Description:
This invention relates to the art of aluminizing metal surfaces by diffusion to provide a surface on the metal which is rendered more resistant to corrosion or oxidation at high temperatures and/or in corrosive atmospheres, such as exist in a combustion engine, turbine, and the like. By diffusion of aluminum into the surface of such metals as high nickel or cobalt alloys and high alloy steels, heat shock erosion, corrosion resistance and other physical and mechanical properties are markedly improved.
To the present, in the aluminizing treatment by diffusion coating, the metal part is heated to a temperature above 1,000° C. in a pack formed of a powdered mixture of metallic aluminum and aluminum oxides, without and preferably with a small amount of halide salt such as ammonium chloride or ammonium fluoride, for about 4 to 10 hours in a nonoxidizing atmosphere.
The aluminum diffuses into the surface, usually to a depth within the range of about 10-20 microns, depending somewhat upon the time and temperature of the aluminizing treatment and the amount of aluminum in the pack, with the amount of aluminum in the diffusion layer decreasing from the surface inwardly toward the center in amounts somewhat proportionate to the distance from the surface.
It is an object of this invention to provide an improved aluminized article and method for preparation of same wherein the diffusion coating of aluminum remains concentrated in a narrow layer on the surface of the article without excessive diffusion into the interior of the article; whereby a better bond is achieved between the diffusion coating and metal substrate; and whereby a complex series of compounds are formed in the diffusion layer to provide an improved coating which offers higher temperature corrosion resistance.
In accordance with the practice of this invention, the parts formed of a super alloy, and preferably nickel and cobalt based alloys, are first processed to provide the surface portions to be aluminized with a thin coating of nickel, in a first coating step. The coated parts are then packed in the conventional manner and conventional compositions for aluminizing the surface by diffusion transfer of aluminum. The presence of nickel as a precoat on the metal surface is believed to operate as a barrier coat which concentrates the diffused aluminum in the surface portions of the metal parts to provide an aluminized surface having greatly improved corrosion resistance, especially when measured at high temperature and in the presence of highly corrosive gases.
In the described two-stage process of first nickel plating and then diffusion coating to aluminize the plated surface by a pack cementation process it is desirable to deposit a nickel coating in the first stage having a thickness greater than 0.0001 inch and preferably having a thickness within the range of 0.0001 to 0.001 inch.
The desired thickness of nickel coating can be deposited by conventional electroplating processes, such as described in the article published by the ASM Committee on Nickel Plating, entitled Nickel Plating, published in the Metals Handbook, Volume II, pages 432-443, under general purpose plating baths. Instead, the desired thickness of nickel coating can be deposited on the surface of the parts nonelectrically, as described on pages 443-445 of the Metals Handbook, Volume II, supra, under the heading Nonelectrolytic Nickel Plating.
The aluminizing pack employed in the pack cementation process for aluminizing the nickel-coated surfaces can be formulated to contain aluminum metal in finely divided form in an amount within the range of 0.1 to 10 percent by weight with the remainder formed of a finely divided filler, preferably alumina. Although it is not essential, use can be made of an energizer, such as ammonium chloride or ammonium fluoride, in an amount within the range of 0.01 to 5 percent by weight of the pack. A hydrogen or inert atmosphere is maintained during diffusion coating while the materials are heated to a temperature within the range of 1,800° to 2,000° F. or a time sufficient to build up a final coating thickness within the range of 0.001 to 0.005 and preferably within the range of 0.0015 to 0.003 inch. The desired coating thickness is obtained with a pack of the type described in about 9 to 10 hours of heating.
