Structures and components having composite unit cell matrix construction

Patent metadata

Field	Value
Publication number	US-11865619-B2
Application number	US-202117381361-A
Country	US
Kind code	B2
Filing date	Jul 21, 2021
Priority date	Dec 8, 2017
Publication date	Jan 9, 2024
Grant date	Jan 9, 2024

Abstract

A structure is provided. The structure defines a first direction, a second direction, and a third direction, the three directions orthogonal to each other. The structure includes a first section, a second section, and a third section. The first section includes a plurality of unit cells joined together, wherein the first section has a first average tensile strength and a first average crack growth resistance. The second substantially solid section is within and surrounding each unit cell of the plurality of first section unit cells, wherein the second section has a second average tensile strength and a second average crack growth resistance, the second average tensile strength different from the first average tensile strength and the second average crack growth resistance different from the first average crack growth resistance. The third section surrounds the first section and the second section.

First claim

What is claimed is:

1. A method of fabricating a composite component, the composite component comprising a first material, a second material, and a third material, said method comprising:
depositing the first material and the third material onto a surface; and
operating a consolidating device of an additive manufacturing system to consolidate the first material and the third material using a first process to form:
a first section comprising the first material, said first section comprising a plurality of first section unit cells joined together;
a third section comprising the third material, said third section surrounding the first section; and
depositing the second material within the third section and within and surrounding each unit cell of the plurality of first section unit cells; and
consolidating the second material using a second consolidation process different from the first process to form a second, solid section within the third section and within and surrounding each unit cell of the plurality of first section unit cells;
wherein the first material and the third material are harder than the second material, and the first material and the third material have a smaller grain size than the second material when the second material is deposited.

2. The method of claim 1 , wherein consolidating the second material comprises using one of hot isostatic pressing, hot pressing, electric current assisted sintering, cold isostatic pressing, dynamic consolidation, and magnetic compaction to consolidate the second material.

3. The method of claim 1 , wherein operating the consolidating device further comprises consolidating the first material to form a lattice structure.

4. The method of claim 3 , wherein depositing the first material and the third material onto a surface further comprises placing at least one mesh structure onto at least a portion of the first material and the third material.

5. The method of claim 1 , wherein the operating the consolidating device of the additive manufacturing system comprises directing an energy beam to generate a melt pool in a powdered material.

6. The method of claim 5 , wherein the powdered material comprises one or more of a metallic powder, a ceramic powder, a glass particle, or a polymer-based powder.

7. The method of claim 1 , wherein the first material and the third material are alloy-steel.

8. The method of claim 7 , wherein, as a result of the consolidation of the first material and the third material via the additive manufacturing system, the first material and third material comprise a first grain size.

9. The method of claim 8 , wherein the second material comprises a consolidated grain size that is greater than or equal to the first grain size after the second material is consolidated.

10. The method of claim 1 , wherein the second material comprises at least one of a cobalt alloy, a nickel alloy, and an iron alloy.

11. The method of claim 1 , wherein the first process results in the first section including a plurality of voids after the first material is consolidated.

12. The method of claim 11 , wherein the second material comprises a powder prior to consolidation that is deposited into the plurality of voids.

13. A method of fabricating a composite component, the method comprising:
forming a powder bed of a powdered material on a surface of an additive manufacturing system;
consolidating the powdered material using a first process facilitated by the additive manufacturing system to form a first section of the composite component and a third section of the composite component, wherein the first section comprising a plurality of first section unit cells joined together and the third section surrounds the first section;
depositing a second material within the first section such that the second material surrounds the plurality of first section unit cells; and
consolidating the second material using a second consolidation process different from the first process to form a second, solid section within the third section and within and surrounding each unit cell of the plurality of first section unit cells;
wherein the third section includes a third material, the powdered material and the third material are harder than the second material, and the powdered material and the third material have a smaller grain size than the second material when the second material is deposited.

14. The method of claim 13 , wherein consolidating the second material comprises using one of hot isostatic pressing, hot pressing, electric current assisted sintering, cold isostatic pressing, dynamic consolidation, and magnetic compaction to consolidate the second material.

15. The method of claim 13 , wherein the first process comprises directing an energy beam to generate a melt pool in the powdered material.

16. The method of claim 15 , wherein:
the powdered material comprises alloy-steel, and
wherein the second material comprises at least one of a cobalt alloy, a nickel alloy, and an iron alloy.

17. The method of claim 13 , wherein:
the first process results in the first section including a plurality of voids after the powdered material is consolidated, and
the second material comprises a powder prior to consolidation that is deposited into the plurality of voids.

18. A method of fabricating a composite component, the composite component comprising a first material, a second material, and a third material, said method comprising:
depositing the first material and the third material onto a surface of an additive manufacturing system; and
operating an energy beam source of the additive manufacturing system to consolidate the first material and the third material using a first process to form:
a first section comprising the first material, said first section comprising a plurality of first section unit cells joined together;
a third section comprising the third material, said third section surrounding the first section; and

depositing a second material within the first section such that the second material surrounds each unit cell of the plurality of first section unit cells; and
consolidating the second material using a second consolidation process different from the first process to form a second section surrounding each unit cell of the plurality of first section unit cells;
wherein the first material and the third material are harder than the second material, and the first material and the third material have a smaller grain size than the second material when the second material is deposited.

19. The method of claim 18 , wherein consolidating the second material comprises using one of hot isostatic pressing, hot pressing, electric current assisted sintering, cold isostatic pressing, dynamic consolidation, and magnetic compaction to consolidate the second material.

20. The method of claim 18 , further comprising consolidating the first material to form a lattice structure.

Assignees

• Gen Electric

Inventors

• Dozier Evan John
• Kelkar Rajendra Madhukar

Classifications

• B22F3/1115 Primary

  comprising complex forms, e.g. honeycombs · CPC title

• B22F1/052

  characterised by a mixture of particles of different sizes or by the particle size distribution · CPC title

• B22F3/156

  by a pressure medium in liquid or powder form · CPC title

• B22F12/44

  characterised by the configuration of the radiation means · CPC title

• B29C64/153

  using layers of powder being selectively joined, e.g. by selective laser sintering or melting · CPC title