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Publication numberUS3819338 A
Publication typeGrant
Publication dateJun 25, 1974
Filing dateSep 17, 1971
Priority dateSep 14, 1968
Publication numberUS 3819338 A, US 3819338A, US-A-3819338, US3819338 A, US3819338A
InventorsH Meinhardt, K Bungardt, G Lehnert
Original AssigneeDeutsche Edelstahlwerke Ag
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Protective diffusion layer on nickel and/or cobalt-based alloys
US 3819338 A
Abstract
Nickel and/or cobalt-based alloys are given a protective coating by diffusing into the surface of the alloy metallic aluminum and one or more metals of the platinum groups.
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Description  (OCR text may contain errors)

United States Patent 1191 Bungardt et a1.

[ 1 June 25, 1974 PROTECTIVE DIFFUSION LAYER ON NICKEL AND/OR COBALT-BASED ALLOYS [75] Inventors: Karl Bungardt; Gunter Lehnert;

Helmut W. Meinhardt, all of Krefeld, Germany [73] Assignee: Deutsche Edelstahlwerke Aktiengesellschaft, Krefeld, Germany 221 Filed: Sept. 17,1971

21 Appl. No.: 181,600

.Related U.S. Application Data [62] Division of Ser. No. 856,539, Sept. 10, 1969, Pat.

30 Foreign Application Priority Data Sept 14, 1968 Germany 1796175 [52] U.S. Cl. 29/194, 29/197 Primary Examiner--L. Dewayne Rutledge Assistant Examiner-E. L. Weise Attorney, Agent, or Firm-Cushman, Darby & Cushman [57] ABSTRACT Nickel and/or cobalt-based alloys are given a protective coating by diffusing into the surface of the alloy metallic aluminum and one or more metals of the platinum groups.

-1 Claim, 1 Drawing Figure PATENTEU JUHZ 5 I974 wwvi y b$$h m mum m mum mum mm I I MR .QEQQQRQW ix 1/1 fl!IIIIIIIIIllIIIIIIIIIIIIIIIIIIIIII/IIIII,

This is a division, of application Ser. No. 856,539 filed Sept. 10, 1969 now US. Pat. No. 3,677,789 dated July 18, 1972.

This invention relates to the production of hightemperature corrosion and scale-resistant protective diffusion layers on parts made of high-temperature nickel and/or cobalt-based alloys, and to methods of producing such layers.

Parts exposed to the action of corrosive media at high temperatures as well as to mechanical stress, for example turbine blades, are conventionally made of high temperature alloys based on nickel and/or cobalt, and are provided with a protective layer produced by diffusion to render them resistant to corrosion and scaling and thereby to prolong their useful life. For the formation of the protective layer aluminum is preferentially diffused into the surface of such parts. Although parts that have been thus aluminized are particularly resistant to corrosion and scaling, their life, particularly turbine blades, is not as long as would be desirable.

It is therefore the object of the invention to provide parts made of high-temperature alloys that are based on nickel and/or cobalt and that areto be subjected to high mechanical stress and to attack by corrosive media, with a surface layer that will prolong the, life of such parts which, primarily due to scaling, will otherwise have a restricted life.

For achieving this object, the present invention provides a protective layer by diffusing into the surface of the parts that are to be protected aluminum and one or more metals of the platinum group of elements, particularly platinum, rhodium and palladium. Tests have shown that parts provided with a protective layer according to the invention have a longer life in service compared with parts into which aluminum alone has been diffused in conventional manner.

One or more metals of the platinum group can be diffused into the parts at the same time as the aluminum, or alternatively in a preferred method of producing the proposed protective diffusion layer according to the invention, one or more metals of the platinum group may first be applied to the surface of the part that is to be protected in the form of'a coating at'least 7p. thick, and in a following diffusion heat treatment aluminum may then be diffused into the 'surface together with the metal or metals of the platinum group already deposited. Thus in the said preferred method, the surface of the part that is to be protected is first coated with a metal or metals of the platinum group, and this metal or these metals of the platinum group are then diffused into the surface simultaneously with the aluminum. The said coating of one or more metals of the platinum group may be provided either electrolytically, or by dipping, spraying, vapor deposition or by mechanical plating. During the followingdiffusion treatment the metal forming this coating together with the aluminum then diffuses into the surface of the part that is to be protected and forms a high-temperature scale-resistant protective layer on the part.

It is also possible to produce a diffused layer according to the invention byfirst applying to the surface of the part that is to be protected a coating of one or more metals of the platinum group and then applying a further layer of aluminum covering the first coating before the pan is submitted to the diffusion treatment,

whereby both the metal or metals of the platinum group and the aluminum diffuse into the said surface.

In a further preferred embodiment of the method of the invention the parts that have been provided with a coating of one or more metals of the platinum group may be embedded for the diffusion treatment in a powder mixture containing metallic aluminum.

In general diffusion may be effected by heating between about 900C and about l,200C for about 2 hours to about 10 hours.

The advantages that can be secured by the invention are illustrated by the diagram of the accompanying drawing, wherein the amount of scale formed in mglsqcm. is plotted against the time the part is in operative use at l,l00C. Test pieces provided with a diffusion layer according to the invention were compared with parts having surfaces that were either left unprotected or that had been protected with a conventional diffused layer of aluminum.

