JP2938151B2 - 研摩層をチタン合金製コンプレッサーエアフォイルへ適用する方法 - Google Patents

研摩層をチタン合金製コンプレッサーエアフォイルへ適用する方法

Info

Publication number
JP2938151B2
JP2938151B2 JP2176107A JP17610790A JP2938151B2 JP 2938151 B2 JP2938151 B2 JP 2938151B2 JP 2176107 A JP2176107 A JP 2176107A JP 17610790 A JP17610790 A JP 17610790A JP 2938151 B2 JP2938151 B2 JP 2938151B2
Authority
JP
Japan
Prior art keywords
nickel layer
nickel
blade
layer
electroplating
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 - Fee Related
Application number
JP2176107A
Other languages
English (en)
Japanese (ja)
Other versions
JPH0347996A (ja
Inventor
ラウトシス コスタス
ジョン パーコス，ジュニア ジャセフ
フレリング メルヴィン
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.)
RTX Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of JPH0347996A publication Critical patent/JPH0347996A/ja
Application granted granted Critical
Publication of JP2938151B2 publication Critical patent/JP2938151B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • C—CHEMISTRY; METALLURGY
    • C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D15/00—Electrolytic or electrophoretic production of coatings containing embedded materials, e.g. particles, whiskers, wires
    • C25D15/02—Combined electrolytic and electrophoretic processes with charged materials
    • C—CHEMISTRY; METALLURGY
    • C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
    • C25D5/10—Electroplating with more than one layer of the same or of different metals
    • C25D5/12—Electroplating with more than one layer of the same or of different metals at least one layer being of nickel or chromium
    • C25D5/14—Electroplating with more than one layer of the same or of different metals at least one layer being of nickel or chromium two or more layers being of nickel or chromium, e.g. duplex or triplex layers
    • C—CHEMISTRY; METALLURGY
    • C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
    • C25D5/48—After-treatment of electroplated surfaces
    • C25D5/50—After-treatment of electroplated surfaces by 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
    • F05D2250/00—Geometry
    • F05D2250/60—Structure; Surface texture
    • F05D2250/62—Structure; Surface texture smooth or fine
    • F05D2250/621—Structure; Surface texture smooth or fine polished

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Electrochemistry (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Electroplating Methods And Accessories (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
JP2176107A 1989-07-03 1990-07-03 研摩層をチタン合金製コンプレッサーエアフォイルへ適用する方法 Expired - Fee Related JP2938151B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US07/375,230 US5074970A (en) 1989-07-03 1989-07-03 Method for applying an abrasive layer to titanium alloy compressor airfoils
US375,230 1989-07-03

Publications (2)

Publication Number Publication Date
JPH0347996A JPH0347996A (ja) 1991-02-28
JP2938151B2 true JP2938151B2 (ja) 1999-08-23

Family

ID=23480054

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2176107A Expired - Fee Related JP2938151B2 (ja) 1989-07-03 1990-07-03 研摩層をチタン合金製コンプレッサーエアフォイルへ適用する方法

Country Status (5)

Country Link
US (1) US5074970A (enExample)
JP (1) JP2938151B2 (enExample)
DE (1) DE4021044A1 (enExample)
FR (1) FR2649125B1 (enExample)
GB (1) GB2234526B (enExample)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5389228A (en) * 1993-02-04 1995-02-14 United Technologies Corporation Brush plating compressor blade tips
GB9303853D0 (en) * 1993-02-25 1993-04-21 Baj Coatings Ltd Rotor blades
FR2708940B1 (fr) * 1993-08-12 1995-09-22 Snecma Procédé de durcissement de pièces métalliques.
US5486281A (en) * 1993-10-15 1996-01-23 United Technologies Corporation Method for CBN tipping of HPC integrally bladed rotors
US5437724A (en) * 1993-10-15 1995-08-01 United Technologies Corporation Mask and grit container
US5476363A (en) * 1993-10-15 1995-12-19 Charles E. Sohl Method and apparatus for reducing stress on the tips of turbine or compressor blades
US5603603A (en) * 1993-12-08 1997-02-18 United Technologies Corporation Abrasive blade tip
US5637921A (en) * 1995-04-21 1997-06-10 Sun Microsystems, Inc. Sub-ambient temperature electronic package
US5935407A (en) * 1997-11-06 1999-08-10 Chromalloy Gas Turbine Corporation Method for producing abrasive tips for gas turbine blades
JP2002371803A (ja) * 2001-06-13 2002-12-26 Mitsubishi Heavy Ind Ltd 動翼用耐摩耗層の形成方法、耐摩耗層及びその再生方法
US9284647B2 (en) * 2002-09-24 2016-03-15 Mitsubishi Denki Kabushiki Kaisha Method for coating sliding surface of high-temperature member, high-temperature member and electrode for electro-discharge surface treatment
KR101063575B1 (ko) * 2002-09-24 2011-09-07 미츠비시덴키 가부시키가이샤 고온부재의 슬라이딩면 코팅 방법 및 고온부재와 방전표면 처리용 전극
TWI272993B (en) * 2002-10-09 2007-02-11 Ishikawajima Harima Heavy Ind Method for coating rotary member, rotary member, labyrinth seal structure and method for manufacturing rotary member
US20060289088A1 (en) * 2005-06-28 2006-12-28 General Electric Company Titanium treatment to minimize fretting
US7506440B2 (en) * 2005-06-28 2009-03-24 General Electric Company Titanium treatment to minimize fretting
FR2915495B1 (fr) * 2007-04-30 2010-09-03 Snecma Procede de reparation d'une aube mobile de turbomachine
DE102008026936A1 (de) 2008-06-05 2009-12-10 Mtu Aero Engines Gmbh Vorrichtung zur Verwendung in einem Verfahren zur Herstellung einer Schutzschicht und Verfahren zur Herstellung einer Schutzschicht
FR2935625B1 (fr) * 2008-09-05 2011-09-09 Snecma Procede de fabrication d'une piece thermamecanique de revolution circulaire comportant un substrat porteur a base de titane revetu d'acier ou superalliage, carter de compresseur de turbomachine resistant au feu de titane
US8236163B2 (en) * 2009-09-18 2012-08-07 United Technologies Corporation Anode media for use in electroplating processes, and methods of cleaning thereof
US8672634B2 (en) 2010-08-30 2014-03-18 United Technologies Corporation Electroformed conforming rubstrip
US20130154192A1 (en) * 2011-12-15 2013-06-20 Trelleborg Sealing Solutions Us, Inc. Sealing assembly
US10053994B2 (en) 2014-05-02 2018-08-21 United Technologies Corporation Abrasive sheathing
DE102014218167B4 (de) 2014-09-11 2018-09-27 MTU Aero Engines AG Verfahren zur Schaufelspitzenpanzerung
US20160237832A1 (en) * 2015-02-12 2016-08-18 United Technologies Corporation Abrasive blade tip with improved wear at high interaction rate
GB201610768D0 (en) * 2016-06-21 2016-08-03 Rolls Royce Plc Gas turbine engine component with protective coating
US10822967B2 (en) 2017-02-01 2020-11-03 Raytheon Technologies Corporation Wear resistant coating, method of manufacture thereof and articles comprising the same
US11225876B2 (en) * 2019-12-19 2022-01-18 Raytheon Technologies Corporation Diffusion barrier to prevent super alloy depletion into nickel-CBN blade tip coating
CN114645306B (zh) * 2022-02-25 2024-04-09 中国航发北京航空材料研究院 在复杂形状工件表面制备大尺寸cBN颗粒镍基镀层的方法

