CA1237609A - Process for applying thermal barrier coatings to metals and resulting product - Google Patents

Process for applying thermal barrier coatings to metals and resulting product

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Publication number
CA1237609A
CA1237609A CA000436457A CA436457A CA1237609A CA 1237609 A CA1237609 A CA 1237609A CA 000436457 A CA000436457 A CA 000436457A CA 436457 A CA436457 A CA 436457A CA 1237609 A CA1237609 A CA 1237609A
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CA
Canada
Prior art keywords
metal
substrate
coating
zirconium
hafnium
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Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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CA000436457A
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French (fr)
Inventor
Ibrahim M. Allam
David J. Rowcliffe
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SRI International Inc
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SRI International Inc
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    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C26/00Coating not provided for in groups C23C2/00 - C23C24/00
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C8/00Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
    • C23C8/06Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases
    • C23C8/08Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases only one element being applied
    • C23C8/10Oxidising

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  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Manufacture And Refinement Of Metals (AREA)
  • Laminated Bodies (AREA)
  • Coating With Molten Metal (AREA)

Abstract

ABSTRACT OF DISCLOSURE

Process for applying a protective coating to a metal substrate which provides a thermal barrier and a barrier against oxidation of the substrate. The coating material is a mixture of (1) zirconium and/or hafnium and (2) a metal such as nickel which does not form a stable oxide at a high temperature in an atmosphere having a very low concentration of oxygen. The coating is subjected to such conditions to produce an outer oxide layer of metal zirconium and/or hafnium and an inner metal layer of the second metal alloyed with one or more components of the substrate. The oxide layer provides thermal and oxidation protection and the inner layer bonds the coating to the substrate.

Description

76~

"PROCESS FOR APPLYING THERMAL BARRIER
COATINGS TO METALS AND RESULTING PRODUCT"

This invention relates to the coaling of metals, particularly certain alloys, with a protective coating that acts as a thermal or oxidative barrier.

Certain alloys known as "superalloy" are used as gas turbine components where high temperature oxidation resistance and high mechanical strengths are required. In order to extend the useful temperature range, the alloys must be provided with a coating which acts as a thermal barrier to insulate and protect the underlying alloy or substrate from high temperatures and oxidizing conditions to which they are exposed.

Zirconium oxide is employed for this purpose because it has a thermal expansion coefficient approximating that of the superalloy and because it functions as an efficient thermal barrier.

~3~6~ -
- 2 -Zirconium oxide has heretofore been applied to alloy substrates by plasma spraying. The ~irconi~ oxide forms an outer layer or thermal barrier and the zirconium oxide is partially stabilized with a second oxide such as ; calcium, magnesium or yttrium oxide. The plasma spray technique often produces nonuniform coatings and it is not applicable or is difficultly applicable, to reentrant surfaces. The plasma sprayed coatings often have micro cracks and pinholes and the adherence between the coating and substrate can be poor. All of these effects can lead to catastrophic fuller.

Thermal barrier coatings can also be applied using sputtering or electron beam vaporization. These methods of application are expensive and limited to line of sight application. Variations in coating compositions often occur during electron beam vaporization because of differences in vapor pressures of the coating constituent elements.
Sputtering produces fibrous and segmented structures which can be penetrated by the corrosive species.

In cop ending Canadian patent application Serial No. 416,214 filed November 24, 1982 entitled "PROCESS FOR
APPLYING THERMAL BARRIER COATINGS TO METALS AND THE
RESULTING PRODUCT" there is described a method of applying thermal barrier coatings to substrate metals such as superalloy in which the free metal whose oxide is to become the thermal barrier is applied to the substrate metal as a physical mixture or as an alloy with another I

. '1 ;,~ .

~37~

metal such as nickel or cobalt and the coating of metal is subjected to selective oxidation by exposure at a high temperature to an atmosphere having a very low partial pressure of oxygen. Under these conditions the metal whose oxide is to provide the thermal barrier, called Ml, forms a stable oxide but the other metal, called My, does not form a stable oxide. As a result a layer or coating of oxide of M and the free metal My is formed. The oxide of Ml provides the thermal barrier and the free metal My serves to bond the oxide to the substrate metal.

This process, often called dip coating because it is advantageously carried out by dipping the articles to be coated into a molten alloy of Ml and My, it easier to carry out than coatings with a metal oxide by the plasma r,lethod and the resulting coat is more adherent and is a better thermal barrier.

