Fused filament fabrication of abradable coatings

Patent metadata

Field	Value
Publication number	US-11976569-B2
Application number	US-202017096227-A
Country	US
Kind code	B2
Filing date	Nov 12, 2020
Priority date	Nov 14, 2019
Publication date	May 7, 2024
Grant date	May 7, 2024

Abstract

In general, techniques are described for fused filament fabrication of abradable coatings. An additive manufacturing system comprising a substrate defining a major surface, a filament delivery device, and a computing device may be configured to perform various aspects of the techniques. The computing device may be configured to control the filament delivery device to deposit a filament on the substrate, the filament including a powder and a binder, wherein the binder is configured to be substantially removed from the filament and the powder includes a metal or alloy configured to be sintered to form an abradable layer.

First claim

What is claimed is:

1. A method comprising:
depositing, by a filament delivery device, a softened filament on a substrate defining a major surface to form an unsintered layer, the filament including a powder and a binder, the powder including a metal or an alloy, wherein the unsintered layer comprises a non-uniform unsintered layer in which a first portion is defined by a first plurality of filament blocks and a second portion is defined by a second plurality of filament blocks;
removing substantially all of the binder; and
sintering the unsintered layer to form an abradable layer for the substrate defining the major surface, wherein the first portion of the unsintered layer forms a first portion of the abradable layer and the second portion of the unsintered layer forms a second portion of the abradable layer, and wherein the first portion of the abradable layer defines a different porosity, density, composition, or microstructure than the second portion of the abradable layer.

2. The method of claim 1 , wherein the unsintered layer comprises a continuous unsintered layer in which the continuous unsintered layer is a single unsintered layer.

3. The method of claim 1 , wherein the unsintered layer further comprises a third portion defined by a third plurality of filament blocks.

4. The method of claim 3 , wherein each filament block of the first plurality of filament blocks defines a first shape, each filament block of the second plurality of filament blocks defines a second shape, and each filament block of the third plurality of filament blocks defines a third shape, and wherein the third shape is different from at least one of the first shape or the second shape in at least one of a surface area, a perimeter length, or a contour shape.

5. The method of claim 3 , wherein respective filament blocks of the third plurality of filament blocks are oriented to substantially align with a blade tip of a blade configured to contact a blade rub portion upon rotation of the blade in a circumferential direction.

6. The method of claim 3 , wherein each filament block of the first plurality of filament blocks defines a first shape, each filament block of the second plurality of filament blocks defines a second shape, and each filament block of the third plurality of filament blocks defines a third shape, and wherein the third shape is circular.

7. The method of claim 3 , wherein each filament block of the first plurality of filament blocks defines a first average coating block size, each filament block of the second plurality of filament blocks defines a second average coating block size, and each filament block of the third plurality of filament blocks defines a third average coating block size, and wherein the first average coating block size and the second average coating block size are less than the third average coating block size.

8. The method of claim 1 , further comprising:
controlling, by a computing device, the filament delivery device to deposit the filament onto the major surface of the substrate.

9. The method of claim 1 , wherein a composition of the first portion of the non-uniform unsintered layer and a composition of the second portion of the non-uniform unsintered layer are different.

10. The method of claim 1 , wherein the first portion includes one or more gaps, relative to air flow through a shroud, from inlet to outlet.

11. A method comprising:
depositing, by a filament delivery device, a softened filament on a substrate defining a major surface to form an unsintered layer, the filament including a powder and a binder, the powder including a metal or an alloy, wherein the unsintered layer comprises a non-uniform unsintered layer in which a first portion is defined by a first plurality of filament blocks, a second portion of the non-uniform unsintered layer is defined by a second plurality of filament blocks, and a third portion of the non-uniform unsintered layer is defined by a third plurality of filament blocks;
removing substantially all of the binder; and
sintering the unsintered layer to form an abradable layer for the substrate defining the major surface, wherein the first portion of the unsintered layer forms a first portion of the abradable layer, the second portion of the unsintered layer forms a second portion of the abradable layer, the third portion of the unsintered layer forms a third portion of the abradable layer,

wherein each filament block of the first plurality of filament blocks defines a first shape, each filament block of the second plurality of filament blocks defines a second shape, and each filament block of the third plurality of filament blocks defines a third shape, and wherein the third shape is rounded such that the third shape does not include relatively sharp edges, and wherein respective filament blocks of the third plurality of filament blocks are oriented to substantially align with a blade tip of a blade configured to contact a blade rub portion upon rotation of the blade in a circumferential direction.

12. An additive manufacturing system comprising:
a substrate defining a major surface;
a filament delivery device; and

a computing device configured to:
control the filament delivery device to deposit a softened filament on the substrate to form an unsintered layer, the filament including a powder and a binder, wherein the unsintered layer comprises a non-uniform unsintered layer in which a first portion is defined by a first plurality of filament blocks and a second portion of the non-uniform unsintered layer is defined by a second plurality of filament blocks;
wherein the binder is configured to be substantially removed from the filament and the powder includes a metal or an alloy configured to be sintered to form an abradable layer, wherein the first portion of the unsintered layer forms a first portion of the abradable layer and the second portion of the unsintered layer forms a second portion of the abradable layer, and wherein the first portion of the abradable layer defines a different porosity, density, composition, or microstructure than the second portion of the abradable layer.

13. The additive manufacturing system of claim 12 , wherein the unsintered layer comprises a continuous unsintered layer in which the continuous unsintered layer is a single unsintered layer.

14. The additive manufacturing system of claim 12 , wherein the unsintered layer further comprises third portion defined by a third plurality of filament blocks.

15. The additive manufacturing system of claim 14 , wherein each filament block of the first plurality of filament blocks defines a first shape, each filament block of the second plurality of filament blocks defines a second shape, and each filament block of the third plurality of filament blocks defines a third shape, and wherein the third shape is different from at least one of the first shape or the second shape in at least one of a surface area, a perimeter length, or a contour shape.

16. The additive manufacturing system of claim 14 , wherein respective filament blocks of the third plurality of filament blocks are oriented to substantially align with a blade tip of a blade configured to contact a blade rub portion upon rotation of the blade in a circumferential direction.

Assignees

• Rolls Royce Corp
• Rolls Royce Nam Tech Inc

Inventors

• Shuck Quinlan Yee
• Nelson Scott
• Xu Raymond Ruiwen
• Ribic Brandon David
• Gold Matthew R

Classifications

• F01D5/288 Primary

  Protective coatings for blades · CPC title

• B29C64/165

  using a combination of solid and fluid materials, e.g. a powder selectively bound by a liquid binder, catalyst, inhibitor or energy absorber · CPC title

• B29C64/245

  Platforms or substrates (support structures intended to be sacrificed after manufacture B29C64/40) · CPC title

• B33Y80/00

  Products made by additive manufacturing · CPC title

• B33Y10/00

  Processes of additive manufacturing · CPC title