CA2591116A1 - Method of electroplating and pre-treating aluminium workpieces - Google Patents
Method of electroplating and pre-treating aluminium workpieces Download PDFInfo
- Publication number
- CA2591116A1 CA2591116A1 CA002591116A CA2591116A CA2591116A1 CA 2591116 A1 CA2591116 A1 CA 2591116A1 CA 002591116 A CA002591116 A CA 002591116A CA 2591116 A CA2591116 A CA 2591116A CA 2591116 A1 CA2591116 A1 CA 2591116A1
- Authority
- CA
- Canada
- Prior art keywords
- nickel
- aluminium
- bath
- metal layer
- group
- 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
Links
- 238000000034 method Methods 0.000 title claims abstract description 41
- 239000004411 aluminium Substances 0.000 title claims abstract description 31
- 229910052782 aluminium Inorganic materials 0.000 title claims abstract description 31
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title claims abstract description 30
- 238000009713 electroplating Methods 0.000 title claims abstract description 7
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims abstract description 89
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 40
- 229910052751 metal Inorganic materials 0.000 claims abstract description 36
- 239000002184 metal Substances 0.000 claims abstract description 36
- 230000004913 activation Effects 0.000 claims abstract description 33
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 30
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 22
- 239000000956 alloy Substances 0.000 claims abstract description 22
- 229910000838 Al alloy Inorganic materials 0.000 claims abstract description 20
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 claims abstract description 20
- 235000011149 sulphuric acid Nutrition 0.000 claims abstract description 20
- 238000002203 pretreatment Methods 0.000 claims abstract description 18
- 229910052742 iron Inorganic materials 0.000 claims abstract description 16
- 229910017052 cobalt Inorganic materials 0.000 claims abstract description 14
- 239000010941 cobalt Substances 0.000 claims abstract description 14
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims abstract description 14
- 239000001117 sulphuric acid Substances 0.000 claims abstract description 8
- 229910021645 metal ion Inorganic materials 0.000 claims abstract description 3
- 239000010410 layer Substances 0.000 claims description 54
- 238000005219 brazing Methods 0.000 claims description 42
- 238000007747 plating Methods 0.000 claims description 21
- LGQLOGILCSXPEA-UHFFFAOYSA-L nickel sulfate Chemical compound [Ni+2].[O-]S([O-])(=O)=O LGQLOGILCSXPEA-UHFFFAOYSA-L 0.000 claims description 12
- 229910052797 bismuth Inorganic materials 0.000 claims description 8
- 239000000080 wetting agent Substances 0.000 claims description 8
- KRHYYFGTRYWZRS-UHFFFAOYSA-M Fluoride anion Chemical compound [F-] KRHYYFGTRYWZRS-UHFFFAOYSA-M 0.000 claims description 7
- KGBXLFKZBHKPEV-UHFFFAOYSA-N boric acid Chemical compound OB(O)O KGBXLFKZBHKPEV-UHFFFAOYSA-N 0.000 claims description 7
- 239000004020 conductor Substances 0.000 claims description 7
- 239000000203 mixture Substances 0.000 claims description 7
- JCXGWMGPZLAOME-UHFFFAOYSA-N bismuth atom Chemical compound [Bi] JCXGWMGPZLAOME-UHFFFAOYSA-N 0.000 claims description 6
- 229910000363 nickel(II) sulfate Inorganic materials 0.000 claims description 6
- MIEVBNQRPTXRQR-IFWQJVLJSA-N 2-hydroxypropane-1,2,3-tricarboxylic acid;(2r,3s,4r,5r)-2,3,4,5,6-pentahydroxyhexanoic acid Chemical compound OC[C@@H](O)[C@@H](O)[C@H](O)[C@@H](O)C(O)=O.OC(=O)CC(O)(C(O)=O)CC(O)=O MIEVBNQRPTXRQR-IFWQJVLJSA-N 0.000 claims description 4
- 229910021586 Nickel(II) chloride Inorganic materials 0.000 claims description 4
- BFNBIHQBYMNNAN-UHFFFAOYSA-N ammonium sulfate Chemical compound N.N.OS(O)(=O)=O BFNBIHQBYMNNAN-UHFFFAOYSA-N 0.000 claims description 4
- 229910052921 ammonium sulfate Inorganic materials 0.000 claims description 4
- 235000011130 ammonium sulphate Nutrition 0.000 claims description 4
- 239000004327 boric acid Substances 0.000 claims description 4
