Chromizing over cathodic arc coating

US10364490B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10364490-B2
Application numberUS-201415103761-A
CountryUS
Kind codeB2
Filing dateNov 19, 2014
Priority dateDec 10, 2013
Publication dateJul 30, 2019
Grant dateJul 30, 2019

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

The present invention provides a Cr-rich cathodic arc coating, an article in turbine blade coated with the chromizing over cathodic arc coating, and a method to produce the coating thereof. The Cr-rich cathodic arc coating in the present invention comprises a cathodic arc coating and a diffusion coating deposited atop the cathodic arc coating to enforce hot corrosion resistance. The hardware coated with the chromizing over cathodic arc coating in the present invention is reinforced with superior-hot corrosion resistance. The present invention further provides a novel method for producing the chromizing over cathodic arc coating by re-sequencing coating deposition order. The method in the present invention is efficient and cost-reducing by eliminating some operations, e.g., DHT and peening, between the cathodic arc coating and the diffusion coating. The hot corrosion resistance in the present invention results from the high Cr content in the surface of the coating.

First claim

Opening claim text (preview).

What is claimed is: 1. A chromium-rich cathodic arc coating comprising: a MCrAlY cathodic arc coating on a substrate, wherein M is a metal alloy comprising nickel, cobalt, iron, or a combination thereof and the cathodic arc coating comprises 25 to 50% chromium by weight based on the weight of the MCrAlY; and a diffused chromide coating atop the MCrAlY cathodic arc coating, wherein the diffused chromide coating has a higher content of chromium than the MCrAlY cathodic arc coating, the combined thickness of the diffused chromide coating and the MCrAlY cathodic arc coating is 2.5 to 3 mil (0.0635 to 0.0762 mm), and the chromium-rich cathodic arc coating has a chromium rich phase with a depth of 0.1 to 2.5 mils (0.00254 to 0.0635). 2. The chromium-rich cathodic arc coating according to claim 1 , wherein the surface of the diffused chromide coating atop the MCrAlY has a chromium content no less than 37% by weight. 3. The chromium-rich cathodic arc coating according to claim 2 , wherein the MCrAlY has a chromium content between 25% and 35% by weight based on the weight of the MCrAlY. 4. The chromium-rich cathodic arc coating according to claim 1 , wherein the MCrAlY comprises hafnium. 5. The chromium-rich cathodic arc coating according to claim 1 , wherein the chromium rich phase has a depth of 0.2 to 1.0 mils (0.00508 to 0.0254 mm). 6. The chromium-rich cathodic arc coating according to claim 1 , wherein the chromium-rich cathodic arc coating is resistant to hot corrosion at a temperature between about 1200° F. and 1600° F. 7. The chromium-rich cathodic arc coating according to claim 1 , wherein the chromium-rich cathodic arc coating is resistant to stress corrosion. 8. The chromium-rich cathodic arc coating according to claim 1 , wherein the chromium-rich cathodic arc coating is resistant to low cycle fatigue. 9. The chromium-rich cathodic arc coating according to claim 1 , wherein the substrate comprises a blade root, internal surface of turbine blade, or the external surface of a turbine blade. 10. An article comprising: a) a substrate; b) a MCrAlY cathodic arc coating on the substrate, wherein M is a metal alloy comprising nickel, cobalt, iron, or a combination thereof and the cathodic arc coating comprises 25 to 50% chromium by weight based on the weight of the MCrAlY; and c) a diffused chromide coating atop the MCrAlY cathodic arc coating; wherein the diffused chromide coating atop the MCrAlY has a higher content of chromium than the MCrAlY cathodic arc coating, the combined thickness of the diffused chromide coating and the MCrAlY cathodic arc coating is 2.5 to 3 mil (0.0635 to 0.0762 mm), and the diffused chromide coating and the MCrAlY cathodic arc coating have a chromium rich phase with a depth of 0.1 to 2.5 mils (0.00254 to 0.0635). 11. The article according to claim 10 , wherein the substrate comprises a blade root, internal surface of turbine blade, or the external surface of a turbine blade. 12. The article according to claim 10 , wherein the MCrAlY further comprises hafnium. 13. The article according to claim 10 , wherein the chromium rich phase has a depth of 0.2 to 1.0 mils (0.00508 to 0.0254 mm). 14. The article according to claim 10 , wherein the article consists of the substrate, the MCrAlY coating and the diffused chromide coating. 15. A method of producing a chromium-rich cathodic arc coating comprising steps of: a) applying a MCrAlY cathodic arc coating on a substrate, wherein M is a metal alloy comprising nickel, cobalt, iron, or a combination thereof and the cathodic arc coating comprises 25 to 50% chromium by weight based on the weight of the MCrAlY; and b) applying a diffused chromide coating atop the MCrAlY cathodic arc coating; wherein the diffused chromide coating has a higher content of chromium than the MCrAlY cathodic arc coating and the combined thickness of the diffused chromide coating, the MCrAlY cathodic arc coating is 2.5 to 3 mil (0.0635 to 0.0762 mm), and the chromium-rich cathodic arc coating has a chromium rich phase with a depth of 0.1 to 2.5 mils (0.00254 to 0.0635). 16. The method of claim 15 , wherein the surface of the diffused chromide coating has a chromium content no less than 37% by weight. 17. The method of claim 16 , wherein the MCrAlY cathodic arc coating has a chromium content of between 25% and 35% by weight based on the weight of the MCrAlY. 18. The method of claim 15 , wherein the MCrAlY further comprises hafnium. 19. The method of claim 15 , wherein the chromium rich phase has a thickness of 0.2 to 1.0 mils (0.00508 to 0.0254 mm). 20. The method of claim 15 , wherein the method of applying the diffused chromide coating atop the MCrAlY comprises pack chromizing, slurry chromizing, vapor diffusion coating, or gas diffusion coating.

Assignees

Inventors

Classifications

  • Containing more than 10% nonferrous elements [e.g., high alloy, stainless] · CPC title

  • Co- or Ni-base component next to Fe-base component · CPC title

  • Co-, Fe-, or Ni-base components, alternative to each other · CPC title

  • Next to Co-, Fe-, or Ni-base component · CPC title

  • Cr-base component · CPC title

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What does patent US10364490B2 cover?
The present invention provides a Cr-rich cathodic arc coating, an article in turbine blade coated with the chromizing over cathodic arc coating, and a method to produce the coating thereof. The Cr-rich cathodic arc coating in the present invention comprises a cathodic arc coating and a diffusion coating deposited atop the cathodic arc coating to enforce hot corrosion resistance. The hardware co…
Who is the assignee on this patent?
United Technologies Corp
What technology area does this patent fall under?
Primary CPC classification C23C14/5846. Mapped technology areas include Chemistry & Metallurgy.
When was this patent published?
Publication date Tue Jul 30 2019 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).