US20060157352A1 - Method of electroplating and pre-treating aluminium workpieces - Google Patents

Method of electroplating and pre-treating aluminium workpieces Download PDF

Info

Publication number
US20060157352A1
US20060157352A1 US11/320,488 US32048805A US2006157352A1 US 20060157352 A1 US20060157352 A1 US 20060157352A1 US 32048805 A US32048805 A US 32048805A US 2006157352 A1 US2006157352 A1 US 2006157352A1
Authority
US
United States
Prior art keywords
bath
nickel
layer
aluminium
metal layer
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.)
Abandoned
Application number
US11/320,488
Inventor
Jacques Hubert Wijenberg
Adrianus Wittebrood
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.)
Novelis Koblenz GmbH
Original Assignee
Corus Aluminium Walzprodukte 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 Corus Aluminium Walzprodukte GmbH filed Critical Corus Aluminium Walzprodukte GmbH
Priority to US11/320,488 priority Critical patent/US20060157352A1/en
Assigned to CORUS ALUMINIUM WALZPRODUKTE GMBH reassignment CORUS ALUMINIUM WALZPRODUKTE GMBH ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: WITTEBROOD, ADRIANUS JACOBUS, WIJENBERG, JACQUES HUBERT OLGA JOSEPH
Publication of US20060157352A1 publication Critical patent/US20060157352A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • 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
    • C25D5/42Pretreatment of metallic surfaces to be electroplated of light metals
    • C25D5/44Aluminium
    • CCHEMISTRY; METALLURGY
    • C25ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25DPROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D3/00Electroplating: Baths therefor
    • C25D3/02Electroplating: Baths therefor from solutions
    • C25D3/12Electroplating: Baths therefor from solutions of nickel or cobalt
    • CCHEMISTRY; METALLURGY
    • C25ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25DPROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D3/00Electroplating: Baths therefor
    • C25D3/02Electroplating: Baths therefor from solutions
    • C25D3/20Electroplating: Baths therefor from solutions of iron
    • 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
    • C25D5/10Electroplating with more than one layer of the same or of different metals
    • C25D5/12Electroplating with more than one layer of the same or of different metals at least one layer being of nickel or chromium

