Multi-layer corrosion resistant coating for fasteners and method of making

Abstract

A corrosion resistant coating and process comprises the following layers applied in sequence over a ferrous metal substrate: a micro-throwing nickel-zinc alloy plating; an optional galvanically protective zinc metal plating; a zinc-nickel alloy plating containing 5 to 30 weight percent nickel; and an organic coating such as paint. In place of the organic coating there may be utilized sequential layers of copper, nickel and chromium or chromium-substitute plating. The coating is preferably used with steel drill screw fasteners.

Description

BACKGROUND OF THE INVENTION

The present invention relates to multi-layered coatings to impart corrosion resistance to ferrous metal fastener substrates.

In areas where corrosion of ferrous metal substrates provide particular and pervasive problems, it is well known to utilize organic films such as paints and metallic coatings such as metal plating to minimize the effects of corrosion. Prior art in the general area of ferrous metal plating discloses nickel plating over an intermediate nickel zinc alloy plating (75 to 90% zinc), as in U.S. Pat. No. 1,564,581, and the use of zinc-rich, zinc-nickel alloy plating over a layer of copper or nickel plating, as in U.S. Pat. No. 2,419,231. Other uses of zinc-nickel plating layers are found in U.S. Pat. Nos. 4,282,073; 3,420,754; 4,407,900; and 4,314,893, and in Japanese Patent Publication 57-207199.

In automotive and other applications where relatively severe corrosive agents are found, and, in particular, for the metal fasteners used in such applications, improvements in corrosion resistance have been disclosed in U.S. Pat. Nos. 4,188,459 and 4,329,402, the disclosures of which are hereby incorporated by reference. Prior to the aforementioned patents, it was known that automotive fasteners can utilize sequential plating layers of copper, cadmium, copper, nickel and chromium or a chromiu substitute such as tin-nickel, tin-cobalt or tin-cobalt-zinc alloys.

U.S. Pat. No. 4,188,459 discloses a multi-layered corrosion resistant plating for fasteners comprising a first micro-throwing alloy layer of nickel alloy followed by a layer of a galvanically protective metal or alloy such as cadmium, cadmium-tin, a dual layer of cadmium and tin, zinc or zinc alloy. Over this galvanically protective layer there is applied a layer of copper plating, followed by a layer of nickel plating, followed by a layer of chromium or metallic chromium substitute. U.S. Pat. No. 4,329,402 discloses the same first layer of a micro-throwing alloy, with the galvanically protective plating layer optionally applied next, and followed by an outer layer of chromate film or an organic coating such as paint.

While the aforementioned plating and coating layers provide good protection, it is advantageous to provide comparable or superior protection with a minimum of coating layers, for obvious cost reasons. While the galvanic protective layers of zinc are desirable, when they are utilized as the final plating layer there is often the problem of the production of an insoluble white corrosion product as they are sacrificially attacked by corrosive agents in use.

In the area of automotive fasteners where the fasteners are often applied manually on the assembly line there is additional problems of fatigue of the assembly worker due to the often high installation torques, and long drill times resulting from the use of high friction and thicker corrosion resistant coatings. Cadmium plating has provided lower friction to ferrous fasteners, but such plating has considerable drawbacks with respect to disposal of plating bath effluent containing cadmium metal and the cyanide often used in such baths, as well as the presence of poisonous metallic cadmium on the fastener.

Bearing in mind these and other deficiencies of the prior art, it is therefore an object of the present invention to provide superior corrosion resistant to ferrous metal substrates which are used in relatively severe corrosive environments such as those found in the automobile.

It is another object of the present invention to provide a corrosion resistant coating which is relatively low in cost yet is reliable in application and performance.

It is a further object of the present invention to provide a superior corrosion resisting protection for metal substrates having surface defects such as pits, cracks, laps, or voids.

It is another object of the present invention to provide the aforementioned corrosion resistant properties for ferrous metal fasteners, in particular.

It is a further object of the present invention to provide a corrosion resistant ferrous metal fastener which has a lower installation force or torque

It is still another object of the present invention to provide improved fastener installation and corrosion resistance without the use of cadmium.

SUMMARY OF THE INVENTION

The above and other objects, which will be obvious to one skilled in the art, are achieved in the present invention which provides, in a first aspect, a process for improving the corrosion resistance of a ferrous metal fastener comprising the steps of applying a layer of nickel or a nickel based alloy over the metal fastener and thereafter applying a second layer of a zinc based alloy over the nickel or nickel alloy layer. In another aspect, the present invention relates to a ferrous metal fastener having a corrosion resisting multi layer coating applied as described above. In both aspects of the invention it is preferred that the first layer be a micro-throwing nickel alloy with the second plating layer being a zinc-nickel alloy having from about 5 to about 30 weight percent nickel, more preferably from about 8 to about 15 weight percent nickel. Optionally, an organic coating or chromate conversion covers the zinc-nickel alloy layer. In place of the organic coating there may be employed plating layers of copper, nickel and chromium substitute, in that order.

