US2970090A - Plating nickel on aluminum - Google Patents
Plating nickel on aluminum Download PDFInfo
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- US2970090A US2970090A US746067A US74606758A US2970090A US 2970090 A US2970090 A US 2970090A US 746067 A US746067 A US 746067A US 74606758 A US74606758 A US 74606758A US 2970090 A US2970090 A US 2970090A
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- aluminum
- nickel
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- plating
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- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 title claims description 92
- 229910052782 aluminium Inorganic materials 0.000 title claims description 76
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title claims description 76
- 229910052759 nickel Inorganic materials 0.000 title claims description 44
- 238000007747 plating Methods 0.000 title description 33
- 238000000034 method Methods 0.000 claims description 59
- 229910052751 metal Inorganic materials 0.000 claims description 34
- 239000002184 metal Substances 0.000 claims description 34
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 27
- KRHYYFGTRYWZRS-UHFFFAOYSA-N Fluorane Chemical compound F KRHYYFGTRYWZRS-UHFFFAOYSA-N 0.000 claims description 20
- VEXZGXHMUGYJMC-UHFFFAOYSA-N Hydrochloric acid Chemical compound Cl VEXZGXHMUGYJMC-UHFFFAOYSA-N 0.000 claims description 20
- HEMHJVSKTPXQMS-UHFFFAOYSA-M Sodium hydroxide Chemical compound [OH-].[Na+] HEMHJVSKTPXQMS-UHFFFAOYSA-M 0.000 claims description 15
- 239000002131 composite material Substances 0.000 claims description 15
- 238000005530 etching Methods 0.000 claims description 15
- NLXLAEXVIDQMFP-UHFFFAOYSA-N Ammonia chloride Chemical compound [NH4+].[Cl-] NLXLAEXVIDQMFP-UHFFFAOYSA-N 0.000 claims description 14
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 claims description 14
- 229910045601 alloy Inorganic materials 0.000 claims description 11
- 239000000956 alloy Substances 0.000 claims description 11
- CSNNHWWHGAXBCP-UHFFFAOYSA-L Magnesium sulfate Chemical compound [Mg+2].[O-][S+2]([O-])([O-])[O-] CSNNHWWHGAXBCP-UHFFFAOYSA-L 0.000 claims description 10
- SQQMAOCOWKFBNP-UHFFFAOYSA-L manganese(II) sulfate Chemical compound [Mn+2].[O-]S([O-])(=O)=O SQQMAOCOWKFBNP-UHFFFAOYSA-L 0.000 claims description 10
- CDBYLPFSWZWCQE-UHFFFAOYSA-L sodium carbonate Substances [Na+].[Na+].[O-]C([O-])=O CDBYLPFSWZWCQE-UHFFFAOYSA-L 0.000 claims description 10
- LGQLOGILCSXPEA-UHFFFAOYSA-L nickel sulfate Chemical compound [Ni+2].[O-]S([O-])(=O)=O LGQLOGILCSXPEA-UHFFFAOYSA-L 0.000 claims description 9
- 229910000363 nickel(II) sulfate Inorganic materials 0.000 claims description 9
- 235000019270 ammonium chloride Nutrition 0.000 claims description 7
- KGBXLFKZBHKPEV-UHFFFAOYSA-N boric acid Chemical compound OB(O)O KGBXLFKZBHKPEV-UHFFFAOYSA-N 0.000 claims description 7
- 239000004327 boric acid Substances 0.000 claims description 7
- 238000000151 deposition Methods 0.000 claims description 7
- 238000007598 dipping method Methods 0.000 claims description 7
- 238000011282 treatment Methods 0.000 claims description 7
- 238000005238 degreasing Methods 0.000 claims description 6
- 238000004070 electrodeposition Methods 0.000 claims description 6
- 229910052943 magnesium sulfate Inorganic materials 0.000 claims description 5
- 235000019341 magnesium sulphate Nutrition 0.000 claims description 5
- 229910000029 sodium carbonate Inorganic materials 0.000 claims description 5
- 238000001035 drying Methods 0.000 claims description 4
- XLYOFNOQVPJJNP-PWCQTSIFSA-N Tritiated water Chemical compound [3H]O[3H] XLYOFNOQVPJJNP-PWCQTSIFSA-N 0.000 claims 5
- 230000008569 process Effects 0.000 description 12
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 10
- 229910052725 zinc Inorganic materials 0.000 description 10
- 239000011701 zinc Substances 0.000 description 10
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 8
- 150000002739 metals Chemical class 0.000 description 8
- 238000000576 coating method Methods 0.000 description 6
- NWONKYPBYAMBJT-UHFFFAOYSA-L zinc sulfate Chemical compound [Zn+2].[O-]S([O-])(=O)=O NWONKYPBYAMBJT-UHFFFAOYSA-L 0.000 description 6
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 5
- 229910052802 copper Inorganic materials 0.000 description 5
- 239000010949 copper Substances 0.000 description 5
- 238000010438 heat treatment Methods 0.000 description 5
- 229910000838 Al alloy Inorganic materials 0.000 description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 3
- XFXPMWWXUTWYJX-UHFFFAOYSA-N Cyanide Chemical compound N#[C-] XFXPMWWXUTWYJX-UHFFFAOYSA-N 0.000 description 3