Definitions

  • alloy designations and temper designations refer to the Aluminium Association designations in Aluminium Standards and Data and the Registration Records, as published by the Aluminium Association.
  • Nickel plating of aluminium products is widely used because nickel provides a bright, shiny appearance, is long lasting and can conduct electricity. Another, more particular use of nickel plating is made in the manufacture of brazing sheet products. Aluminium alloy brazing sheets comprise an aluminium alloy core and a clad layer of filler alloy on one or both sides. Aluminium brazing sheets are widely used, e.g., in the production of heat exchangers.
  • aluminium-silicon alloys as filler material is problematic because the aluminium oxide layer has to be disrupted during brazing. This may be effected by applying a chemical flux onto the workpiece before brazing.
  • Fluxes for use in brazing aluminium alloys usually consist of mixtures of alkali and alkaline earth chlorides and fluorides or cryolite. The flux operates at the brazing temperature to disrupt, spread and dissolve the oxide film.
  • applying the chemical flux onto the workpiece is a rather laborious and therefore expensive process.
  • a braze-promoting metal of cobalt, iron, or more preferably nickel is coated on a part to be brazed.
  • the nickel reacts exothermically with the underlying aluminium alloy, thereby disrupting the aluminium oxide layer and permitting the underlying molten aluminium clad metal to flow together and join.
  • this method does not require a fluoride flux, it is also suitable for utilization with magnesium-enriched aluminium alloys, such as are beneficially used in heat-exchanger constructions.
  • the method of applying a metal layer onto at least one surface of an aluminium or aluminium alloy workpiece comprises the steps of pre-treating the surface by cathodic activation in a pre-treatment bath containing sulphuric acid and metal-ions selected from the group consisting of nickel, iron and cobalt, and applying a metal layer by electroplating the pre-treated workpiece, and wherein the metal layer is selected from the group consisting of nickel, iron, cobalt, and alloys thereof.
  • FIG. 1 shows an angle-on-coupon for brazing tests.
  • the invention is based on the finding that direct metal, for example nickel, plating of aluminium alloy products is possible after cathodic activation in a simple sulphuric acid solution to which only nickel ions, e.g. in the form of nickel sulphate, has been added. No fluoride components are needed in this activation process. Because the activation bath contains the same ingredients as a Watts bath which is preferably used as nickel plating bath, cross-contamination is excluded. Also, no problems in effluent treatment are expected.
  • the cathodic activation step has the same effect as the creation of a thin bonding layer between the aluminium surface and the nickel coating. The same applies mutatis mutandis for the situation where iron or cobalt is being used.
  • the pre-treatment bath preferably contains about 15 to 200 g/l, and preferably 80 to 150 g/l, of NiSO 4 .H 2 O, and about 50 to 350 g/l, preferably about 150 to 250 g/l of H 2 SO 4 .
  • the pre-treatment bath also contains boric acid as a buffer, e.g. in a range of 1 to 50 g/l, and preferably 20 to 40 g/l.
  • the preferred bath for pure nickel plating is a Watts bath containing nickel sulphate, nickel chloride and boric acid.
  • a preferred bath for nickel-bismuth plating is a citrate-gluconate bath containing nickel sulphate, nickel chloride, (NH 4 ) 2 SO 4 , bismuth concentrate, sodium citrate and sodium gluconate.
  • Preferred concentration ranges of these substances are 100 to 180 g/l of NiSO 4 .6H 2 O, 10 to 50 g/l of NiCl 2 .6H 2 O, 1 to 10 ml/l of a bismuth concentrate containing 100 g/l of Bi, 10 to 50 g/l of (NH 4 ) 2 SO 4 , 100 to 180 g/l of sodium citrate.2H 2 O, and 10 to 50 g/l of sodium gluconate.
  • This bath may be used for pure nickel plating as well, in which case the bismuth concentrate is omitted.
  • the pre-treatment is already effective at elevated temperatures of from above room temperature to less than, or up to, 95° C., and preferably in the range of 55° C. to 80° C. This is a great advantage, since working at lower temperatures makes the introduction into a strip plating line much easier, because evaporation losses will be limited. Furthermore, aluminium dissolution is much lower at temperatures below 70° C., thereby increasing the lifetime of the activation bath.
  • the pre-treatment bath is preferably maintained at temperatures between 55° C. and 80° C., and most preferred between about 60° C. and 70° C.
  • the activation current is cathodic. As demonstrated by the examples, the current density is not critical to the quality of the final product. The same applies to activation time of the product in the pre-treatment bath.
  • the activation current of the cathodic activation is preferably in a range of ⁇ 200 to ⁇ 2000 A/Nm 2 , and more preferably in a range of ⁇ 500 to ⁇ 1400 A/m 2 .
  • the time spent by the product in the pre-treatment bath is typically in the range of 1 to 50 sec., and preferably in the range of 5 to 15 sec.
  • the average thickness of the applied metal layer of Ni, Co, Fe or alloys of each of these metals is preferably less than 2 ⁇ m, more preferably less than 1.0 ⁇ m, and even more preferably in a range of 0.2 to 1.0 ⁇ m.
  • the method is preferably carried out as a continuous plating operation, which allows the continuous treatment of an infinite strip of metal.
  • a further metal layer may be applied on top of the layer of Ni, Fe, Co, or alloys thereof, in order to improve for example the corrosion resistance of the final product.
  • a thin layer of tin can be applied onto the nickel-layer on a brazing sheet product, which results in a significant improvement of the post-braze corrosion resistance.
  • the method according to this invention may include the additional step of degreasing of the surface prior to the cathodic activation and/or the electroplating step in order the clean the surface.
  • full hard material is easier to slit than soft annealed material.
  • the coils may be soft annealed afterwards.
  • the aluminium workpiece is a brazing sheet product, the brazing sheet product including a core layer and a clad layer formed of a brazing alloy including aluminium and 2-18 wt. % silicon, preferably in the range of 7 to 14%, (such as AA4343 and 4045 alloys), and whereby the metal layer is applied on the clad layer.
  • a brazing alloy including aluminium and 2-18 wt. % silicon, preferably in the range of 7 to 14%, (such as AA4343 and 4045 alloys)
  • the metal layer of nickel, iron, cobalt or alloys of each of these metals act as a braze-promoting element during brazing.
  • the clad layer further comprises a wetting agent as alloying element in a range of up to 1 wt. % in order to improve the wettability of the clad alloy during the brazing process.
  • the wetting agent is selected from the group consisting of lead, bismuth, lithium, antimony, tin, silver, thallium and any mixture thereof.
  • the aluminium workpiece is an aluminium conductor, and preferably made of an alloy selected from the group consisting of AA1370, AA1110 and AA6101.
  • the aluminium conductor can be in the form of an aluminium strip or aluminium wire or aluminium tube.
  • the applied metal layer is preferably consisting of nickel in order to improve the electrical contact properties.
  • the aluminium conductors can be used for the transmission of electrical and/or thermal energy. These conductors are usually in the form of bars, wire or cables when used as electrical conductors, and in the form of strips, bars or tubes when used as thermal conductors.
  • an aluminium alloy product preferably a brazing sheet product, electroplated with a metal layer selected from the group consisting of nickel, iron, cobalt and alloys thereof manufactured with the method of the invention as set out in the present specification and claims.
  • a brazing sheet product can be applied successfully in a Controlled Atmosphere Brazing (“CAB”) process in the absence of a brazing flux.
  • CAB Controlled Atmosphere Brazing
  • the aluminium alloy product according to the invention has an excellently adhering nickel or nickel-bismuth coating.
  • the product is an aluminium alloy brazing sheet comprising a core, a clad layer and a nickel-containing layer plated on top of the clad layer.
  • This brazing sheet will have good brazeability and low manufacturing costs. It may either contain a wetting agent like Bi in the clad alloy, or in the nickel-containing layer.
  • aluminium brazing sheets products of 0.4 mm thickness have been used for plating with a nickel or nickel-alloy layer having an average thickness of 0.5 ⁇ m.
  • the aluminium brazing sheets used consisted of an AA3003-series aluminium core alloy conventionally clad on both sides with an AlSi brazing alloy, whereby clad layer A contained, in wt. %, 10% Si, 1.5% Mg and 0.08% Bi, whereas clad layer B contained, in wt. %, 12% Si and no Mg or Bi.
  • Ni or Ni-Bi plating using a current density of ⁇ 1000A/m 2 , followed by rinsing.
  • the cathodic activation bath in accordance with the invention was prepared on basis of sulphuric acid (see Table 1). Nickel sulphate was selected to supply nickel-ions to the solution, and preferably boric acid was added as buffer. As an alternative a fluoride based activation bath was used (see Table 2) and consisting of anodic activation at a current density of +1000A/m 2 , and which is disclosed in U.S. Pat. No. 6,780,303 B2, incorporated herein by reference. The cathodic activation was carried at various temperatures. Two Samples 10 and 11 have been carried out using the same activation bath but whereby the current was reversed such that anodic activation occurred.
  • a nickel layer was plated from a Watts bath (see Table 3) or a nickel-bismuth alloy layer from a citrate-gluconate bath (see Table 4).
  • the quality of the resulting plated substrates were evaluated using an adhesion test and a brazeability test.
  • the adhesion tests consisted on the Erichsen dome test (cup height of 5 mm), whereafter adhesive tape (Scotch Tape 3M No. 610) is applied to the deformed area and pulled off in one move. Adhesion is quantified by classifying the amount of nickel on the tape. An overall adhesion assessment was rated from 1 (poor) to 10 (excellent), wherein a level of 6 was considered acceptable as it was comparable to existing commercially available brazing sheet with a Ni-Pb layer.
  • a wetting agent such as Bi is favourable for the brazeability performance of the resultant brazing sheet product. From the Samples 1 and 8 it can be seen that the wetting agent might be added either to the Ni layer or to the brazing clad layer without affecting the adhesion or the brazeability. Adding the wetting agent to both the clad layer and the nickel layer has no adverse effect on the brazeability.

Abstract

Disclosed is a method of applying a metal layer onto at least one surface of an aluminium or aluminium alloy workpiece, including the steps of pre-treating the surface by cathodic activation in a pre-treatment bath containing sulphuric acid and metal-ions selected from the group consisting of nickel, iron and cobalt, and applying a metal layer by electroplating the pre-treated workpiece. The metal layer is selected from the group consisting of nickel, iron, cobalt, and alloys thereof.

