USRE33800E - Method for electroplating nickel onto titanium alloys - Google Patents

Method for electroplating nickel onto titanium alloys Download PDF

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Publication number
USRE33800E
USRE33800E US07/634,854 US63485490A USRE33800E US RE33800 E USRE33800 E US RE33800E US 63485490 A US63485490 A US 63485490A US RE33800 E USRE33800 E US RE33800E
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Prior art keywords
layer
nickel
etching
nickel onto
electroplating
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US07/634,854
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Donald E. Fornwalt
Gary M. Lomasney
Kostas Routsis
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Raytheon Technologies Corp
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United Technologies Corp
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Priority claimed from US07/375,231 external-priority patent/US4902388A/en
Application filed by United Technologies Corp filed Critical United Technologies Corp
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    • CCHEMISTRY; METALLURGY
    • C25ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25DPROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D5/00Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
    • C25D5/34Pretreatment of metallic surfaces to be electroplated
    • C25D5/38Pretreatment of metallic surfaces to be electroplated of refractory metals or nickel
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23FNON-MECHANICAL REMOVAL OF METALLIC MATERIAL FROM SURFACE; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL; MULTI-STEP PROCESSES FOR SURFACE TREATMENT OF METALLIC MATERIAL INVOLVING AT LEAST ONE PROCESS PROVIDED FOR IN CLASS C23 AND AT LEAST ONE PROCESS COVERED BY SUBCLASS C21D OR C22F OR CLASS C25
    • C23F1/00Etching metallic material by chemical means
    • C23F1/10Etching compositions
    • C23F1/14Aqueous compositions
    • C23F1/16Acidic compositions
    • C23F1/26Acidic compositions for etching refractory metals

Definitions

  • This invention relates to electroplating, and in particular, to a method for electroplating a layer of nickel onto titanium and titanium base alloys.
  • Turner indicates that it is difficult to achieve good adhesion between the titanium substrate and the layer of electroplated nickel because an oxide film is typically present on the surface of the substrate.
  • Turner's invention is to use an aqueous solution of hydrofluoric acid and formamide to remove to oxide.
  • Ruben removes the oxide by connecting the substrate as the cathode in an acid solution such as sulfuric acid, and then forming a layer of titanium hydride on the substrate.
  • Temprano pickles the substrate surface with a 95% sulfuric acid solution.
  • Other prior art methods for removing the oxide scale include a solution containing hydrofluoric acid and nitric acid.
  • components having a titanium base alloy composition are nickel plated by the steps which include etching the surface of the component in a hydrofluoric acid-hydrochloric acid solution followed by electroplating in a nickel sulfamate bath.
  • the solution should have a composition corresponding to that obtained by mixing, by volume, 4-6% of 70% HF, balance 35-38% HCl. Specimens which have been etched in such a solution and then are electroplated in a nickel sulfamate bath have excellent bond strength.
  • This invention relates to a process for electroplating a layer of nickel onto titanium and titanium base alloys.
  • titanium base means those alloys in which titanium is the predominant element in the alloy composition.
  • This invention has shown to be particularly applicable to the electrodeposition of nickel onto titanium base alloys which include refractory metal elements.
  • Such alloys include, but are not limited to, the following compositions: Ti-3Al-2.5V; Ti-6Al-4V; Ti-8Al-1V-1Mo; Ti-6Al-2Sn-4Zr-6Mo; and Ti-6Al-2Sn-4Zr-2Mo.
  • the key aspect of the invention is the use of a particular chemical solution for cleaning the surface of the titanium substrate prior to the electrodeposition step.
  • the chemical solution etches the substrate surface, and, as a result, the step is referred to as an etching step.
  • the preferred manner for carrying out this invention is described below.
  • Portions of the component (an alloy whose composition was Ti-8Al-1V-1Mo) which are not to be etched or electroplated are masked with an appropriate masking material; wax and polymer based resins are preferred. Dirt, oil and other residue which are present on the surface are removed by a dry pumice swab followed by a wet pumice swab. The surface is vapor blasted with aluminum oxide grit and then rinsed, preferably in water. The substrate is then immersed in a solution whose composition corresponds to that obtained by mixing, by volume, 4-6% of 70% hydrofluoric acid and 94-96% of 35-38% hydrochloric acid.
  • the substrate is immersed in such solution for a period of time sufficient to clean and etch the surface but not so long as to excessively etch or pit the surface. Periods of time between about 8 and 45 seconds are useful; 10 to 20 seconds are preferred, and about 15 seconds is the most preferred immersion time.
  • the substrate is removed from the HF-HCl bath and rinsed in water. To insure that no residual acid and/or smut is present on the substrate, it is ultrasonically cleaned for about 10 seconds in deionized water.
  • the substrate may be etched in a solution containing hydrofluoric acid, glacial acetic acid and water.
  • the preferred solution contains, by volume, 11-15% of 70% hydrofluoric acid, 81-85% glacial acetic acid, and 2-6% water.
  • the etching is done anodically, at a current of about .[.1.4.]. .Iadd.161 .Iaddend.amperes per square meter (ASM) for about 6 minutes.
  • the substrate is then rinsed and then cathodically plated in a conventional nickel sulfgmate solution. The plating process takes place for about 30 minutes at .[.2.7.]. .Iadd.323 .Iaddend.ASM.
  • the substrate is then preferably heat treated at about 400° C. for 4 hours in air.

