IP Library Granted Patent US 9,943,929
Granted Patent B2
US 9,943,929 · App. 15/489,389 · Granted Apr 17, 2018

Metal matrix composite creation

Inventors: Jeffrey Patrick Schultz (Blacksburg, VA); Kevin D. Creehan (Blacksburg, VA)
Assignee: AEROPROBE CORPORATION
B23K20/1215B23K20/1205B23K20/128B23K20/1245B23K20/1255C23C24/06
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 9,943,929
App. No.
15/489,389
Granted
Apr 17, 2018
Kind
B2
Abstract

The present invention relates to tooling and methods for disposing, coating, building up, repairing, or otherwise modifying the surface of a metal substrate using frictional heating and compressive loading of a consumable metal material against the substrate. Embodiments of the invention include friction-based fabrication tooling comprising a non-consumable member with a throat and a consumable member disposed in the throat, wherein the throat is operably configured such that during rotation of the non-consumable member at a selected speed, the throat exerts normal forces on and rotates the consumable member at the selected speed; and comprising means for dispensing the consumable member through the throat and onto a substrate using frictional heating and compressive loading. Embodiments of the invention also include fabrication methods using the tools described herein.

Claims (46)

1. A friction-based fabrication tool comprising:

a non-consumable member having a body and a throat;

a coating material disposed within the throat;

wherein the throat is shaped to exert a normal force on the coating material disposed therein along an entire length of the coating material disposed within the throat and imparts a rotation to the coating material from the body when rotated at a speed sufficient for imposing frictional heating of the coating material against a substrate;

wherein the body is operably connected with a downward force actuator which pushes the coating material through the throat of the non-consumable member resulting in frictional heating and compressive loading of the coating material onto the substrate and a motor for rotating and translating the body relative to the substrate; and

wherein the body comprises a surface for trapping coating material loaded on the substrate in a volume between the body and the substrate and for forming and shearing a surface of a coating on the substrate.

2. The tool of claim 1 , wherein the throat of the non-consumable member is shaped with a non-circular cross-sectional shape.

3. The tool of claim 2 , wherein the non-circular cross-sectional shape is a square, rectangle, ellipse, oval, triangle, non-circular polygon, star, daisy, key, or diamond.

4. The tool of claim 2 , wherein the throat of the non-consumable member is shaped to exert normal forces on a solid, powder, or powder-filled tube type coating material disposed therein.

5. The tool of claim 1 , wherein the throat of the non-consumable member is shaped to exert normal forces on a plurality of surfaces of the coating material disposed therein.

6. The tool of claim 5 , wherein the throat of the non-consumable member is shaped to exert normal forces on four or more surfaces of the coating material disposed therein.

7. The tool of claim 1 , wherein the frictional heating and compressive loading are of a degree sufficient to enable mixing of dispensed coating material with material of the substrate at a coating-substrate interface.

8. The tool of claim 1 , wherein the frictional heating and compressive loading are of a degree sufficient to enable coating of a wrought metal or metal matrix composite (MMC) material on a metal substrate with interfacial bonding.

9. The tool of claim 1 , wherein the frictional heating and compressive loading are of a degree sufficient to enable coating of a wrought metal or metal matrix composite (MMC) material on a polymer substrate with interfacial bonding.

10. The tool of claim 1 , wherein the frictional heating and compressive loading are of a degree sufficient to enable coating of a wrought metal or metal matrix composite (MMC) material on a ceramic substrate with interfacial bonding.

11. The tool of claim 1 , wherein the frictional heating and compressive loading are of a degree sufficient to enable local changes in the surface composition or large area substrate surface modification.

12. The tool of claim 1 , wherein the throat is shaped to enable fabrication of in-situ metal matrix composite (MMC) material with enhanced mechanical properties and its consequent deposition on the substrate.

13. The tool of claim 1 , wherein the frictional heating and compressive loading are of a degree sufficient to enable fabrication of Al—SiC coating with 10% SiC loading with improved hardness on Al-substrate.

14. The tool of claim 1 , wherein the frictional heating and compressive loading are of a degree sufficient to enable fabrication of Al—SiC coating with 10% SiC loading with improved ductility/toughness.

15. The tool of claim 1 , wherein the frictional heating and compressive loading are of a degree sufficient to enable metal matrix composite (MMC) coating with a homogenously dispersed ceramic phase into a metal phase.

16. The tool of claim 1 , wherein the frictional heating and compressive loading are of a degree sufficient to enable Ni—Al bronze coating with refined microstructure for extreme wear applications.

17. The tool of claim 1 , wherein the frictional heating and compressive loading are of a degree sufficient to enable coatings of Cu-alloys and steels with high interfacial bond strength and improved hardness.

18. The tool of claim 1 , wherein the frictional heating and compressive loading are of a degree sufficient to disperse any oxides and enable coatings with high interfacial bond strength due to low oxide content at a coating-substrate interface.

