Claims
- 1. A reciprocating frame saw blade for cutting a workpiece, comprising:
a) a blade member having a concave cutting edge; and b) a plurality of superabrasive tool segments brazed along the cutting edge of the blade member.
- 2. The reciprocating frame saw blade of claim 1, wherein the blade member is steel.
- 3. The reciprocating frame saw blade of claim 1, wherein the blade member is flexible, and the concave configuration of the cutting edge is a result of the flexibility.
- 4. The reciprocating frame saw blade of claim 1, wherein the superabrasive tool segments further comprise:
a plurality of substrate layers arranged in a substantially parallel relationship, each layer having a plurality of superabrasive particles bonded thereto.
- 5. A saw blade for cutting a workpiece, comprising:
a) a blade member; and b) a plurality of superabrasive tool segments, each brazed along a cutting edge and at least a portion of each side of the blade member.
- 6. The saw blade of claim 5, wherein the widths of the plurality of superabrasive tool segments are substantially uniform.
- 7. The saw blade of claim 6, wherein the widths of the plurality of superabrasive tool segments are substantially equal to the width of the blade member.
- 8. The saw blade of claim 7, wherein the widths of the plurality of superabrasive tool segments vary from one another.
- 9. The saw blade of claim 7, wherein the superabrasive tool segments further comprise:
a plurality of substrate layers arranged in a substantially parallel relationship, each matrix layer having a plurality of superabrasive particles bonded thereto.
- 10. A superabrasive tool segment for use in a saw blade comprising:
a plurality of substrate layers arranged in a substantially parallel relationship, each layer having a plurality of superabrasive particles bonded thereto.
- 11. The superabrasive tool segment of any of claims 4, 9, or 10, wherein the superabrasive particles are chemically bonded with a brazing alloy.
- 12. The superabrasive tool segment of any of claims 4, 9, or 10, wherein the superabrasive tool segment has a porosity of at least about 5%.
- 13. The superabrasive tool segment of claim 12, wherein the porosity is at least about 10%.
- 14. The superabrasive tool segment of claim 11, wherein the brazing alloy is provided as a layer of amorphous braze alloy between the diamond particles and the substrate layers.
- 15. The superabrasive tool segment of claim 11, wherein the brazing alloy is provided as a solidified coating of molten braze alloy on each superabrasive particle.
- 16. The superabrasive tool segment of claim 11, wherein the brazing alloy is provided as a powder in communication with the superabrasive particles and the substrate layers.
- 17. The superabrasive tool segment of any of claims 4, 9, or 10, wherein the plurality of substrate layers have a width that is sufficient to allow an uncut ridge in a kerf to crumble to swarf.
- 18. The superabrasive tool segment of claim 17, wherein the width of the substrate layers is less than about 1 mm.
- 19. The superabrasive tool segment of claim 17, wherein the width of the substrate layers is about 0.5 mm.
- 20. The superabrasive tool segment of any of claims 4, 9, or 10, wherein the plurality of substrate layers comprise a material selected from the group consisting essential of: cobalt, nickel, iron, copper, carbon, tungsten, tungsten carbide, steel, stainless steel, bronze, and mixtures thereof.
- 21. The superabrasive tool segment of claim 20, wherein the substrate layer material is copper.
- 22. A method of making a superabrasive tool saw segment as recited in any of claims 4, 9, or 10, comprising the steps of:
a) providing a plurality of substrate layers; b) arranging superabrasive particles on the substrate layers; c) assembling, or placing the substrate layers in a substantially parallel relationship; and d) chemically bonding the superabrasive particles to the substrate layers with a brazing alloy, such that the segment receives a porosity of at least about 5%.
PRIORITY INFORMATION
[0001] This application is a continuation-in-part of U.S. patent application Ser. No. 09/935,204, filed Aug. 22, 2001, which is a continuation-in-part of U.S. patent application Ser. No. 09/399,573, filed Sep. 20, 1999, now issued as U.S. Pat. No. 6,286,498, which is a continuation-in-part application of U.S. patent application Ser. No. 08/835,117, filed Apr. 4, 1997, now issued as U.S. Pat. No. 6,039,641, and of U.S. patent application Ser. No. 08/832,852, filed Apr. 4, 1997, now abandoned, all of which are incorporated herein by reference.
[0002] This patent application is also a continuation-in-part of U.S. patent application Ser. No. 10/109,531 filed Mar. 27, 2002, which is a continuation-in-part of U.S. patent application Ser. No. 09/588,582 filed Apr. 26, 2000, now issued as U.S. Pat. No. 6,368,198, which is a continuation-in-part of U.S. patent application Ser. No. 09/447,620 filed Nov. 22, 1999, now abandoned, all of which are incorporated herein by reference.
Continuation in Parts (7)
|
Number |
Date |
Country |
Parent |
09935204 |
Aug 2001 |
US |
Child |
10627448 |
Jul 2003 |
US |
Parent |
09399573 |
Sep 1999 |
US |
Child |
09935204 |
Aug 2001 |
US |
Parent |
08835117 |
Apr 1997 |
US |
Child |
09399573 |
Sep 1999 |
US |
Parent |
08832852 |
Apr 1997 |
US |
Child |
09399573 |
Sep 1999 |
US |
Parent |
10109531 |
Mar 2002 |
US |
Child |
10627448 |
Jul 2003 |
US |
Parent |
09558582 |
Apr 2000 |
US |
Child |
10109531 |
Mar 2002 |
US |
Parent |
09447620 |
Nov 1999 |
US |
Child |
09558582 |
Apr 2000 |
US |