In accordance with the present invention, an alloy or a physical mixture of (l) the metal My and (2) zirconium, hafnium or a mixture or alloy of the two metals is provided.
In the case where the second metal is zirconium, additions of me is such as yttrium, calcium or magnesium can be made in quantities that are sufficient to stabilize zirconium oxide in the cubic form. The metal My is selected in accordance with the criteria described below. This alloy or metal mixture is then melted to provide a uniform melt which is then applied to a metal substrate by dipping the substrate in the melt. Alternatively, the metal mixture or alloy is reduced to a finely divided ~3~6~

state, and the finely divided metal is incorporated in a volatile solvent to form a slurry which is applied to the metal substrate by spraying or brushing. The resulting coating is heated to accomplish evaporation of the volatile solvent and the fusing of the alloy or Natalie mixture onto the surface of the substrate. (Where physical mixtures of metals are used, they are converted to an alloy by melting or they are alloyed in situ in the slurry method of application.) Zirconium and hafnium form thermally stable oxides when exposed to an atmosphere containing a small concentration of oxygen such as that produced by a mixture of carbon dioxide and carbon monoxide at a temperature of about ~00C. The metal My, under such conditions, does not form a stable oxide and remains entirely or substantially entirely in the form of the unoxidized metal. Further, My is compatible with the substrate metal. It will be understood that My may be a mixture or an alloy of two or more metals meeting the requirements of My.

Zirconium and hafnium have one or more of the following advantages over curium and other lanthanide metals:
The coatings are considerably more adherent to the substrate.
When curium is used, unoxidized metal from the substrate tends to become incorporated in the oxide layer. This metal ~37~

may then be oxidized when the coated article is exposed to an oxidizing atmosphere. This leads to spallation and ultimate fracture of the coating. When zirconium is used rather than curium, this difficulty is not encountered or is encountered in much lesser degree.

When a coating of suitable thickness has been applied to the substrate alloy by the dip coating process or by the slurry process described above (and in the latter case after the solvent has been evaporated and the zirconium and/or hafnium-~12 alloy or mixture is fused onto the surface of the substrate) the surface is then exposed to a selectively oxidizing atmosphere such as a mixture of carbon dioxide and carbon monoxide (hereinafter referred to as COOK).
typical COOK mixture contains 99 percent of COY and 1 percent of CO. When such a mixture is heated to a high temperature, an equilibrium mixture results in accordance with the following equation:

CO 1/2 2 = C2 The concentration of oxygen in this equilibrium mixture is very small, e.g., at 827C the equilibrium oxygen partial pressure is approximately 2 x lo I atmosphere, but is I sufficient at such temperature to bring about selective oxidation of zirconium and/or hafnium. Other oxidizing ~23~7~

atmospheres may be used, e.g., mixtures of oxygen and inert gases such as argon or mixtures of hydrogen and water vapor which provide oxygen partial pressures lower than the dissociation pressures of the oxides of the elements in My, and higher than the dissociation pressure of zirconium oxide and hafnium oxide. A mixture of hydrogen, water vapor and an inert gas such as argon is indeed preferred because it will not produce an unwanted carbide. Such carbides may result at elevated temperatures, e.g. at 627C, by reason of the 80udouard reaction:

2 C0 = C + C02 The metal My is, depending upon the type of service and the nature of the substrate alloy, preferably selected from Table I.

Table I (My) Nickel No Cobalt Co Iron Fe It will be understood that two or more metals chosen from Table I may be employed to form the My component of the coating alloy or mixture. In such alloys or mixtures minor ~;~3~6~

amounts of aluminum, yttrium and/or chromium may be present.
In general any metal My may be used which does not form a stable oxide at a high temperature in the presence of a very small concentration of oxygen, which serves to bond the 5 zirconium and/or hafnium oxide to the substrate and which is suitable for the intended type of service. These also include platinum, palladium ruthenium or rhodium.

Proportions of zirconium, hafnium (or mixtures or alloys of both) and My may vary from about 50 to 90% by weight of zirconium and/or hafnium to from about 50 to lot by weight of My, preferably about 70 to 90% of zirconium and/or hafnium and about 30 to 10% of My. The alloy resulting from a mixture of zirconium and/or hafnium with My (plus any minor alloying additions) must have a melting point that is sufficiently low that the properties of the substrate alloy are not degraded by being exposed to the dipping temperature. The proportion of zirconium and/or hafnium should be sufficient to form an outer oxide layer sufficient to provide a thermal barrier and to inhibit oxidation of the substrate and the proportion of My should be sufficient to bond the coating to the substrate.

