WO2004111306A3 - Verfahren zur schaufelspitzenpanzerung der laufschaufeln eines gasturbinentriebwerkes und vorrichtung zur durchführung des verfahrens - Google Patents

Verfahren zur schaufelspitzenpanzerung der laufschaufeln eines gasturbinentriebwerkes und vorrichtung zur durchführung des verfahrens Download PDF

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Publication number
WO2004111306A3
WO2004111306A3 PCT/DE2004/001158 DE2004001158W WO2004111306A3 WO 2004111306 A3 WO2004111306 A3 WO 2004111306A3 DE 2004001158 W DE2004001158 W DE 2004001158W WO 2004111306 A3 WO2004111306 A3 WO 2004111306A3
Authority
WO
WIPO (PCT)
Prior art keywords
armour
tips
plating
gas turbine
carrying
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.)
Ceased
Application number
PCT/DE2004/001158
Other languages
English (en)
French (fr)
Other versions
WO2004111306A2 (de
Inventor
Reinhold Meier
Mario Schmidt
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.)
MTU Aero Engines AG
Original Assignee
MTU Aero Engines GmbH
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 MTU Aero Engines GmbH filed Critical MTU Aero Engines GmbH
Priority to EP04738612A priority Critical patent/EP1631700A2/de
Priority to US10/560,564 priority patent/US20070090152A1/en
Publication of WO2004111306A2 publication Critical patent/WO2004111306A2/de
Publication of WO2004111306A3 publication Critical patent/WO2004111306A3/de
Anticipated expiration legal-status Critical
Ceased 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/286—Particular treatment of blades, e.g. to increase durability or resistance against corrosion or erosion
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
    • C23C2/04—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor characterised by the coating material
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C26/00—Coating not provided for in groups C23C2/00 - C23C24/00
    • C23C26/02—Coating not provided for in groups C23C2/00 - C23C24/00 applying molten material to the substrate
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/02—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
    • B23K35/0222—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape for use in soldering or brazing
    • B23K35/0233—Sheets or foils
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
    • B23K35/24—Selection of soldering or welding materials proper
    • B23K35/32—Selection of soldering or welding materials proper with the principal constituent melting at more than 1550°C
    • B23K35/327—Selection of soldering or welding materials proper with the principal constituent melting at more than 1550°C comprising refractory compounds, e.g. carbides

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Verfahren zur Panzerung der Schaufelspitzen (12) von Verdichterschaufeln (10) eines Gasturbinentriebwerkes unter Verwendung eines Zuschnitts (16), der aus einer, mit einer eingebettete harte Partikel aufweisenden Metallschicht versehenen Lötfolie besteht und der der Geometrie der zu panzernden Schaufelspitze angepasst ist, wel­cher Zuschnitt (16) unter Anwendung von Druck auf die Schaufelspitze aufgeschmol­zen wird und dabei eine gerippte oder genoppte Struktur in seine Oberfläche einge­prägt erhält
PCT/DE2004/001158 2003-06-12 2004-06-04 Verfahren zur schaufelspitzenpanzerung der laufschaufeln eines gasturbinentriebwerkes und vorrichtung zur durchführung des verfahrens Ceased WO2004111306A2 (de)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP04738612A EP1631700A2 (de) 2003-06-12 2004-06-04 Verfahren zur schaufelspitzenpanzerung der laufschaufeln eines gasturbinentriebwerkes und vorrichtung zur durchführung des verfahrens
US10/560,564 US20070090152A1 (en) 2003-06-12 2004-06-04 Method for cladding the blade tips of rotor blades of a gas turbine power plant and device for carrying out the method

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10326541.4 2003-06-12
DE10326541A DE10326541A1 (de) 2003-06-12 2003-06-12 Verfahren zur Schaufelspitzenpanzerung der Laufschaufeln eines Gasturbinentriebwerkes und Vorrichtung zur Durchführung des Verfahrens

Publications (2)

Publication Number Publication Date
WO2004111306A2 WO2004111306A2 (de) 2004-12-23
WO2004111306A3 true WO2004111306A3 (de) 2005-03-03

Family

ID=33494990

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/DE2004/001158 Ceased WO2004111306A2 (de) 2003-06-12 2004-06-04 Verfahren zur schaufelspitzenpanzerung der laufschaufeln eines gasturbinentriebwerkes und vorrichtung zur durchführung des verfahrens

Country Status (4)

Country Link
US (1) US20070090152A1 (de)
EP (1) EP1631700A2 (de)
DE (1) DE10326541A1 (de)
WO (1) WO2004111306A2 (de)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7556477B2 (en) * 2005-10-04 2009-07-07 General Electric Company Bi-layer tip cap
EP1865258A1 (de) 2006-06-06 2007-12-12 Siemens Aktiengesellschaft Gepanzerte Maschinenkomponente und Gasturbine
DE102007010256A1 (de) * 2007-03-02 2008-09-04 Mtu Aero Engines Gmbh Verfahren und Vorrichtung zum Beschichten von Bauteilen einer Gasturbine
DE102011100025A1 (de) * 2011-04-29 2012-10-31 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Bauteil mit Verschleißschutz- oder Antihaft-Foliesowie Verfahren zu dessen Herstellung
EP2581468A1 (de) * 2011-10-14 2013-04-17 Siemens Aktiengesellschaft Verfahren zum Aufbringen einer Verschleißschutzschicht auf eine Strömungsmaschinenkomponente
US9982358B2 (en) 2014-06-04 2018-05-29 United Technologies Corporation Abrasive tip blade manufacture methods
EP3269842A1 (de) * 2016-07-12 2018-01-17 Siemens Aktiengesellschaft Verfahren zum herstellen eines bauteils und bauteil

Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2166998A (en) * 1938-08-02 1939-07-25 Westinghouse Electric & Mfg Co Method of brazing turbine blades
DE3208068A1 (de) * 1982-03-05 1983-09-15 Kähny Maschinenbau GmbH, 7150 Backnang Vorrichtung zum automatischen anloeten von hartmetallzaehnen
US4622445A (en) * 1984-09-28 1986-11-11 The Boeing Company Method of inductively brazing honeycomb panels
US4795313A (en) * 1986-05-28 1989-01-03 Alsthom Protective tip for a titanium blade and a method of brazing such a tip
JPH0210926A (ja) * 1988-06-28 1990-01-16 Nec Corp 無線通信方式
US5264011A (en) * 1992-09-08 1993-11-23 General Motors Corporation Abrasive blade tips for cast single crystal gas turbine blades
JPH0855865A (ja) * 1994-08-11 1996-02-27 Fuji Electric Co Ltd 半導体デバイスの製造方法および装置
EP0961038A1 (de) * 1998-05-28 1999-12-01 Elektroschmelzwerk Kempten GmbH Verbindungselement zur kraftschlüssigen Verbindung von Bauteilen
EP1029629A2 (de) * 1999-02-17 2000-08-23 EUROMAT Gesellschaft für Werkstofftechnologie und Transfer mbH Verfahren zum Herstellen einer Schutzschicht auf der Oberfläche eines Bauteils od.dgl. Werkstückes sowie Legierung und Lotwerkstoff dafür
EP1065297A2 (de) * 1999-06-29 2001-01-03 General Electric Company Verfahren zur Erzeugung verschleissfester Beschichtungen und daraus hergestellte Artikel
US20020119338A1 (en) * 1999-06-29 2002-08-29 Wayne Charles Hasz Tubine engine component having wear coating and method for coating a turbine engine component
WO2002097160A1 (en) * 2001-05-31 2002-12-05 Mitsubishi Heavy Industries, Ltd. Coating forming method and coating forming material, and abrasive coating forming sheet

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1478219A (en) * 1921-02-02 1923-12-18 Hammitt Howard Pocket memorandum holder
GB217876A (en) * 1923-06-19 1925-01-08 Felix Kirschner Process for the production of galvanic coatings
US3594288A (en) * 1968-07-31 1971-07-20 Boeing Co Process for electroplating nickel onto metal surfaces
US6347905B1 (en) * 1998-05-28 2002-02-19 Elektroschmelzwerk Kempten Gmbh Connecting element for the frictional connection of components

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2166998A (en) * 1938-08-02 1939-07-25 Westinghouse Electric & Mfg Co Method of brazing turbine blades
DE3208068A1 (de) * 1982-03-05 1983-09-15 Kähny Maschinenbau GmbH, 7150 Backnang Vorrichtung zum automatischen anloeten von hartmetallzaehnen
US4622445A (en) * 1984-09-28 1986-11-11 The Boeing Company Method of inductively brazing honeycomb panels
US4795313A (en) * 1986-05-28 1989-01-03 Alsthom Protective tip for a titanium blade and a method of brazing such a tip
JPH0210926A (ja) * 1988-06-28 1990-01-16 Nec Corp 無線通信方式
US5264011A (en) * 1992-09-08 1993-11-23 General Motors Corporation Abrasive blade tips for cast single crystal gas turbine blades
JPH0855865A (ja) * 1994-08-11 1996-02-27 Fuji Electric Co Ltd 半導体デバイスの製造方法および装置
EP0961038A1 (de) * 1998-05-28 1999-12-01 Elektroschmelzwerk Kempten GmbH Verbindungselement zur kraftschlüssigen Verbindung von Bauteilen
EP1029629A2 (de) * 1999-02-17 2000-08-23 EUROMAT Gesellschaft für Werkstofftechnologie und Transfer mbH Verfahren zum Herstellen einer Schutzschicht auf der Oberfläche eines Bauteils od.dgl. Werkstückes sowie Legierung und Lotwerkstoff dafür
EP1065297A2 (de) * 1999-06-29 2001-01-03 General Electric Company Verfahren zur Erzeugung verschleissfester Beschichtungen und daraus hergestellte Artikel
US20020119338A1 (en) * 1999-06-29 2002-08-29 Wayne Charles Hasz Tubine engine component having wear coating and method for coating a turbine engine component
WO2002097160A1 (en) * 2001-05-31 2002-12-05 Mitsubishi Heavy Industries, Ltd. Coating forming method and coating forming material, and abrasive coating forming sheet
EP1391537A1 (de) * 2001-05-31 2004-02-25 Mitsubishi Heavy Industries, Ltd. Verfahren zur herstellung einer beschichtung und beschichtungsmasse sowie schleifüberzug bildende folie

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
PATENT ABSTRACTS OF JAPAN vol. 1996, no. 06 28 June 1996 (1996-06-28) *
PATENT ABSTRACTS OF JAPAN vol. 1997, no. 05 30 May 1997 (1997-05-30) *

Also Published As

Publication number Publication date
EP1631700A2 (de) 2006-03-08
DE10326541A1 (de) 2005-01-05
WO2004111306A2 (de) 2004-12-23
US20070090152A1 (en) 2007-04-26

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