- QMMRZOWCJAIUJA-UHFFFAOYSA-L nickel dichloride Chemical compound Cl[Ni]Cl QMMRZOWCJAIUJA-UHFFFAOYSA-L 0.000 claims description 4
- 229910052710 silicon Inorganic materials 0.000 claims description 4
- AEQDJSLRWYMAQI-UHFFFAOYSA-N 2,3,9,10-tetramethoxy-6,8,13,13a-tetrahydro-5H-isoquinolino[2,1-b]isoquinoline Chemical compound C1CN2CC(C(=C(OC)C=C3)OC)=C3CC2C2=C1C=C(OC)C(OC)=C2 AEQDJSLRWYMAQI-UHFFFAOYSA-N 0.000 claims description 3
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 3
- 239000001509 sodium citrate Substances 0.000 claims description 3
- NLJMYIDDQXHKNR-UHFFFAOYSA-K sodium citrate Chemical compound O.O.[Na+].[Na+].[Na+].[O-]C(=O)CC(O)(CC([O-])=O)C([O-])=O NLJMYIDDQXHKNR-UHFFFAOYSA-K 0.000 claims description 3
- 239000000176 sodium gluconate Substances 0.000 claims description 3
- 229940005574 sodium gluconate Drugs 0.000 claims description 3
- 235000012207 sodium gluconate Nutrition 0.000 claims description 3
- 229910052718 tin Inorganic materials 0.000 claims description 3
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 2
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 claims description 2
- 238000005275 alloying Methods 0.000 claims description 2
- 229910052787 antimony Inorganic materials 0.000 claims description 2
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 claims description 2
- 239000012792 core layer Substances 0.000 claims description 2
- 229910052744 lithium Inorganic materials 0.000 claims description 2
- 239000010703 silicon Substances 0.000 claims description 2
- 229910052709 silver Inorganic materials 0.000 claims description 2
- 239000004332 silver Substances 0.000 claims description 2
- 229910052716 thallium Inorganic materials 0.000 claims description 2
- BKVIYDNLLOSFOA-UHFFFAOYSA-N thallium Chemical compound [Tl] BKVIYDNLLOSFOA-UHFFFAOYSA-N 0.000 claims description 2
- 235000011083 sodium citrates Nutrition 0.000 claims 1
- 238000001994 activation Methods 0.000 description 33
- 239000000047 product Substances 0.000 description 25
- PNEYBMLMFCGWSK-UHFFFAOYSA-N Alumina Chemical compound [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 9
- 230000008569 process Effects 0.000 description 7
- 238000012360 testing method Methods 0.000 description 7
- KRHYYFGTRYWZRS-UHFFFAOYSA-N Fluorane Chemical group F KRHYYFGTRYWZRS-UHFFFAOYSA-N 0.000 description 6
- 239000011248 coating agent Substances 0.000 description 6
- 238000000576 coating method Methods 0.000 description 6
- 230000004907 flux Effects 0.000 description 6
- VEQPNABPJHWNSG-UHFFFAOYSA-N Nickel(2+) Chemical compound [Ni+2] VEQPNABPJHWNSG-UHFFFAOYSA-N 0.000 description 4
- 239000012141 concentrate Substances 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 229910001453 nickel ion Inorganic materials 0.000 description 4
- 238000011282 treatment Methods 0.000 description 4
- 230000015572 biosynthetic process Effects 0.000 description 3
- LGRDPUAPARTXMG-UHFFFAOYSA-N bismuth nickel Chemical compound [Ni].[Bi] LGRDPUAPARTXMG-UHFFFAOYSA-N 0.000 description 3
- 238000004140 cleaning Methods 0.000 description 3
- 229910052749 magnesium Inorganic materials 0.000 description 3
- 239000011777 magnesium Substances 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 229910000990 Ni alloy Inorganic materials 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000012864 cross contamination Methods 0.000 description 2
- 238000004090 dissolution Methods 0.000 description 2
- 238000001704 evaporation Methods 0.000 description 2
- 230000008020 evaporation Effects 0.000 description 2
- 238000002474 experimental method Methods 0.000 description 2
- 239000000945 filler Substances 0.000 description 2
- 239000012467 final product Substances 0.000 description 2
- 239000004615 ingredient Substances 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 229910000789 Aluminium-silicon alloy Inorganic materials 0.000 description 1
- 229910001152 Bi alloy Inorganic materials 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- JQGGAELIYHNDQS-UHFFFAOYSA-N Nic 12 Natural products CC(C=CC(=O)C)c1ccc2C3C4OC4C5(O)CC=CC(=O)C5(C)C3CCc2c1 JQGGAELIYHNDQS-UHFFFAOYSA-N 0.000 description 1