Table II provides examples of substrate alloys to which the protective coatings are applied in accordance with the present invention. It will be noted that the invention may be applied to superalloy in general and specifically to cobalt and nickel based superalloy.

~37~

Table II

Nickel Base Superalloy IN 738 Cobalt Base Superalloy MIRIAM
~iCrAlY Type Bond Coating Alloy CoCrAlY Type sound Coating Alloy The invention may also be applied to any metal substrate which benefits from a coating which is adherent and which lo provides a thermal barrier and/or protection from oxidation by the ambient atmosphere. The metal or metals of the substrate should, of course, be nobler than zirconium or hafnium such that they do not form stable oxides under the conditions of selective oxidation.

The dip coating method is preferred. In this method a molten zirconium and/or hafnium-M2 alloy is provided and the substrate alloy is dipped into a body of the coating alloy. The temperature of the alloy and the time during which the substrate is held in the molten alloy will control the thickness of the coating. The thickness of the applied coating can range between lo micrometers to Lowe micrometers. Preferably, a coating of about 300 micrometers to 400 micrometers is applied. It will be understood that the thickness of the coating will be provided in accordance with the requirements of a particular end use.

I

The slurry fusion method has the advantage that it dilutes the coating alloy or metal mixture and therefore makes it possible to effect better control over the thickness of coating applied to the substrate. Typically, the slurry coating technique may be applied as follows: on alloy or a mixture of zirconium and/or hafnium with My is mixed with a mineral spirit and an organic cement such as Nicrobraz 500, (Well Coleman Corp.) and MOE (Baker Coaster Oil Co.).
Typical proportions used in -the slurry are coating metal 45 weight percent, mineral spirit lo weight percent, and organic cement 45 weight percent. This mixture is then ground, for example, in a ceramic ball mill using aluminum oxide balls.
After separation of the resulting slurry from the alumina balls, it is applied (keeping it stirred to insure uniform dispersion of the particles of alloy in the liquid medium) to the substrate surface and the solvent is evaporated, for example, in air a-t ambient temperature or at a somewhat elevated temperature. The residue of metal and cement is then fused onto the surface by heating it to a suitable temperature, for example, 1000C in an inert atmosphere such as argon that has been passed over hot calcium chips to getter oxygen. The cement will be decomposed and the products of decomposition are volatilized.

I The following specific example will serve further to illustrate the practice and advantages of the invention.

~L~376~

Example 1 The Crating alloy composition was 70%Zr-25~Ni-5%Y
by weight. Yttrium was added to the Zr-Ni crating alloy to Jo provide a Dupont to stabilize 3r2 in the cubic structure during the selective oxidation stage, and also because there is some evidence that yttrium improves the adherence of plasma-sprayed Zro2 coatings. The weight ratio of or to No in this alloy was 2.7, which is similar to that of the NiZr2-NiZr eutectic composition. The YO-YO did not significantly alter the melting temperature of the Zr-Ni eutectic. The substrates were dipped into the molten coating alloy at 1027C.

Two substrate alloys were coated, namely MIRIAM

and Co- cry. The results obtained indicate that the ZrO2-based coatings applied by this technique are highly adherent, uniform and have very low porosity. Virtually no diffusion zone was observed between the coating and the substrate alloy. The coating layer was established totally above the substrate surface, and its composition was not significantly altered by the substrate constituents.

I 76(~

EDAX-concentration profiles were determined of different elements within the Russia layer after hot dipping the substrate alloy (Caulker) in the coating alloy, followed by an annealing treatment. The coating layer was about 150-160 sum thick with a relatively thin (= 20 us) diffusion zone at the interface with the under-lying substrate. Or was virtually nonexistent within the coating layer and a small amount of Co diffused from the substrate right through the coating to the external surface.

Selective oxidation was conducted at 1027C in a gas mixture of hydrogen/water vapor/argon at appropriate proportions to provide an oxygen partial pressure of about lo 17 elm. At this pressure, both nickel and cobalt are thermodynamically stable in the metallic form. The scale produced by this process consists of an outer oxide layer about I sum thick and an inner sub scale composite layer of about 120 sum thick. The outer layer contained only ZrO2 and Yo-yo. The sub scale also consisted of a ZrO2/Y203 matrix, but contained a large number of finely dispersed metallic particles, essentially nickel and cobalt.

Although nickel and cobalt were present uniformly within the outer region of the metallic coating after hot dipping and annealing and before the conversion of Or and Y
into oxides, they were virtually absent from this same region after the selective oxidation treatment. X-ray diffraction analysis of the surface of the sample indicated that this outer oxide layer was formed exclusively of a mixture of monoclinic zircon and yttria.