- XSTXAVWGXDQKEL-UHFFFAOYSA-N Trichloroethylene Chemical group ClC=C(Cl)Cl XSTXAVWGXDQKEL-UHFFFAOYSA-N 0.000 description 3
- 239000002253 acid Substances 0.000 description 3
- 230000001464 adherent effect Effects 0.000 description 3
- 238000003486 chemical etching Methods 0.000 description 3
- 229910052804 chromium Inorganic materials 0.000 description 3
- 239000011651 chromium Substances 0.000 description 3
- 239000011248 coating agent Substances 0.000 description 3
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 3
- 229910052737 gold Inorganic materials 0.000 description 3
- 239000010931 gold Substances 0.000 description 3
- 238000007654 immersion Methods 0.000 description 3
- 230000006872 improvement Effects 0.000 description 3
- 238000002844 melting Methods 0.000 description 3
- 230000008018 melting Effects 0.000 description 3
- 150000003839 salts Chemical class 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical group [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 2
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 2
- 238000007743 anodising Methods 0.000 description 2
- 239000002585 base Substances 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- TVZPLCNGKSPOJA-UHFFFAOYSA-N copper zinc Chemical compound [Cu].[Zn] TVZPLCNGKSPOJA-UHFFFAOYSA-N 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 239000002659 electrodeposit Substances 0.000 description 2
- 230000004927 fusion Effects 0.000 description 2
- 239000001257 hydrogen Substances 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 239000003921 oil Substances 0.000 description 2
- 230000001590 oxidative effect Effects 0.000 description 2
- 238000007528 sand casting Methods 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- 229910052718 tin Inorganic materials 0.000 description 2
- UBOXGVDOUJQMTN-UHFFFAOYSA-N trichloroethylene Natural products ClCC(Cl)Cl UBOXGVDOUJQMTN-UHFFFAOYSA-N 0.000 description 2
- 229920001353 Dextrin Polymers 0.000 description 1
- 239000004375 Dextrin Substances 0.000 description 1
- 241000080590 Niso Species 0.000 description 1
- GRYLNZFGIOXLOG-UHFFFAOYSA-N Nitric acid Chemical compound O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 0.000 description 1
- NPXOKRUENSOPAO-UHFFFAOYSA-N Raney nickel Chemical class [Al].[Ni] NPXOKRUENSOPAO-UHFFFAOYSA-N 0.000 description 1
- BZHJMEDXRYGGRV-UHFFFAOYSA-N Vinyl chloride Chemical group ClC=C BZHJMEDXRYGGRV-UHFFFAOYSA-N 0.000 description 1
- PQLVXDKIJBQVDF-UHFFFAOYSA-N acetic acid;hydrate Chemical compound O.CC(O)=O PQLVXDKIJBQVDF-UHFFFAOYSA-N 0.000 description 1
- 239000003513 alkali Substances 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 235000010338 boric acid Nutrition 0.000 description 1
- 229910052793 cadmium Inorganic materials 0.000 description 1
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- KRVSOGSZCMJSLX-UHFFFAOYSA-L chromic acid Substances O[Cr](O)(=O)=O KRVSOGSZCMJSLX-UHFFFAOYSA-L 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 230000001143 conditioned effect Effects 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- -1 degrease Chemical compound 0.000 description 1
- 235000019425 dextrin Nutrition 0.000 description 1
- 238000004512 die casting Methods 0.000 description 1
- AWJWCTOOIBYHON-UHFFFAOYSA-N furo[3,4-b]pyrazine-5,7-dione Chemical compound C1=CN=C2C(=O)OC(=O)C2=N1 AWJWCTOOIBYHON-UHFFFAOYSA-N 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 229910001234 light alloy Inorganic materials 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 229910017604 nitric acid Inorganic materials 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 229910052703 rhodium Inorganic materials 0.000 description 1
- 239000010948 rhodium Substances 0.000 description 1
- MHOVAHRLVXNVSD-UHFFFAOYSA-N rhodium atom Chemical compound [Rh] MHOVAHRLVXNVSD-UHFFFAOYSA-N 0.000 description 1
- 238000002791 soaking Methods 0.000 description 1
- 229910000679 solder Inorganic materials 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
- 239000011135 tin Substances 0.000 description 1
- YNJBWRMUSHSURL-UHFFFAOYSA-N trichloroacetic acid Chemical compound OC(=O)C(Cl)(Cl)Cl YNJBWRMUSHSURL-UHFFFAOYSA-N 0.000 description 1
- 229960004319 trichloroacetic acid Drugs 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
Definitions
- the present invention relates to an improved method for plating nickel on aluminum and more particularly, to I an improved method of nickel plating on aluminum that forms a plated aluminum base upon which any subsequent metal can be plated with firm adherent adhesion.
