Method for coating a component of a turbomachine and coated component for a turbomachine

US9850566B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9850566-B2
Application numberUS-201414214980-A
CountryUS
Kind codeB2
Filing dateMar 16, 2014
Priority dateMar 19, 2013
Publication dateDec 26, 2017
Grant dateDec 26, 2017

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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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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

The invention relates to a coating system for a component of a turbomachine, which includes at least two different base powders. Each of the at least two different base powders has an individual predetermined distribution within the coating system. Further, each of the at least two different base powders is responsible for a specific property of the coating system.

First claim

Opening claim text (preview).

The invention claimed is: 1. A coating system for a component of a turbomachine, comprising: a first powder feeder configured to feed a first composite powder to a sprayer via a first line for applying the first composite powder onto the surface of the component; a second powder feeder configured to feed a second composite powder to the sprayer via a second line for applying the second composite powder onto the surface of the component, the second composite powder having a composition that differs from a composition of the first composite powder; wherein the first powder feeder and second powder feeder are configured such that oxidizing media, fuel, the first composite powder and the second composite powder are simultaneously feedable onto the surface of the component to deposit the coating on the surface of the component such that a first portion of the coating covering a first portion of the surface adjacent a leading edge of the component has a first composition and a second portion of the coating covering a second portion of the surface adjacent a trailing edge of the component has a second composition via adjustment of a ratio between the first composite powder and second composite powder fed to the sprayer controlled during feeding of the multiple different powders, fuel, and oxidizing media onto the surface of the component; the first powder feeder and the second powder feeder configured to be controlled such that the first composition has a greater proportion of the first composite powder than the second composition such that the first portion of the coating has a greater ductility than the second portion of the coating and the second portion of the coating has a greater oxidation resistance than the first portion of the coating; a source of the first composite powder that is connected to the sprayer via the first line such that the first composite powder is passable to the first powder feeder to feed the first composite powder onto the surface of the component via the sprayer, wherein said first composite powder is a powder blend of two or more different powders having one of a different size distribution, composition and particle shape; and a source of the second composite powder that is connected to the sprayer via the second line such that the second composite powder is passable to the sprayer to feed the second composite powder onto the surface of the component via the sprayer, wherein said second composite powder is a powder blend of two or more different powders having one of a different size distribution, composition and particle shape. 2. The coating system as claimed in claim 1 , wherein at least one of said first composite powder and said second composite powder contains particles, which are agglomerated and sintered. 3. The coating system as claimed in claim 1 , wherein at least one of said first composite powder and said second composite powder contains particles, the particles having at least one of a core structure and a shell structure. 4. The coating system as claimed in claim 3 , wherein said core of said particles is agglomerated and sintered. 5. The coating system as claimed in claim 3 , wherein said core of said particles has at least one chemical composition that differs from a chemical composition of said shell of said particles. 6. The coating system as claimed in claim 1 , wherein the first and second composite powders are configured to be feedable such that fractions of the first and second composite powders vary along a depth and a length of the coating. 7. The coating system as claimed in claim 1 , wherein the first and second composite powders are configured to be feedable such that fractions of the first and second composite powders vary along a lateral direction of the coating.

Assignees

Inventors

Classifications

  • C23C4/12Primary

    characterised by the method of spraying · CPC title

  • by flame or combustion · CPC title

  • Pretreatment of the material to be coated, e.g. for coating on selected surface areas · CPC title

  • C23C4/04Primary

    characterised by the coating material · CPC title

  • designed for spraying particulate materials (B05B7/16 takes precedence) · CPC title

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Frequently asked questions

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What does patent US9850566B2 cover?
The invention relates to a coating system for a component of a turbomachine, which includes at least two different base powders. Each of the at least two different base powders has an individual predetermined distribution within the coating system. Further, each of the at least two different base powders is responsible for a specific property of the coating system.
Who is the assignee on this patent?
Ansaldo Energia Ip Uk Ltd
What technology area does this patent fall under?
Primary CPC classification C23C4/12. Mapped technology areas include Chemistry & Metallurgy.
When was this patent published?
Publication date Tue Dec 26 2017 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).