DETAILED DESCRIPTION OF THE INVENTION

The multiple coating layers of the present invention can be applied to any ferrous metal substrate, e.g., iron or steel, and are particularly advantageous when applied to fasteners such as rivets or drill screws or other metal cutting screws subject to relatively severe corrosive environments. Fasteners used on automobile or truck exteriors fall into this category Examples of drill screw fasteners are disclosed in U.S. Pat. Nos. 4,692,080; 4,730,970 and 4,713,855, the disclosures of which are hereby incorporated by reference.

The first layer applied to and directly over the ferrous metal fastener substrate is a plating of nickel or nickel based alloy such as nickel-zinc, nickel-iron or nickel-cobalt. The preferred first layer is a micro-throwing nickel alloy as described in U.S. Pat. Nos. 4,188,459 and 4,329,402. The micro-throwing alloy is particularly advantageous in that it has the ability to preferentially plate in surface defects of metal substrates such as pits, cracks, laps, or voids as small as 0.00002 inches in size. The micro-throwing alloy deposits and forms a layer which is even thicker inside of the surface defects, seams, pits or the like than on the plane surface from which the surface defect is formed.

The micro-throwing nickel alloy preferably utilizes a second, alloying metal component selected from zinc, iron, cobalt or cadmium. Preferably, the nickel comprises about 97.0 to 99.9% by weight of the alloy, while the zinc or cadmium comprises 0.1 to 3.0 percent by weight. Most preferably, zinc is employed as the alloying agent in an amount less than 1.0% by weight of the alloy, with the nickel comprising the balance. Ternary or quaternary alloy containing nickel and zinc may also be advantageously utilized. The thickness of the first micro-throwing alloy layer is preferably between 0.0005 and 0.00005 inches, more preferably over 0.0001 and up to 0.0004 inches. This layer is not generally considered to be a so-called "strike" layer but is meant to level irregularities on the fastener surface and provide corrosion protection on its own.

The micro-throwing nickel alloy may be applied by conventional electroplating baths and techniques. For example, nickel-cadmium alloys can be electroplated from sulfate or sulfate-chloride type baths as are conventionally known and commercially available. Likewise, nickel-zinc alloys can be plated from chloride, sulfate, sulfamate, ammoniacial or pyrophosphate type baths.

To protect the underlying nickel plating layer and metal substrate, a second layer of a galvanically protective zinc is optionally applied to and directly over the nickel first layer. This second layer, when present, acts as the primary sacrificial anode which corrodes preferentially and protects the underlying metal if and when it is perforated. The property of the micro-throwing alloy to level out or fill any surface defects in the underlying metal substrate acts to remove areas of low current density which provide problems when electroplating this galvanic layer. The preferential galvanic layer is electrodeposited essentially pure zinc which may be plated in a zinc bath commercially available from MacDermid, Inc., Waterbury, Connecticut under the trade name "Kenlevel II" The preferred thickness of the galvanic layer is about 0.003 to 0.00010 inches, with a minimum thickness of 0.0005 inches being more preferred.

Although the protection given the underlying metal by an essentially pure zinc galvanic layer is desirable, the corrosion product formed by oxidation of this galvanic layer is not. From both a functional and aesthetic view point, it is advantageous to minimize the formation of this corrosion product which, in the case of zinc, is white, insoluble and may comprise zinc carbonate (Zn.sub.2 CO.sub.3), zinc oxide (ZnO) and other compounds. To retain the advantages of this galvanic layer while minimizing its disadvantages, the present invention provides in combination a separate layer of a zinc based alloy which is applied either to the aforementioned essentially pure zinc layer or directly onto the first nickel or nickel alloy layer. For simplicity of manufacturing and significant cost advantages, it is preferred that this zinc alloy layer is applied directly over and to the first nickel or nickel alloy layer. This separate zinc alloy contains a major amount of zinc but does not as readily form the white corrosion product which results from essentially pure zinc. Additionally, it provides increased life to the ferrous part. Consequently, this zinc alloy layer provides a better appearance and gives additional protection when used over ferrous metal substrates. Suitable alloying elements are nickel, cobalt and iron, with nickel being preferred. The zinc-nickel alloy should contain a major amount of zinc and is preferably from about 70 to 95 weight percent zinc and from about 5 to 30 weight percent nickel, more preferably about 8 to 15 weight percent nickel, balance zinc. Good results have been achieved with 12% nickel.