Abstract

This invention relates to an improved method for electroplating a layer of nickel into titanium base alloy substrates. It is particularly useful in electroplating a layer of nickel onto titanium alloys which contain refractory metal elements, such as the alloy Ti-8Al-1V-1Mo. The method includes the steps of etching the surface of the substrate with a solution containing hydrofluoric acid and hydrochloric acid, followed by electroplating the etched surface in a nickel sulfamate solution.

Description

TECHNICAL FIELD
This invention relates to electroplating, and in particular, to a method for electroplating a layer of nickel onto titanium and titanium base alloys.
BACKGROUND
U.S. Pat. Nos. 4,127,209 to Ruben, 4,416,739 to Turner and 4,787,962 to Temprano all describe methods for electroplating a layer of nickel onto titanium and titanium base alloys. Turner indicates that it is difficult to achieve good adhesion between the titanium substrate and the layer of electroplated nickel because an oxide film is typically present on the surface of the substrate. Turner's invention is to use an aqueous solution of hydrofluoric acid and formamide to remove to oxide. Ruben removes the oxide by connecting the substrate as the cathode in an acid solution such as sulfuric acid, and then forming a layer of titanium hydride on the substrate. Temprano pickles the substrate surface with a 95% sulfuric acid solution. Other prior art methods for removing the oxide scale include a solution containing hydrofluoric acid and nitric acid.
While the aforementioned methods may be successful with some titanium alloys, they are not useful on some specialty titanium alloys of the type used in the gas turbine industry. Accordingly, workers in this field seek improved techniques for applying electroplated layers of nickel onto state-of-the-art titanium alloys. This invention satisfies such a need.
SUMMARY OF THE INVENTION
According to this invention, components having a titanium base alloy composition are nickel plated by the steps which include etching the surface of the component in a hydrofluoric acid-hydrochloric acid solution followed by electroplating in a nickel sulfamate bath. The solution should have a composition corresponding to that obtained by mixing, by volume, 4-6% of 70% HF, balance 35-38% HCl. Specimens which have been etched in such a solution and then are electroplated in a nickel sulfamate bath have excellent bond strength.
Other features and aspects of this invention will be apparent in light of the following description of the best mode for carrying out the invention.
BEST MODE FOR CARRYING OUT THE INVENTION
This invention relates to a process for electroplating a layer of nickel onto titanium and titanium base alloys. It should be understood that the term "titanium base" means those alloys in which titanium is the predominant element in the alloy composition.
This invention has shown to be particularly applicable to the electrodeposition of nickel onto titanium base alloys which include refractory metal elements. Such alloys include, but are not limited to, the following compositions: Ti-3Al-2.5V; Ti-6Al-4V; Ti-8Al-1V-1Mo; Ti-6Al-2Sn-4Zr-6Mo; and Ti-6Al-2Sn-4Zr-2Mo.
The key aspect of the invention is the use of a particular chemical solution for cleaning the surface of the titanium substrate prior to the electrodeposition step. The chemical solution etches the substrate surface, and, as a result, the step is referred to as an etching step. The preferred manner for carrying out this invention is described below.
Portions of the component (an alloy whose composition was Ti-8Al-1V-1Mo) which are not to be etched or electroplated are masked with an appropriate masking material; wax and polymer based resins are preferred. Dirt, oil and other residue which are present on the surface are removed by a dry pumice swab followed by a wet pumice swab. The surface is vapor blasted with aluminum oxide grit and then rinsed, preferably in water. The substrate is then immersed in a solution whose composition corresponds to that obtained by mixing, by volume, 4-6% of 70% hydrofluoric acid and 94-96% of 35-38% hydrochloric acid. The substrate is immersed in such solution for a period of time sufficient to clean and etch the surface but not so long as to excessively etch or pit the surface. Periods of time between about 8 and 45 seconds are useful; 10 to 20 seconds are preferred, and about 15 seconds is the most preferred immersion time. The substrate is removed from the HF-HCl bath and rinsed in water. To insure that no residual acid and/or smut is present on the substrate, it is ultrasonically cleaned for about 10 seconds in deionized water.
The substrate may be etched in a solution containing hydrofluoric acid, glacial acetic acid and water. The preferred solution contains, by volume, 11-15% of 70% hydrofluoric acid, 81-85% glacial acetic acid, and 2-6% water. The etching is done anodically, at a current of about .[.1.4.]. .Iadd.161 .Iaddend.amperes per square meter (ASM) for about 6 minutes. The substrate is then rinsed and then cathodically plated in a conventional nickel sulfgmate solution. The plating process takes place for about 30 minutes at .[.2.7.]. .Iadd.323 .Iaddend.ASM. The substrate is then preferably heat treated at about 400° C. for 4 hours in air.
Use of the aforementioned plating process produces an electrodeposited layer of nickel having a thickness of about 12-18 microns. The bond strength of the layer after heat treatment is in excess of 475 kilograms per square centimeter, as determined by lap shear specimens.
The use of conventional prior art cleaning techniques produced nickel layers which were generally nonadherent to a Ti-8Al-1V-1Mo substrate. In particular, etching solutions containing, by volume, about 12% of 70% hydrofluoric acid and 1% of 70% nitric acid were not useful, as they produced a tenacious smut which could not readily be removed from the substrate surface. The HF-HNO3 solution is commonly used with much success on titanium alloys which are substantially free of refractory elements.
While this invention has been shown and described with respect to a preferred embodiment, it should be understood by those skilled in the art that various changes in the form and detail may be made without departing from the spirit and scope of the invention. For example, other concentrations of hydrofluoric acid and hydrochloric acid may be used other than the aforementioned 70% HF and 36-38% HCl. Regardless of the particular concentrations used, the solution should have a composition corresponding to that obtained by mixing 4-6% of the 70% HF and 94-96% of the 36-38% HCl. The fluoride ion content of such solutions are readily measured using a conventional fluoride ion specific electrode.