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3488263A (en) * 1968-04-22 1970-01-06 Gen Electric Codeposition of metallics and non-metallics
BE791008A (fr) * 1971-11-09 1973-05-07 Citroen Sa Perfectionnements apportes aux procedes pour la formation sur une paroiexposee a des forces de friction et appartenant a une pieceen alliage leger, d'une revetement metallique composite resistant a l'usure
US3871840A (en) * 1972-01-24 1975-03-18 Christensen Diamond Prod Co Abrasive particles encapsulated with a metal envelope of allotriomorphic dentrites
JPS5242134B2 (enExample) * 1972-12-30 1977-10-22
US4127709A (en) * 1977-08-24 1978-11-28 Samuel Ruben Process for electro-plating nickel on titanium
US4148494A (en) * 1977-12-21 1979-04-10 General Electric Company Rotary labyrinth seal member
US4169020A (en) * 1977-12-21 1979-09-25 General Electric Company Method for making an improved gas seal
US4232995A (en) * 1978-11-27 1980-11-11 General Electric Company Gas seal for turbine blade tip
US4249913A (en) * 1979-05-21 1981-02-10 United Technologies Corporation Alumina coated silicon carbide abrasive
US4226055A (en) * 1979-06-08 1980-10-07 General Electric Company Dressing and conditioning resin-bonded diamond grinding wheel
GB2074189A (en) * 1980-04-16 1981-10-28 Rolls Royce Treating a titanium or titanium base alloy surface prior to electroplating
US4390320A (en) * 1980-05-01 1983-06-28 General Electric Company Tip cap for a rotor blade and method of replacement
DE3038289A1 (de) * 1980-10-10 1982-05-27 Egon 5650 Solingen Evertz Verfahren zum abscheiden von metallschichten auf den waenden von kokillen
JPS59159993A (ja) * 1983-03-02 1984-09-10 Nisshin Kikai Seisakusho:Kk 電着砥石の創成方法及びその装置
US4589823A (en) * 1984-04-27 1986-05-20 General Electric Company Rotor blade tip
US4608145A (en) * 1984-07-23 1986-08-26 General Electric Company Electroplating tape
US4608128A (en) * 1984-07-23 1986-08-26 General Electric Company Method for applying abrasive particles to a surface
FR2599052B1 (fr) * 1986-05-26 1988-07-22 Alcatel Espace Procede et depot metallique sur titane par voie electrolytique
DE3627779A1 (de) * 1986-08-16 1988-02-18 Bbc Brown Boveri & Cie Erneuertes turbinenbauteil
US4802828A (en) * 1986-12-29 1989-02-07 United Technologies Corporation Turbine blade having a fused metal-ceramic tip
GB8720248D0 (en) * 1987-08-27 1987-10-07 Imi Titanium Ltd Turbines

Also Published As

Publication number Publication date
DE4021044A1 (de) 1991-01-17
GB2234526B (en) 1993-11-10
FR2649125B1 (fr) 1992-08-21
GB2234526A (en) 1991-02-06
FR2649125A1 (fr) 1991-01-04
GB9014728D0 (en) 1990-08-22
US5074970A (en) 1991-12-24
DE4021044C2 (enExample) 1993-04-08
JPH0347996A (ja) 1991-02-28

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