Duplex-phase CrAl coating for improved corrosion/oxidation protection
09689270 ยท 2017-06-27
Assignee
Inventors
- Horst Pillhoefer (Roehrmoos, DE)
- Stefan Mueller (Munich, DE)
- Erwin Bayer (Dachau, DE)
- Thomas Dautl (Weichs, DE)
Cpc classification
Y10T428/12639
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F01D5/288
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F01D5/28
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
Disclosed is a coating for protecting a component against high temperatures and aggressive media, which coating has at least one subregion whose main constituent is chromium. The layer additionally comprises aluminum, the chromium content at least in the subregion in which chromium is the main constituent being greater than 30% by weight and the aluminum content being greater than or equal to 5% by weight. The invention further provides a process for producing such a coating, comprising chromizing the surface to be coated and subsequently alitizing the chromium-rich layer produced during chromizing.
Claims
1. A process for producing a coating for protecting a component against high temperatures and aggressive media, the component being formed by an alloy having one or more metallic main constituents which make up the largest proportion of the alloy, wherein the process comprises chromizing a surface to be coated and subsequently aluminizing a chromium-rich layer produced during chromizing, the chromizing being carried out with a chemical chromium activity of at least 0.4, and wherein the process affords a coating that has an outer zone and an inner zone, the outer zone comprising -chromium phases in a matrix of a mixture of mixed crystals comprising essentially chromium, aluminum, and the one or more metallic main constituents of the alloy, and the inner zone comprising a mixed crystal zone comprising essentially chromium, aluminum, and the one or more metallic main constituents of the alloy, the proportion of chromium in a total coating being greater than 30% by weight and a proportion of aluminum in a total coating being at least 5% by weight, and wherein at least one of: (i) a proportion of chromium in the outer zone is from 30% by weight to 95% by weight of chromium; (ii) a proportion of chromium in the -chromium phases is at least 70% by weight; (iii) a proportion of aluminum in the outer zone is from 10% to 40% by weight of aluminum; (iv) the one or more metallic main constituents in the outer zone are present in a proportion of not higher than 40% by weight; (v) in the inner zone a proportion of chromium is not higher than 30% by weight, a proportion of aluminum is not higher than 30% by weight, and a proportion of the one or more main constituents is at least 30% by weight; (vi) a proportion of chromium in the total coating is from greater than 30% by weight to 90% by weight; (vii) a proportion of aluminum in the total coating is from 10% to 40% by weight; (viii) the outer zone of the coating makes up a proportion of at least 50% of the total coating; (ix) the coating has up to 10% by volume of pores having average diameters of from 2 m to 20 m; (x) the coating comprises from 1% to 15% by weight of oxides; (xi) the one or more metallic main constituents of the alloy are one or more of nickel, iron and cobalt; (xii) the chromizing is carried out using a Cr-rich slip containing a liquid phase.
2. The process of claim 1, wherein the chromizing is carried out using a Cr-rich slip containing a liquid phase.
3. The process of claim 2, wherein the slip is applied by injection molding.
4. The process of claim 1, wherein the chromizing is carried out at a temperature of from 1020 C. to 1180 C. for a period of from 2 to 20 hours.
5. The process of claim 1, wherein the aluminizing is carried out at a temperature of from 1050 C. to 1150 C. for a period of from 3 to 20 hours.
6. The process of claim 1, wherein the chemical aluminum activity during aluminizing is at least 0.3.
7. The process of claim 1, wherein a first aluminizing is followed by a second aluminizing at a lower chemical aluminum activity at a temperature of greater than or equal to 1050 C. for a period of from 3 to 20 hours.
8. The process of claim 1, wherein the chromizing and aluminizing are followed by a diffusion heat treatment at a temperature of greater than or equal to 1050 C. for a period of from 2 to 8 hours.
9. The process of claim 1, wherein a surface treatment by PVD, CVD, surface coating, electrochemical deposition and/or direct application of a material, in which one or more elements from the group platinum, palladium, hafnium, zirconium, yttrium and silicon are applied, is carried out before, during or after chromizing and/or aluminizing.
10. The process of claim 1, wherein a proportion of chromium in the outer zone is from 30% by weight to 95% by weight of chromium.
11. The process of claim 1, wherein a proportion of chromium in the -chromium phases is at least 70% by weight.
12. The process of claim 1, wherein a proportion of aluminum in the outer zone is from 10% to 40% by weight of aluminum.
13. The process of claim 1, wherein the one or more metallic main constituents in the outer zone are present in a proportion of not higher than 40% by weight.
14. The process of claim 1, wherein in the inner zone a proportion of chromium is not higher than 30% by weight, a proportion of aluminum is not higher than 30% by weight, and a proportion of the one or more main constituents is at least 30% by weight.
15. The process of claim 1, wherein a proportion of chromium in the total coating is from greater than 30% by weight to 90% by weight.
16. The process of claim 5, wherein a proportion of aluminum in the total coating is from 10% to 40% by weight.
17. The process of claim 4, wherein the outer zone of the coating makes up a proportion of at least 50% of the total coating.
18. The process of claim 3, wherein the coating has up to 10% by volume of pores having average diameters of from 2 m to 20 m.
19. The process of claim 2, wherein the coating comprises from 1% to 15% by weight of oxides.
20. The process of claim 1, wherein the one or more metallic main constituents of the alloy are one or more of nickel, iron and cobalt.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The attached drawings show in
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DETAILED DESCRIPTION OF THE PRESENT INVENTION
(7) The particulars shown herein are by way of example and for purposes of illustrative discussion of the embodiments of the present invention only and are presented in the cause of providing what is believed to be the most useful and readily understood description of the principles and conceptual aspects of the present invention. In this regard, no attempt is made to show details of the present invention in more detail than is necessary for the fundamental understanding of the present invention, the description in combination with the drawings making apparent to those of skill in the art how the several forms of the present invention may be embodied in practice.
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(10) The component bearing a correspondingly configured intermediate layer is subjected in a second step to an alitizing step in which aluminum diffuses into the intermediate layer so as to form an AlNiCr matrix in which -chromium phases are incorporated in an outer zone, as shown in
(11) The AlNiCr matrix of the outer zone comprises, in particular, Al.sub.xNi.sub.y, AlNi, Al.sub.3Ni.sub.2, Al.sub.3Ni and Cr.sub.2Al phases, while essentially NiAl mixed crystals having proportions of chromium are present in the NiAlCr mixed crystal zone of the inner zone.
(12) The -chromium phase of the outer zone has chromium contents of greater than or equal to 70% by weight of chromium, with essentially nickel being additionally dissolved in the -chromium phases. The total layer has a chemical composition of from 30% to 90% by weight of chromium, from 10% to 35% by weight of aluminum, up to 60% by weight of nickel, proportions of up to 25% by weight of platinum, palladium, up to 15% by weight of silicon, up to 15% by weight of hafnium, zirconium. The total layer thickness can be from 20 to 150 m.
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(14) It is noted that the foregoing examples have been provided merely for the purpose of explanation and are in no way to be construed as limiting of the present invention. While the present invention has been described with reference to exemplary embodiments, it is understood that the words which have been used herein are words of description and illustration, rather than words of limitation. Changes may be made, within the purview of the appended claims, as presently stated and as amended, without departing from the scope and spirit of the present invention in its aspects. Although the present invention has been described herein with reference to particular means, materials and embodiments, the present invention is not intended to be limited to the particulars disclosed herein; rather, the present invention extends to all functionally equivalent structures, methods and uses, such as are within the scope of the appended claims.