- the old methods of plating on aluminum require that first, a layer of zinc be put on the aluminum either by immersion or by electrodeposition, then secondly, followed by a layer of electrodeposited copper. After these two layers of metals have been put on the aluminum, then the desired finish metal may be deposited over the zinccopper coated aluminum.
- the disadvantages of the old method are that two metals must be plated on the aluminum before a desired finish metal may be plated. Fur ther, the plating of the zinc coating, especially by the immersion method, must be controlled within very narrow limits or blisters will occur during the copper plating as well as any subsequent plating. Also, the copper bath, which is cyanide in nature, must be kept below a maximum limit in free cyanide.
- the finish metal is a metal that must be plated from a molten salt bath
- the zinc which has a low melting point will be melted and become a liquid, thus no longer giving protection to the aluminum for electrodepositing the finished metal.
- the results of plating on zinc-copper coated aluminum in a molten salt bath above the temperature at which zinc melts, will give blistered non-adherent deposits of the finish metal.
- the principal object of the present invention is to provide a method of plating on aluminum in which nickel is used instead of thezinc and copper platings as the underlaying metal plating between aluminum and the finished metal.
- Another object of the invention is to provide a method of plating nickel on aluminum in which the nickel is fused with the aluminum before the finish plate is applied lightness.
- Decorative finishes on .aluminum have found wide usage in household appliances and in the jewelry industry.
- plated aluminum of good quality has found wide application in all industries because of its relative economy, attractive finish, strength and
- the plating of aluminum can generally be divided into two broad categories. The first is chemical etching, in which the aluminum article'is chemically-etched and a subsequent metal is deposited on theconditioned surface either by immersion or by electrodeposition.
- the different methods of plating on aluminum only a few procedures have merit. Most give only fair results or are impractical or uneconomical.
- the plated aluminum was subjected to a furnace temperature of 800 F. to 1050 F. for five minutes.
- nickel could be the plated metal and the aluminum prepared and processed by the following operations:
- the degreasing step removes oils and organic contamination on the surface of the aluminum. This may be accomplished by vapor degreasing or by soaking the aluminum in any solvent ordinarily used for this purpose.
- the etching operation involves the use of two types of etches.
- the aluminum article is first etched in a 10% by volume solution of hydrofluoric acid (48-52%) for 10 to 15 seconds.
- the article is then rinsed and transferred to a second etch of 50% hydrochloric acid containing 9 to 10 g./l. of manganous sulfate (MnSO .H O).
- the etching time varies from 10 to 80 seconds, depending upon the aluminum alloy.
- an etching time of 20 to 30 seconds is usually suificient.
- a more severe etch than hydrofluoric acid and water may be needed.
- an etch which consists of 3 parts of nitric acid and one part of hydrofluoric acid may be substituted.
- the nickel plate is obtained from a nickel bath of the following composition:
- Nickel sulfate NiSO,.6H,O
- Magnesium sulfate MgsOflH O
- Ammonium chloride Water 95 Boric acid 2
- the aluminum article is made the cathode and plated at amp./ sq. ft. for approximately 10 minutes to obtain the desired thickness of the nickel plate which ranges from 0.0001 to 0.0005" thick.
- the temperature during the heat treatment should be between 800-l050 F. for the islands to form.
- Several temperatures were investigated to determine at which points the islands would form. Since each different alloy of aluminum will have a different melting point and will, therefore, form islands at different temperatures, it was found that the islands always form when the temperature range is 800-1050 F.
- the formation of the aluminum nickel alloy and the formation of the islands provides a suitable surface upon which other metals may be electrodeposited. Metals plated on this surface have improved adhesion around the regions of the islands.
- the heat treatment is carried out in air, a thin layer of oxide is formed on the surface of the article. Before subsequent plating can be accomplished the oxide must be removed by giving the article a reverse current treatment in 25% sulfuric acid solution. If the nickel-plated aluminum is heat treated in the non-oxidizing atmosphere, oxidizing atmosphere, oxidization is minimized and the article need only be dipped in a 25% sulfuric acid solution for a few seconds to activate the surface before subsequent plating is carried out.
- the heat treatment step may be omitted and fair adhesion of the nickel and aluminum will be obtained. It was found that with 24 ST aluminum good adhesion could be obtained using an etch time of 18-22 seconds. However, if the best adhesion is to be obtained in every case and, if the process is to be reproducible, the heat treatment step is essential.
- Example 1 Degrease the aluminum with trichloroethylene vapors, acetone or any organic solution commonly used for this purpose.
- the nickel coated aluminum is placed in the oven at 1000 F. for 2.5-5 minutes in which time the under coat of the nickel is fused into the aluminum. During this fusion a light blue oxide is formed on the nickel which must be removed before any subsequent plating may be carried out on the fused nickel-coated aluminum. This oxide is removed by the following method:
- Example 2 This example illustrates a method of plating 24 ST aluminum.
- Example 3 This example illustrates a method for plating on Alcoa No. 38D aluminum.
