Compliant layer for ceramic components and methods of forming the same

US2016137559A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2016137559-A1
Application numberUS-201414205010-A
CountryUS
Kind codeA1
Filing dateMar 11, 2014
Priority dateMar 11, 2013
Publication dateMay 19, 2016
Grant date

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  1. Title

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  2. Abstract

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  5. First independent claim

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Abstract

Official abstract text for this publication.

An apparatus includes a ceramic matrix composite (CMC) component and an interface coating on the CMC component, wherein the interface coating includes a layer of at least one of the following compositions: 100 wt % Ir; 90-95 wt % Ir, 5-10 wt % Co, 1-2 wt % Al, 1-2 wt % Si; 40-50 wt % Nb, 28-42 wt % Al, 4-15 wt % Cr, 1-2 wt % Si; 90-92 wt % Mo, 4-5 wt % Si, 4-5 wt % B; or 60-80 wt % V, 20-30 wt % Cr, 2-15 wt % Ti.

First claim

Opening claim text (preview).

1 . An apparatus, comprising: a ceramic matrix composite (CMC) component; and an interface coating on the CMC component, wherein the interface coating comprises a layer of at least one of the following compositions: 100 wt % Ir; 90-95 wt % Ir, 5-10 wt % Co, 1-2 wt % Al, 1-2 wt % Si; 40-50 wt % Nb, 28-42 wt % Al, 4-15 wt % Cr, 1-2 wt % Si; 90-92 wt % Mo, 4-5 wt % Si, 4-5 wt % B; or 60-80 wt % V, 20-30 wt % Cr, 2-15 wt % Ti. 2 . The apparatus of claim 1 , wherein the interface coating further comprises at least one of Ti, Ni—Co—Fe, or Ni—Mo—Cr. 3 . The apparatus of claim 1 , wherein the interface coating has a coefficient of thermal expansion (CTE) of about 4×10−6 to about 6×10−6/° F. 4 . The apparatus of claim 1 , further comprising a bond layer between a surface of the CMC component and the interface coating. 5 . The apparatus of claim 4 , wherein the bond layer comprises Si. 6 . The apparatus of claim 4 , wherein the bond layer consists of Si. 7 . The apparatus of claim 1 , further comprising a corrosion-resistant coating on the interface coating, wherein the corrosion-resistant coating comprises an alloy comprising at least one of Ti, Al, or V, an alloy comprising at least one of Ti, Al, Sn, Zr, or Mo, or an alloy comprising Ni and Cr. 8 . The apparatus of claim 7 , wherein the corrosion-resistant coating comprises at least one of Ti—Al—V, Ti—Al—Sn—Zr—Mo, Ni—Cr, or Ni—Mo—Cr. 9 . The apparatus of claim 1 , further comprising a compliance-enhancing coating on the interface coating, wherein the compliance-enhancing coating comprises at least one of Pt, Ag, Cu, Ni, Cr, Co, or Mo. 10 . The apparatus of claim 9 , wherein the compliance-enhancing coating comprises at least one of a Cu alloy, an Ag alloy, or Co—Cr—Mo. 11 . The apparatus of claim 1 , further comprising an outer coating on the interface coating, wherein the outer coating is selected from at least one of an environmental barrier coating or a thermal barrier coating. 12 . A ceramic matrix composite (CMC) component with an interface coating system thereon, the interface coating system comprising; a bond coating on a surface of the CMC component, wherein the bond coating comprises Si; an interface coating on the bond coating, wherein the interface coating comprises a layer of at least one of the following compositions: 100 wt % Ir; 90-95 wt % Ir, 5-10 wt % Co, 1-2 wt % Al, 1-2 wt % Si; 40-50 wt % Nb, 28-42 wt % Al, 4-15 wt % Cr, 1-2 wt % Si; 90-92 wt % Mo, 4-5 wt % Si, 4-5 wt % B; or 60-80 wt % V, 20-30 wt % Cr, 2-15 wt % Ti; a corrosion-resistant coating on the interface coating, wherein the corrosion resistant coating comprises an alloy comprising at least one of Ti, Al, or V, an alloy comprising at least one of Ti, Al, Sn, Zr, or Mo, or an alloy comprising Ni and Cr; and a compliance-enhancing coating on the corrosion-resistant coating, wherein the compliance-enhancing coating comprises at least one of Pt, Ag, Cu, Ni, Cr, Co, or Mo. 13 . The apparatus of claim 12 , further comprising at least one outer coating on the compliance-enhancing coating. 