The zinc-nickel alloy layer is preferably deposited by electroplating directly over the aforementioned layers by conventional and well-known techniques. The thickness of the zinc-nickel alloy layer is preferably about 0.00005 to 0.0007 inches, with a minimum thickness of 0.0001 inches being more preferred. Best results have been found at a thickness of 0.00045.+-.0.0002 in. for the preferred embodiment where the zinc-nickel alloy layer is deposited directly onto the nickel or nickel alloy layer.

The zinc-nickel layer may be utilized as the outer coating for the steel fastener or other ferrous metal substrate with which it is employed. However, as a preferred final, outer coating directly over the zinc-nickel alloy layer, there may be applied a conversion coating of a chromate or the like or a layer of an organic coating, preferably a paint or metal dye, to provide additional corrosion protection or for aesthetic reasons. Conventional formulations of such coatings and conventional application techniques may be employed, with a substantially continuous film or coating being applied. The thickness of the organic or other coating is not limited and can be varied to obtain the desired level of protection.

The organic coating layer may also include filler material, for example, metal particles, as conventionally employed in metallic paints. The organic coatings which may be utilized include but are not limited to any thermosetting, thermoplastic or nonpolymeric films and preferably may be any conventional paint formulation. Electrophoretic paints such as "E-Coat" , available from Man-Gill Chemical Co. of Cleveland, Ohio, are desirable for uniformity of coating. Other paints may be used, such as those having either a thermosetting phenolic resin, or an alkyd, epoxy, melamine or acrylic base. These paints may be applied in any conventional manner including, but not limited to, dipping, spinning, spraying, rolling, brushing or the like These paints may be either baked or air dried, depending on their formulation and the manufacturer's instructions.

Testing of steel fasteners coated according to the preferred embodiment of the present invention utilizing the intermediate galvanic layer shows salt-spray corrosion resistance essentially equivalent to fasteners utilizing prior art coating of, sequentially, cadmium, copper, nickel and paint layers over a micro-throwing nickel first layer. This excellent corrosion resistance is achieved at considerably lower processing cost than fasteners with the prior art coating.

In an alternate preferred embodiment, in place of the organic coating layer, a layer of copper is applied, followed by a layer of nickel. Each of these layers is preferably provided in a thickness ranging between about 0.0001 to 0.001 inches and are applied from conventional plating baths for each metal or alloy, preferably by electroplating. It is, nevertheless, within the purview of the invention that these layers of metal or alloys thereof can be applied in any suitable manner from any type of plating bath or coating process.

Finally, in the alternate preferred embodiment, a layer of chromium or metallic chromium substitute is applied over the layer of nickel. This layer is preferably 0.00001 to 0.00005 inches in thickness and may also be applied from a conventional plating bath, preferably by electroplating.

The chromium substitutes which may be utilized in accordance with the invention, include but are not limited to, the ternary alloys disclosed and claimed in U.S. Pat. No. Re29,239, the disclosure of which is hereby incorporated by reference. These metals and alloys can all be utilized to provide performance qualities and/or appearance which may be substituted for chromium. The preferred metallic chromium substitutes are the aforementioned ternary alloys of tin, cobalt and a third metal which is either antimony, zinc or a metal of Periodic Table Group III.sub.A or VI.sub.B.

These chromium substitutes are applied as metallic layers in place of or in combination with chromium as the final layer in the alternate preferred plating and method of the invention. For example, the preferred ternary alloys may be applied from aqueous plating bath formulations and utilizing electroplating conditions, as disclosed in the aforementioned U.S. Pat. No. Re29,239. Other ternary alloys including substantial portions of tin and cobalt, as well as simple binary alloys of tin and cobalt, may be utilized as chromium substitutes.

Each layer of the multi-layer plating of the invention may be applied in any conventional manner, utilizing any conventional bath or method for application of the metal or alloy, for example, the baths and methods disclosed in U.S. Pat. No. 4,188,459.

The result of this alternate preferred embodiment is a fastener having applied thereon, in order, the following layers: (1) nickel or nickel alloy (preferably micro-throwing nickel alloy), (2) zinc-nickel alloy (3) copper, (4) nickel, and (5) chromium or chromium substitute. This alternate embodiment dispenses with the cadmium layer disclosed in U.S. Pat. No. 4,188,459 and, with it, the attendant problems of pollution control relating to cadmium plating baths.

While this invention has been described with reference to specific embodiments, it will be recognized by those skilled in the art that variations are possible without departing from the spirit and scope of the invention, and that it is intended to cover all changes and modifications of the invention disclosed herein for the purposes of illustration which do not constitute departure from the spirit and scope of the invention.