Description

    CROSS-REFERENCE TO RELATED APPLICATIONS
  • This claims the benefit of U.S. provisional patent application No. 60/644,530, filed Jan. 19, 2005 and European patent application number EP-05075082.7 filed Jan. 19, 2005, both incorporated herein by reference in their entirety.
  • FIELD OF THE INVENTION
  • The present invention relates to a method of applying a metal layer onto at least one surface of an aluminium or aluminium alloy workpiece or article, comprising the steps of a simple pre-treating step of cleaning and activating the surface and yet producing good adhesion of the subsequently applied metal layer. The invention also relates to an aluminium alloy product plated on at least one surface with a metal layer. More specifically, the invention relates to a method of applying a metal layer of a braze-promoting metal onto the clad layer of an aluminium alloy brazing sheet product to be used in a fluxless brazing operation.
  • As will be appreciated herein below, except as otherwise indicated, all alloy designations and temper designations refer to the Aluminium Association designations in Aluminium Standards and Data and the Registration Records, as published by the Aluminium Association.
  • BACKGROUND OF THE INVENTION
  • Nickel plating of aluminium products is widely used because nickel provides a bright, shiny appearance, is long lasting and can conduct electricity. Another, more particular use of nickel plating is made in the manufacture of brazing sheet products. Aluminium alloy brazing sheets comprise an aluminium alloy core and a clad layer of filler alloy on one or both sides. Aluminium brazing sheets are widely used, e.g., in the production of heat exchangers.
  • However, the use of aluminium-silicon alloys as filler material is problematic because the aluminium oxide layer has to be disrupted during brazing. This may be effected by applying a chemical flux onto the workpiece before brazing. Fluxes for use in brazing aluminium alloys usually consist of mixtures of alkali and alkaline earth chlorides and fluorides or cryolite. The flux operates at the brazing temperature to disrupt, spread and dissolve the oxide film. However, applying the chemical flux onto the workpiece is a rather laborious and therefore expensive process.
  • In the past, fluxless brazing techniques have therefore been developed and employed as described for example in US2003/0098338-A1, incorporated herein by reference in its entirety. In one such technique, a braze-promoting metal of cobalt, iron, or more preferably nickel, is coated on a part to be brazed. During brazing, the nickel reacts exothermically with the underlying aluminium alloy, thereby disrupting the aluminium oxide layer and permitting the underlying molten aluminium clad metal to flow together and join. As this method does not require a fluoride flux, it is also suitable for utilization with magnesium-enriched aluminium alloys, such as are beneficially used in heat-exchanger constructions.
  • In addition to the nickel, iron or cobalt coating, a wetting agent may also be added in order to improve the wettability of the clad alloy during the brazing process. However, nickel plating requires extensive pre-treatment of the metal surface such as cleaning, etching, desmutting, etc. This is again due to the presence of the tenacious oxide layer. If the aluminium alloy surface has not been properly pre-treated, the nickel coating will either have poor adhesion, or will be contaminated and thereby impede the brazeability of the product. Therefore, nickel plating with all necessary pre-treatment steps is an expensive and environmentally unfriendly process.
  • SUMMARY OF THE INVENTION
  • It is an object of the invention to provide a method for applying by electroplating a metal layer onto an aluminium alloy product, which method requires as few steps as possible, and does not require the use of fluoride containing components.
  • It is furthermore an object of the present invention to obtain a metal coated aluminium alloy product, wherein the applied metal coating adheres well and may serve to break up the oxide layer during a subsequent brazing operation.
  • The present invention solves one or more of these objects through a method of applying a metal coating and an aluminium alloy product.
  • The method of applying a metal layer onto at least one surface of an aluminium or aluminium alloy workpiece, comprises the steps of pre-treating the surface by cathodic activation in a pre-treatment bath containing sulphuric acid and metal-ions selected from the group consisting of nickel, iron and cobalt, and applying a metal layer by electroplating the pre-treated workpiece, and wherein the metal layer is selected from the group consisting of nickel, iron, cobalt, and alloys thereof. It will be immediately clear to the skilled person that when the applied metal layer contains nickel or an a nickel-alloy that the pre-treatment bath should contain nickel-ions, and where iron or cobalt or alloys thereof are being applied that the pre-treatment bath contains iron-ions and cobalt-ions respectively.
  • BRIEF DESCRIPTION OF THE DRAWING
  • FIG. 1 shows an angle-on-coupon for brazing tests.
  • DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
  • The invention is based on the finding that direct metal, for example nickel, plating of aluminium alloy products is possible after cathodic activation in a simple sulphuric acid solution to which only nickel ions, e.g. in the form of nickel sulphate, has been added. No fluoride components are needed in this activation process. Because the activation bath contains the same ingredients as a Watts bath which is preferably used as nickel plating bath, cross-contamination is excluded. Also, no problems in effluent treatment are expected.
  • It is believed that, during cathodic activation in the sulphuric acid solution containing nickel ions, nickel nuclei may be created through the thin aluminium oxide film on the surface, thereby forming anchor spots for the nickel layer which is applied in a subsequent plating step. Thus, the cathodic activation step has the same effect as the creation of a thin bonding layer between the aluminium surface and the nickel coating. The same applies mutatis mutandis for the situation where iron or cobalt is being used.
  • The pre-treatment bath preferably contains about 15 to 200 g/l, and preferably 80 to 150 g/l, of NiSO4.H2O, and about 50 to 350 g/l, preferably about 150 to 250 g/l of H2SO4. In a preferred embodiment, the pre-treatment bath also contains boric acid as a buffer, e.g. in a range of 1 to 50 g/l, and preferably 20 to 40 g/l.
  • The preferred bath for pure nickel plating is a Watts bath containing nickel sulphate, nickel chloride and boric acid.
  • A preferred bath for nickel-bismuth plating is a citrate-gluconate bath containing nickel sulphate, nickel chloride, (NH4)2SO4, bismuth concentrate, sodium citrate and sodium gluconate. Preferred concentration ranges of these substances are 100 to 180 g/l of NiSO4.6H2O, 10 to 50 g/l of NiCl2.6H2O, 1 to 10 ml/l of a bismuth concentrate containing 100 g/l of Bi, 10 to 50 g/l of (NH4)2SO4, 100 to 180 g/l of sodium citrate.2H2O, and 10 to 50 g/l of sodium gluconate. This bath may be used for pure nickel plating as well, in which case the bismuth concentrate is omitted.
  • It has been found that the pre-treatment is already effective at elevated temperatures of from above room temperature to less than, or up to, 95° C., and preferably in the range of 55° C. to 80° C. This is a great advantage, since working at lower temperatures makes the introduction into a strip plating line much easier, because evaporation losses will be limited. Furthermore, aluminium dissolution is much lower at temperatures below 70° C., thereby increasing the lifetime of the activation bath. Hence, the pre-treatment bath is preferably maintained at temperatures between 55° C. and 80° C., and most preferred between about 60° C. and 70° C.
  • The activation current is cathodic. As demonstrated by the examples, the current density is not critical to the quality of the final product. The same applies to activation time of the product in the pre-treatment bath. The activation current of the cathodic activation is preferably in a range of −200 to −2000 A/Nm2, and more preferably in a range of −500 to −1400 A/m2. The time spent by the product in the pre-treatment bath is typically in the range of 1 to 50 sec., and preferably in the range of 5 to 15 sec.
  • The average thickness of the applied metal layer of Ni, Co, Fe or alloys of each of these metals, is preferably less than 2 μm, more preferably less than 1.0 μm, and even more preferably in a range of 0.2 to 1.0 μm.
  • The method is preferably carried out as a continuous plating operation, which allows the continuous treatment of an infinite strip of metal.
  • In an optional additional step a further metal layer may be applied on top of the layer of Ni, Fe, Co, or alloys thereof, in order to improve for example the corrosion resistance of the final product. For example a thin layer of tin can be applied onto the nickel-layer on a brazing sheet product, which results in a significant improvement of the post-braze corrosion resistance.
  • The method according to this invention may include the additional step of degreasing of the surface prior to the cathodic activation and/or the electroplating step in order the clean the surface.
  • To avoid work hardening of soft annealed coils while processing them in a (vertical) plating line, it is advantageous to plate full hard material. Moreover, full hard material is easier to slit than soft annealed material. Thus, it is preferred to plate wide coils in full hard condition and split them afterwards into multiple coils of desired width, thereby reducing conversion costs. The coils may be soft annealed afterwards.
  • In an embodiment of the method according to the invention the aluminium workpiece is a brazing sheet product, the brazing sheet product including a core layer and a clad layer formed of a brazing alloy including aluminium and 2-18 wt. % silicon, preferably in the range of 7 to 14%, (such as AA4343 and 4045 alloys), and whereby the metal layer is applied on the clad layer. The metal layer of nickel, iron, cobalt or alloys of each of these metals act as a braze-promoting element during brazing.
  • In a preferred embodiment of the brazing sheet product the clad layer further comprises a wetting agent as alloying element in a range of up to 1 wt. % in order to improve the wettability of the clad alloy during the brazing process. And preferably the wetting agent is selected from the group consisting of lead, bismuth, lithium, antimony, tin, silver, thallium and any mixture thereof.
  • In another embodiment of the method according to the invention the aluminium workpiece is an aluminium conductor, and preferably made of an alloy selected from the group consisting of AA1370, AA1110 and AA6101. The aluminium conductor can be in the form of an aluminium strip or aluminium wire or aluminium tube. For the embodiment the applied metal layer is preferably consisting of nickel in order to improve the electrical contact properties. The aluminium conductors can be used for the transmission of electrical and/or thermal energy. These conductors are usually in the form of bars, wire or cables when used as electrical conductors, and in the form of strips, bars or tubes when used as thermal conductors.
  • In a further aspect of the invention there is provided an aluminium alloy product, preferably a brazing sheet product, electroplated with a metal layer selected from the group consisting of nickel, iron, cobalt and alloys thereof manufactured with the method of the invention as set out in the present specification and claims. Such a brazing sheet product can be applied successfully in a Controlled Atmosphere Brazing (“CAB”) process in the absence of a brazing flux.
  • As shown by the following examples, the aluminium alloy product according to the invention has an excellently adhering nickel or nickel-bismuth coating. In a particularly preferred embodiment, the product is an aluminium alloy brazing sheet comprising a core, a clad layer and a nickel-containing layer plated on top of the clad layer. This brazing sheet will have good brazeability and low manufacturing costs. It may either contain a wetting agent like Bi in the clad alloy, or in the nickel-containing layer.
  • The following non-limiting examples illustrate the invention.
  • EXAMPLES
  • Two different types aluminium brazing sheets products of 0.4 mm thickness have been used for plating with a nickel or nickel-alloy layer having an average thickness of 0.5 μm. The aluminium brazing sheets used consisted of an AA3003-series aluminium core alloy conventionally clad on both sides with an AlSi brazing alloy, whereby clad layer A contained, in wt. %, 10% Si, 1.5% Mg and 0.08% Bi, whereas clad layer B contained, in wt. %, 12% Si and no Mg or Bi.
  • In producing nickel plated brazing sheet products the following procedure has been used:
  • Cleaning for 180 sec. at 50° C. using 35 g/l ChemTec 30014 (a commercial available bath), followed by rinsing;
  • Activation using a current density of −1000A/m2, followed by rinsing;
  • Ni or Ni-Bi plating using a current density of −1000A/m2, followed by rinsing.
  • The cathodic activation bath in accordance with the invention was prepared on basis of sulphuric acid (see Table 1). Nickel sulphate was selected to supply nickel-ions to the solution, and preferably boric acid was added as buffer. As an alternative a fluoride based activation bath was used (see Table 2) and consisting of anodic activation at a current density of +1000A/m2, and which is disclosed in U.S. Pat. No. 6,780,303 B2, incorporated herein by reference. The cathodic activation was carried at various temperatures. Two Samples 10 and 11 have been carried out using the same activation bath but whereby the current was reversed such that anodic activation occurred.
  • After activation, either a nickel layer was plated from a Watts bath (see Table 3) or a nickel-bismuth alloy layer from a citrate-gluconate bath (see Table 4).
  • The quality of the resulting plated substrates were evaluated using an adhesion test and a brazeability test. The adhesion tests consisted on the Erichsen dome test (cup height of 5 mm), whereafter adhesive tape (Scotch Tape 3M No. 610) is applied to the deformed area and pulled off in one move. Adhesion is quantified by classifying the amount of nickel on the tape. An overall adhesion assessment was rated from 1 (poor) to 10 (excellent), wherein a level of 6 was considered acceptable as it was comparable to existing commercially available brazing sheet with a Ni-Pb layer.
  • On a laboratory scale of testing the brazing tests were carried out in a small quartz furnace. Small coupons of 25 mm×25 mm were cut out of the nickel-bismuth-plated sheets. A small strip of a bare AA3003 alloy measuring 30 mm×7 mm×1 mm was bent in the centre to an angle of 45° and laid on the coupons (see FIG. 1). The angle-on-coupon samples were heated under flowing nitrogen, with heating from room temperature to 580° C., dwell time at 580° C. for 1 minute, cooling from 580° C. to room temperature. The brazing process was judged on possible formation of wrinkles, capillary depression and fillet formation. An overall assessment was given where: (−)=poor brazeability, (±)=fair brazeability, and (+)=good brazeability.
  • The results of the experiments carried out and the adhesion and brazing performance for the various samples are summarized in Table 5.
    TABLE 1
    Composition of the cathodic activation bath
    NiSO4.6H2O 100 g/l
    96% H2SO4 (S.G. 1.84 kg l−1) 200 g/l 113.2 ml/l
    H3BO3 30 g/l
  • TABLE 2
    Composition of the hydrofluoric acid bath
    NiCl2.6H2O 125 g/l
    40% HF (S.G. 1.13 kg l−1) 2.7 g/l 6 ml/l
    H3BO3 12.5 g/l
  • TABLE 3
    Composition of the Watts bath
    NiSO4.6H2O 270 g/l
    NiCl2.6H2O 50 g/l
    H3BO3 30 g/l
  • TABLE 4
    Composition of the citrate-gluconate bath
    NiSO4.6H2O 142 g/l
    NiCl2.6H2O 30 g/l
    (NH4)2SO4 34 g/l
    Na-citrate.2H2O 140 g/l
    Na-gluconate 30 g/l
    bismuth concentrate (100 g/l Bi) 5 ml/l
  • TABLE 5
    Summary of the experiments carried and the results on adhesion
    and brazeability
    Activation Plating
    Clad Activation Temperature Ni/ Braze-
    Sample layer bath (° C.) Ni—Bi Adhesion ability
    1 B H2SO4 70 Ni—Bi 5 ±
    2 B H2SO4 93 Ni—Bi 4 ±
    3 A H2SO4 50 Ni 6 +
     4* A HF 50 Ni 9 +
    5 A none Ni 1
    6 A H2SO4 45 Ni 4 +
    7 A H2SO4 60 Ni 9 +
    8 A H2SO4 70 Ni 10 +
    9 A H2SO4 93 Ni 9 +
    10* A H2SO4 70 Ni 9
    11* A H2SO4 93 Ni 10