The test pieces consisted of an alloy containing 0.12 percent carbon, less than 0.25 percent silicon, less than 0.25 percent manganese, 13.5 percent chromium, 4.5 percent molybdenum, 6.25 percent aluminum, 2.3 percent niobium/tantalum, less than 1.0 percent cobalt, 0.9 percent titanium, less than 1.5 percent iron, traces of boron and zirconium, the remainder being nickel.

The test pieces that had been provided with the protective diffusion layer were first subjected to a preliminary treatment consisting of wet blasting, degreasing in a cyanide bath 10 seconds cathodically and 30 seconds anodically, followed by rinsing in water and anodic pickling at 40C first 3 seconds in a 10 percent by volume H SO bath followed by rinsing in water and then 30 seconds cathodically and 10 seconds anodically, pickling in a 10 percent by weight solution NaOl-l bath, followed by rinsing in water.

For the production of the diffusion layer according to the invention the test pieces were then platinum coated in a bath consisting of 13 g/l of hexachloroplatinic acid, H PtCl 45g/] of triammonium phosphate, (NH.,) PO,,

240 g/l of di-sodium hydrogen phosphate, Na HPO The temperature of the bath was 65C, the current density 9.0 arnp/dm and the voltage 1.5 volts. Different thicknesses of the platinum coating were provided by altering the treatment times accordingly.

After having been platinum coated, the parts were heat treated first for 2 hours at 260C and then for 3 hours at 400C to drive off hydrogen and to reduce the hardness of the platinum coating. Finally the surface was degreased by rinsing in methanol.

The test pieces which had thus been heated according to the invention, together with the control pieces, were then submitted to an aluminum diffusion treatment. The test pieces were packed into a powder mixture consisting of 5 percent aluminum and percent A1 0 and diffusion treated for 2% hours at l,l00C under hydrogen as a protective gas.

The accompanying diagram reveals the difference in scale formation between completely untreated parts, parts that had been merely diffusion treated with aluminum and parts that had been provided with the protective layer according to the invention, the considerable superiority of which is apparent. Whereas the untreated parts underwent considerable deterioration due to scaling after 20 to 30 hours at the test temperature of l,lC, parts that had been subjected to aluminum diffusion in conventional manner did not begin to scale until much later. However, the scaling resistance of the parts provided with the protective layer according to the invention was several times better than the best of the comparative test pieces. Thus when a 7p. platinum layer had been applied the parts still disclosed no significant scaling after 1,000 hours.

When considering the diagram it is to be noted that the areas surrounded by full lines and by dashed lines are the areas of scatter of the results achieved with untreated parts and with parts that had been exclusively aluminized by diffusion, whereas the other indicated lines for parts provided with the protective layers according to the invention relate to individual tests and do not comprise an area of scatter. However, the tendency of the test pieces that had been provided with the diffusion layer according to the invention to last longer is very clearly apparent.

Turbine blades made of the above-specified base ma-- terial provided with a 7 1. platinum coating by electrodeposition in the above-described manner and then submitted to the above-described aluminum diffusion treatment to form a layer having a total depth of 65 were also subjected to thermal shock tests to examine their liability to crack. For this purpose the turbine blades were affixed to a wheel which was rotated. Two burners operated with kerosene generated a peak temperature of l,050C on the surface of the turbine blades. After having passed through the burner zones the turbine blades were quenched to about C by exposing them to a blast of compressed air. The heating time in each case was 60 seconds and the quenching time was also 60 seconds.

Simultaneously with this exposure to thermal stress, the turbine blades were subjected to mechanical stresses by mounting them eccentrically on the rotating wheel and thereby subjecting the trailing edges of the turbine blades to tension. I

After 10,000 temperature reversals, the turbine blades provided with the protective diffusion layer according to the invention showed no damage due to cracking or chipping. The appearance of the protective surface layer when inspected by the naked eye was still excellent after 10,000 temperature reversals, whereas after the same number of temperature reversals blades that had been provided with other conventional types of surface protection had scaled surfaces as well as cracks.

What we claim is:

1. An object made of an alloy selected from the group consisting of nickel based alloys, cobalt based alloys and nickel/cobalt based alloy having a protective diffusion layer thereon and into the surface thereof, said diffusion layer consisting of the nickel based, cobalt based, or nickel/cobalt based alloy, aluminum and at least one metal of the group consisting of platinum,

palladium and rhodium.

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Referenced by
Citing PatentFiling datePublication dateApplicantTitle
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US3979273 *May 27, 1975Sep 7, 1976United Technologies CorporationMethod of forming aluminide coatings on nickel-, cobalt-, and iron-base alloys
US3999956 *Feb 21, 1975Dec 28, 1976Chromalloy American CorporationResistance to high temperature oxidation and sulfidation
US4070507 *Jul 29, 1976Jan 24, 1978Chromalloy American CorporationPlatinum-rhodium-containing high temperature alloy coating method
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Classifications
U.S. Classification428/652, 428/938, 428/926, 428/678, 428/670, 428/941
International ClassificationC23C10/00, C23C10/52
Cooperative ClassificationC23C10/00, Y10S428/926, C23C10/52, Y10S428/941, Y10S428/938
European ClassificationC23C10/52, C23C10/00