~2~7~

It is believed that the final distribution of elements across the duplex coating layer and the subsequent oxide morphology are determined largely by the conditions of the final selective oxidation treatment. ye believe that oxidation proceeds as follows: The melt composition at the sample surface before the selective oxidation treatment consists largely of Or and Nix smaller con-cent rations of Y and Co, and virtually no Cr. Once oxygen is admitted at PO = 10 17 elm, Or and Y atoms diffuse rapidly in the melt toward the outer oxygen/metal interface to form a solid ZrO2/Y2O3 mixture. The more noble elements (No and Co) are then excluded Eros the melt and accumulate in the metal side of the interface. The depletion of Or from this melt increases the nickel content of the alloy and renders it more refractory. Once the coating alloy solidifies, atoms of all elements in the remaining metallic part of the coating become less mobile than in the molten state, and further oxidation proceeds as a solid state reaction. The continued growth of the ZrO2/Y2O3 continues to promote a counter-current solid state diffusion process in the metal side of the interface in which Or and Y diffuse toward the interface, while nickel and cobalt diffuse away from the interface.

~2376~

The profile indicated that, under the external ZrO2~Y203 layer, nickel and cobalt exist as small particles embedded in the sub scale composite layer. The reason for their existence in such a distribution within a matrix of the ZrO2/Y203 sub scale is not well understood. It should be emphasized that the weight fraction of nickel present in the coating layer, before oxidation, amounts to about 25~, which corresponds to about 20% in volume fraction. This amount will increase in the sub scale after the exclusion of nickel from the outer ZrO2/Y2O3 external scale during selective oxidation. This substantial amount of nickel, added to cobalt diffusing from the substrate, is expected to remain trapped in the sub scale layer of the coating during the completion Ox selective oxidation of Or and Y.

The configuration and distribution of nickel and cobalt within this zone is likely to be determined by the mechanisms of oxidation of Or and Y within the sub scale zone. At least two possibilities exist:

(l) The concentration of nickel and cobalt in the metal ahead of the interface becomes very high as a result of their exclusion from the ZrO2/Y2O3 scale initially formed from the melt. Some back-diffusion of both elements in the solid state is likely to continue during further exposure, but the remaining portion of both elements may be overrun by the advancing oxide/metal interface.

aye (2) A transition from internal to external oxidation occurs. After the initial formation of a ZrO2/Y203 layer at the surface, ZrO2 internal oxide particles may form ahead of the interface when the con-cent ration of dissolved oxygen and zirconium exceeds thesolubility product necessary for their nucleation. Then, these particles may partially block further Roy reaction because the diffusion of oxygen atoms to the reaction front (of internal oxidation) can occur only in the lo channels between the particles that were previously precipitated. Further reaction at the reaction front may occur either by sideways growth of the existing particles, which requires a very small supersaturation, or by nucleation of a new particle. The sideways growth of the particles can thus lead to a compact oxide layer, which can entrap metallic constituents existing within the same region.

I

In general, regardless of the mechanism involved, in determining the morphology and distribution of the metallic particles within the sub scale zone, the formation of such a ceramlc/metallic composite layer between the outer ceramic layer and the inner metallic substrate is highly advantageous. This is due to its ability to reduce the stresses generated from the mismatch in coefficients of thermal expansion of the outer ceramic coating and the inner metallic substrate.

Coating adhesion was evaluated by exposure of several test specimens to 10 thermal cycles between 1000C
and ambient temperature in elf. The ZrO2/Y203 coating on the alloy Caulker remained completely adherent and showed no sign of spallation or cracking. Careful metallurgical examination along the whole length of the specimen did not reveal any sign of cracking. The coating appears completely pore free. Furthermore, micro probe analyses across this section showed that the distributions of Or, Y, Nix Co, and Or were essentially the same as those samples that had not been cycled. The coatings are not equally effective on all substrates. For example, a similar ZrO2/Y203 coating on the alloy MIRIAM spelled after the second cycle.

It will therefore be apparent that a new and advantageous method and product are provided.