19. A friction-based fabrication tool comprising:

a spindle member comprising a hollow interior for housing a coating material disposed therein prior to deposition on a substrate;

a coating material disposed within the hollow interior;

wherein the interior of the spindle is shaped to exert a normal force on the coating material disposed therein along an entire length of the coating material disposed within the hollow interior and imparts a rotation to the coating material during rotation of the spindle at a speed sufficient for imposing frictional heating of the coating material against the substrate;

wherein the spindle is operably connected with a downward force actuator which pushes the coating material through the throat of the non-consumable member resulting in frictional heating and compressive loading of the coating material onto the substrate and a motor for rotating and translating the spindle relative to the substrate; and

wherein the spindle comprises a shoulder surface with a flat surface geometry or a surface geometry with spiral or other surface features, and/or surface nubs for enhancing mechanical stirring of the loaded coating material, which shoulder surface is operably configured for trapping the loaded coating material in a volume between the shoulder and the substrate and for forming and shearing a surface of a coating on the substrate.

20. The tool of claim 19 , wherein the interior of the spindle is shaped with a non-circular cross-sectional shape.

21. The tool of claim 20 , wherein the non-circular cross-sectional shape is a square, rectangle, ellipse, oval, triangle, non-circular polygon, star, daisy, key, or diamond.

22. The tool of claim 20 , wherein the interior of the spindle is shaped to exert normal forces on a solid, powder, or powder-filled tube type coating material disposed therein.

23. The tool of claim 19 , wherein the interior of the spindle is shaped to exert normal forces on a plurality of surfaces of the coating material disposed therein.

24. The tool of claim 23 , wherein the interior of the spindle is shaped to exert normal forces on four or more surfaces of the coating material disposed therein.

25. The tool of claim 19 , wherein the frictional heating, compressive loading, and mechanical stirring are of a degree sufficient to enable mixing of dispensed coating material with material of the substrate at a coating-substrate interface.

26. The tool of claim 19 , wherein the frictional heating and compressive loading are of a degree sufficient to enable coating of a wrought metal or metal matrix composite (MMC) material on a metal substrate with interfacial bonding.

27. The tool of claim 19 , wherein the frictional heating and compressive loading are of a degree sufficient to enable coating of a wrought metal or metal matrix composite (MMC) material on a polymer substrate with interfacial bonding.

28. The tool of claim 19 , wherein the frictional heating and compressive loading are of a degree sufficient to enable coating of a wrought metal or metal matrix composite (MMC) material on a ceramic substrate with interfacial bonding.

29. The tool of claim 19 , wherein the frictional heating and compressive loading are of a degree sufficient to enable local changes in the surface composition or large area substrate surface modification.

30. The tool of claim 19 , wherein the throat is shaped to enable fabrication of in-situ metal matrix composite (MMC) material with enhanced mechanical properties and its consequent deposition on the substrate.

31. The tool of claim 19 , wherein the frictional heating and compressive loading are of a degree sufficient to enable fabrication of Al—SiC coating with 10% SiC loading with improved hardness on Al-substrate.

32. The tool of claim 19 , wherein the frictional heating and compressive loading are of a degree sufficient to enable fabrication of Al—SiC coating with 10% SiC loading with improved ductility/toughness.

33. The tool of claim 19 , wherein the frictional heating and compressive loading are of a degree sufficient to enable metal matrix composite (MMC) coating with a homogenously dispersed ceramic phase into a metal phase.

34. The tool of claim 19 , wherein the frictional heating and compressive loading are of a degree sufficient to enable Ni—Al bronze coating with refined microstructure for extreme wear applications.

35. The tool of claim 19 , wherein the frictional heating and compressive loading are of a degree sufficient to enable coatings of Cu-alloys and steels with high interfacial bond strength and improved hardness.

36. The tool of claim 19 , wherein the frictional heating and compressive loading are of a degree sufficient to disperse any oxides and enable coatings with high interfacial bond strength due to low oxide content at a coating-substrate interface.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 11, 2019
From: AEROPROBE CORPORATION
To: MELD MANUFACTURING CORPORATION
Reel/Frame 050972/0010 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 5, 2018
From: SCHULTZ, JEFFREY PATRICK; CREEHAN, KEVIN D
To: AEROPROBE CORPORATION
Reel/Frame 044543/0207 →
Continuity (14)
Continuation 14926447 · Oct 29, 2015
Continuation 14159105 · Jan 20, 2014
Division 12987588 · Jan 10, 2011
Continuation In Part 13442201 · Apr 9, 2012
Continuation In Part 12792655 · Jun 2, 2010
Continuation In Part 12792655 · Jun 2, 2010
Continuation 11527149 · Sep 26, 2006
Continuation In Part 12792655 · Jun 2, 2010
Continuation In Part 12987588 · Jan 10, 2011
Provisional Application 61293543 · Jan 8, 2010
Provisional Application 60720521 · Sep 26, 2005
Provisional Application 61472918 · Apr 7, 2011
Provisional Application 61473221 · Apr 8, 2011
Related Publication 20170216962A1 · Aug 3, 2017