IL47407A

IL47407A - Mcraiy type coating alloy

Info

Publication number: IL47407A
Application number: IL47407A
Authority: IL
Original assignee: United Technologies Corp
Priority date: 1974-07-10
Filing date: 1975-06-03
Publication date: 1977-08-31
Also published as: SE7507095L; GB1500780A; NO141371B; FR2277902A1; AU8156075A; IT1039467B; CA1158075A; US3918139A; NO752355L; JPS5842255B2; FR2277902B1; IL47407A0; NO141371C; DE2530197A1; BR7504327A; SE410477B; JPS5130530A; CH606455A5; DE2530197C2; IN144076B

Abstract

There is described nickel, cobalt and nickel-cobalt alloy coating compositions having improved hot corrosion resistance. In particular, an improved MCrAlY type alloy coating composition consists essentially of, by weight, approximately 8-30 percent chromium, 5-15 percent aluminum, up to 1 percent reactive metal selected from the group consisting of yttrium, scandium, thorium and the other rare earth elements and 3-12 percent of a noble metal selected from the group consisting of platinum or rhodium, the balance being selected from the group consisting of nickel, cobalt and nickel-cobalt. [US3918139A]

Description

MCrALY TYPE COATING ALLOBf MCrALY >WB B»s Γ#ΪΟΛΟ The present invention relates to alloys and more particularly to nickel, cobalt or nickel-cobalt coating alloys having improved hot corrosion resistance.

It is known that the modern day jet engine super-alloys are susceptible to oxidation-erosion and hot corrosion at very high temperatures and that it is the usual practice to coat the superalloys with a composition different from and more oxidation-erosion and corrosion resistant than the substrate alloy.

In general, there are two primary types of coatings (1) aluminide coatings, such as those described in the U.S. patent 3 , 102,044 or the U.S. patents 3 , 677 , 789 and 3 , 692 , 554 wherein aluminides are formed by a reaction with or diffusion of a coating on, the substrate surface, and (2) overlay coatings such as those of the MCrAlY type, e.g., NiCrAlY described in the U.S. patent 3 , 754,903 , described in the U.S. patent d li aUlfoii- -flD-Pdal To. 46 ,186 filed Moy 13 , 1974 and FeOrAlY described in the U.S. patent to 3,542, 530. Particularly useful overlay MOrAlY coatings are those consisting essentially of, by weight, approximately 8-30 percent chromium, 5-15 percent aluminum, up to 1 percent reactive metal selected from the group consisting of yttrium, scandium, thorium and lanthanum and the other rare earth elements, balance selected from the group consisting of nickel, cobalt and nickel-cobalt, preferably applied to a thickness of approximately 0.012-0.015 cm.

In contrast to the overlay coatings, the diffusion aluminide coatings are typically provided by reacting aluminum with the deoxidized surface of the artid.e to be protected — the aluminide layer being formed as a barrier zone of varying component concentration with consumption of the substrate components. This aluminide layer in turn oxidizes to form the inert barrier oxide.

In the U.S. patents 3,677,789 and 3,692,554-, a separate layer of metal from the platinum group is applied before the aluminum diffusion treatment. However, because of the complex nature of most of the contemporary alloys, and because the coating composition thereon is derived in part from the components of the substrate alloys, it is difficult to control the coating composition so as to cause the formation of a suitable barrier oxide. In addition, it is inherent in the diffusion technique that the coating formed is nonhomogeneous and, with respect to platinum group metal content for example, there appears a high concentration of the platinum group metal on the surface. The existence of such a gradient, of course, is disadvantageous since, with use, the coating diminishes in effectiveness as its composition changes.

Although the prior art coating compositions have represented improvements over various of their predecessor alloy compositions, the need for further improvements, particularly for example, in hot corrosion resistance, has remained.