- 230000003213 activating effect Effects 0.000 description 1
- 239000002390 adhesive tape Substances 0.000 description 1
- 239000003513 alkali Substances 0.000 description 1
- AZDRQVAHHNSJOQ-UHFFFAOYSA-N alumane Chemical group [AlH3] AZDRQVAHHNSJOQ-UHFFFAOYSA-N 0.000 description 1
- 150000001398 aluminium Chemical class 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 150000001805 chlorine compounds Chemical class 0.000 description 1
- 229910001429 cobalt ion Inorganic materials 0.000 description 1
- XLJKHNWPARRRJB-UHFFFAOYSA-N cobalt(2+) Chemical compound [Co+2] XLJKHNWPARRRJB-UHFFFAOYSA-N 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000004320 controlled atmosphere Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 229910001610 cryolite Inorganic materials 0.000 description 1
- 238000005238 degreasing Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005530 etching Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 150000002222 fluorine compounds Chemical class 0.000 description 1
- 229940050410 gluconate Drugs 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- XLYOFNOQVPJJNP-ZSJDYOACSA-N heavy water Substances [2H]O[2H] XLYOFNOQVPJJNP-ZSJDYOACSA-N 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000005923 long-lasting effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 231100000989 no adverse effect Toxicity 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 239000010453 quartz Substances 0.000 description 1
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N silicon dioxide Inorganic materials O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 239000002470 thermal conductor Substances 0.000 description 1
- 230000037303 wrinkles Effects 0.000 description 1
Classifications
-
- 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
- C25D5/34—Pretreatment of metallic surfaces to be electroplated
- C25D5/42—Pretreatment of metallic surfaces to be electroplated of light metals
- C25D5/44—Aluminium
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D3/00—Electroplating: Baths therefor
- C25D3/02—Electroplating: Baths therefor from solutions
- C25D3/12—Electroplating: Baths therefor from solutions of nickel or cobalt
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D3/00—Electroplating: Baths therefor
- C25D3/02—Electroplating: Baths therefor from solutions
- C25D3/20—Electroplating: Baths therefor from solutions of iron
-
- 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
- C25D5/60—Electroplating characterised by the structure or texture of the layers
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Electroplating Methods And Accessories (AREA)
- Electroplating And Plating Baths Therefor (AREA)
Abstract
The invention relates to 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 pretreated workpiece, and wherein the metal layer is selected from the group consisting of nickel, iron, cobalt, and alloys thereof.
Description
Method of electroplating and pre-treating aluminium workpieces 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 US-2003/0098338-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.
r The present invention solves one or more of these objects through the method of applying a metal coating according to claim 1 and the aluminium alloy product according to claim 14.
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/1, and preferably 80 to 150 g/l, of NiSO4-H2O, and about 50 to 350 g/I, preferably about 150 to 250 g/I of H2SO4. In a preferred embodiment, the pre-treatment bath also contains boric acid as a buffer, e.g. in a range of I 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/I of NiSOa.-6H2O, 10 to 50 g/I of NiC12=6H2O, I to mI/I of a bismuth concentrate containing 100 g/I of Bi, 10 to 50 g/l of (NH4)2SO4, 100 to 180 g/I of sodium citrate=2H2O, and 10 to 50 g/I of sodium gluconate. This bath may be used for pure nickel plating as well, in which case the bismuth concentrate is omitted.