    *Samples 4, 10 and 11 involved anodic activation instead of cathodic activation as per Samples 1 to 3 and 6 to 9.
  • From the comparison of Samples 3, 4 and 5 it can be seen that if no activation is used both the adhesion and the brazeability is poor. Whereas a hydrofluoric acid bath obtains good adhesion and good brazeability, comparable to a sulphuric acid bath. However, a hydrofluoric acid bath contains fluoride and is therefore not the environmentally preferred method.
  • From examples 10 and 11 it can be seen that anodic activation provides excellent adhesion, but brazeability is seriously undermined possibly due to the formation of an oxide film. In accordance with the invention it has been found that both good adhesion and brazeability were obtained by cathodic activation. However, for those applications were brazeability is not required such as with aluminium conductors it might be a valuable pre-treatment method.
  • The temperature of the cathodic activation bath appeared to have a strong influence on the adhesion of the plated Ni layer. Sample 7 shows that adhesion and brazeability are still excellent at temperatures of about 60° C. However, if the temperature is lowered further to below 50° C. (Sample 6), the adhesion level becomes unacceptable. From Samples 1 and 2 and 8 and 9 it can be seen that neither adhesion nor brazeability suffers when the temperature is lowered from 93° C. to 70° C. This makes introduction into a continuous strip plating line much easier, because evaporation losses will be limited. Furthermore, aluminium dissolution is much less at 70° C. or lower, thereby increasing the lifetime of the activation bath.
  • The addition of a wetting agent such as Bi is favourable for the brazeability performance of the resultant brazing sheet product. From the Samples 1 and 8 it can be seen that the wetting agent might be added either to the Ni layer or to the brazing clad layer without affecting the adhesion or the brazeability. Adding the wetting agent to both the clad layer and the nickel layer has no adverse effect on the brazeability.
  • Thus, it has been demonstrated that direct nickel plating of a brazing sheet product is possible after cathodic activation in a simple sulphuric acid solution to which only nickel sulphate is added. No fluoride is needed in this activation process. Because the activation bath contains the same ingredients as a Watts bath, cross-contamination is excluded. Also, no problems in effluent treatment are expected. Satisfying results are obtained at bath temperatures of about 60 ° C. The process can be operated in a reliable manner over a wide range of current densities and treatments times.
  • It is believed that similar results will be obtained where iron or cobalt instead of nickel is used as braze-promoting metal on the brazing sheet product.
  • Having now fully described the invention, it will be apparent to one of ordinary skill in the art that many changes and modifications can be made without departing from the spirit or scope of the invention as herein described.