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- 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)
Description
2,910,090 PLATING NICKEL N ALUMINUM James c. Withers, Fairfax, and Paul E. Rltt, In, Vienna,
Va., assignors to Melpar, Inc., Falls Church, Va., a cor!- poration of New York No Drawing. Filed July 2, 1958, sex. No. 746,067 3 Claims. c1. 204-33 The present invention relates to an improved method for plating nickel on aluminum and more particularly, to I an improved method of nickel plating on aluminum that forms a plated aluminum base upon which any subsequent metal can be plated with firm adherent adhesion.
The old methods of plating on aluminum require that first, a layer of zinc be put on the aluminum either by immersion or by electrodeposition, then secondly, followed by a layer of electrodeposited copper. After these two layers of metals have been put on the aluminum, then the desired finish metal may be deposited over the zinccopper coated aluminum. The disadvantages of the old method are that two metals must be plated on the aluminum before a desired finish metal may be plated. Fur ther, the plating of the zinc coating, especially by the immersion method, must be controlled within very narrow limits or blisters will occur during the copper plating as well as any subsequent plating. Also, the copper bath, which is cyanide in nature, must be kept below a maximum limit in free cyanide. If the finish metal is a metal that must be plated from a molten salt bath, the zinc, which has a low melting point will be melted and become a liquid, thus no longer giving protection to the aluminum for electrodepositing the finished metal. The results of plating on zinc-copper coated aluminum in a molten salt bath above the temperature at which zinc melts, will give blistered non-adherent deposits of the finish metal.
The method of the invention described herein corrects these deficiencies of the prior art. Broadly, a new Patented Jan. 31, 1961 "ice Other objects and advantages will become apparent as the description proceeds.
Since the applications of electroplated aluminum are manifold and continually increasing, a great deal of interest has been created in the development of methods for plating on aluminum. Some of the applications for metallic coatings on aluminum are to decrease contact refsistance, toimprove surface conductivity, to improve method of obtaining electrodeposits 'on aluminum with trols on the dips and plating bath. Excellent adhesion is always assured because of the fusion of the nickel and the aluminum. Nickel is a high melting metal, thus when nickel is used as the underlaying metal a subsequent finish can be given that, is plated from a molten salt bath.
The principal object of the present invention is to provide a method of plating on aluminum in which nickel is used instead of thezinc and copper platings as the underlaying metal plating between aluminum and the finished metal.
Another object of the invention is to provide a method of plating nickel on aluminum in which the nickel is fused with the aluminum before the finish plate is applied lightness.
solderability, toreduce friction, to facilitate the bonding of rubber, and to increase wear resistance.
Decorative finishes on .aluminum have found wide usage in household appliances and in the jewelry industry. In general, plated aluminum of good quality has found wide application in all industries because of its relative economy, attractive finish, strength and The plating of aluminum can generally be divided into two broad categories. The first is chemical etching, in which the aluminum article'is chemically-etched and a subsequent metal is deposited on theconditioned surface either by immersion or by electrodeposition. The second, a which is no concern here, includes the various anodizing processes which produce an oxide coating upon which subsequent metals can be deposited. Of the different methods of plating on aluminum, only a few procedures have merit. Most give only fair results or are impractical or uneconomical.
One of the most practical and economically-sound methods of plating on aluminum is, categorically, a
chemical-etching process. Various degrees of the chemical-etching process are used more often throughout industry than any other process because of the low-operating cost of the etch bath as compared to the high power cost for operating anodizing baths. The method explained herein consists of chemically-etching and then electrodepositing nickel on the aluminum.
Several methods of plating on aluminum were evaluated to determine the best technique for obtaining good adhesion between the plated metal and the aluminum. One of the first methods approached was the familiar zincate. In the hands of those who are skilled in the art of plating on aluminum, the method works with good success; however, in production-type operations, the method is not consistent because of the different procedures .and the high degree of skill that must be utilized when the different alloys of aluminum are encountered.
A modification of the zincate method was investigated and found to give more consistent-results. This pro cedure consists of the standard process for cleaning aluminum i.e., degrease, alkaline etch, deoxidize. After the deoxidation treatment, the aluminum article is given a dip in fiuoroboric acid. A thin film of zinc is then electrodeposited n the aluminum from a standard alkaline zinc bath. An improvement over the normal zincate procedure was observed; however, the procedure did Since none of the methods investigated, using zinc asan intermediate coating between aluminum and wine quent 'electrodeposits, gave the results desired, further investigation was carried out. This led to the use of :a
method developed inCambridge, England, by Dr. J. MI
Bryan. It consisted of placing the aluminum article in an etch which consisted of dextrin, water and trichloracetic acid, rinsing in acetone, and plating nickel on the etched surface from a nickel sulfate bath. Dr. Bryan's to give maximum adhesion which has never before been 7 nickel to the aluminum, the method was notaccepted as obtained with plated metals on aluminum.
the best. However, there were some alternate procedures developed from this method which later led to the development of the present method. It was found that, after etching, tin, rhodium, and chromium could be plated directly on the etched surface of the aluminum just as the nickel had been plated in other instances. The plated metals of the pieces processed appeared to have good adhesion to the aluminum.
