Fused filament fabrication method using filaments that include a binder configured to release a secondary material

Patent metadata

Field	Value
Publication number	US-11697243-B2
Application number	US-202017097940-A
Country	US
Kind code	B2
Filing date	Nov 13, 2020
Priority date	Nov 14, 2019
Publication date	Jul 11, 2023
Grant date	Jul 11, 2023

Abstract

A method may include fused filament fabricating a fused filament fabricated component by delivering a softened filament to selected locations at or adjacent to a build surface. The softened filament may include a binder and a primary material. The binder is configured to release a secondary material upon heating at or above a conversion temperature. The method also may include heating the fused filament fabricated component to a temperature at or above the conversion temperature to sinter the primary material to form a sintered part and cause the binder to release the secondary material within the sintered part.

First claim

What is claimed is:

1. A method comprising:
fused filament fabricating a fused filament fabricated component by at least:
delivering a softened first filament to a first set of selected locations at or adjacent to a build surface, and
delivering a softened second filament to a second set of selected locations at or adjacent to the build surface, wherein the softened first filament comprises a binder and a metal or alloy powder, wherein the binder is configured to release at least one of a secondary material or an alloying element upon heating at or above a conversion temperature, wherein the softened second filament comprises a sacrificial binder and the metal or the alloy powder, the sacrificial binder being different from the binder of the first filament, wherein the first set of locations where the softened first filament is delivered include locations at or near a surface of the fused filament fabricated component, and wherein the second set of locations where the softened second filament is delivered include locations within a bulk volume of the fused filament fabricated component such that the delivered softened first filament is located between the surface of the fused filament fabricated component and the softened second filament within the bulk volume of the fused filament fabricated component;

removing substantially all of the sacrificial binder of the delivered second filament from the fused filament fabricated component; and
heating the fused filament fabricated component to a temperature at or above the conversion temperature to sinter the metal or the alloy powder to form a sintered part and cause the binder to release the at least one of the secondary material or the alloying element within the sintered part, wherein the release of the secondary material or the alloying element with the heating is configured such that the sintered metal or the sintered alloy powder is case hardened at the locations at or near the surface of the sintered part but not the second set of locations within the bulk volume to increase a wear resistance of the sintered part at the locations at or near the surface.

2. The method of claim 1 , wherein the first filament further comprises a ceramic.

3. The method of claim 1 , wherein the secondary material comprises carbon, and wherein the binder is configured to release carbon upon heating at or above the conversion temperature.

4. The method of claim 3 , wherein the binder comprises a high char yielding binder.

5. The method of claim 1 , wherein the secondary material comprises nitrogen, and wherein the binder is configured to release nitrogen upon heating at or above the conversion temperature.

6. The method of claim 5 , wherein the binder comprises a polyamide.

7. The method of claim 1 , wherein the secondary material comprises silicon, and wherein the binder is configured to release silicon upon heating at or above the conversion temperature.

8. The method of claim 7 , wherein the binder comprises a silicone polymer.

9. The method of claim 1 , wherein the secondary material comprises a ceramic, and wherein the binder comprises a preceramic polymer.

10. The method of claim 1 , wherein the secondary material comprises a metal, and wherein the binder comprises an organometallic compound.

11. The method of claim 1 , wherein the alloying element comprises carbon, wherein the binder is configured to release carbon upon heating at or above the conversion temperature, and wherein the release of the carbon is configured to case harden the sintered metal or the sintered alloy powder at the locations at or near the surface of the sintered part to increase the wear resistance of the sintered part at the locations at or near the surface.

12. The method of claim 11 , wherein the binder comprises a high char yielding binder.

13. The method of claim 1 , wherein the alloying element comprises nitrogen, and wherein the binder is configured to release nitrogen upon heating at or above the conversion temperature, and wherein the release of the nitrogen is configured to case harden the sintered metal or the sintered alloy powder at the locations at or near the surface of the sintered part to increase the wear resistance of the sintered part at the locations at or near the surface.

14. The method of claim 13 , wherein the binder comprises a polyamide.

15. The method of claim 1 , wherein the alloying element comprises silicon, and wherein the binder is configured to release silicon upon heating at or above the conversion temperature.

16. The method of claim 1 , wherein the alloying element comprises a metal, and wherein the binder comprises an organometallic compound.

17. The method of claim 1 , wherein the release of the secondary material or the alloying element with the heating effects metallurgical changes in the sintered metal or the sintered alloy powder at the first set of selected locations of the sintered part.

Assignees

• Rolls Royce Corp

Inventors

• Raeker Evan
• Shuck Quinlan Yee
• Nelson Scott
• Xu Raymond Ruiwen

Classifications

• B33Y70/00

  Materials specially adapted for additive manufacturing · CPC title

• B29C64/245

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

• B29C64/118 Primary

  using filamentary material being melted, e.g. fused deposition modelling [FDM] · CPC title

• B29K2103/06

  Metal powders, metal carbides or the like · CPC title

• B29K2077/00

  Use of {PA, i.e.} polyamides, e.g. polyesteramides {or derivatives thereof}, as moulding material · CPC title