14 . The apparatus of claim 12 , wherein the bond coating consists of Si. 15 . A method, comprising: forming an interface coating on a ceramic matrix composite (CMC) component such that the interface coating is bonded to the ceramic component, wherein the interface coating comprises layer of at least one of the following compositions: 100 wt % Ir; 90-95 wt % Ir, 5-10 wt % Co, 1-2 wt % Al, 1-2 wt % Si; 40-50 wt % Nb, 28-42 wt % Al, 4-15 wt % Cr, 1-2 wt % Si; 90-92 wt % Mo, 4-5 wt % Si, 4-5 wt % B; or 60-80 wt % V, 20-30 wt % Cr, 2-15 wt % Ti. 16 . The method of claim 15 , further comprising forming a bond coating on the CMC part prior to forming the interface coating, wherein the bond coating comprises Si. 17 . The method of claim 16 , further comprising heat treating the bond coating and the interface coating to about 1100° C. to about 1325° C. 18 . The method of claim 15 , further comprising forming a corrosion-resistant coating on the interface coating, wherein the corrosion resistant coating comprises an alloy comprising at least one of Ti, Al, or V, an alloy comprising at least one of Ti, Al, Sn, Zr, or Mo, or an alloy comprising Ni and Cr. 19 . The method of claim 18 , further comprising heating the interface coating and the corrosion-resistant coating to a temperature of about 1100° C. 20 . The method of claim 18 , further comprising forming a compliance-enhancing coating on the corrosion-resistant coating, wherein the compliance-enhancing coating comprises at least one of Pt, Ag, Cu, Ni, Cr, Co, or Mo. 21 . The method of claim 20 , further comprising forming at least one outer coating on the compliance-enhancing coating. 22 . A turbine engine component comprising a ceramic matrix composite (CMC) component, wherein the CMC component is loaded against a metal part, wherein the CMC component comprises an interface coating adjacent to the metal part, the interface coating comprising a layer of at least one of the following compositions: 100 wt % Ir; 90-95 wt % Ir, 5-10 wt % Co, 1-2 wt % Al, 1-2 wt % Si; 40-50 wt % Nb, 28-42 wt % Al, 4-15 wt % Cr, 1-2 wt % Si; 90-92 wt % Mo, 4-5 wt % Si, 4-5 wt % B; or 60-80 wt % V, 20-30 wt % Cr, 2-15 wt % Ti.

Assignees

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Classifications

  • with a composition mainly composed of one or more of the noble metals or copper · CPC title

  • with a composition mainly composed of one or more of the refractory metals · CPC title

  • Coating; Surface treatment · CPC title

  • for obtaining at least two superposed coatings having different compositions · CPC title

  • Metals, alloys or intermetallic compounds · CPC title

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What does patent US2016137559A1 cover?
An apparatus includes a ceramic matrix composite (CMC) component and an interface coating on the CMC component, wherein the interface coating includes a layer of at least one of the following compositions: 100 wt % Ir; 90-95 wt % Ir, 5-10 wt % Co, 1-2 wt % Al, 1-2 wt % Si; 40-50 wt % Nb, 28-42 wt % Al, 4-15 wt % Cr, 1-2 wt % Si; 90-92 wt % Mo, 4-5 wt % Si, 4-5 wt % B; or 60-80 wt % V, 20-30 wt …
Who is the assignee on this patent?
Rolls Royce Corp
What technology area does this patent fall under?
Primary CPC classification C04B41/5133. Mapped technology areas include Chemistry & Metallurgy.
When was this patent published?
Publication date Thu May 19 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). 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).