Although this alternative method offered some satisfaction, it was felt that further improvement in the adhesion characteristic of the plating could be obtained if the deposited metal were fused with the aluminum. To accomplish this fusing operation, the plated aluminum was subjected to a furnace temperature of 800 F. to 1050 F. for five minutes. As an example, nickel could be the plated metal and the aluminum prepared and processed by the following operations:
, The degreasing step removes oils and organic contamination on the surface of the aluminum. This may be accomplished by vapor degreasing or by soaking the aluminum in any solvent ordinarily used for this purpose.
The etching operation involves the use of two types of etches. The aluminum article is first etched in a 10% by volume solution of hydrofluoric acid (48-52%) for 10 to 15 seconds. The article is then rinsed and transferred to a second etch of 50% hydrochloric acid containing 9 to 10 g./l. of manganous sulfate (MnSO .H O). The etching time varies from 10 to 80 seconds, depending upon the aluminum alloy.
For the light alloys of aluminum, an etching time of 20 to 30 seconds is usually suificient. For some die and sand castings, a more severe etch than hydrofluoric acid and water may be needed. In such cases, an etch which consists of 3 parts of nitric acid and one part of hydrofluoric acid may be substituted. After the aluminum article has been given the two etching treatments, it is dip rinsed and transferred to the nickel bath.
The nickel plate is obtained from a nickel bath of the following composition:
. z./gal. Nickel sulfate (NiSO,.6H,O) 19 Magnesium sulfate (MgsOflH O) Ammonium chloride 2 Water 95 Boric acid 2 The aluminum article is made the cathode and plated at amp./ sq. ft. for approximately 10 minutes to obtain the desired thickness of the nickel plate which ranges from 0.0001 to 0.0005" thick.
It is presumed that during the heat-treating process some of the nickel diffuses into the aluminum, and, because of the high surface energy of the nickel, readily agglomerates into islands. The temperature during the heat treatment should be between 800-l050 F. for the islands to form. Several temperatures were investigated to determine at which points the islands would form. Since each different alloy of aluminum will have a different melting point and will, therefore, form islands at different temperatures, it was found that the islands always form when the temperature range is 800-1050 F.
The formation of the aluminum nickel alloy and the formation of the islands provides a suitable surface upon which other metals may be electrodeposited. Metals plated on this surface have improved adhesion around the regions of the islands. However, if the heat treatment is carried out in air, a thin layer of oxide is formed on the surface of the article. Before subsequent plating can be accomplished the oxide must be removed by giving the article a reverse current treatment in 25% sulfuric acid solution. If the nickel-plated aluminum is heat treated in the non-oxidizing atmosphere, oxidizing atmosphere, oxidization is minimized and the article need only be dipped in a 25% sulfuric acid solution for a few seconds to activate the surface before subsequent plating is carried out.
If the time in the hydrochloric acid etch is controlled very closely with each difierent type of alloy used, the heat treatment step may be omitted and fair adhesion of the nickel and aluminum will be obtained. It was found that with 24 ST aluminum good adhesion could be obtained using an etch time of 18-22 seconds. However, if the best adhesion is to be obtained in every case and, if the process is to be reproducible, the heat treatment step is essential.
As a more specific illustration of the present invention, reference is made to the following examples:
Example 1 (1) Degrease the aluminum with trichloroethylene vapors, acetone or any organic solution commonly used for this purpose.
(2) Cold water rinse.
(3) Dip for 10-15 seconds in one part of hydrofluoric acid to nine parts of water.
(4) Cold water rinse.
(5) Dip in a 50% solution of hydrochloric acid containing 9.0 to 10.0 g./l. of manganous sulfate for 10-60 seconds. This time depends upon the alloy of aluminum and must be worked out for each alloy.
(6) Cold water rinse.
(7) Plate in the following aqueous nickel bath at 15 amperes/sq. ft. for 10-20 minutes:
19 oz./gal. nickel sulfate.
10 oz./gal. manganous sulfate.
2 oz./ gal. ammonium chloride.
2 oz./ gal. boric acid. (8) Rinse and air blast part dry. (9) Place in an oven at 1000 F. for 2.5-5 minutes.
To insure the best adhesion of the nickel to the aluminum, the nickel coated aluminum is placed in the oven at 1000 F. for 2.5-5 minutes in which time the under coat of the nickel is fused into the aluminum. During this fusion a light blue oxide is formed on the nickel which must be removed before any subsequent plating may be carried out on the fused nickel-coated aluminum. This oxide is removed by the following method:
(1) Anodic alkali clean for 30-45 seconds at 4V in 3 oz./ gal. sodium hydroxide, 2 oz./ga1. sodium carbonate.
(2) Rinse.
(3) Reverse current clean in 25% sulfuric acid at 4V using lead cathode until the blue oxide is removed. Approximate time is 60-70 seconds.
(4) Rinse and plate any desired metal.
Example 2 This example illustrates a method of plating 24 ST aluminum.
(l) Degrease the aluminum with trichloroethylene vapors, acetone or any organic solution commonly used for this purpose.