The present inventio contemplates alloy compositions and more particularly nickel, cobalt and nickel-cobalt coating alloy compositions having improved hot corrosion resistance. In particular, the present invention contemplates an improved MOrAlY type alloy coating composition consisting essentially of, by weight, approximately 8-30 percent chromium, 5-15 percent aluminum, up to 1 percent reactive metal selected from the group consisting of yttrium, scandium, thorium and the other rare earth elements, and 3-12 percent of a noble metal selected from the group consisting of platinum or rhodium, the balance being selected from the group consisting of nickel, cobalt and nickel-cobalt. As will be appreciated, the inclusion of the noble metal as an alloying ingredient results in a substantially uniform dispersion thereof throughout the composition and thus retains the homogeneity which is characteristic of MCrAlY type overlay coatings.

In a preferred embodiment, the reactive metal is yttrium and the noble metal is 5-10 percent platinum.

In another embodiment, the reactive metal is yttrium and the noble metal is 5 percent rhodium.

An understanding of the invention will become more apparent to those skilled in the art by reference to the following detailed description when viewed in light of the accompanying drawings, wherein: Figure 1 is a graph depicting the sulfidation behavior of various NiCrAl alloys at 1 , 000°C; Figures 2 and 3 are graphs depicting the oxidation behavior of various NiCrAl alloys at 1 , 100°C and 1 , 200°0 respectively, in air; Figure is a graph showing the hot corrosion behavior of various CoCrAlY and NiCrAlY alloys at 955°C Figure 5 is a graph showing the hot corrosion behavior of NiCrAlY alloys at 955°C - 0.5 mg.cm"2 Na2S0 The alloys of the present invention exhibit markedly improved hot corrosion resistance and are considered particularly useful as coatings on the contemporary superalloys. The inventive alloys are in themselves corrosion resistant and do not depend for their protective effect upon a reaction with the substrate material. In addition, these alloys are uniform throughout their Thickness and thus will exhibit their protective properties more continuously and consistently than do the aluminide coatings.

The desired results are obtained with a basic alloy containing approximately, by weight, 8-30 percent chromium, 5-15 percent aluminum, -10 percent platinum or rhodium, up to 1 percent reactive metal selected from the group consisting of yttrium, scandium, thorium and lanthanum and the other rare earth elements, balance nickel and/or cobalt. A preferred alloy composition utilizes 0.5 percent yttrium and 5-10 percent platinum.

It was surprising to find that the addition, as alloying ingredients, of specified amounts of platinum or rhodium to the MGrAlY type coatings would not only greatly enhance sulfidation resistance but also, even without the presence of the reactive metals (Y, Sc, Th, La and the other rare earths) which normally provide oxide adherence to the underlying substrate, would promote additional oxide adherence.

With respect to the processes whereby the alloy may be applied as a coating to the surface to be protected the presence of platinum or rhodium to the coating alloy, because of the low vapor pressure of platinum or rhodium, generally precludes use of the vapor deposition technique. Other techniques are, however, efficacious to obtaining the properly composed coating. It is recognized, for example, that the coatings may be deposited by using a process involving simultaneous vapor deposition of the MCrAlY and sputter deposition of platinum or rhodium. As an alternative, the coatings may be accomplished by plasma spraying techniques.

A better understanding of the invention will result when viewed in light of the following examples : Example 1 Alloys of Ni-8Cr-6Al with alloying additions of platinum and rhodium were made by the conventional arc melt-drop cast technique. Specimens of the compositions depicted in the graph of Fig. 1 had dimensions of 1 cm x ' 1 cm x 0.2 cm and were subjected to hot corrosion tests as follows. Specimens of the alloys were spray coated with an aqueous solution of dried and weighed.

After achieving a coating of 0.5 mg.cm IJ^SO^, they were oxidized for 20 hours at 1,000°C in one atmosphere in a thermal balance. The specimen weight was recorded continuously as a function of time with the weight changes converted to weight gain per unit surface area and shown in Fig. 1.

As can be seen, the addition of 2.5 weight percent Pt did not significantly improve the performance of the JP-Ni-8Cr-6Al alloy in this test. However a significant improvement in performance was obtained when 5 or 10 weight percent Pt was added. Specimens of the Ni-8Cr-6Al-5Rh alloy were approximately equivalent to that of the 10 Pt alloy.

