Aluminide/MCrAlY coating system

Abstract: High temperature oxidation resistance of an aluminide diffusion overcoated MCrAlY coating system is substantially improved by CVD over-aluminizing the MCrAlY type overlay coating under CVD conditions that result in reduced concentrations of such tramp impurities as S and P in the aluminized MCrAlY overlay coating region of the coating system. The CVD aluminizing conditions yield an outwardly grown aluminide over-coat on the underlying MCrAlY type coating.

Description: The present invention relates to an aluminide overcoated MCrAlY coating system on a substrate and to a method of making such a coating system; in particular, the present invention relates to such coating systems for superalloy substrates. U.S. Patent 4 080 486 describes a protective coating system for nickel base and cobalt base superalloy substrates, such as turbine blades and vanes, exposed to high temperature in a gas turbine engine. The patented coating system comprises an MCrAlY type overlay coating, where M is an element selected from the group consisting of iron, nickel and cobalt, that is aluminized by pack cementation to increase the corrosion and oxidation resistance of the coated substrate. It is an object of the present invention to provide a gas turbine engine component with an overcoated MCrAlY coating system having substantially improved high temperature oxidation resistance, as well as to propose a method of providing a substrate with such a coating system. In accordance with the present invention, this object is achieved by the turbine engine component defined by claim 1 and by the method defined by claim 13, respectively. The present invention substantially increases the high temperature oxidation resistance of an aluminide diffusion overcoated MCrAlY coating system by chemical vapor deposition (CVD) over-aluminizing the MCrAlY type coating under CVD conditions that produce an outwardly grown aluminide over-coat on the MCrAlY coating. WO 96/34130 discloses a coated gas turbine engine component having a substrate, a first MCrAlY type coating, a diffusion aluminide layer and an outer ceramic layer as a thermal barrier coating. According to the teaching of this document, the sole purpose of the aluminide layer is to act as a bonding layer for bonding the ceramic layer to the MCrAlY type first coating and the substrate. Further, this document teaches that in this known coating system the aluminide layer is in fact unnecessary, not even desired and in fact disadvantageous, but rather a hardly avoidable byproduct of the process of placing an aluminide layer on an inner wall of the component (see page 10, lines 26 - 30 in combination with page 11, lines 19 - 24). Further, this document only discloses that the aluminide layer can be formed on the MCrAlY type coating by gas phase aluminizing, which may comprise any of numerous gas phase processes which may produce different aluminide coatings, and there is no teaching with respect to using any particular aluminizing process and/or with respect to achieving substantially increased oxidation resistance of a coating system that includes no ceramic thermal barrier layer. Preferred embodiments of the inventive engine component and method, respectively, defined in one or several of claims 2, 3 and 14 to 16 show a still further improved high temperature oxidation resistance. In accordance with this aspect of the present invention, the diffusion aluminide overcoating formed on the MCrAlY coating exhibits reduced concentrations of such tramp impurities as S and P and others. The CVD aluminizing conditions involve a substrate coating temperature of at least about 1000 degrees C and a high purity coating gas comprising a mixture of hydrogen and aluminum trichloride gases with such conditions being effective to reduce the concentrations of such tramp impurities as S and P in the aluminized MCrAlY region of the coating system. The aluminide diffusion overcoating preferably has a concentration of sulfur and phosphorous that is about 50 % less than the sulfur and phosphorous concentrations of the underlying MCrAlY coating. WO 96/13622 (and its equivalent US-A-5 658 614) discloses a method of improving the oxidation resistance of a platinum modified aluminide coating formed on a nickel base superalloy substrate. This known method comprises providing a platinum layer