Claims (4)

We claim:
1. A method for electroplating a layer of nickel onto a titanium base alloy containing refractory metal element, comprising the steps of etching the component surface in a solution having a composition corresponding to, by volume, about 4-6% of 70% HF and 94-96% of 36-38% HCl, and then cathodically plating a layer of nickel onto the etched surface.
2. A method for electroplating a layer of nickel onto the surface of a titanium base alloy component containing at least 1% by weight of a refractory metal element, comprising the steps of:
(a) etching the component surface in a room temperature solution containing, by volume, about 94-96% of 36-38% HCl and about 4-6% of 70% HF for at least about 10 seconds;
(b) anodically etching the component in a room temperature solution containing, by volume, about 11-15% of 70% HF, 81-85% glacial acetic acid and 2-6% H2 O; and
(c) cathodically plating a layer of nickel onto the surface.
3. A method for applying a layer of nickel onto a titanium base alloy component containing at least 1 weight % of a refractory metal element, comprising the steps of:
(a) etching the surface of the component in a room temperature solution consisting essentially of, by volume, about 94-96% of 36-38% HCl and about 4-6% of 70% HF for at least about 10 seconds;
(b) anodically etching the component surface at about .[.1.4.]. .Iadd.161 .Iaddend.amperes per square meter for about 6 minutes in a room temperature solution consisting essentially of, by volume, about 11-15% of 70% HF, 81-85% glacial acetic acid and 2-6% H2 O; and
(c) cathodically plating a layer of nickel onto the etched component surface at .[.2.7.]. .Iadd.323 .Iaddend.amperes per square meter for about 30 minutes in a nickel sulfamate solution.
4. The method of claim 3, wherein said etching step is conducted is a solution containing 95% of 36-38% HCl and 5% of 70% HF.
US07/634,854 1989-07-03 1990-12-27 Method for electroplating nickel onto titanium alloys Expired - Lifetime USRE33800E (en)

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US07/375,231 US4902388A (en) 1989-07-03 1989-07-03 Method for electroplating nickel onto titanium alloys
US07/634,854 USRE33800E (en) 1989-07-03 1990-12-27 Method for electroplating nickel onto titanium alloys

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040173465A1 (en) * 2003-03-03 2004-09-09 Com Dev Ltd. Method of surface treating titanium-containing metals followed by plating in the same electrolyte bath and parts made in accordance therewith
US6932897B2 (en) 2003-03-03 2005-08-23 Com Dev Ltd. Titanium-containing metals with adherent coatings and methods for producing same
US20060102586A1 (en) * 1998-04-07 2006-05-18 Whonchee Lee High selectivity BPSG to TEOS etchant
US20090090634A1 (en) * 2007-10-03 2009-04-09 Sifco Selective Plating Method of plating metal onto titanium
US20100028713A1 (en) * 2008-07-29 2010-02-04 Nardi Aaron T Method and article for improved adhesion of fatigue-prone components
US7831204B1 (en) 1981-11-03 2010-11-09 Personalized Media Communications, Llc Signal processing apparatus and methods

