Fabrication of laminate tooling using closed-loop direct metal deposition

• US 20020165634A1
• Filed: 04/03/2002
• Published: 11/07/2002
• Est. Priority Date: 03/16/2000
• Status: Abandoned Application

• Current Assignee: The POM Group
• Original Assignee: The POM Group
• Inventors: Skszek, Timothy W.
• Application Number:
  US10/116,197
• Publication Number:
  US 20020165634A1
• Time in Patent Office: Days
• US Class Current: 700/118
• CPC Class Codes: B23K 2101/20 Tools
• CPC Class Codes: B23K 2103/04 Steel or steel alloys
• CPC Class Codes: B23K 2103/10 Aluminium or alloys thereof
• CPC Class Codes: B23K 2103/12 Copper or alloys thereof
• CPC Class Codes: B23K 2103/18 Dissimilar materials
• CPC Class Codes: B23K 2103/26 Alloys of Nickel and Cobalt and Chromium
• CPC Class Codes: B23K 2103/50 Inorganic material, e.g. metals, not provided for in B23K2103/02 – B23K2103/26
• CPC Class Codes: B23K 26/32 taking account of the properties of the material involved
• CPC Class Codes: B23K 26/34 Laser welding for purposes other than joining
• CPC Class Codes: B29C 33/3828 Moulds made of at least two different materials having different thermal conductivities
• CPC Class Codes: B29C 33/56 Coatings , e.g. enameled or galvanised; Releasing, lubricating or separating agents in-mould coating B29C37/0028; using or applying separating agents B29C37/0067
• CPC Class Codes: B29C 45/37 Mould cavity walls , i.e. the inner surface forming the mould cavity, e.g. linings
• CPC Class Codes: B29C 45/7312 Construction of heating or cooling fluid flow channels

Abstract

A laser-assisted, direct metal deposition (DMD^tm), preferably in a closed-loop arrangement, is used to fabricate designed articles and components such as molds and tools with improved properties. A laminate substrate or structure is provided having a surface onto which a layer of a material is deposited having the desired characteristic using the laser-assisted DMD process. In different embodiments, the substrate/layer combination may be tailored for improved wear resistance, thermal conductivity, density/hardness, corrosion and/or resistance to corrosion, oxidation or other desirable effects. Alternatively, the layer of material may be tailored to have a phase which is different from that of the substrate. In particular, the layer material itself may be chosen to promote a phase which is different from that of the substrate. To enhance throughput, the outer layer(s) of material may be fabricated using a robotic closed-loop DMD arrangement. In concert with the improvements made possible through the laminate fabrication method, tailored outer layer(s), the method may further include the step of incorporating one or more conformal cooling channels within the component or the formation of one or more conductive heat sinks or thermal barriers during the DMD fabrication of the component itself.

Claims

1. A method of fabricating a component having improved properties, comprising the steps of:

a) providing a laminated substrate having a surface; and

b) depositing a layer of a material having a desired characteristic onto at least a portion of the surface of the laminate substrate using a laser-assisted direct metal deposition process.

2. The method of claim 1, wherein the layer of material exhibits improved wear or abrasion resistance relative to the laminate substrate.

3. The method of claim 1, wherein the layer of material has a thermal conductivity different from than that of the substrate.

4. The method of claim 1, wherein the layer of material exhibits improved elevated temperature material properties as compared to the laminate substrate.

5. The method of claim 1, wherein the layer of material has a different density than that of the substrate.

6. The method of claim 1, wherein the layer of material is more resistant to corrosion than the substrate.

7. The method of claim 1, wherein the layer of material is more resistant to oxidation than the substrate.

8. The method of claim 1, wherein the layer of material has a phase which is different from that of the substrate.

9. The method of claim 8, further including the step of choosing the material of the layer to promote a phase which is different from that of the substrate.

10. The method of claim 1, further including the step of dissolving a low-solubility material into the layer of material to enhance hardness, toughness, corrosion or oxidation resistance.

11. The method of claim 1, wherein the laminate substrate is itself fabricated using a direct metal deposition process.

12. The method of claim 1, wherein the laminate substrate and layer form part of a die, mold or other tool.

13. The method of claim 1, further including the step of robotically applying the layer of material.

15. The method of claim 14, wherein the desired property is greater wear resistance.

16. The method of claim 14, wherein the desired property is a higher or lower thermally conductivity.

17. The method of claim 14, wherein the desired property is greater density.

18. The method of claim 14, wherein the desired property is increased resistance to corrosion.

19. The method of claim 14, wherein the desired property is greater resistance to oxidation.

20. The method of claim 14, wherein the layer of material has a phase which is different from that of the underlying laminate structure.

21. The method of claim 20, further including the step of choosing the material of the layer to promote a phase which is different from that of the substrate.

22. The method of claim 14, further including the step of dissolving a low solubility substance into the layer of material to enhance hardness, toughness, corrosion, or oxidation resistance.

23. The method of claim 14, wherein the component is a die, mold or other tool.

24. The method of claim 14, further including the step of applying the layer of material using a robotic closed-loop DMD arrangement.

25. The method of claim 14, further including the step of incorporating one or more conformal cooling channels within the component during its fabrication.

27. The method of claim 14, further including the step of incorporating one or more conductive heat sinks or thermal barriers during its fabrication.

14. A method of fabricating a component having improved properties, comprising the steps of:

a) providing a computer-aided design (CAD) description of the component to be fabricated;

b) using a laser-assisted, direct metal deposition (MD) process to fabricate a laminate structure in accordance with the CAD description; and

c) completing the component by depositing a layer of a material onto the structure using a laser-assisted, direct metal deposition (DMD) process, the layer of material providing at least one desired property when compared to the underlying laminate structure.