ES475940A1 - Procedimiento para reparar alabes de turbinas desgastados. - Google Patents

Procedimiento para reparar alabes de turbinas desgastados.

Info

Publication number
ES475940A1
ES475940A1 ES475940A ES475940A ES475940A1 ES 475940 A1 ES475940 A1 ES 475940A1 ES 475940 A ES475940 A ES 475940A ES 475940 A ES475940 A ES 475940A ES 475940 A1 ES475940 A1 ES 475940A1
Authority
ES
Spain
Prior art keywords
blade
shroud
edge
notch
restoring
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
ES475940A
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
Original Assignee
CRETELLA SALVATORE
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 filed Critical CRETELLA SALVATORE
Publication of ES475940A1 publication Critical patent/ES475940A1/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
    • 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
    • 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
    • F01D5/12—Blades
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
    • 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
    • Y10T29/49318—Repairing or disassembling
    • 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
    • Y10T29/4998—Combined manufacture including applying or shaping of fluent material
    • Y10T29/49982—Coating
    • Y10T29/49986—Subsequent to metal working

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Powder Metallurgy (AREA)

Abstract

Procedimiento para reparar álabes de turbinas desgastados, cuyos álabes son de una aleación metálica, que comprende las fases de rectificar hasta una dimensión predeterminada con precisión, un borde de la parte de escotadura en Z del refuerzo de montaje en un extremo del álabe, enmascarar el refuerzo en ambos lados del borde después de rectificado; someter el borde rectificado a una corriente de plasma que contiene una aleación metálica para recrecer el borde prácticamente a su dimensión original, y después sinterizar el álabe a temperaturas elevadas durante un periodo de tiempo predeterminado para templar la reparación.
ES475940A 1977-12-12 1978-12-12 Procedimiento para reparar alabes de turbinas desgastados. Expired ES475940A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/859,438 US4155152A (en) 1977-12-12 1977-12-12 Method of restoring the shrouds of turbine blades

Publications (1)

Publication Number Publication Date
ES475940A1 true ES475940A1 (es) 1979-05-01

Family

ID=25330926

Family Applications (1)

Application Number Title Priority Date Filing Date
ES475940A Expired ES475940A1 (es) 1977-12-12 1978-12-12 Procedimiento para reparar alabes de turbinas desgastados.

Country Status (13)

Country Link
US (1) US4155152A (es)
JP (1) JPS5493657A (es)
AU (1) AU531630B2 (es)
BE (1) BE872693A (es)
CA (1) CA1119896A (es)
CH (1) CH628559A5 (es)
DE (1) DE2853545A1 (es)
ES (1) ES475940A1 (es)
FR (1) FR2411063A1 (es)
GB (1) GB2009635B (es)
IT (1) IT1100539B (es)
NL (1) NL7812087A (es)
SE (1) SE436173B (es)