on the substrate, heating the substrate to a temperature of at least about 1000°C, forming a high purity coating gas comprising hydrogen and aluminum trichloride, and contacting the heated substrate with the coating gas to form an outwardly grown, single phase platinum modified aluminide coating having reduced concentration of at least one of a substrate substitutional alloying element and a surface active tramp element selected from at least one of B, P, and S in said coating as compared to a platinum modified aluminide coating formed at a lower temperature. Therefore, WO 96/13622 teaches to directly coat the substrate provided with the platinum layer and does not disclose or suggest an aluminide overcoating on a MCrAlY type coating. One embodiment of the present invention envisions CVD aluminizing an MCrAlY coated substrate without a platinum layer on the MCrAlY overlay coating. Another embodiment of the present invention envisions CVD aluminzing a platinum coated MCrAlY coated substrate without prediffusion of the platinum to form a platinum modified aluminide diffusion overcoating on the MCrAlY coating. Still another embodiment of the present invention can be employed to form a CVD aluminide diffusion overcoated MCrAlY coating system on an exterior of a substrate, such as a superalloy turbine blade or vane. A further embodiment of the present invention can be employed to form a CVD aluminide diffusion coating on an interior of the substrate, in particular to concurrently form such coating on interior cooling passages of the substrate. Further preferred embodiments of the present invention are defined in claims 4 to 12 and 17 to 20. The objects and advantages of the present invention will become more readily apparent when taken with the following detailed description and drawings which show the following: Figure 1 is a schematic illustration of a coating system of the present invention, and Figure 2 is a graph depicting comparative cyclic oxidation resistance at 2012 degrees F (1100°C) of MDC-210 and MDC-150L coating systems in accordance with the present invention compared with other coating systems designated MDC-15 and MDC-51 outside the invention. DETAILED DESCRIPTION OF THE INVENTION An embodiment of the present invention relates to CVD over-aluminizing an MCrAlY type overlay coating under CVD conditions that produce an outwardly grown aluminide over-coat on the MCrAlY coating with the diffusion aluminide overcoating having reduced concentrations of such tramp impurities as S and P that adversely affect oxidation resistance. Other such tramp impurities may include boron and refractory elements such as W, Mo, and Ti. The CVD conditions are controlled to substantially reduce concentrations of such tramp impurities as S and P in the aluminized MCrAlY overlay coating region of the coating system to 20 ppm by weight or less, for example only. An exemplary coating system in accordance with an embodiment of the invention is illustrated schematically in Figure 1. The coating system comprises a first coating 10 referred to as an MCrAlY coating and an aluminide diffusion overcoating 12 formed in-situ on the first coating 10 and having an outwardly grown additive layer 12a and diffusion zone 12b proximate the MCrAlY coating 10. The first coating 10 is referred to as an MCrAlY coating for purposes of illustration and not limitation. Generally, the MCrAlY coating 10 consists essentially of chromium, aluminum, a reactive element selected from the group consisting of yttrium (Y), rare earth elements such as Ce and La and other reactive elements such as Si, Hf, Zr, and element M where M is selected from nickel and/or cobalt and/or iron. The MCrAlY coating 10 typically consists essentially of, in weight %, 14% to 35% Cr, 4% to 30% Al, 0.1% to 3% of Y, rare earth element such as Ce and/or La, and/or other reactive element(s) such as Hf, Zr, Si, and the balance essentially iron and/or nickel and/or cobalt. Such MCrAlY coating alloys are well known and described in U.S. Patent 4 080 486. Although the invention is described below for purposes of illustration, and not limitation, as using a CoNiCrAlY coating 10, the invention can be practiced using any other CoCrAlY, NiCrAlY, CoNiCrAlY, and FeCrAlY coating alloys. Typically, the MCrAlY first coating is applied to a thickness in the range of 0,051 mm (0.002 inch) to 0,508 mm (0.020 inch) as an overlay coating onto a nickel or cobalt based superalloy substrate S, such as gas turbine engine blade or vane. The MCrAlY coating preferably is applied to the substrate by known low pressure plasma spraying or high velocity oxy-fuel spraying techniques. In low pressure plasma spray, powder particles of the coating alloy are heated and propelled towards a substrate inside a vacuum chamber which maintains the spray environment at some low pressure below 1 atmosphere, typically below 50 torr. Powder particle heat and velocity are achieved using a plasma torch designed or modified for operation under reduced ambient pressure. The high velocity oxygen fuel coating method transfers thermal and kinetic energy to powder particles of the coating alloy using a combustion torch, rather than a plasma. The method typically is performed in a spray environment at local atmospheric pressure, and the torch may be manipulated manually or using automated systems. The component being coated is typically fixtured and attached to a table or drive system. However, other well known techniques, such as air plasma spray, shrouded arc plasma spray, and entrapment plating, or physical vapor deposition pursuant to U.S. Patent 4 080 486 can be used to deposit the MCrAlY coating on the substrate. The aluminide diffusion overcoating 12 is formed in-situ on the first coating 10 by chemcial vapor deposition (CVD) using a low acitvity aluminum coating gas and substrate coating temperature of at least about 1000°C (1832 degrees F) in accordance with U.S. Patent 5 658 614. The aluminide diffusion overcoating 12 includes an outwardly grown, outer single phase additive layer 12a and inner diffusion zone 12b proximate the MCrAlY coating 10, leaving some of the MCrAlY coating intact on the substrate S. The outwardly grown additive layer 12a comprises MA1 or (M,Pt)Al single phase, where M is selected from the Co, Ni and/or Fe from the underlying MCrAlY coating and where Pt is present when the MCrAlY coating is Pt plated prior to aluminizing as described below. The aluminide diffusion overcoating 12 typically has a total thickness of 0,0127mm (0.5 mils) to 0,1016mm (4.0 mils) including both the outwardly grown additive layer 12a and diffusion zone 12b. In forming the aluminide diffusion overcoating 12, a high purity, low aluminum activity coating gas is used comprising a mixture of hydrogen and aluminum trichloride gases effective under the substrate coating temperature employed to reduce the concentrations of tramp impurites such as S and P and others in the aluminized MCrAlY region of the coating system, particularly the outwardly grown, outer additive layer. The low activity coating gas is generated by passing high purity hydrogen chloride and hydrogen carrier gases over a high purity source comprising aluminum at a relatively low temperature, such as an aluminum bed at a temperature not exceeding 316°C (600 degrees F). Preferably, the high purity aluminum source (at least 99.999 weight % Al) comprises aluminum granny P pellets employed in the external coating gas generator. High purity hydrogen typically comprises less than 30 ppb (parts per billion by volume) impurities and high purity hydrogen chloride typically comprises less than 25 ppm (parts per million by volume) impurities. The purification effects of the aforementioned CVD aluminizing conditions on the aluminized region of the MCrAlY coating (i.e. on the alumiide overcoating 12) were demonstrated in a series of coating experiments using coating specimens having dimensions of 12 mm by 25 mm by 2 mm thickness cut from a monolithic deposit of CoNiCrAlY alloy applied by high velocity oxy-fuel spraying onto a nickel based superalloy substrate using Hobat-Taffa Model JP-5000 HVOF equipment. The deposition parameters were 19 Ltr (5 gallons)per hour kerosene and 45,3 m 3 /h under standard conditions (1600 scfh/standard cubic feet per hour) oxygen at an alloy powder flow rate (particle size smaller than 64 µm mesh size (-270 mesh)) of 7,3 kg (16 pounds) per hour in ambient atmosphere. The deposit of CoNiCrAlY alloy had a composition, in weight %, of 29.5% Ni, 23.6% Cr, 11.7% Al, 0.7% Y, and balance Co. The CoNiCrAlY tab specimens were CVD aluminized and tested without being applied to a substrate since substrate effects on the aluminide diffusion layer 12 were deemed minimal. The test