(2) Cold water rinse.
(3) Dip for 10 to 12 seconds in one part of hydrofluoric acid to nine parts of water.
(4) Cold water rinse.
(5) Dip in a 50% solution of hydrochloric acidcontaining 9 to 10 g./l. of manganous-sulfatefor 18-22 seconds.
(6) Cold water rinse.
(7) Plate in the following aqueous nickel bath at 15 amperes/sq. ft. for 10-20 minutes:
19 oz./gal. nickel sulfate.
-.(3 Etch for 8-12 seconds in one part Example 3 This example illustrates a method for plating on Alcoa No. 38D aluminum.
(1) Degrease the aluminum with tn'chloroethylene vapors, acetone or any organic solution commonly used for this purpose.
(2) Cold waterrinse.
acid to 9 parts of water.
(4) Cold water rinse.
(5) Dip in a 50% solution of hydrochloric acid containing 9 to g./l. of manganous sulfate for 10 to seconds.
(6) Cold water rinse.
(7) Plate in the following aqueous nickel bath at 15 amperes/sq. ft. for 10-20 minutes:
19 oz./gal. nickel sulfate.
10 oz./gal. manganous sulfate. 2 oz./gal. ammonium chloride. 2 oz./gal. boric acid.
(8) Rinse and air blast part dry.
(9) Heat in an 800 to 950 F. oven for 5 to 15 minutes while passing a pure hydrogen atmosphere or an atmosphere comprising principally hydrogen and the remainder is argon or any inert gas.
(10) Dip in a dilute solution of hydrochloric acid.
(11) Plate any desired metal; an example is chromium from a chromic acid solution.
Over 50 samples of aluminum of varying alloy composition, specifically 24ST, 3S, and sand castings, were treated as outlined above, including the heat treatment step. After the prepared samples had been activated, copper (acid and cyanide), chromium, nickel, zinc, cadmium, gold, tin, and solder were plated on the conditioned surface. After these metals had been plated on of hydrofluoric 6 This process, too, was not acceptable because of high operating cost and because perfect adhesion was not obtained in every case.
Although the above nickel process appeared to'be satisfactory, a method was developed which would be acceptable in every case. This method consisted of etching the aluminum article in a hydrofluoric acid solution, in a hydrochloric acid and manganous sulfate solution, nickel plating, heat treating, and then subsequent plating a desired metal. It was found that this process,
in every case, produced firm adherent coatings on varying alloys of aluminum.
Other modes of applying the principle of our invention may be employed instead of those explained, change being made as regards the method herein disclosed, provided the step or steps stated by any of the following claims or the equivalent of such stated step or steps be employed.
We therefor particularly point out and distinctly claim as our invention:
1. In a method of depositing an electroplate of a nickel group metal upon articles of aluminum and aluminumbase alloys, the steps which include degreasing the article; rinsing in water; subjecting the article to two etching actions, the first, dipping in hydrofluoric acid, rinsing in water, and the second, dipping in a solution of hydrochloric acid containing manganous sulfate, the total etching time varying from 10 to 80 seconds, rinsing in water; cathodically treating the article in an aqueous nickel bath comprising nickel sulfate, magnesium sulfate, ammonium chloride, and boric acid and subjecting the bath to a current density of circa 15 amperes per square foot for a period of approximately 10 minutes, electrodepositing a layer of nickel on the article and controlling the electrodeposition to produce a thickness which ranges from 0.0001 inch to 0.0005 inch; rinsing in water and then partially drying with an air blast; heat treating the composite plated article at a temperature of about 1000" F. for a period of 2V; to 5 minutes; then removing'the light blue oxide that forms thereon during the heat treating step by anodically treating the composite plated article in a solution of sodium hydroxide and sodium carbonate;
I rinsing in water; subjecting the composite plated article the aluminum samples, they were subjected to the following tests to evaluate the adhesion. Some samples were heated to 600 C. for 30 minutes; some were dipped in a 500 F. oil bath for 10 minutes; some were given bend tests; and others were left untouched in the labo-' ratory for six months. In no case did the samples show any degree of blistering, peeling, or other evidences of poor adhesion.
In summary it may be stated that several methods of plating on aluminum were evaluated to establish a method which would give perfect adhesion between the plated metal and the aluminum and, to a lesser extent, a method which could be utilized by the general type of plating personnel. The familiar zincate process was evaluated 'but did not give the desired results unless used by skilled personnel. A modification of the zincate process was investigated and found to give more consistent results than the normal zincate method. However, this method did not fulfill the requirements desired. A method which was developeddn England of putting nickel on aluminum, instead of zinc, wa investigated and found to be to a reverse current treatment in sulfuric acid; rinsing in water; and thereafter electrically depositing a metal upon the composite plated article other than nickel.