Citations (10)

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US2829091A (en) * 1956-06-04 1958-04-01 Menasco Mfg Company Method for electroplating titanium
US3087874A (en) * 1961-02-13 1963-04-30 Don H Greisl Electropolishing of titanium base alloys
US3647647A (en) * 1969-02-19 1972-03-07 United Aircraft Corp Process for plating titanium
US3725217A (en) * 1969-07-18 1973-04-03 Ionitech Labor Inc Plating titanium and zirconium and their alloys with nickel,chromium and other heavy metals
US4127709A (en) * 1977-08-24 1978-11-28 Samuel Ruben Process for electro-plating nickel on titanium
US4416739A (en) * 1980-04-16 1983-11-22 Rolls-Royce Limited Electroplating of titanium and titanium base alloys
US4588480A (en) * 1983-06-11 1986-05-13 Mtu Motoren-Und Turbinen-Union Munchen Gmbh Method of producing wear-protection layers on surfaces of structural parts of titanium or titanium-base alloys
US4655884A (en) * 1985-08-19 1987-04-07 General Electric Company Nickel plating of refractory metals
US4787962A (en) * 1986-05-26 1988-11-29 Alcatel Espace Method of electrolytically depositing metal on titanium
US4938850A (en) * 1988-09-26 1990-07-03 Hughes Aircraft Company Method for plating on titanium

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2829091A (en) * 1956-06-04 1958-04-01 Menasco Mfg Company Method for electroplating titanium
US3087874A (en) * 1961-02-13 1963-04-30 Don H Greisl Electropolishing of titanium base alloys
US3647647A (en) * 1969-02-19 1972-03-07 United Aircraft Corp Process for plating titanium
US3725217A (en) * 1969-07-18 1973-04-03 Ionitech Labor Inc Plating titanium and zirconium and their alloys with nickel,chromium and other heavy metals
US4127709A (en) * 1977-08-24 1978-11-28 Samuel Ruben Process for electro-plating nickel on titanium
US4416739A (en) * 1980-04-16 1983-11-22 Rolls-Royce Limited Electroplating of titanium and titanium base alloys
US4588480A (en) * 1983-06-11 1986-05-13 Mtu Motoren-Und Turbinen-Union Munchen Gmbh Method of producing wear-protection layers on surfaces of structural parts of titanium or titanium-base alloys
US4655884A (en) * 1985-08-19 1987-04-07 General Electric Company Nickel plating of refractory metals
US4787962A (en) * 1986-05-26 1988-11-29 Alcatel Espace Method of electrolytically depositing metal on titanium
US4938850A (en) * 1988-09-26 1990-07-03 Hughes Aircraft Company Method for plating on titanium

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Title
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Larissa Domnikov, Metal Finishing, pp. 59-62, Mar. 1962.

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7831204B1 (en) 1981-11-03 2010-11-09 Personalized Media Communications, Llc Signal processing apparatus and methods
US20060102586A1 (en) * 1998-04-07 2006-05-18 Whonchee Lee High selectivity BPSG to TEOS etchant
US7378353B2 (en) 1998-04-07 2008-05-27 Micron Technology, Inc. High selectivity BPSG to TEOS etchant
US20080233759A1 (en) * 1998-04-07 2008-09-25 Micron Technology, Inc. High selectivity bpsg to teos etchant
US7977251B2 (en) 1998-04-07 2011-07-12 Round Rock Research, Llc High selectivity BPSG to TEOS etchant
US20040173465A1 (en) * 2003-03-03 2004-09-09 Com Dev Ltd. Method of surface treating titanium-containing metals followed by plating in the same electrolyte bath and parts made in accordance therewith
US6913791B2 (en) 2003-03-03 2005-07-05 Com Dev Ltd. Method of surface treating titanium-containing metals followed by plating in the same electrolyte bath and parts made in accordance therewith
US6932897B2 (en) 2003-03-03 2005-08-23 Com Dev Ltd. Titanium-containing metals with adherent coatings and methods for producing same
US20090090634A1 (en) * 2007-10-03 2009-04-09 Sifco Selective Plating Method of plating metal onto titanium
US20100028713A1 (en) * 2008-07-29 2010-02-04 Nardi Aaron T Method and article for improved adhesion of fatigue-prone components
US8065898B2 (en) 2008-07-29 2011-11-29 Hamilton Sundstrand Corporation Method and article for improved adhesion of fatigue-prone components
US8297094B2 (en) 2008-07-29 2012-10-30 Hamilton Sundstrand Corporation Article for improved adhesion of fatigue-prone components

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