results from these CoNiCrAlY tab specimens are representative of a variety of MCrAlY type coating alloys in commerical use. The CoNiCrAlY tab specimens were divided into five groups of specimens (5 specimens per group) with one group being reserved as baseline specimens for pre-aluminizing composition analysis. Two groups of tab specimens were subjected to high activity pack cementation aluminizing, one of the groups being aluminized without an activator (designated hereafter as MDC-15 aluminized specimens) and the other group being aluminized with a halide salt activator (designated herafter as MDC-51 specimens). The two groups of MCrAlY tab specimens were aluminized by pack cementation (MDC-15 and MDC-51 tab specimens) to produce inwardly grown aluminide coatings. The unactivated MDC-15 pack comprised 33% weight % Al alloy powder and the balance alumina. The tab specimens were placed in the powder pack and heated at 982°C (1800 degrees F) for 3 hours in a hydrogen atmosphere for aluminizing. The MDC-51 pack involved an ammonium chloride (NH 4 Cl) activated powder pack comprising 0.03% weight % ammonium chloride, 67 weight % Al alloy powder, and the balance aluminum oxide. The aluminizing cycle of the tab specimens in the powder pack involved 19 hours at 1038°C (1900 degrees F) in an argon atmosphere. The MDC-51 pack cementation aluminized CoNiCrAlY tab specimens were representative of the MCrAlY coating systen described in U.S. Patnet 4 080 486. Two other groups of the CoNiCrAlY tab specimens were CVD aluminized using a low activity aluminum trichloride process described above and in the aforementioned US-A-5 658 614, to produce the aluminide diffusion overcoating 12. In particular, one group of tab specimens designated MDC-210 were CVD aluninized at a substrate temperature of 1080 degrees C using a coating gas mixture comprising 9 volume % aluminum trichloride and 91 volume % hydrogen at a flow rate of 8,50 m 3 /h under standard conditions (300 scfh) and total pressure of 98 kg/cm 2 (500 Torr). The coating mixture was generated by passing high purity hydrogen (e.g. less than 30 parts per billion impurities) and high purity hydrogen chloride (e.g. less than 25 parts per million impurities) in mixture of hydrogen/13 volume % HCl over a 99.999% pure source of aluminum at 290 degrees C in a generator external of the coating retort. Hydrogen chloride which produces a purification of the MCrAlY overlay coating (i.e. reductions in concentration of the tramp element P in this particular CVD coating) was produced by hydrogen reduction of aluminium trichloride on the sample surface. The surface active tramp impurity S was removed from the MCrAlY coating by reaction with the hydrogen carrier gas forming hydrogen sulfide gas. Another group of tab specimens was first electroplated using a used potassium hydroxide based aqueous electroplating solution having KOH in the range of 30-90 grams KOH per liter and 10 grams of Pt per liter at a current density of 0.015 Ampere/cm 2 to deposit 9-11 milligrams Pt/cm 2 on the tab specimens. This electroplating solution is described in detail in US-A-5 788 823, and results in reduced concentration of S and P in the electroplated Pt layer as well as introduction of K (or other alkali or alklaine earth element from the hydroxide in solution) into the Pt layer as described in aforementioned US-A-5 788 823. The Pt electroplated group of tab specimens designated MDC-150L were CVD aluninized, without prediffusion of the Pt layer into the MCrAlY coating, at a substrate temperature of 1080 degrees C using a coating gas mixture comprising 9 volume % aluminum trichloride and 91 volume % hydrogen at a flow rate of 8,50 m 3 /h under standard conditions (300 scfh) and total pressure of 98 kg/cm 2 (500 Torr). The coating mixture was generated by passing high purity hydrogen (e.g. less than 30 parts per billion impurities) and high purity hydrogen chloride (e.g. less than 25 parts per million impurities) in mixture of hydrogen/13 volume % HCl over a 99.999% pure source of aluminum at 290 degrees C. The as-deposited baseline tab specimens and alumnized tab specimens were analyzed for major elements using electron microprobe, for trace phosphorous impurities by glow discharge mass spectroscopy (GDMS) through the overcoating to MCrAlY coating (average of measured P levels), and for trace sulfur impurities