2. In a method of depositing an electroplate of a nickel group metal upon articles of aluminum and aluminum-base alloys, the steps which include degreasing the article; subjecting the article to two etching actions, the first, dipping in a 10% by volume solution of 48- 52% hydrofluoric acid, and the second, dipping in a solution of 50% hydrochloric acid containing 9 to 10 grams per liter of manganous sulfate, the total etching time varying from 10 to 80 seconds, depending upon the aluminum alloy; cathodically treating the article in an aqueous nickel bath comprising 19 ounces per gallon of nickel sulfate, 10 ounces per gallon of magnesium sulfate, 2 ounces per gallon of ammonium chloride, and 2 ounces per gallon of boric acid and subjecting the bath to a current density of 15 amperes per square foot for a period of approximately 10 minutes, electrodepositing a layer of nickel on the article and controlling the electrodeposition to produce a thickness whichranges from 0.0001 inch to 0.0005 inch; and then partially drying with an air blast; heat treating the composite plated article in an oven at a temperature of about 1000 F. for a period of 2V: to 5 minutes; then removing the light blue oxide that forms thereon during the heat treating step by anodically treating the composite plated article for a period of 30 to 45 seconds at 4 volts in a solution of 3 ounces per gallon of sodium hydroxide and 2 ounces per gallon of sodium carbonate; subjecting the composite plated article to a reverse current treatment in 25% sulfuric acid a great improvement over the zinc coating methods. 75 for the period of approximately to seconds at 4 7 volts; and thereafter electrically depositing a metal upon the composite plated article other than nickel.
3. In a method of depositing an electroplate of a nickel group metal upon articles of aluminum and aluminumbase alloys, the steps which include degreasing the article with trichlorethylene vapors; rinsing in water; subjecting the article to two etching actions, the first, dipping in a by volume solution of 48-52% hydrofluoric acid, rinsing in water, and the second, dipping in a solution of 50% hydrochloric acid containing 9 to 10 gallons per liter of manganous sulfate, the total etching time varying from 10 to 80 seconds, depending upon the aluminum alloy; rinsing in water; cathodically treating the article in an aqueous nickel bath comprising 19 ounces per gallon of nickel sulfate, 10 ounces per gallon of magnesium sulfate, 2 ounces per gallon of ammonium chloride, and 2 ounces per gallon of boric acid, electrodepositing a layer of nickel on the article and controlling the electrodeposition to produce a thickness which ranges from 0.0001 inch to 0.0005 inch; rinsing in water and then partially drying with an air blast; heat treating the composite plated article in an oven at a temperature of about 1000 F. for a period of about 5 minutes; then removing the light blue oxide that forms thereon during the heat treating step by anodically treating the composite plated articles for a period of to seconds at 4 volts in a solution of 3 ounces per gallon of sodium hydroxide and 2 ounces per gallon of sodium carbonate; rinsing in water; subjecting the composite plated article to a reverse current treatment in 25% sulfuric acid for the period of approximately to seconds at 4 volts; rinsing in water; and plating the article with gold from a basic gold plating solution.
References Cited in the file of this patent UNITED STATES PATENTS 1,791,642 Schulte Feb. 10, 1931 1,975,818 Work Oct. 9, 1934 2,233,410 Frasch Mar. 4, 1941 2,637,686 McKay May 5, 1953 2,683,835 Freedman July 13, 1954 2,894,884 Gray July 14, 1959
Claims (1)
1. IN A METHOD OF DEPOSITING AN ELECTROPLATE OF A NICKEL GROUP METAL UPON ARTICLES OF ALUMINUM AND ALUMINUMBASE ALLOYS, THE STEPS WHICH INCLUDE DEGREASING THE ARTICLE, RISING IN WATER, SUBJECTING THE ARTICLE TO TWO ETCHING ACTIONS, THE FIRST, DIPPING IN HYDROFLUORIC ACID, RISING IN WATER, AND THE SECOND, DKPPING IN A SOLUTION OF HYDROCHLORIC ACID CONTAINING MANGANOUS SULFATE, THE TOTAL ETCHING TIME VARYING FROM 10 TO 80 SECONDS, RINSING IN WATER, CATHODICALLY TREATING THE ARTICLE IN AN AQUEOUS NICKEL BATH COMPRISING NICKEL SULFATE, MAGNESIUM SULFATE, AMMONIUM CHLORIDE, AND BORIC ACID AND SUBJECTING THE BATH TO A CURRENT DENSITY OF CIRCA 15 AMPERES PER SQUARE FOOT FOR A PERIOD OF APPROXIMATELY 10 MINUTES, ELECTRODEPOSITING A LAYER OF NICKEL ON THE ARTICLE AND CONTROLLING THE ELECTRODEPOSITION TO PRODUCE A THICKNESS WHICH RANGES FROM 0.0001 INCH TO 0.0005 INCH, RINSING IN WATER AND THEN PARTIALLY DRYING WITH AN AIR BLAST, HEAT TREATING THE COMPOSITE PLATED ARTICLE AT A TEMPERATURE OF ABOUT 1000*F. FOR A PERIOD OF 21/2 TO 5 MINUTES, THEN REMOVING THE LIGHT BLUE OXIDE THAT FORMS THERON DURING THE HEAT TREATING STEP BY ANODICALLY TREATING THE COMPOSITE PLATED ARTICLE IN A SOLUTION OF SODIUM HYDROXIDE AND SODIUM CARBONATE, RISING IN WATER, SUBJECTING THE COMPOSITE PLATED ARTICLE TO A REVERSE CURRENT TREATMENT IN SULFURIC ACID, RISING IN WATER, AND THEREAFTER ELECTRICALLY DEPOSITING A METAL UPON THE COMPOSITE PLATED ARTICLE OTHER THAN NICKEL.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US746067A US2970090A (en) | 1958-07-02 | 1958-07-02 | Plating nickel on aluminum |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US746067A US2970090A (en) | 1958-07-02 | 1958-07-02 | Plating nickel on aluminum |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2970090A true US2970090A (en) | 1961-01-31 |
