ES2099596T3 - METHOD FOR PRODUCING AN ABRASIVE EDGE ON A TURBINE WING. - Google Patents

METHOD FOR PRODUCING AN ABRASIVE EDGE ON A TURBINE WING.

Info

Publication number
ES2099596T3
ES2099596T3 ES94907629T ES94907629T ES2099596T3 ES 2099596 T3 ES2099596 T3 ES 2099596T3 ES 94907629 T ES94907629 T ES 94907629T ES 94907629 T ES94907629 T ES 94907629T ES 2099596 T3 ES2099596 T3 ES 2099596T3
Authority
ES
Spain
Prior art keywords
producing
deposition
pallets
assembly
turbine wing
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 - Lifetime
Application number
ES94907629T
Other languages
Spanish (es)
Inventor
John Foster
Alan Taylor
Martin Patrick Chatterley
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.)
Praxair ST Technology Inc
Praxair Technology Inc
Original Assignee
Praxair ST Technology Inc
Praxair Technology Inc
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 Praxair ST Technology Inc, Praxair Technology Inc filed Critical Praxair ST Technology Inc
Application granted granted Critical
Publication of ES2099596T3 publication Critical patent/ES2099596T3/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Electroplating Methods And Accessories (AREA)
  • Finish Polishing, Edge Sharpening, And Grinding By Specific Grinding Devices (AREA)
  • Grinding And Polishing Of Tertiary Curved Surfaces And Surfaces With Complex Shapes (AREA)
  • Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
  • Chemically Coating (AREA)

Abstract

UN METODO PARA PRODUCIR PUNTAS ABRASIVAS EN PALETAS DE ROTOR DE COMPRESORES O TURBINAS MEDIANTE DEPOSICION ELECTROLITICA O SIN ELECTRICIDAD EN EL CUAL AL MENOS PARTE DEL PROCESO DE DEPOSICION SE LLEVA A CABO EN LAS PALETAS ENSAMBLADAS EN UN DISCO ROTOR DE COMPRESOR O TURBINA. LAS PUNTAS SE FORMAN POR TANTO EN LAS PALETAS DESPUES DE PONERLAS EN SUS POSICIONES DE FUNCIONAMIENTO FINALES EN EL DISCO PARA QUE EL DESENSAMBLAJE SUBSECUENTE QUE HA SIDO NECESARIO HASTA ESTOS MOMENTOS SE EVITE. EL ENSAMBLAJE ESTA MONTADO PREFERIBLEMENTE CON SU EJE DE ROTACION HORIZONTAL Y LA DEPOSICION PUEDE ESTAR ACOMPAÑADA POR LA VIBRACION DEL ENSAMBLAJE EN DIRECCION VERTICAL.A METHOD FOR PRODUCING ABRASIVE TIPS ON COMPRESSOR OR TURBINE ROTOR PALLETS THROUGH ELECTROLYTIC OR NO ELECTRICITY DEPOSITION WHICH IS AT LEAST PART OF THE DEPOSITION PROCESS CARRIED OUT ON COMPRESSOR ROTOR PADS. THE TIPS ARE THEREFORE FORMED ON THE PALLETS AFTER PUTTING THEM IN THEIR FINAL OPERATING POSITIONS ON THE DISC SO THAT SUBSEQUENT DISASSEMBLY THAT HAS BEEN NECESSARY UNTIL THESE MOMENTS IS AVOIDED. THE ASSEMBLY IS PREFERABLY MOUNTED WITH ITS HORIZONTAL ROTATION AXIS AND THE DEPOSITION MAY BE ACCOMPANIED BY THE VIBRATION OF THE ASSEMBLY IN A VERTICAL DIRECTION.

ES94907629T 1993-02-25 1994-02-25 METHOD FOR PRODUCING AN ABRASIVE EDGE ON A TURBINE WING. Expired - Lifetime ES2099596T3 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB939303853A GB9303853D0 (en) 1993-02-25 1993-02-25 Rotor blades

Publications (1)

Publication Number Publication Date
ES2099596T3 true ES2099596T3 (en) 1997-05-16

Family

ID=10731055

Family Applications (1)

Application Number Title Priority Date Filing Date
ES94907629T Expired - Lifetime ES2099596T3 (en) 1993-02-25 1994-02-25 METHOD FOR PRODUCING AN ABRASIVE EDGE ON A TURBINE WING.