The following examples are given by way of illustration, but not by way of limitation, of the practice of this invention:
Alloy Compositions: ------------------------------------------------------------
--------------- Example 1
Percent by Weight Ni 70.0 Cr 12.0 W 5.0 Al 5.0 Mo 3.5 Ti, Nb, Ta 2.5 Fe, C, Mn, Si Balance ------------------------------------------------------------
--------------- Example 2
Percent by Weight Co 60.0 Cr 20.0 W 10.0 Nb 2.0 Ni 1.0 Fe, C, Mn, Si Balance ------------------------------------------------------------
--------------- Example 3
Percent by Weight C 0.08 Mn 0.75 Si 0.75 Cr 19.0 Co 19.5 Mo 4.0 Ti 2.9 Al 2.9 Fe 4.0 Ni Balance ------------------------------------------------------------
--------------- Example 4
Percent by Weight C 0.12 Mn 0.15 Si 0.4 Cr 13.0 Mo 4.5 Ti 0.6 Al 6.0 Fe 1.0 Cb 2.25 Ni Balance
First stage of nickel coating: ------------------------------------------------------------
--------------- Example 5
Composition of Electrolytic Bath
Nickel sulfate, NiSO 4 6H 2 O 30 to 55 Nickel chloride, NiCl 2 6H 2 O 4 to 8(a) Nickel sulfamate, Ni(SO 3 NH 2 ) 2 -- Nickel fluoborate, Ni(BF 4 ) 2 -- Total nickel as metal 7.7 to 14.2 Boric acid, H 3 BO 3 4 to 6 Antipitting additives (b)
Operating Conditions
pH 1.5 to 5.2 Temperature F. 115 to 160 Current density, a. per sq. ft. 10 to 100 ____________________________________________________________
______________ ------------------------------------------------------------
--------------- Example
Composition of Electrolytic Bath
Nickel sulfate, NiSO 4 6H 2 O -- Nickel chloride, NiCl 2 6H 2 O 0 to 4 Nickel sulfamate, Ni(SO 3 NH 2 ) 2 35 to 60 Nickel fluoborate, Ni(BF 4 ) 2 -- Total nickel as metal 8.2 to 15 Boric acid, H 3 BO 3 4 to 6 Antipitting additives (b)
Operating Conditions
pH 3 to 5 Temperature F. 100 to 140 Current density, a. per sq. ft. 25 to 300 ____________________________________________________________
______________ ------------------------------------------------------------
--------------- Example 7
Composition of Electrolytic Bath
Nickel sulfate, NiSO 4 6H 2 O -- Nickel chloride, NiCl 2 6H 2 O 0 to 2 Nickel sulfamate, Ni(SO 3 NH 2 ) 2 -- Nickel fluoborate, Ni(BF 4 ) 2 30 to 40 Total nickel as metal 7.6 to 10.5 Boric acid, H 3 BO 3 2 to 4 Antipitting additives (b)
Operating Conditions
pH 2.5 to 4 Temperature, F. 100 to 160 Current density, a. per sq. ft. 25 to 300 ____________________________________________________________
______________ ------------------------------------------------------------
--------------- Example 8
Composition Nonelectrolytic Bath
Nickel chloride (NiCl 2 6H 2 O 80 oz. per gal. Boric acid (H 3 BO 3 ) 4 oz. per gal. Operating Conditions pH 3.5 to 4.5 Temperature 160° F. ____________________________________________________________
______________ ------------------------------------------------------------
--------------- Example 9
Composition Nonelectrolytic Bath
Nickel chloride 30 Nickel sulfate -- Sodium hypophosphite 10 Sodium acetate -- Sodium hydroxyacetate 50 Sodium succinate -- Lactic acid (80%) -- Propionic acid (100%) --
Operating Conditions
pH 4 to 6 Temperature, F. 190 to 210 Plating rate (approx.), mil per hr. 0.5 ____________________________________________________________
______________ ------------------------------------------------------------
--------------- Example 10
Aluminizing Pack: 5 pounds powdered aluminum metal 100 pounds powdered alumina ____________________________________________________________
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--------------- Example 11
7 pounds powdered aluminum metal 100 pounds powdered alumina 0.2 pound ammonium chloride ____________________________________________________________
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In the electrolytic plating systems of examples 5 to 7, the part is suspended as a cathode in the electrolyte until a coating thickness within the range of 0.0001 to 0.001 inch has been deposited. The part is then removed and rinsed with water to remove electrolyte.
In the nonelectrolytic systems of examples 8 and 9, a thinner nickel coating is deposited on the metal surfaces. In practice, the parts are immersed in the bath with continuous movement until a nickel coating having a thickness within the range of 0.0001 to 0.001 inch is deposited and the part is then removed and rinsed.
The nickel plated parts are packed with the pack composition of examples 10 and 11 in a retort. The parts formed of the cobalt alloy of example 2 are heated in a hydrogen atmosphere for 10 hours at 1950° F. while the parts formed of the nickel-based alloys of examples 1, 3 and 4 are heated in a hydrogen atmosphere for 9 hours at 1,950° F. to form parts having a final coating thickness within the range of 0.0015 to 0.003 inch.
Instead of making use of the nickel or cobalt based alloys of examples 1 to 4, use can be made of parts formed of nickel or cobalt based superalloys in which corrosion resistance at high temperature and resistance to deterioration by the sulfides present in corrosive gases is greatly improved.
The term "powdered" or "finely divided" form, as applied to the elements in the pack composition, is meant to refer to aluminum metal particles of preferably less than 5 microns and is meant to refer to particles of less than 100 microns and preferably within the range of 5-100 microns for the filler or alumina component of each pack.
It will be understood that changes may be made in the details of formulation and operation without departing from the spirit of the invention, especially as defined in the following claims.