Claims (32)

1. A method of applying a metal layer onto at least one surface of an aluminium or aluminium alloy workpiece, comprising the steps of pre-treating the surface by cathodic activation in a pre-treatment bath containing sulphuric acid and metal-ions selected from the group consisting of nickel, iron and cobalt, and applying a metal layer by electroplating the pre-treated workpiece, and wherein the metal layer is selected from the group consisting of nickel, iron, cobalt, and alloys thereof.
2. The method according to claim 1, wherein the pre-treatment bath comprises 15 to 200 g/l of NiSO4.H2O and 50 to 350 g/l of H2SO4.
3. The method according to claim 1, wherein the pre-treatment bath comprises 80 to 150 g/l of NiSO4.H2O and 150 to 250 g/l of H2SO4.
4. The method according to claim 1, wherein the pre-treatment bath further comprises boric acid (H3BO3).
5. The method according to claim 1, wherein the pre-treatment bath further comprises 1 to 50 g/l boric acid (H3BO3).
6. The method according to claim 1, wherein the pre-treatment bath further comprises 20 to 40 g/l boric acid (H3BO3).
7. The method according to claim 1, wherein the plating bath comprises a Watts bath.
8. The method according to any one of claims 1, wherein the plating bath comprises a Watts bath comprising a mixture of nickel sulphate (NiSO4), nickel chloride (NiCl2) and boric acid (H3BO3).
9. The method according to claim 1, wherein the plating bath comprises a citrate-gluconate bath comprising a mixture of NiSO4, and (NH4)2SO4 and sodium citrate and sodium gluconate.
10. The method according to claim 1, wherein the plating bath comprises a citrate-gluconate bath comprising a mixture of NiSO4, nickel chloride, (NH4)2SO4, bismuth concentrate, sodium citrate and sodium gluconate.
11. The method according to claim 1, wherein the plating bath comprises a citrate-gluconate bath comprising a mixture of 100 to 180 g/l of NiSO4.6H2O, 10 to 50 g/l of NiCl2.6H2O, 1 to 10 ml/l of a bismuth concentrate containing 100 g/l of Bi, 10 to 50 g/l of (NH4)2SO4, 100 to 180 g/l of sodium citrate.2H2O, and 10 to 50 g/l of sodium gluconate.
12. The method according to claim 1, wherein the plating bath comprises a citrate-gluconate bath comprising a mixture of NiSO4, nickel chloride, (NH4)2SO4, sodium citrate and sodium gluconate.
13. The method according to claim 1, wherein the plating bath comprises a citrate-gluconate bath comprising a mixture of 100 to 180 g/l of NiSO4.6H2O, 10 to 50 g/l of NiCl2.6H2O, 10 to 50 g/l of (NH4)2SO4, 100 to 180 g/l of sodium citrate.2H2O, and 10 to 50 g/l of sodium gluconate.
14. The method according to claim 1, wherein the pre-treatment bath is devoid of any fluoride containing components.
15. The method according to claim 1, wherein the temperature of the pre-treatment bath is maintained at an elevated temperature in a range of above room temperature to 95° C.
16. The method according to claim 1, wherein the temperature of the pre-treatment bath is maintained at a temperature in a range of 55° C. to 80° C.
17. The method according to claim 1, wherein the temperature of the pre-treatment bath is maintained at a temperature in a range of between about 60° C. and 70° C.
18. The method according to claim 1, wherein the cathodic activation applies an activation current in a range of −200 to −2000 A/m2,
19. The method according to claim 1, wherein the cathodic activation applies an activation current in a range of −500 to −1400 A/m2.
20. The method according to claim 1, wherein the time spent by the product in the pre-treatment bath is in the range of 1 to 50 sec.
21. The method according to claim 1, wherein the time spent by the product in the pre-treatment bath is in the range of 5 to 15 sec.
22. The method according to claim 1, wherein the applied metal layer has an average thickness of less than 2 μm.
23. The method according to claim 1, wherein the applied metal layer has an average thickness of less than 1.0 μm.
24. The method according to claim 1, wherein the applied metal layer has an average thickness of 0.2 to 1.0 μm.
25. The method according to claim 1, further comprising applying a second metal layer on top of the layer of Ni, Fe, Co, or alloys thereof.
26. The method according to claim 1, wherein the layer of Ni, Fe, Co, or alloys thereof is a nickel-containing layer, further comprising applying a tin-containing layer on top of the nickel-containing layer.
27. The method according to claim 1, wherein the method is carried out as a continuous plating operation.
28. The method according to claim 1, wherein the aluminium workpiece is a brazing sheet product, the brazing sheet product including a core layer and a clad layer formed of a brazing alloy including aluminium and 2-18 wt. % silicon, and whereby the metal layer is applied on the clad layer.
29. The method according to claim 28, wherein the clad layer further comprises as alloying element a wetting agent in a range of up to 1 wt. %.
30. The method according to claim 29, wherein the wetting agent is selected from the group consisting of lead, bismuth, lithium, antimony, tin, silver, thallium and any mixture thereof.
31. The method according to claim 1, wherein the aluminium workpiece is an aluminium conductor, and preferably made of an alloy selected from the group consisting of AA1370, AA1110 and AA6101.
32. An aluminium alloy product, electrolytically plated with a metal layer selected from the group consisting of nickel, iron, cobalt and alloys thereof by using the method of claim 1.
US11/320,488 2005-01-19 2005-12-29 Method of electroplating and pre-treating aluminium workpieces Abandoned US20060157352A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US11/320,488 US20060157352A1 (en) 2005-01-19 2005-12-29 Method of electroplating and pre-treating aluminium workpieces

