Additive layer method for application of slurry-based features

US11351696B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11351696-B2
Application numberUS-201916278265-A
CountryUS
Kind codeB2
Filing dateFeb 18, 2019
Priority dateFeb 19, 2018
Publication dateJun 7, 2022
Grant dateJun 7, 2022

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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.

A system and method for forming a porous ceramic preform is provided. The method may include forming a stacked powder structure including a binder layer and a powder layer on the binder layer. The binder layer may be formed by depositing a binder with a spray nozzle on a substrate. The powder layer may be formed by depositing a powder on the binder layer. The porous ceramic preform may be formed by heating the stacked powder structure to pyrolyze the binder. The porous ceramic preform is configured to be infiltrated by a molten material. The substrate may comprise a ceramic fiber preform. After melt infiltration of the porous ceramic preform and the ceramic fiber preform, a densified ceramic feature having a predetermined geometry may be formed on a ceramic matrix composite (CMC) component.

First claim

Opening claim text (preview).

What is claimed is: 1. A method comprising: forming a stacked powder structure on a substrate comprising a previously formed ceramic fiber preform, the stacked powder structure comprising a binder layer and a powder layer on the binder layer, wherein forming the stacked powder structure comprises forming the binder layer by depositing a binder with a spray nozzle on the substrate and forming the powder layer on the binder layer by depositing a powder on the binder layer, the binder comprising at least one of phenolic resin, poly(furfuryl alcohol), and polycarbosilane, and the powder comprising silicon carbide; and heating the stacked powder structure to pyrolyze the binder, and infiltrating the stacked powder structure and the previously formed ceramic fiber preform with molten silicon metal or silicon alloy, thereby forming a CMC component including a densified composite feature on the CMC component. 2. The method of claim 1 , further comprising: removing an amount of the powder from the stacked powder structure prior to the heating. 3. The method of claim 1 , wherein the powder comprises fibers, and the method further comprises: wherein the densified composite feature has a fiber-to-ceramic matrix material ratio of between 20% and 45%. 4. The method of claim 1 , wherein the spray nozzle comprises an array of nozzles for supplying the binder to selected regions of the substrate. 5. The method of claim 1 , further comprising controlling the spray nozzle to supply the binder to predetermined portions of the substrate. 6. The method of claim 1 , wherein the powder comprises a plurality of chopped fibers, each having a diameter in a range of between 5 microns and 10 microns, inclusively, and the chopped fibers have an aspect ratio between 4 and 20, inclusively. 7. The method of claim 1 , wherein the binder layer is a first binder layer and the powder layer is a first powder layer, and forming the stacked powder structure further comprises forming a second binder layer by depositing the binder on the first powder layer and forming a second powder layer by depositing the powder on the second binder layer. 8. The method of claim 1 , further comprising: placing the substrate on a stage; and lowering the stage before depositing the powder on the binder. 9. The method of claim 1 , wherein the powder further comprises a reactive additive. 10. The method of claim 9 , wherein the reactive additive comprises at least one of graphite, diamond, and carbon black. 11. The method of claim 9 , wherein the reactive additive comprises acicular particulate. 12. The method of claim 11 , wherein the acicular particulate comprises at least one of carbon fiber and graphene. 13. The method of claim 1 , wherein heating the stacked powder structure causes the binder to produce silicon carbide. 14. The method of claim 1 , wherein the powder comprises a unimodal particle size distribution. 15. The method of claim 1 , wherein the powder comprises a bimodal particle size distribution. 16. The method of claim 1 , wherein the previously formed ceramic fiber preform has been infiltrated by a slurry, the slurry comprising silicon carbide. 17. A method comprising: forming a stacked powder structure on a substrate comprising a previously formed ceramic fiber preform, the stacked powder structure comprising a first binder layer, a first powder layer on the first binder layer, a second binder layer on the first powder layer, and a second powder layer on the second binder layer, wherein forming the stacked powder structure comprises forming the first binder layer by depositing a binder with a spray nozzle on the substrate, the binder comprising at least one of phenolic resin, poly(furfuryl alcohol), and polycarbosilane, forming the first powder layer on the first binder layer by depositing a powder on the first binder layer, forming the second binder layer on the first powder layer by depositing the binder with the spray nozzle on the first powder layer, and forming the second powder layer by depositing the powder on the second binder layer, the powder comprising fibers, including silicon carbide fibers wherein the fibers comprise chopped fibers having a diameter in a range of between 5 microns and 10 microns, inclusively, and the chopped fibers have an aspect ratio between 4 and 20, inclusively; heating the stacked powder structure to pyrolyze the binder, and infiltrating the stacked powder structure and the previously formed ceramic fiber preform with molten silicon metal or silicon alloy, thereby forming a CMC component including a densified composite feature on the CMC component; and wherein the densified composite feature has a fiber-to-matrix material ratio of between 20% and 45%. 18. The method of claim 17 , wherein the densified composite feature includes a seal land, labyrinth seal, strip seal, load pad, locating pad, and/or clocking feature.

Assignees

Inventors

Classifications

  • Post-treatment, e.g. curing, coating or polishing · CPC title

  • B28B1/001Primary

    Rapid manufacturing of 3D objects by additive depositing, agglomerating or laminating of material (selective deposition modelling of metallic powder B22F10/00; rapid manufacturing of 3D objects in general and in particular of plastics B29C64/00) · CPC title

  • Carbon, e.g. graphite · CPC title

  • based on silicon carbide (C04B35/571 takes precedence) · CPC title

  • B33Y10/00Primary

    Processes of additive manufacturing · CPC title

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What does patent US11351696B2 cover?
A system and method for forming a porous ceramic preform is provided. The method may include forming a stacked powder structure including a binder layer and a powder layer on the binder layer. The binder layer may be formed by depositing a binder with a spray nozzle on a substrate. The powder layer may be formed by depositing a powder on the binder layer. The porous ceramic preform may be forme…
Who is the assignee on this patent?
Rolls Royce Corp, Rolls Royce High Temperature Composites Inc
What technology area does this patent fall under?
Primary CPC classification B28B1/001. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Jun 07 2022 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 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).