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US4291448A (en) * 1977-12-12 1981-09-29 Turbine Components Corporation Method of restoring the shrouds of turbine blades
AU546843B2 (en) * 1981-01-12 1985-09-26 Refurbished Turbine Components Limited Turbine blade repair
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
JPS59131703A (ja) * 1983-01-18 1984-07-28 Toshiba Corp 蒸気タ−ビン動翼の補修方法
JPH0660563B2 (ja) * 1984-08-02 1994-08-10 株式会社東芝 動翼カバ−
US4822248A (en) * 1987-04-15 1989-04-18 Metallurgical Industries, Inc. Rebuilt shrouded turbine blade and method of rebuilding the same
DE3802741C2 (de) * 1988-01-30 1997-02-13 Asea Brown Boveri Verfahren zur Verspannung von Schaufeln
AU605378B2 (en) * 1988-11-01 1991-01-10 Sermatech International, Inc. Shrouded turbine blade
US5272809A (en) * 1990-09-04 1993-12-28 United Technologies Corporation Technique for direct bonding cast and wrought materials
GB2251034B (en) * 1990-12-20 1995-05-17 Rolls Royce Plc Shrouded aerofoils
US5140737A (en) * 1991-01-10 1992-08-25 Noland Edmund B In situ flywheel repair method
US5146679A (en) * 1991-01-16 1992-09-15 Ortolano Ralph J Method of converting grouped blading to equivalent integral covered blading
US5238368A (en) * 1991-01-16 1993-08-24 Ortolano Ralph J Converting grouped blading to equivalent integral covered blading
DE4237052A1 (de) * 1992-11-03 1994-05-05 Mtu Muenchen Gmbh Vorrichtung zur Reparaturschweißung der Blattspitzen von Leit- oder Laufschaufeln für Turbomaschinen
DE4310896C1 (de) * 1993-04-02 1994-03-24 Thyssen Industrie Verfahren zum Herstellen von verschleißfesten Kanten an Turbinenschaufeln
US5525429A (en) * 1995-03-06 1996-06-11 General Electric Company Laser shock peening surface enhancement for gas turbine engine high strength rotor alloy repair
US5735044A (en) * 1995-12-12 1998-04-07 General Electric Company Laser shock peening for gas turbine engine weld repair
JP3178327B2 (ja) * 1996-01-31 2001-06-18 株式会社日立製作所 蒸気タービン
US6037004A (en) * 1997-12-19 2000-03-14 United Technologies Corporation Shield and method for protecting an airfoil surface
SG80000A1 (en) * 1997-12-19 2001-04-17 United Technologies Corp A fixture for use in disposing a region of material on the shroud of a rotor blade
US6034344A (en) * 1997-12-19 2000-03-07 United Technologies Corp. Method for applying material to a face of a flow directing assembly for a gas turbine engine
US5916638A (en) * 1997-12-19 1999-06-29 United Technologies Corporation Method for applying a coating to the tip of a flow directing assembly
US6233822B1 (en) * 1998-12-22 2001-05-22 General Electric Company Repair of high pressure turbine shrouds
EP1143030A1 (en) 2000-04-03 2001-10-10 ABB Alstom Power N.V. Tip material for a turbine blade and method of manufacturing or repairing a tip of a turbine blade
US6363612B1 (en) * 2000-12-27 2002-04-02 General Electric Company Method of reducing burr formation during turbine bucket cover machining
GB0112876D0 (en) 2001-05-26 2001-07-18 Rolls Royce Plc A method of manufacturing an article
JP4028442B2 (ja) * 2002-06-26 2007-12-26 株式会社東芝 ガスタービン翼の変形修正装置及び方法
US6875476B2 (en) 2003-01-15 2005-04-05 General Electric Company Methods and apparatus for manufacturing turbine engine components
US7009137B2 (en) 2003-03-27 2006-03-07 Honeywell International, Inc. Laser powder fusion repair of Z-notches with nickel based superalloy powder
FR2860741B1 (fr) * 2003-10-10 2007-04-13 Snecma Moteurs Procede de reparation de pieces metalliques notamment d'aubes de turbine de moteur a turbine a gaz
US8205334B2 (en) * 2005-07-15 2012-06-26 United Technologies Corporation Method for repairing a gas turbine engine component
US20070141261A1 (en) * 2005-12-20 2007-06-21 General Electric Company Method and apparatus for fabricating turbine engine components
US8703044B2 (en) * 2006-01-03 2014-04-22 General Electric Company Machine components and methods of fabricating and repairing
US7653994B2 (en) * 2006-03-22 2010-02-02 General Electric Company Repair of HPT shrouds with sintered preforms
EP2213837A1 (en) * 2009-01-29 2010-08-04 Siemens Aktiengesellschaft Turbine blade system
US8277189B2 (en) * 2009-11-12 2012-10-02 General Electric Company Turbine blade and rotor
US8708655B2 (en) 2010-09-24 2014-04-29 United Technologies Corporation Blade for a gas turbine engine
US9810069B2 (en) 2012-07-02 2017-11-07 Ansaldo Energia Switzerland AG Repair of a shrouded blade
US9863249B2 (en) 2012-12-04 2018-01-09 Siemens Energy, Inc. Pre-sintered preform repair of turbine blades
FR3001758B1 (fr) * 2013-02-01 2016-07-15 Snecma Aube de rotor de turbomachine
RU2542035C2 (ru) * 2013-03-22 2015-02-20 Александр Александрович Макушин Способ ремонта цилиндропоршневой группы двигателей внутреннего сгорания
RU2533236C1 (ru) * 2013-08-15 2014-11-20 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Саратовский государственный аграрный университет имени Н.И. Вавилова" Способ восстановления изношенного крестового ножа
DE102016207863A1 (de) * 2016-05-09 2017-11-09 MTU Aero Engines AG Verfahren zum Bearbeiten wenigstens eines Bauteilbereichs eines Bauteils und Maskierungselement zum partiellen Abdecken eines zu bearbeitenden Bauteils
CN106862789A (zh) * 2017-03-03 2017-06-20 贵州凯阳航空发动机有限公司 K4208合金在低压涡轮转子叶片叶冠耐磨合金焊接的应用
CN108326510A (zh) * 2018-03-02 2018-07-27 河钢股份有限公司承德分公司 离心风机叶轮修复结构及修复方法
FR3079847B1 (fr) * 2018-04-10 2023-11-10 Safran Aircraft Engines Procede de fabrication d'un element aubage metallique d'une turbomachine d'aeronef

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US3436512A (en) * 1966-04-13 1969-04-01 Coast Metals Inc Method of spray coating gas seals of gas turbines and the like
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US3814447A (en) * 1972-11-02 1974-06-04 Ramsey Corp Sealing element for use in internal combustion engines
US3981688A (en) * 1973-07-05 1976-09-21 Ford Motor Company Coating for rotary engine rotor housings and method of making
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US4050133A (en) * 1976-06-07 1977-09-27 Cretella Salvatore Method of refurbishing turbine vanes and the like

Also Published As

Publication number Publication date
US4155152A (en) 1979-05-22
IT1100539B (it) 1985-09-28
AU4241178A (en) 1979-06-21
CA1119896A (en) 1982-03-16
SE436173B (sv) 1984-11-19
CH628559A5 (fr) 1982-03-15
DE2853545A1 (de) 1979-06-13
SE7812706L (sv) 1979-06-13
FR2411063A1 (fr) 1979-07-06
GB2009635B (en) 1982-03-17
BE872693A (fr) 1979-03-30
JPS5493657A (en) 1979-07-24
GB2009635A (en) 1979-06-20
NL7812087A (nl) 1979-06-14
IT7830745A0 (it) 1978-12-12
AU531630B2 (en) 1983-09-01
FR2411063B1 (es) 1984-02-17

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 19991007