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US64453005P 2005-01-19 2005-01-19
EP05075082 2005-01-19
EP05075082.7 2005-01-19
US11/320,488 US20060157352A1 (en) 2005-01-19 2005-12-29 Method of electroplating and pre-treating aluminium workpieces

Publications (1)

Publication Number Publication Date
US20060157352A1 true US20060157352A1 (en) 2006-07-20

Family

ID=36682746

Family Applications (1)

Application Number Title Priority Date Filing Date
US11/320,488 Abandoned US20060157352A1 (en) 2005-01-19 2005-12-29 Method of electroplating and pre-treating aluminium workpieces

Country Status (1)

Country Link
US (1) US20060157352A1 (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102534715A (en) * 2012-02-18 2012-07-04 沈阳飞机工业(集团)有限公司 Process method for electroplating copper on surface of micro aluminum wire
AT13521U1 (en) * 2013-01-18 2014-02-15 Plansee Se module
CN110121575A (en) * 2016-12-27 2019-08-13 古河电气工业株式会社 Finish materials and the part made using the finish materials
EP3467152A4 (en) * 2016-06-03 2019-12-04 Furukawa Electric Co., Ltd. Surface treatment material, production method thereof, and component formed using surface treatment material
EP3564413A4 (en) * 2016-12-27 2020-08-12 Furukawa Electric Co., Ltd. Surface treatment material and method for manufacturing same, and article fabricated using surface treatment material
EP3564412A4 (en) * 2016-12-27 2020-09-02 Furukawa Electric Co., Ltd. Surface treatment material and article fabricated using same
EP3604624A4 (en) * 2017-03-31 2021-01-13 Furukawa Electric Co., Ltd. Plated wire rod material, method for producing same, and cable, electric wire, coil and spring member, each of which is formed using same

Citations (54)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2745799A (en) * 1951-03-16 1956-05-15 Pechiney Prod Chimiques Sa Processes for coating aluminum and alloys thereof
US2821014A (en) * 1951-05-31 1958-01-28 Aluminum Co Of America Composite aluminous metal article
US2821505A (en) * 1954-04-01 1958-01-28 John G Beach Process of coating metals with bismuth or bismuth-base alloys
US3482305A (en) * 1968-07-11 1969-12-09 Borg Warner Method of bonding aluminum
US3489657A (en) * 1968-09-30 1970-01-13 Sylvania Electric Prod Process for producing solderable aluminum materials
US3597658A (en) * 1969-11-26 1971-08-03 Rca Corp High current semiconductor device employing a zinc-coated aluminum substrate
US3692583A (en) * 1971-03-01 1972-09-19 Fmc Corp Desmutting etched aluminum alloys
US3862018A (en) * 1971-11-12 1975-01-21 Pat F Mentone Rigidizing process for screens with aluminum frames
US3881999A (en) * 1973-05-25 1975-05-06 Westinghouse Electric Corp Method of making abrasion resistant coating for aluminum base alloy
US3896009A (en) * 1974-05-21 1975-07-22 Kioritz Corp Aluminum alloy cylinder
US3963454A (en) * 1974-12-10 1976-06-15 Reynolds Metals Company Brazing materials
US3970237A (en) * 1972-11-07 1976-07-20 Borg-Warner Corporation Method of brazing aluminum parts
US4028200A (en) * 1975-06-24 1977-06-07 Borg-Warner Corporation Plating baths for depositing cobalt-lead nickel-lead alloys or combinations thereof and method of coating aluminum articles therewith
US4097342A (en) * 1975-05-16 1978-06-27 Alcan Research And Development Limited Electroplating aluminum stock
US4126522A (en) * 1976-08-09 1978-11-21 Telefonaktiebolaget L M Ericsson Method of preparing aluminum wire for electrical conductors
US4157154A (en) * 1977-11-21 1979-06-05 Hughes Aircraft Company Method for forming patterns of brazing alloy
US4164454A (en) * 1977-11-01 1979-08-14 Borg-Warner Corporation Continuous line for plating on metal strip material
US4177325A (en) * 1977-08-31 1979-12-04 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Aluminium or copper substrate panel for selective absorption of solar energy
US4225397A (en) * 1978-11-06 1980-09-30 Ford Motor Company New and unique aluminum plating method
US4346128A (en) * 1980-03-31 1982-08-24 The Boeing Company Tank process for plating aluminum substrates including porous aluminum castings
US4388159A (en) * 1981-05-18 1983-06-14 Borg-Warner Corporation Surface preparation of aluminum articles
US4397721A (en) * 1981-02-12 1983-08-09 Fokker B.V. Pickling of aluminum
US4602731A (en) * 1984-12-24 1986-07-29 Borg-Warner Corporation Direct liquid phase bonding of ceramics to metals
US4721653A (en) * 1985-09-25 1988-01-26 Kabushiki Kaisha Kobe Seiko Sho Vacuum brazing sheet for use in aluminum heat exchanger
US4735867A (en) * 1985-12-06 1988-04-05 Kaiser Aluminum & Chemical Corporation Corrosion resistant aluminum core alloy
US4741811A (en) * 1987-01-06 1988-05-03 Aluminium Pechiney Process and apparatus for electrolytically depositing in a moving mode a continuous film of nickel on metal wire for electrical use
US5069980A (en) * 1990-02-08 1991-12-03 Sumitmo Light Metal Industries, Ltd. Vacuum-brazing aluminum cladding material consisting of Al or Al alloy core and two superposed aluminum alloy clads which cover at least one surface of the core
US5234574A (en) * 1991-01-30 1993-08-10 Sumitomo Metal Industries, Ltd. Process for direct zinc electroplating of aluminum strip
US5246565A (en) * 1992-05-07 1993-09-21 The United States Of America As Represented By The United States Department Of Energy High adherence copper plating process
US5245847A (en) * 1991-02-07 1993-09-21 Sumitomo Metal Industries, Ltd. Process for zinc electroplating of aluminum strip
US5368719A (en) * 1993-05-12 1994-11-29 Hughes Aircraft Company Method for direct plating of iron on aluminum
US5422191A (en) * 1994-02-14 1995-06-06 Kaiser Aluminum & Chemical Corporation Aluminum-lithium filler alloy for brazing
US5466360A (en) * 1994-10-13 1995-11-14 Robert Z. Reath Method for preparing aluminum for subsequent electroplating
US5516419A (en) * 1994-05-26 1996-05-14 Hughes Aircraft Company Hard iron plating of aluminum/aluminum alloys using sulfamate/sulfate solutions
US5601695A (en) * 1995-06-07 1997-02-11 Atotech U.S.A., Inc. Etchant for aluminum alloys
US5643434A (en) * 1995-02-02 1997-07-01 Aluminum Pechiney Process for coating the face of a part made of aluminum or aluminum alloy
US5961853A (en) * 1993-11-26 1999-10-05 Ford Global Technologies, Inc. Weld/brazing of light metal alloys
US5997721A (en) * 1994-12-19 1999-12-07 Alcan International Limited Cleaning aluminum workpieces
US6060174A (en) * 1999-05-26 2000-05-09 Siemens Westinghouse Power Corporation Bond coats for turbine components and method of applying the same
US6129262A (en) * 1997-02-24 2000-10-10 Ford Global Technologies, Inc. Fluxless brazing of unclad aluminum using selective area plating
US6165630A (en) * 1996-05-13 2000-12-26 Corus Bausysteme Gmbh Galvanized aluminum sheet
US6379818B1 (en) * 1999-05-21 2002-04-30 Corus Aluminium Walzprodukte Gmbh Brazing sheet product and method of its manufacture
US6383661B2 (en) * 2000-05-18 2002-05-07 Corus Aluminium Walzprodukte Gmbh Method of manufacturing an aluminum product
US6391476B2 (en) * 2000-03-10 2002-05-21 Corus Aluminium Walzprodukte Gmbh Brazing sheet product and method of manufacturing an assembly using the brazing sheet product
US6503640B2 (en) * 2000-05-19 2003-01-07 Corus Aluminium Walzeprodukte Gmbh Method of manufacturing an assembly of brazed dissimilar metal components
US6528468B2 (en) * 1999-12-01 2003-03-04 Nippon Paint Co., Ltd. Pickling agent for the chemical conversion coating of heat exchanger, method of pickling heat exchanger
US6568584B2 (en) * 2000-07-26 2003-05-27 Corus Aluminium Walzprodukte Gmbh Nickel-plated brazing sheet product
US6596413B2 (en) * 2000-11-08 2003-07-22 Corus Aluminium Walzprodukte Gmbh Brazing product having a low melting point
US6599645B2 (en) * 2000-05-19 2003-07-29 Corus Aluminium Walzprodukte Gmbh Composite metal panel
US6605370B2 (en) * 2001-07-12 2003-08-12 Corus Aluminum Walzprodukte Gmbh Method of manufacturing an aluminium joined product
US6780303B2 (en) * 1999-07-22 2004-08-24 Aluminium Pechiney Continuous nickel plating process for an aluminum conductor and corresponding device
US6796484B2 (en) * 2001-02-02 2004-09-28 Corus Aluminum Walzprodukte Gmbh Nickel-plated brazing product having improved corrosion performance
US6815086B2 (en) * 2001-11-21 2004-11-09 Dana Canada Corporation Methods for fluxless brazing
US6846401B2 (en) * 2001-04-20 2005-01-25 Corus Aluminium Walzprodukte Gmbh Method of plating and pretreating aluminium workpieces