Example 2 Specimens were formed as in Example 1 to the compositions as shown in Pigs. 2 and 3· The specimens were subjected to high temperature cyclic oxidation tests and surprisingly, those containing platinum or rhodium, were found to have improved oxide adherence of the -A-^O^ i°rme Example 3 Alloy specimens having dimensions of 1 cm x 0.8 cm x 0.1-0.2 cm and compositions of Ni-17Cr-12Al-0.5Y, Ni-17Cr-12Al-5Rh-0.5Y, Ni-17Cr-12Al-10Pt-0. Y, Co-17Cr-llAl-0.5Y, 0o-17Gr-llAl-5Rh-0.5Y and Co-170r-llAl-10Pt-0.5Y were prepared, measured and weighed, then coated with 0.5-2.0 mg/c They were then subjected to up to 14- cycles, each cycle consisting of oxidizing in air for 20 hours at 955°C» cooling to room temperature, washing and reweighing. The sequence was Q repeated to failure. The results obtained for one set of experiments at 9 5°C using 2 mg/cm of salt is illustrated in Fig. 4-. Although CoCrAlY is basically more resistant to hot corrosion than is NiCrAlY, it can be seen that additions of either Pt or Eh to either CoCrAlY, or NiCrAlY dramatically improve their hot corrosion resistance Example 4- Erosions bars of Ni-17Cr-12Al-0.5Y, Ni-17Cr-12Al-5Sh-0.5Y, Ni-17Cr-12Al-5Pt-0.5Y and Ni-17Cr-12Al-10Pt-0. Y were evaluated in a cyclic hot corrosion burner rig at 955°C usin 35 ppm of sea salt ingested in the fuel prior to combustion. Severe attack of the tip of both the NiCrAlY base composition and the rhodium modified composition occurred after 110 hours. Hot zone faiilures were observed between 300 and 400 hours for both tMese bars, the rhodium modified specimen surviving for a slightly longer time than the base composition. Although the rfi-odium modified composition showed little improvement ove " the base alloy in this test, the nature of its failure was musual and rendered these results somewhat dubious and inconclusive. In contrast, the platinum modified compositions were found to be dramatically more resistant to; Ihot corrosion than the base composition. For these compositions no sign of failure was observed up to 675 hours „ when testing was terminated.

What has been set forth above is intended primarily as exemplary to enable those skilled in the art in the practice of the invention and it shomld therefore be understood that, within the scope of the appended claims, the invention may be practiced in other ways than as specifically described.

Claims

WHAT WE CLAIM IS :

1. Coating composition of the MCrAlY type wherein the coating composition consists essentially of, by weight, approximately 8-30 percent chromium, 5-15 percent aluminum, up to 1 percent reactive metal selected from the group consisting of yttrium, scandium, thorium and the other rare earth elements, balance selected from the group consisting of nickel, cobalt and nickel-cobalt, characterized in the improvement for increasing hot corrosion resistance which comprises 3-12 percent of a noble metal selected from the group consisting of platinum and rhodium as an alloying ingredient.

2. Coating composition according to claim 1 characterized in that said reactive metal is yttrium.

3. Coating composition according to claim 2, characterized in that said noble metal is 5-10 percent platinum.

4. Coating composition according to claim 2 wherein said noble metal is 5 percent rhodiia.

5. Coating composition according to anyone of the claims 1 to 4- characterized in that it is applied on an article of a nickel base or cobalt base alloy and that said platinum or rhodium is substantially uniformly dispersed throughout said coating.

6. A method of preparing the coating composition according to claim 1-5 for improving the hot corrosion resistance of a coating of the MCrAlY type wherein the coating composition consists essentially of, by weight, approximately 8-30 percent chromium, 5-15 percent aluminum, up to 1 percent reative metal selected from the group consisting of yttrium, scandium, thorium, and the other rare earth ^ elements, balance nickel and/or cobalt characterized in comprising incorporating, as an alloying ingredient to said MCrAlX coating, 5-12 percent of a noble metal selected from the group consisting of platinum or rhodium.

7. Method according to claim 8 characterized in that said noble metal is 5-10 percent platinum.

8. Coating composition as hereinbefore described with reference to the accompanying figures 1 to 5·

9. Method of preparing the coating composition as claimed in any of the claims 1 to 5 and 7·