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 US-2003/0098338-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.
r The present invention solves one or more of these objects through the method of applying a metal coating according to claim 1 and the aluminium alloy product according to claim 14.
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/1, and preferably 80 to 150 g/l, of NiSO4-H2O, and about 50 to 350 g/I, preferably about 150 to 250 g/I of H2SO4. In a preferred embodiment, the pre-treatment bath also contains boric acid as a buffer, e.g. in a range of I 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/I of NiSOa.-6H2O, 10 to 50 g/I of NiC12=6H2O, I to mI/I of a bismuth concentrate containing 100 g/I of Bi, 10 to 50 g/l of (NH4)2SO4, 100 to 180 g/I of sodium citrate=2H2O, and 10 to 50 g/I of sodium gluconate. This bath may be used for pure nickel plating as well, in which case the bismuth concentrate is omitted.
5 It has been found that the pre-treatment is already effective at elevated temperatures of less than 95 C, and preferably in the range of 55 C and 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 10 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/m2, 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 pm, more preferably less than 1.0 pm, and even more preferably in a range of 0.2 to 1.0 pm.
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.
5 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 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.
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 10 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/m2, 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 pm, more preferably less than 1.0 pm, and even more preferably in a range of 0.2 to 1.0 pm.
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.
5 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 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.
EXAMPLE
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 pm. The aluminium brazing sheets used consisted of an AA3003-series aluminium core alloy conventionally clad on both sides with an AISi 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/I 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 US-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.
The following non-limiting examples illustrate the invention.
EXAMPLE
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 pm. The aluminium brazing sheets used consisted of an AA3003-series aluminium core alloy conventionally clad on both sides with an AISi 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/I 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 US-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 x 25 mm were cut out of the nickel-bismuth-plated sheets. A small strip of a bare AA3003 alloy measuring 30 mm x 7 mm x 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/I
96 % H2SO4 (S.G. 1.84 kg 1") 200 g/l 113.2 mi/I
H3BO3 30 g/l Table 2. Composition of the hydrofluoric acid bath.
NiCI2=6H20 125 g/I
40 /a HF (S.G. 1.13 kg 1-1) 2.7 g/I 6 ml/I
H3BO3 12.5 g/I
Table 3. Composition of the Watts bath.
NiSO4=6H20 270 g/I
NiCI2=6H20 50 g/I
H3B03 30 g/I
Table 4. Composition of the citrate-gluconate bath.
NiSO4=6H20 142 g/I
NiCI2=6H2O 30 g/I
(NH4)2SO4 34 g/I
Na-citrate=2H20 140 g/I
Na-gluconate 30 g/I
bismuth concentrate (100 g/I Bi) 5 mI/I
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 x 25 mm were cut out of the nickel-bismuth-plated sheets. A small strip of a bare AA3003 alloy measuring 30 mm x 7 mm x 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/I
96 % H2SO4 (S.G. 1.84 kg 1") 200 g/l 113.2 mi/I
H3BO3 30 g/l Table 2. Composition of the hydrofluoric acid bath.
NiCI2=6H20 125 g/I
40 /a HF (S.G. 1.13 kg 1-1) 2.7 g/I 6 ml/I
H3BO3 12.5 g/I
Table 3. Composition of the Watts bath.
NiSO4=6H20 270 g/I
NiCI2=6H20 50 g/I
H3B03 30 g/I
Table 4. Composition of the citrate-gluconate bath.
NiSO4=6H20 142 g/I
NiCI2=6H2O 30 g/I
(NH4)2SO4 34 g/I
Na-citrate=2H20 140 g/I
Na-gluconate 30 g/I
bismuth concentrate (100 g/I Bi) 5 mI/I
Table 5. Summary of the experiments carried and the results on adhesion and brazeability.
Sample Clad Activation Plating Adhesion Brazeability layer Ni / Ni-Bi Activation Temperature bath [ C ]
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 +
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 +
Sample Clad Activation Plating Adhesion Brazeability layer Ni / Ni-Bi Activation Temperature bath [ C ]
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 +
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 5 activation as per Sample I 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 5 adhesion level becomes unacceptable. From Samples I 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, 10 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 I and 8 it can be seen that the wetfiing 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.
