Claims
- 1. A method of forming a cutting tool comprising:
- (a) forming a cutting tool base having a metal portion thereof which is operable to be formed with a cutting edge,
- (b) scanning said portion of said tool base with an intense radiation beam in a manner to remove material from said base and to form a cutting edge along the portion of said base from which said material is removed,
- (c) transferring a portion of the heat of said radiation beam to the material of said cutting tool to melt a select portion of said material adjacent said cutting edge of said tool, and
- (d) rapidly cooling at least a portion of the melted material in a manner to form a layer of non-crystalline metal of high wear resistence adjacent said cutting edge.
- 2. A method in accordance with claim 1 wherein said scanning step is effected by means of an intense light beam generated by a laser.
- 3. A method in accordance with claim 1 wherein said scanning step is effected by means of an intense electron beam generated by an electron gun.
- 4. A method in accordance with claim 1 including implantating ions with said radiation beam in a select portion of the material of said cutting tool to improve the wear resistance of the cutting tool.
- 5. A method in accordance with claim 1 wherein the noncrystalline metal formed on said cutting tool base is formed so as to define the cutting edge of said tool.
- 6. A method in accordance with claim 1 including depositing a hard surfacing material on said cutting tool base to form said metal portion to be formed thereafter with said cutting edge.
- 7. A method in accordance with claim 1 including depositing a plurality of layers of metal, one above the other on said base and forming the cutting edge portion of said tool of said plurality of layers.
- 8. A method in accordance with claim 7 wherein each of said layers of metal deposited one above the other on said base is formed in and retains a non-crystalline structure.
- 9. A method in accordance with claim 1 wherein steps (b) to (d) are performed while said tool base is supported by a machine in a tool holder.
- 10. A method in accordance with claim 1 wherein steps (b) to (d) are performed while said tool base is supported by a tool holder supported by a machien operable to use said cutting tool in cutting work.
- 11. A method in accordance with claim 10 wherein said tool base contains a cutting edge portion requiring sharpening, step (b) to (b) being operable to sharpen said cutting edge while said tool base is supported in a tool holder which is operatively supported by said machine for use in cutting material.
- 12. A method in accordance with claim 10 wherein steps (b) to (d) are performed while said cutting tool is operating.
- 13. A method in accordance with claim 1 wherein said cutting tool is supported by a machine and step (b) to (d) are performed while the machine is not operating.
- 14. A method in accordance with claim 1 wherein said tool is a composite structure formed of a substrate with a coating of metal secured to at least a portion of said substrate, which metal coating is crystalline in structure, said method including converting at least a portion of the metal coating said substrate to said amorphous metal by rendering at least a portion thereof molten and rapidly cooling the molten metal.
- 15. A method in accordance with claim 14 wherein said heating is effected by scanning a select portion of the surface of said article with a high intensity radiation beam and the rapid cooling of the molten portion of said metal is effected by directing a stream of cooling fluid against that portion of the surface said article immediately rendered molten by said radiation beam to rapidly cool and solidify the metal shortly after it is rendered molten by said beam.
CROSS REFERENCE TO RELATED APPLICATIONS
This is a continuation-in-part of Ser. No. 674,933 filed 11/26/84 and a continuation-in-part of Ser. No. 364,497 filed 4/1/82 and a continuation-in-part of Ser. No. 167,672 filed 7/11/80, all now abandoned.
US Referenced Citations (4)
Continuation in Parts (1)
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Number |
Date |
Country |
Parent |
674933 |
Nov 1984 |
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