Patent Citations (56)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2745799A (en) * 1951-03-16 1956-05-15 Pechiney Prod Chimiques Sa Processes for coating aluminum and alloys thereof
US2821014A (en) * 1951-05-31 1958-01-28 Aluminum Co Of America Composite aluminous metal article
US2821505A (en) * 1954-04-01 1958-01-28 John G Beach Process of coating metals with bismuth or bismuth-base alloys
US3482305A (en) * 1968-07-11 1969-12-09 Borg Warner Method of bonding aluminum
US3489657A (en) * 1968-09-30 1970-01-13 Sylvania Electric Prod Process for producing solderable aluminum materials
US3597658A (en) * 1969-11-26 1971-08-03 Rca Corp High current semiconductor device employing a zinc-coated aluminum substrate
US3692583A (en) * 1971-03-01 1972-09-19 Fmc Corp Desmutting etched aluminum alloys
US3862018A (en) * 1971-11-12 1975-01-21 Pat F Mentone Rigidizing process for screens with aluminum frames
US3970237A (en) * 1972-11-07 1976-07-20 Borg-Warner Corporation Method of brazing aluminum parts
US3881999A (en) * 1973-05-25 1975-05-06 Westinghouse Electric Corp Method of making abrasion resistant coating for aluminum base alloy
US3896009A (en) * 1974-05-21 1975-07-22 Kioritz Corp Aluminum alloy cylinder
US3963454A (en) * 1974-12-10 1976-06-15 Reynolds Metals Company Brazing materials
US4097342A (en) * 1975-05-16 1978-06-27 Alcan Research And Development Limited Electroplating aluminum stock
US4028200A (en) * 1975-06-24 1977-06-07 Borg-Warner Corporation Plating baths for depositing cobalt-lead nickel-lead alloys or combinations thereof and method of coating aluminum articles therewith
US4126522A (en) * 1976-08-09 1978-11-21 Telefonaktiebolaget L M Ericsson Method of preparing aluminum wire for electrical conductors
US4177325A (en) * 1977-08-31 1979-12-04 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Aluminium or copper substrate panel for selective absorption of solar energy
US4164454A (en) * 1977-11-01 1979-08-14 Borg-Warner Corporation Continuous line for plating on metal strip material
US4157154A (en) * 1977-11-21 1979-06-05 Hughes Aircraft Company Method for forming patterns of brazing alloy
US4225397A (en) * 1978-11-06 1980-09-30 Ford Motor Company New and unique aluminum plating method
US4346128A (en) * 1980-03-31 1982-08-24 The Boeing Company Tank process for plating aluminum substrates including porous aluminum castings
US4397721A (en) * 1981-02-12 1983-08-09 Fokker B.V. Pickling of aluminum
US4388159A (en) * 1981-05-18 1983-06-14 Borg-Warner Corporation Surface preparation of aluminum articles
US4602731A (en) * 1984-12-24 1986-07-29 Borg-Warner Corporation Direct liquid phase bonding of ceramics to metals
US4721653A (en) * 1985-09-25 1988-01-26 Kabushiki Kaisha Kobe Seiko Sho Vacuum brazing sheet for use in aluminum heat exchanger
US4735867A (en) * 1985-12-06 1988-04-05 Kaiser Aluminum & Chemical Corporation Corrosion resistant aluminum core alloy
US4741811A (en) * 1987-01-06 1988-05-03 Aluminium Pechiney Process and apparatus for electrolytically depositing in a moving mode a continuous film of nickel on metal wire for electrical use
US5069980A (en) * 1990-02-08 1991-12-03 Sumitmo Light Metal Industries, Ltd. Vacuum-brazing aluminum cladding material consisting of Al or Al alloy core and two superposed aluminum alloy clads which cover at least one surface of the core
US5234574A (en) * 1991-01-30 1993-08-10 Sumitomo Metal Industries, Ltd. Process for direct zinc electroplating of aluminum strip
US5245847A (en) * 1991-02-07 1993-09-21 Sumitomo Metal Industries, Ltd. Process for zinc electroplating of aluminum strip
US5246565A (en) * 1992-05-07 1993-09-21 The United States Of America As Represented By The United States Department Of Energy High adherence copper plating process
US5368719A (en) * 1993-05-12 1994-11-29 Hughes Aircraft Company Method for direct plating of iron on aluminum
US5961853A (en) * 1993-11-26 1999-10-05 Ford Global Technologies, Inc. Weld/brazing of light metal alloys
US5422191A (en) * 1994-02-14 1995-06-06 Kaiser Aluminum & Chemical Corporation Aluminum-lithium filler alloy for brazing
US5516419A (en) * 1994-05-26 1996-05-14 Hughes Aircraft Company Hard iron plating of aluminum/aluminum alloys using sulfamate/sulfate solutions
US5466360A (en) * 1994-10-13 1995-11-14 Robert Z. Reath Method for preparing aluminum for subsequent electroplating
US5997721A (en) * 1994-12-19 1999-12-07 Alcan International Limited Cleaning aluminum workpieces
US5643434A (en) * 1995-02-02 1997-07-01 Aluminum Pechiney Process for coating the face of a part made of aluminum or aluminum alloy
US5601695A (en) * 1995-06-07 1997-02-11 Atotech U.S.A., Inc. Etchant for aluminum alloys
US6165630A (en) * 1996-05-13 2000-12-26 Corus Bausysteme Gmbh Galvanized aluminum sheet
US6129262A (en) * 1997-02-24 2000-10-10 Ford Global Technologies, Inc. Fluxless brazing of unclad aluminum using selective area plating
US6379818B1 (en) * 1999-05-21 2002-04-30 Corus Aluminium Walzprodukte Gmbh Brazing sheet product and method of its manufacture
US6060174A (en) * 1999-05-26 2000-05-09 Siemens Westinghouse Power Corporation Bond coats for turbine components and method of applying the same
US6780303B2 (en) * 1999-07-22 2004-08-24 Aluminium Pechiney Continuous nickel plating process for an aluminum conductor and corresponding device
US6528468B2 (en) * 1999-12-01 2003-03-04 Nippon Paint Co., Ltd. Pickling agent for the chemical conversion coating of heat exchanger, method of pickling heat exchanger
US6391476B2 (en) * 2000-03-10 2002-05-21 Corus Aluminium Walzprodukte Gmbh Brazing sheet product and method of manufacturing an assembly using the brazing sheet product
US6383661B2 (en) * 2000-05-18 2002-05-07 Corus Aluminium Walzprodukte Gmbh Method of manufacturing an aluminum product
US6503640B2 (en) * 2000-05-19 2003-01-07 Corus Aluminium Walzeprodukte Gmbh Method of manufacturing an assembly of brazed dissimilar metal components
US6599645B2 (en) * 2000-05-19 2003-07-29 Corus Aluminium Walzprodukte Gmbh Composite metal panel
US6568584B2 (en) * 2000-07-26 2003-05-27 Corus Aluminium Walzprodukte Gmbh Nickel-plated brazing sheet product
US6596413B2 (en) * 2000-11-08 2003-07-22 Corus Aluminium Walzprodukte Gmbh Brazing product having a low melting point
US6796484B2 (en) * 2001-02-02 2004-09-28 Corus Aluminum Walzprodukte Gmbh Nickel-plated brazing product having improved corrosion performance
US6846401B2 (en) * 2001-04-20 2005-01-25 Corus Aluminium Walzprodukte Gmbh Method of plating and pretreating aluminium workpieces
US6605370B2 (en) * 2001-07-12 2003-08-12 Corus Aluminum Walzprodukte Gmbh Method of manufacturing an aluminium joined product
US6815086B2 (en) * 2001-11-21 2004-11-09 Dana Canada Corporation Methods for fluxless brazing
US6913184B2 (en) * 2001-11-21 2005-07-05 Dana Canada Corporation Alloy composition and method for low temperature fluxless brazing
US7000823B2 (en) * 2001-11-21 2006-02-21 Dana Canada Corporation Fluxless brazing