Country Status (10)

Country Link
EP (1) EP0686229B1 (en)
JP (1) JPH08506872A (en)
AU (1) AU684263B2 (en)
CA (1) CA2153899A1 (en)
DE (1) DE69402305T2 (en)
ES (1) ES2099596T3 (en)
GB (1) GB9303853D0 (en)
RU (1) RU2118717C1 (en)
SG (1) SG47413A1 (en)
WO (1) WO1994019583A1 (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9326082D0 (en) * 1993-12-21 1994-02-23 Baj Coatings Ltd Rotor blades
US5935407A (en) * 1997-11-06 1999-08-10 Chromalloy Gas Turbine Corporation Method for producing abrasive tips for gas turbine blades
JP2002256808A (en) 2001-02-28 2002-09-11 Mitsubishi Heavy Ind Ltd Combustion engine, gas turbine and polishing layer
JP3801452B2 (en) 2001-02-28 2006-07-26 三菱重工業株式会社 Abrasion resistant coating and its construction method
JP3902179B2 (en) 2001-05-31 2007-04-04 三菱重工業株式会社 Film forming method, film forming material, and abrasive film forming sheet
JP2002371803A (en) * 2001-06-13 2002-12-26 Mitsubishi Heavy Ind Ltd Method of forming wear-resistant layer for rotor blade, wear-resistant layer, and method of regenerating the same
JP2003148103A (en) * 2001-11-09 2003-05-21 Mitsubishi Heavy Ind Ltd Turbine and method of manufacturing the same
DE10251902B4 (en) * 2002-11-07 2009-05-07 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Process for coating a substrate and coated article
FR2915495B1 (en) * 2007-04-30 2010-09-03 Snecma PROCESS FOR REPAIRING A TURBOMACHINE MOBILE DARK
DE102009007666A1 (en) * 2009-02-05 2010-08-12 Mtu Aero Engines Gmbh Method for producing a wear-resistant coating on a component
US9957629B2 (en) 2014-08-27 2018-05-01 Praxair S.T. Technology, Inc. Electroplated coatings
DE102015213555A1 (en) 2015-07-20 2017-03-09 MTU Aero Engines AG Sealing ridge armor and method of making the same
CN116121831A (en) * 2022-12-13 2023-05-16 中国科学院金属研究所 cBN ceramic particle/aluminide composite coating and preparation method thereof

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4279706A (en) * 1980-03-27 1981-07-21 Alsthom-Atlantique Method and assembly for depositing a metal on a cylindrical bore which passes through a central portion of a large part
FR2563540B1 (en) * 1984-04-26 1989-05-05 Alsthom Atlantique DEVICE FOR CARRYING OUT A METAL DEPOSIT ON THE FRICTING PARTS OF A TURBINE ROTOR
US4608128A (en) * 1984-07-23 1986-08-26 General Electric Company Method for applying abrasive particles to a surface
GB2167446B (en) * 1984-10-05 1988-05-05 Baj Ltd Electrode deposited composite coating
GB2182055B (en) * 1985-10-28 1989-10-18 Baj Ltd Improvements relating to electrodeposited coatings
GB8818069D0 (en) * 1988-07-29 1988-09-28 Baj Ltd Improvements relating to electrodeposited coatings
GB8914156D0 (en) * 1989-06-20 1989-08-09 Refurbished Turbine Components Apparatus for use in the repair of machines
US5074970A (en) * 1989-07-03 1991-12-24 Kostas Routsis Method for applying an abrasive layer to titanium alloy compressor airfoils
GB2241506A (en) * 1990-02-23 1991-09-04 Baj Ltd Method of producing a gas turbine blade having an abrasive tip by electrodepo- sition.

Also Published As

Publication number Publication date
WO1994019583A1 (en) 1994-09-01
DE69402305T2 (en) 1997-10-16
RU2118717C1 (en) 1998-09-10
EP0686229A1 (en) 1995-12-13
AU684263B2 (en) 1997-12-11
GB9303853D0 (en) 1993-04-21
AU6112694A (en) 1994-09-14
DE69402305D1 (en) 1997-04-30
SG47413A1 (en) 1998-04-17
JPH08506872A (en) 1996-07-23
CA2153899A1 (en) 1994-09-01
EP0686229B1 (en) 1997-03-26

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