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 5 adhesion level becomes unacceptable. From Samples I 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, 10 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 I and 8 it can be seen that the wetfiing 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 (14)
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.cndot.H2O and 50 to 350 g/l of H2SO4.
3. The method according to claim 1 or 2, wherein the pre-treatment bath also contains boric acid (H3BO3), preferably in the range of 1 to 50 g/l.
4. The method according to any one of claims 1 to 3, wherein the plating bath is a Watts bath, and preferably containing nickel sulphate (NiSO4), nickel chloride (NiCI2) and boric acid (H3B03).
5. The method according to any one of claims 1 to 4, wherein the plating bath is a citrate-gluconate bath containing NiSO4, and (NH4)2SO4 and sodium citrate and sodium gluconate.
6. The method according to any one of claims 1 to 5, wherein the pre-treatment bath is devoid of any fluoride containing components.
7. The method according to any one of claims I to 6, wherein the temperature of the pre-treatment bath is maintained at an elevated temperature in a range of up to 95°C, and preferably in a range of 55°C to 80°C.
8. The method according to any one of claims 1 to 7, wherein the applied metal layer has an average thickness of less than 2 µm, and preferably less than 1.0 µm, and more preferably in a range of 0.2 to 1.0 µm.
9. The method according to any one of claims 1 to 8, wherein the method is carried out as a continuous plating operation.
10. The method according to any one of claims 1 to 9, 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 preferably 7-14 wt.%, and whereby the metal layer is applied on the clad layer.
11. The method according to claim 10, wherein the clad layer further comprises as alloying element a wetting agent in a range of up to 1 wt.%.
12. The method according to claim 11, wherein the wetting agent is selected from the group consisting of lead, bismuth, lithium, antimony, tin, silver, thallium and any mixture thereof.
13. The method according to any one of claims 1 to 9, wherein the aluminium workpiece is an aluminium conductor, and preferably made of an alloy selected from the group consisting of AA1370, AA1110 and AA6101.
14. 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 any one of claims 1 to 13.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP05075082 | 2005-01-19 | ||
| EP05075082.7 | 2005-01-19 | ||
| PCT/EP2006/000185 WO2006077041A1 (en) | 2005-01-19 | 2006-01-09 | Method of electroplating and pre-treating aluminium workpieces |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA2591116A1 true CA2591116A1 (en) | 2006-07-27 |
Family
ID=34937992
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002591116A Abandoned CA2591116A1 (en) | 2005-01-19 | 2006-01-09 | Method of electroplating and pre-treating aluminium workpieces |
Country Status (10)
| Country | Link |
|---|---|
| EP (1) | EP1838490A1 (en) |
| JP (1) | JP2008527178A (en) |
| KR (1) | KR20070095331A (en) |
| CN (1) | CN101098771A (en) |
| AU (1) | AU2006207665A1 (en) |
| BR (1) | BRPI0606419A2 (en) |
| CA (1) | CA2591116A1 (en) |
| FR (1) | FR2880899A1 (en) |
| MX (1) | MX2007007955A (en) |
| WO (1) | WO2006077041A1 (en) |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101619475B (en) * | 2008-06-30 | 2011-03-30 | 比亚迪股份有限公司 | A kind of aluminum alloy electroplating method |
| CN102330130A (en) * | 2011-11-02 | 2012-01-25 | 沈阳飞机工业(集团)有限公司 | Process method for preplating nickel on surface of minuteness aluminum wire before copper plating |
| JP6195745B2 (en) * | 2013-06-19 | 2017-09-13 | 地方独立行政法人東京都立産業技術研究センター | Electro nickel plating solution, method for producing plating solution and electro plating method |