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102534715A (en) * 2012-02-18 2012-07-04 沈阳飞机工业(集团)有限公司 Process method for electroplating copper on surface of micro aluminum wire
AT13521U1 (en) * 2013-01-18 2014-02-15 Plansee Se module
EP3467152A4 (en) * 2016-06-03 2019-12-04 Furukawa Electric Co., Ltd. Surface treatment material, production method thereof, and component formed using surface treatment material
CN110121575A (en) * 2016-12-27 2019-08-13 古河电气工业株式会社 Finish materials and the part made using the finish materials
EP3564413A4 (en) * 2016-12-27 2020-08-12 Furukawa Electric Co., Ltd. Surface treatment material and method for manufacturing same, and article fabricated using surface treatment material
EP3564412A4 (en) * 2016-12-27 2020-09-02 Furukawa Electric Co., Ltd. Surface treatment material and article fabricated using same
EP3604624A4 (en) * 2017-03-31 2021-01-13 Furukawa Electric Co., Ltd. Plated wire rod material, method for producing same, and cable, electric wire, coil and spring member, each of which is formed using same

Similar Documents

Publication Publication Date Title
US6379818B1 (en) Brazing sheet product and method of its manufacture
EP1265725B1 (en) Brazing sheet product and method of manufacturing an assembly using the brazing sheet product
WO2006077041A1 (en) Method of electroplating and pre-treating aluminium workpieces
US6383661B2 (en) Method of manufacturing an aluminum product
US6596413B2 (en) Brazing product having a low melting point
EP1339523B1 (en) Brazing method with use of a brazing material having a low melting point
US20060157352A1 (en) Method of electroplating and pre-treating aluminium workpieces
AU2001281769A1 (en) Method of manufacturing an aluminium product
AU2002224816A1 (en) Brazing product having a low melting point
US6796484B2 (en) Nickel-plated brazing product having improved corrosion performance
CA2436513C (en) Brazing product
AU2002229739A1 (en) Brazing product
EP1526944B1 (en) Brazing product and method of its manufacture
US6994919B2 (en) Brazing product and method of manufacturing a brazing product
EP1526943B1 (en) Brazing product and method of manufacturing a brazing product with use of a plating bath
US7294411B2 (en) Brazing product and method of its manufacture

Legal Events

Date Code Title Description
AS Assignment

Owner name: CORUS ALUMINIUM WALZPRODUKTE GMBH, GERMANY

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:WIJENBERG, JACQUES HUBERT OLGA JOSEPH;WITTEBROOD, ADRIANUS JACOBUS;REEL/FRAME:017720/0099;SIGNING DATES FROM 20060222 TO 20060303

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION