
SG157392A1 (en) 2009-12-29
EP1857217A1 (en) 2007-11-21
CA2587311C (en) 2015-06-30
JP2007308798A (ja) 2007-11-29
CA2587311A1 (en) 2007-11-17
SG137786A1 (en) 2007-12-28
SG190599A1 (en) 2013-06-28
US7875135B2 (en) 2011-01-25
EP1857217B1 (en) 2018-01-17
JP5350603B2 (ja) 2013-11-27
US20070267109A1 (en) 2007-11-22

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B11D Dismissal acc. art. 38, par 2 of ipl - failure to pay fee after grant in time