Family
ID=24999344
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US746067A Expired - Lifetime US2970090A (en) | 1958-07-02 | 1958-07-02 | Plating nickel on aluminum |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2970090A (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3223598A (en) * | 1962-11-23 | 1965-12-14 | Germaine F Jacky | Method for determining the adhesion of metal plating |
| US3244628A (en) * | 1963-05-22 | 1966-04-05 | Texaco Inc | Method of grease manufacture |
| US3342330A (en) * | 1964-05-05 | 1967-09-19 | M & T Chemicals Inc | New product and process |
| US3515650A (en) * | 1966-06-02 | 1970-06-02 | Toyoda Chuo Kenkyusho Kk | Method of electroplating nickel on an aluminum article |
| US4104134A (en) * | 1977-08-31 | 1978-08-01 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Method for making an aluminum or copper substrate panel for selective absorption of solar energy |
| US4115211A (en) * | 1975-12-26 | 1978-09-19 | Nihon Kagaku Sangyo Co., Ltd. | Process for metal plating on aluminum and aluminum alloys |
| 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 |
| US20040232211A1 (en) * | 2003-05-19 | 2004-11-25 | Kayser Gregory F. | Diffusion bonded composite material and method therefor |
| GB2517006A (en) * | 2013-08-06 | 2015-02-11 | Saudi Internat Petrochemical Company | Nickel direct-plating |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1791642A (en) * | 1926-05-29 | 1931-02-10 | Schulte Louis | Process of plating aluminum |
| US1975818A (en) * | 1932-08-24 | 1934-10-09 | Aluminum Co Of America | Coating for pistons |
| US2233410A (en) * | 1936-07-02 | 1941-03-04 | Produits Chim Terres Rares Soc | Process for direct nickel-plating of aluminum and its alloys |
| US2637686A (en) * | 1949-04-02 | 1953-05-05 | Int Nickel Co | Process of producing drawn articles |
| US2683835A (en) * | 1949-02-19 | 1954-07-13 | Rca Corp | Electron tube structure |
| US2894884A (en) * | 1945-01-09 | 1959-07-14 | Allen G Gray | Method of applying nickel coatings on uranium |
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1958
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Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1791642A (en) * | 1926-05-29 | 1931-02-10 | Schulte Louis | Process of plating aluminum |
| US1975818A (en) * | 1932-08-24 | 1934-10-09 | Aluminum Co Of America | Coating for pistons |
| US2233410A (en) * | 1936-07-02 | 1941-03-04 | Produits Chim Terres Rares Soc | Process for direct nickel-plating of aluminum and its alloys |
| US2894884A (en) * | 1945-01-09 | 1959-07-14 | Allen G Gray | Method of applying nickel coatings on uranium |
| US2683835A (en) * | 1949-02-19 | 1954-07-13 | Rca Corp | Electron tube structure |
| US2637686A (en) * | 1949-04-02 | 1953-05-05 | Int Nickel Co | Process of producing drawn articles |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3223598A (en) * | 1962-11-23 | 1965-12-14 | Germaine F Jacky | Method for determining the adhesion of metal plating |
| US3244628A (en) * | 1963-05-22 | 1966-04-05 | Texaco Inc | Method of grease manufacture |
| US3342330A (en) * | 1964-05-05 | 1967-09-19 | M & T Chemicals Inc | New product and process |
| US3515650A (en) * | 1966-06-02 | 1970-06-02 | Toyoda Chuo Kenkyusho Kk | Method of electroplating nickel on an aluminum article |
| US4115211A (en) * | 1975-12-26 | 1978-09-19 | Nihon Kagaku Sangyo Co., Ltd. | Process for metal plating on aluminum and aluminum alloys |
| US4104134A (en) * | 1977-08-31 | 1978-08-01 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Method for making an aluminum or copper substrate panel for selective absorption of solar energy |
| 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 |
| US20040232211A1 (en) * | 2003-05-19 | 2004-11-25 | Kayser Gregory F. | Diffusion bonded composite material and method therefor |
| US8225481B2 (en) * | 2003-05-19 | 2012-07-24 | Pratt & Whitney Rocketdyne, Inc. | Diffusion bonded composite material and method therefor |
| GB2517006A (en) * | 2013-08-06 | 2015-02-11 | Saudi Internat Petrochemical Company | Nickel direct-plating |
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