Having thus described the invention, what is claimed is:

Claims

1. A process for providing corrosion resistance to a ferrous metal fastener comprising the steps of:

(a) applying a first layer of non-strike nickel or a nickel based alloy of at least 0.00005 in. thickness over said metal fastener;

(b) applying a second layer of a zinc based alloy containing from about 8 to 15 weight percent nickel over said first layer; and

(c) applying a third layer of an organic coating over said second layer.

2. The process of claim 1 wherein said layers in steps (a) and (b) are applied by electroplating.

3. The process of claim 2 wherein said nickel or nickel based alloy first layer (a) comprises a micro-throwing nickel-zinc alloy.

4. The process of claim 1 wherein said metal fastener comprises a drill screw.

5. The process of claim 1 wherein said first layer (a) is nickel of greater than 0.0001 in. thickness.

6. The process of claim 1 wherein said first layer (a) is a nickel based alloy of greater than 0.0001in thickness.

7. A process for providing corrosion resistance to a ferrous metal fastener comprising the steps of:

(a) electroplating a first layer of a non-strike micro-throwing nickel based alloy of at least 0.00005 in. thickness over said fastener;

(b) electroplating a second layer of a zinc based alloy containing from about 85 to 92 weight percent zinc and from about 8 to 15 weight percent nickel over said first layer; and

(c) applying a layer of an organic coating over said zinc based alloy layer.

8. The process of claim 7 wherein said micro-throwing nickel based alloy first layer includes zinc in an amount less than one (1) weight percent.

9. The process of claim 7 wherein said fastener comprises a drill screw.

10. A process for providing corrosion resistance to a ferrous metal drill screw fastener comprising the steps of:

(a) electroplating a first layer of a micro-throwing nickel based alloy containing less than 3 weight percent zinc and of at least 0.00005 in. thickness over said fastener;

(b) electroplating a second layer of a zinc based alloy containing from about 85 to 92 weight percent zinc and from about 8 to 15 weight percent nickel over said first layer; and

(c) applying a layer of an organic coating over said second layer.

11. The process of claim 10 wherein said nickel based alloy first layer (a) comprises zinc in an amount less than 1 weight percent.

12. The process of claim 11 wherein said nickel based first layer (a) is at least 0.0001 in. thickness.

13. A process for providing corrosion resistance to a ferrous metal fastener comprising the steps of:

(a) applying a first layer of non-strike nickel or a nickel based alloy of at least 0.00005 in. thickness over said metal fastener;

(b) applying a second layer of a zinc based alloy containing from about 8 to 15 weight percent nickel over said first layer;

(c) applying a third layer of copper coating over said second layer.

(d) applying a fourth layer of nickel over said third layer; and

(e) applying a fifth layer of chromium or a metallic chromium substitute selected from the group consisting of ternary alloys of tin, cobalt and a third metal selected from antimony, zinc, or a metal of Periodic Table Group III.sub.A or VI.sub.B and a binary alloy comprising cobalt or tin over said fourth layer.

14. The process of claim 13 wherein said layers in steps (a) through (e) are applied by electroplating.

15. The process of claim 14 wherein said nickel or nickel based alloy first layer (a) comprises a micro-throwing nickel-zinc alloy which includes zinc in an amount less than three (3) weight percent.

16. The process of claim 13 wherein said metal fastener comprises a drill screw.

17. The process of claim 13 wherein said first layer (a) is nickel of greater than 0.0001 in. thickness.

18. The process of claim 13 wherein said first layer (a) is a nickel based alloy of greater than 0.0001 in thickness.

19. A corrosion resistant fastener having a ferrous metal substrate and, in sequence, the following layers over said substrate:

(a) a first layer of a non-strike nickel or nickel based alloy of at least 0.00005 in. thickness;

(b) a second layer of a zinc based alloy containing from about 8 to 15 weight percent nickel;

(d) a fourth layer of nickel; and

(e) a fifth layer of chromium or metallic chromium substitute selected from the group consisting of ternary alloys of tin, cobalt and a third metal selected from antimony, zinc or a metal of Periodic Table Group III.sub.A or VI.sub.B and a binary alloy comprising cobalt or tin.

20. The fastener of claim 19 wherein said layers in steps (a) through (e) have been produced by electroplating.

21. The fastener of claim 20 wherein said nickel or nickel based alloy first layer (a) comprises a micro-throwing nickel-zinc alloy which includes zinc in an amount less than three (3) weight percent.

22. The fastener of claim 19 wherein said metal fastener comprises a drill screw.

23. The fastener of claim 19 wherein said first layer (a) is nickel of greater than 0.0001 in. thickness.

24. The fastener of claim 19 wherein said first layer (a) is a nickel based alloy of greater than 0.0001 in. thickness.