using a LECO CS444LS analyzer. Sulfur analysis is a bulk measurement including the aluminide coating and MCrAlY coating. The electron microprobe analysis of the as-deposited CoNiCrAlY tab specimens yielded the alloy composition set forth above; namely, a CoNiCrAlY composition, in weight %, of 29.5% Ni, 23.6% Cr, 11.7% Al, 0.7% Y, and balance Co. The results of the GDMS and LECO analyses of the tab specimens are set forth in the Table I below where CoNiCrAlY HVOF represents the as-deposited tab specimens without aluminizing. CHEMICAL ANALYSIS OF CoNiCrAlY TABS GLOW DISCHARGE MASS SPECTROSCOPY ELEMENT CoNiCrAlY HVOF Halide Salt Activated HIGH ACTIVITY PACK (MDC-51) LOW ACTIVITY CVD (MDC-210/MDC-150L) P 10 ppmw 20 ppmw 5 ppmw LECO LOW SULFUR ELEMENT CoNiCrAlY HVOF Unactivated HIGH ACTIVITY PACK (MDC-15) LOW ACTIVITY CVD (MDC-210/MDC-150L) S 4 ppmw 5 ppmw 2 ppmw The data of the Table I illustrate the purification effects of the CVD low activity aluminizing of the MDC-150L and MDC-210 CoNiCrAlY tab specimens in that S and P concentrations are reduced by at least about 50% in these specimens as compared to the S and P present in the as-deposited CoNiCrAlY HVOF tab specimens without aluminizing. In contrast, the S concentration of the inwardly grown aluminide diffusion coatings of the high activity pack cemenatation aluminized MDC-15 tab specimens was increased, while the P concentration of the high activity pack cementation aluminized MDC-51 tab specimens was increased as compared to the as-deposited CoNiCrAlY HVOF tab specimens without aluminizing. As mentioned, the MDC-51 pack cementation aluminized CoNiCrAlY tab specimens were representative of the aluminized MCrAlY coating system described in U.S. Patent 4 080 486. Cyclic oxidation testing of tab specimens MDC-15, MDC-51, MDC-150L, and MDC-210 was conducted using a one hour cycle that consisted of 50 minutes at a temperature of 1100°C (2012 degrees F) and 10 minutes rapid air cooling. Four specimens were used for each of these type of coating specimens and the results averaged. The aluminide diffusion coating thickness was 72,4 µm (2.85 mils) for the MDC-15 specimens, 68,6 µm (2.7 mils) for the MDC-51 specimens, 38,1 µm (1.5 mils) for the MDC-150L specimens, and 27,9 µm (1.1 mils) for the MDC-210 specimens. The cyclic oxidation specimens were weighed prior to testing and after each fifty cycles of testing until a zero cross-over (failure) occurred (failure occurred only for MDC-15, MDC-51 and MDC-210 specimens). Table II below sets forth the oxidation test results with the second column being normalized to account for the different aluminide diffusion coating thicknesses involved. Weight change (ΔM/A in milligrams/centimeter squared) data is plotted in Figure 2. 1373K CYCLIC OXIDATION NORMALIZED AND RELATIVE OXIDATION LIFE CYCLES TO FAILURE NORMALIZED LIFE cycles 25,4 µm (mil) RELATIVE LIFE MDC-15 162 57 1 MDC-51 237 88 1.54 MDC-210 1425 1295 22.7 MDC-150L >1800 >1200 >21 As shown in Table II and illustrated in Figure 2, the MDC-150L (Pt electroplated) specimens and MDC-210 (no Pt electroplate) specimens CVD low activity aluminized pursuant to the invention exhibited significantly greater oxidation resistance than the inwardly grown specimens MDC-15 and MDC-51 aluminized by high activity pack cementation. Note that the weight change data for the MDC-150L and MDC-210 specimens indicates no coating failure at the times the MDC-15 and MDC-51 specimens reached zero cross-over (failure). The MDC-210 CVD over-coated specimens reached failure after 1425 oxidation cycles, which indicates a life improvement of greater than 22 times (see Table II). Based upon the available data, the MDC-150L CVD over-coated specimens will exhibit the best oxidation resistance of any coating system tested. In particular, the MDC-150L specimens still had not failed and were undergoing further on-going test cycles at the time the MDC-210 speicmens exhibited zero cross-over (failure). Although the MDC-150L and MDC-210 specimens exhibited similar outwardly grown aluminide diffusion overcoated structures with the similar reductions in S and P concentrations and similar aluminum concentrations in the coatings, the MDC-150L specimens exhibited better oxidation resistance than the MDC-210 specimens as a result of the presence of Pt and K in the aluminide diffusion overcoating of MDC-150L specimens.