| KR102471172B1 (en) * | 2016-06-03 | 2022-11-25 | 후루카와 덴끼고교 가부시키가이샤 | Surface treatment material, its manufacturing method, and parts formed using the surface treatment material |
| JP6326591B2 (en) | 2016-10-25 | 2018-05-23 | 石原ケミカル株式会社 | Method for forming heat-treatable conductive film on non-conductive metal |
| US20210130968A1 (en) * | 2016-12-27 | 2021-05-06 | Furukawa Electric Co., Ltd. | Surface-treated material and method for producing the same, and member produced with this surface-treated material |
| WO2018124114A1 (en) * | 2016-12-27 | 2018-07-05 | 古河電気工業株式会社 | Surface treatment material and article fabricated using same |
| CN110494597A (en) * | 2017-03-31 | 2019-11-22 | 古河电气工业株式会社 | Plating wire and rod and its manufacturing method and cable, electric wire, coil and the spring member formed using it |
| WO2019193960A1 (en) * | 2018-04-06 | 2019-10-10 | 古河電気工業株式会社 | Plated wire rod |
| CN111893525A (en) * | 2020-08-10 | 2020-11-06 | 扬州市景杨表面工程有限公司 | Nickel-tin electroplating process for passive component |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1378164A (en) * | 1963-09-24 | 1964-11-13 | Aluminium Francais | Process for electrolytic coating of aluminum |
| US5368719A (en) * | 1993-05-12 | 1994-11-29 | Hughes Aircraft Company | Method for direct plating of iron on aluminum |
| US6815086B2 (en) * | 2001-11-21 | 2004-11-09 | Dana Canada Corporation | Methods for fluxless brazing |
| US20040038070A1 (en) * | 2001-11-21 | 2004-02-26 | Dockus Kostas F. | Fluxless brazing |
-
2006
- 2006-01-09 BR BRPI0606419-1A patent/BRPI0606419A2/en not_active Application Discontinuation
- 2006-01-09 WO PCT/EP2006/000185 patent/WO2006077041A1/en not_active Ceased
- 2006-01-09 CN CNA2006800018028A patent/CN101098771A/en active Pending
- 2006-01-09 EP EP06706199A patent/EP1838490A1/en not_active Withdrawn
- 2006-01-09 KR KR1020077016083A patent/KR20070095331A/en not_active Withdrawn
- 2006-01-09 JP JP2007551588A patent/JP2008527178A/en not_active Withdrawn
- 2006-01-09 MX MX2007007955A patent/MX2007007955A/en unknown
- 2006-01-09 AU AU2006207665A patent/AU2006207665A1/en not_active Abandoned
- 2006-01-09 CA CA002591116A patent/CA2591116A1/en not_active Abandoned
- 2006-01-16 FR FR0600371A patent/FR2880899A1/en active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| BRPI0606419A2 (en) | 2009-06-30 |
| JP2008527178A (en) | 2008-07-24 |
| FR2880899A1 (en) | 2006-07-21 |
| KR20070095331A (en) | 2007-09-28 |
| MX2007007955A (en) | 2007-11-23 |
| AU2006207665A1 (en) | 2006-07-27 |
| WO2006077041A1 (en) | 2006-07-27 |
| EP1838490A1 (en) | 2007-10-03 |
| CN101098771A (en) | 2008-01-02 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| AU757702B2 (en) | Brazing sheet product and method of its manufacture | |
| AU2001281769B2 (en) | Method of manufacturing an aluminium product | |
| AU2002224816B2 (en) | Brazing product having a low melting point | |
| CA2440756A1 (en) | Method of plating and pretreating aluminium workpieces | |
| AU2002224816A1 (en) | Brazing product having a low melting point | |
| KR20040063786A (en) | Brazing product having a low melting point | |
| US6796484B2 (en) | Nickel-plated brazing product having improved corrosion performance | |
| JP4080330B2 (en) | Method of manufacturing an assembly of different brazed metal components | |
| CA2436513C (en) | Brazing product | |
| CA2591116A1 (en) | Method of electroplating and pre-treating aluminium workpieces | |
| AU2002229739A1 (en) | Brazing product | |
| US20060157352A1 (en) | Method of electroplating and pre-treating aluminium workpieces | |
| EP1526943B1 (en) | Brazing product and method of manufacturing a brazing product with use of a plating bath | |
| EP1526944A1 (en) | Brazing product and method of its manufacture | |
| JP2007136490A (en) | Member for heat exchanger, and heat exchanger |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FZDE | Discontinued |