ES459464A1 - Procedimiento para preparar una pieza de turbina de aleacionmetalica y forma aerodinamica. - Google Patents

Procedimiento para preparar una pieza de turbina de aleacionmetalica y forma aerodinamica.

Info

Publication number
ES459464A1
ES459464A1 ES459464A ES459464A ES459464A1 ES 459464 A1 ES459464 A1 ES 459464A1 ES 459464 A ES459464 A ES 459464A ES 459464 A ES459464 A ES 459464A ES 459464 A1 ES459464 A1 ES 459464A1
Authority
ES
Spain
Prior art keywords
vane
cracks
build
cool
excess
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
ES459464A
Other languages
English (en)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
CRETELLA SALVATORE
MATLHEW BERNADO Y RALPH THOMAS
Original Assignee
CRETELLA SALVATORE
MATLHEW BERNADO Y RALPH THOMAS
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 CRETELLA SALVATORE, MATLHEW BERNADO Y RALPH THOMAS filed Critical CRETELLA SALVATORE
Publication of ES459464A1 publication Critical patent/ES459464A1/es
Expired legal-status Critical Current

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
    • 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
    • B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/04—Making 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
    • 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
    • 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
    • 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
    • Y10T29/49746—Repairing by applying fluent material, e.g., coating, casting
    • 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
    • Y10T29/49748—Repairing by shaping, e.g., bending, extruding, turning, etc.
    • Y10T29/4975—Repairing by shaping, e.g., bending, extruding, turning, etc. including heating
    • 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
    • Y10T29/49805—Shaping by direct application of fluent pressure

Abstract

Procedimiento para reparar una pieza de turbina de aleación metálica y forma aerodinámica, que tiene una composición de cantidades sustancias de cobalto, con cantidades de silicio en un cierto porcentaje, caracterizado porque comprende las fases de mezclar un preparado de una aleación metálica de recrecimiento que comprende prácticamente la misma cantidad respectiva de cobalto que el contenido en la pieza de la turbina, habiendo presente silicio en cantidad prácticamente de un cierto porcentaje.
ES459464A 1976-06-07 1977-06-03 Procedimiento para preparar una pieza de turbina de aleacionmetalica y forma aerodinamica. Expired ES459464A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/693,640 US4050133A (en) 1976-06-07 1976-06-07 Method of refurbishing turbine vanes and the like

Publications (1)

Publication Number Publication Date
ES459464A1 true ES459464A1 (es) 1978-04-01

Family

ID=24785499

Family Applications (1)

Application Number Title Priority Date Filing Date
ES459464A Expired ES459464A1 (es) 1976-06-07 1977-06-03 Procedimiento para preparar una pieza de turbina de aleacionmetalica y forma aerodinamica.

Country Status (13)

Country Link
US (1) US4050133A (es)
JP (1) JPS5946302B2 (es)
AU (1) AU508087B2 (es)
BE (1) BE854759A (es)
CA (1) CA1079043A (es)
CH (1) CH620623A5 (es)
DE (1) DE2722263A1 (es)
ES (1) ES459464A1 (es)
FR (1) FR2354391A1 (es)
GB (1) GB1579950A (es)
IT (1) IT1081806B (es)
NL (1) NL7705409A (es)
SE (1) SE7705688L (es)

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US4155152A (en) * 1977-12-12 1979-05-22 Matthew Bernardo Method of restoring the shrouds of turbine blades
US4176433A (en) * 1978-06-29 1979-12-04 United Technologies Corporation Method of remanufacturing turbine vane clusters for gas turbine engines
US4334495A (en) * 1978-07-11 1982-06-15 Trw Inc. Method and apparatus for use in making an object
US4309848A (en) * 1980-02-25 1982-01-12 United Technologies Corporation Turbine blade tip finishing apparatus
US4307280A (en) * 1980-06-06 1981-12-22 Westinghouse Electric Corp. Method for filling internal casting voids
US4370789A (en) * 1981-03-20 1983-02-01 Schilke Peter W Fabrication of gas turbine water-cooled composite nozzle and bucket hardware employing plasma spray process
GB2107628B (en) * 1981-10-17 1985-08-21 Rolls Royce Improvements in or relating to filling fissures in metal articles
US4402992A (en) * 1981-12-07 1983-09-06 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Covering solid, film cooled surfaces with a duplex thermal barrier coating
GB2154614B (en) * 1984-02-22 1987-11-18 H I P Densified coatings by application of direct fluid pressure
US4562332A (en) * 1984-03-26 1985-12-31 Rockwell International Corporation Surface crack healing with high-energy beam
FR2564350B1 (fr) * 1984-05-17 1987-11-20 Snecma Procede de reparation par diffusion
US4837389A (en) * 1984-06-04 1989-06-06 Turbine Components Corporation Composite alloy structures
US4743462A (en) * 1986-07-14 1988-05-10 United Technologies Corporation Method for preventing closure of cooling holes in hollow, air cooled turbine engine components during application of a plasma spray coating
US4726101A (en) * 1986-09-25 1988-02-23 United Technologies Corporation Turbine vane nozzle reclassification
US4726104A (en) * 1986-11-20 1988-02-23 United Technologies Corporation Methods for weld repairing hollow, air cooled turbine blades and vanes
US4808055A (en) * 1987-04-15 1989-02-28 Metallurgical Industries, Inc. Turbine blade with restored tip
US4878953A (en) * 1988-01-13 1989-11-07 Metallurgical Industries, Inc. Method of refurbishing cast gas turbine engine components and refurbished component
GB2227191B (en) * 1988-09-16 1993-03-03 Refurbished Turbine Components Turbine blade repair
US4893388A (en) * 1988-12-08 1990-01-16 Westinghouse Electric Corp. Method of modifying turbine rotor discs
US5004722A (en) * 1989-01-19 1991-04-02 International Superconductor Corp. Method of making superconductor wires by hot isostatic pressing after bending
US5232789A (en) * 1989-03-09 1993-08-03 Mtu Motoren- Und Turbinen-Union Muenchen Gmbh Structural component with a protective coating having a nickel or cobalt basis and method for making such a coating
GB8929005D0 (en) * 1989-12-22 1990-02-28 Refurbished Turbine Components Turbine blade repair
GB2244943B (en) * 1990-06-12 1994-03-30 Turbine Blading Ltd Method of repair of turbines
GB2264446A (en) * 1992-02-27 1993-09-01 Turbine Blading Ltd Turbine blade repair
US5584662A (en) * 1995-03-06 1996-12-17 General Electric Company Laser shock peening for gas turbine engine vane repair
US6454156B1 (en) * 2000-06-23 2002-09-24 Siemens Westinghouse Power Corporation Method for closing core printout holes in superalloy gas turbine blades
US6606541B2 (en) * 2001-04-30 2003-08-12 United Technologies Corporation Automated system for repairing components
EP1371812A1 (de) * 2002-06-04 2003-12-17 ALSTOM (Switzerland) Ltd Verfahren zum Reparieren von beschädigten Laufschaufeln des Turbinenteils einer Gasturbine
US7097425B2 (en) * 2003-08-08 2006-08-29 United Technologies Corporation Microcircuit cooling for a turbine airfoil
US6905728B1 (en) 2004-03-22 2005-06-14 Honeywell International, Inc. Cold gas-dynamic spray repair on gas turbine engine components
US20050220995A1 (en) * 2004-04-06 2005-10-06 Yiping Hu Cold gas-dynamic spraying of wear resistant alloys on turbine blades
DE102004036066A1 (de) * 2004-07-24 2006-02-16 Mtu Aero Engines Gmbh Verfahren zum Reparieren bzw. Fertigen eines Bauteils
US8844090B2 (en) * 2005-06-17 2014-09-30 United Technologies Corporation Tool for filling voids in turbine vanes and other articles
US20080145688A1 (en) 2006-12-13 2008-06-19 H.C. Starck Inc. Method of joining tantalum clade steel structures
US8197894B2 (en) 2007-05-04 2012-06-12 H.C. Starck Gmbh Methods of forming sputtering targets
US8220150B2 (en) * 2007-05-22 2012-07-17 United Technologies Corporation Split vane cluster repair method
US20090274562A1 (en) * 2008-05-02 2009-11-05 United Technologies Corporation Coated turbine-stage nozzle segments
US8246903B2 (en) 2008-09-09 2012-08-21 H.C. Starck Inc. Dynamic dehydriding of refractory metal powders
US9630277B2 (en) * 2010-03-15 2017-04-25 Siemens Energy, Inc. Airfoil having built-up surface with embedded cooling passage
US8460760B2 (en) 2010-11-30 2013-06-11 United Technologies Corporation Coating a perforated surface
CN102251904B (zh) * 2011-06-13 2013-01-30 深圳市百安百科技有限公司 一种水轮机抗气蚀节能改造方法
US9412568B2 (en) 2011-09-29 2016-08-09 H.C. Starck, Inc. Large-area sputtering targets
US10100650B2 (en) * 2012-06-30 2018-10-16 General Electric Company Process for selectively producing thermal barrier coatings on turbine hardware
US9631517B2 (en) 2012-12-29 2017-04-25 United Technologies Corporation Multi-piece fairing for monolithic turbine exhaust case
US10309002B2 (en) * 2013-12-05 2019-06-04 General Electric Company Coating methods and a template for use with the coating methods
CN104858607A (zh) * 2015-04-24 2015-08-26 湘潭杰熙环境科技有限责任公司 脱硫循环泵泵壳的全修复工艺
JP6550000B2 (ja) * 2016-02-26 2019-07-24 三菱日立パワーシステムズ株式会社 タービン翼

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1914774A (en) * 1931-06-10 1933-06-20 Indian Refining Co Method of coating vessels
US2120525A (en) * 1937-06-01 1938-06-14 Thomas J Mckerihan Method of building up pitted holes in a metal sheet
US2575656A (en) * 1948-11-26 1951-11-20 Jr Harry D Coe Means for finishing workpieces of irregular shapes
US2878140A (en) * 1957-05-01 1959-03-17 Vitro Corp Of America Densification of coating by use of isostatic hydraulic pressure
GB838839A (en) * 1957-10-15 1960-06-22 Cincinnati Milling Machine Co Method of manufacturing bushing type spool valves
US3015880A (en) * 1957-11-12 1962-01-09 Power Jets Res & Dev Ltd Corrosion resistant treatment of metal articles
US3576065A (en) * 1969-03-24 1971-04-27 Chromalloy American Corp Repair of apertured machine components
US3650635A (en) * 1970-03-09 1972-03-21 Chromalloy American Corp Turbine vanes

Also Published As

Publication number Publication date
FR2354391B3 (es) 1980-03-07
FR2354391A1 (fr) 1978-01-06
AU508087B2 (en) 1980-03-06
US4050133A (en) 1977-09-27
SE7705688L (sv) 1977-12-08
IT1081806B (it) 1985-05-21
GB1579950A (en) 1980-11-26
BE854759A (fr) 1977-09-16
JPS52155141A (en) 1977-12-23
CA1079043A (en) 1980-06-10
JPS5946302B2 (ja) 1984-11-12
CH620623A5 (es) 1980-12-15
AU2484677A (en) 1978-11-09
NL7705409A (nl) 1977-12-09
DE2722263A1 (de) 1977-12-15

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