Claims: Coated gas turbine engine component, comprising a first coating on said component and consisting essentially of chromium, aluminum, an element selected from the group consisting of yttrium, rare earth element and a reactive element selected from the group consisting of Hf, Zr, and Si, and an element selected from the group consisting of nickel, cobalt and iron, and a chemical vapor deposition outwardly grown aluminide diffusion overcoating on said first coating. The component of claim 1 wherein said aluminide diffusion overcoating is formed under chemical vapor deposition conditions to reduce concentration of a tramp impurity effective to improve oxidation resistance of the coating system. The component of claim 2 wherein said aluminide diffusion overcoating has a reduced concentration of at least one of S and P as compared to said first coating. The component of claim 3 wherein said aluminide diffusion overcoating has a concentration of sulfur therein that is at least 50% less than the sulfur concentration of the first coating. The component of claim 3 wherein said aluminide diffusion overcoating has a concentration of phosphorous therein that is at least 50% less than the phosphorous concentration of the first coating. The component of claim 3 wherein said aluminide diffusion overcoating includes a sulfur concentration of 20 ppm by weight or less. The component of claim 2 wherein said aluminide diffusion overcoating includes a phosphorus concentration of 20 ppm by weight or less. The component of claim 1 wherein said aluminide diffusion overcoating includes platinum therein. The component of claim 1 wherein said aluminide diffusion overcoating has a thickness of about 0,0127 mm (0.0005 inch) to about 0,1016 mm (0.004 inch). The component of claim 1 which includes said first coating and said aluminide diffusion overcoating on an exterior surface thereof. The component of claim 10 which includes an aluminide diffusion coating on an interior surface thereof. The component of claim 1 wherein said aluminide diffusion overcoating includes an alkali element or alkaline earth element therein. A method of coating a substrate comprising, providing a first coating on said substrate, said first coating consisting essentially of chromium, aluminum, an element selected from the group consisting of yttrium, rare earth element and a reactive element selected from the group consisting of Hf, Zr, and Si, and an element selected from the group consisting of nickel, cobalt and iron, and aluminizing the first coating under chemical vapor deposition conditions and a substrate coating temperature of at least about 1000°C to form an outwardly grown aluminide diffusion overcoating on said first coating. The method of claim 13 wherein said chemical vapor deposition conditions include use of a coating gas effective under said substrate coating temperature to reduce concentration of a tramp impurity in the overcoating effective to improve oxidation resistance. The method of claim 14 including reducing the concentration of at least one of S and P. The method of claim 13 wherein said chemical vapor deposition uses high purity coating gas formed by passing high purity hydrogen and hydrogen chloride gases over a high purity source of aluminum. The method of claim 13 wherein the first coating is coated with platinum prior to aluminizing without a prediffusion of platinum layer into the first coating. The method of claim 17 wherein the platinum layer is plated onto the substrate from a hydroxide aqueous plating solution. The method of claim 13 wherein an exterior surface of the substrate is coated with said first coating that is aluminized. The method of claim 19 wherein an interior surface of the substrate is concurrently aluminized under said conditions.

Inventors: DUSHANE NICK S, HONICK RONALD J JR, SHRIVER WILLIAM J, WARNES BURCE M, DUSHANE, NICK S., HONICK, RONALD J., JR., SHRIVER, WILLIAM J., WARNES, BURCE M.
Applicants: HOWMET RES CORP A DELAWARE COR, HOWMET RESEARCH CORPORATION (A DELAWARE CORPORATION)
Application year: 1998
Main classification: C23C16
IPC codes: C23C28, C23C10, F01D5, C23C16