Claims (12)

WE CLAIM:
1. A method of coating a metal substrate with a protective coating which comprises:

(a) providing a substrate metal to be coated, (b) providing an alloy or mixture of (1) zirconium and/or hafnium, and (2) at least one other metal M2 which does not form a stable oxide at an elevated temperature in an atmosphere having a very small partial pressure of oxygen, and which forms an alloy with at least one component of the substrate on heat treatment of the coated material;

(c) applying such alloy or mixture to a surface of the substrate, under conditions such that the surface is coated with an alloy of zirconium and/or hafnium with M2 and (d) effecting selective oxidation of the zirconium and/or hafnium at an elevated temperature in the coating without substantial oxidation of M2, (e) the proportion of zirconium and/or hafnium to M2 in the coating alloy being substantial and sufficient to result in a coating containing sufficient oxide of zirconium and/or hafnium to function as a sub-stantial thermal barrier.
2. The method of Claim 1 wherein the substrate metal is nobler than zirconium and hafnium.
3. The method of Claim 2 wherein after step (d) the coating is annealed.
4. The method of Claim 2 wherein the substrate metal is a superalloy.
5. The method of Claim 2 wherein the first mentioned metal is zirconium.
6. The method of Claim 2 wherein the first mentioned metal is hafnium.
7. The method of Claim 2 wherein M2 is selected predominantly from the group nickel, cobalt and iron.
8. A coated metal article comprising:

(a) a metal substrate whose surface is subject to oxidation and deterioration at high temperature in an oxidizing atmosphere, and (b) a protective coating on and adherent to at least one surface of the substrate alloy, such coating comprising an outer layer of an oxide of zirconium and/or hafnium and an inner layer of at least one metal M2 which is bonded to the substrate, said metal M2 being a metal which does not form a stable oxide when exposed at an elevated temperature to an atmosphere having a very small partial pressure of oxygen.
9. The coated metal of Claim 8 wherein the substrate is nobler than zirconium and hafnium.
10. The coated metal article of Claim 9 wherein the metal substrate is a superalloy.
11. The coated metal article of Claim 9 wherein the oxide is predominatly zirconium oxide.
12. The coated metal article of Claim 9 wherein M2 is selected predominantly from the group nickel, cobalt and iron.
CA000436457A 1983-04-22 1983-09-12 Process for applying thermal barrier coatings to metals and resulting product Expired CA1237609A (en)

Applications Claiming Priority (2)

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US48774583A 1983-04-22 1983-04-22
US487,745 1983-04-22

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JP (1) JPS60501162A (en)
CA (1) CA1237609A (en)
DE (1) DE3390480T1 (en)
GB (1) GB2158844A (en)
IT (1) IT1209837B (en)
NL (1) NL8320222A (en)
NO (1) NO845144L (en)
SE (1) SE8406442L (en)
WO (1) WO1984004335A1 (en)

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* Cited by examiner, † Cited by third party
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DE3822802A1 (en) * 1988-07-06 1990-03-22 Atilla Dipl Chem Dr Ing Akyol Process for improving the adhesion of wear-resistant layers to tools
US6532657B1 (en) * 2001-09-21 2003-03-18 General Electric Co., Pre-service oxidation of gas turbine disks and seals
US20030118873A1 (en) * 2001-12-21 2003-06-26 Murphy Kenneth S. Stabilized zirconia thermal barrier coating with hafnia

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US375784A (en) * 1888-01-03 Apparatus for electric welding
US2269601A (en) * 1934-06-02 1942-01-13 Electrochimie D Electro Metall Process for the manufacture of articles resistant to gaseous corrosion
GB1086708A (en) * 1966-02-01 1967-10-11 Gen Electric Co Ltd Improvements in or relating to metal bodies and their manufacture
CA850045A (en) * 1966-07-11 1970-08-25 Cominco Ltd. Process for the production of coloured coatings
FR1536493A (en) * 1966-07-22 1968-08-16 Montedison Spa High strength protective coatings and method thereof for their application to interior surfaces of hydrocarbon cracking reactors
GB1194600A (en) * 1967-11-03 1970-06-10 Gen Electric & English Elect Improvements in or relating to Metal Bodies and their Manufacture
US4483720A (en) * 1981-11-27 1984-11-20 S R I International Process for applying thermal barrier coatings to metals

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SE8406442D0 (en) 1984-12-18
EP0140889A1 (en) 1985-05-15
IT1209837B (en) 1989-08-30
SE8406442L (en) 1984-12-18
EP0140889A4 (en) 1986-02-13
JPS60501162A (en) 1985-07-25
GB8426443D0 (en) 1984-11-28
WO1984004335A1 (en) 1984-11-08
NL8320222A (en) 1985-02-01
DE3390480T1 (en) 1985-04-18
GB2158844A (en) 1985-11-20
IT8448073A0 (en) 1984-04-19
NO845144L (en) 1984-12-20

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