US2012192499A1PendingUtilityA1

Brazed Diamond Tools and Methods for Making the Same

Assignee: SUNG CHIEN-MINPriority: Aug 22, 2001Filed: Jan 31, 2012Published: Aug 2, 2012
Est. expiryAug 22, 2021(expired)· nominal 20-yr term from priority
Inventors:Chien-Min Sung
B24D 2203/00B01J 2203/0635C22C 2204/00B01J 2203/0655B01J 2203/061B01J 3/062B23P 15/28E21B 10/5676B01J 2203/0645B24D 18/00B23D 61/18B22F 2005/001B22F 2999/00B24D 7/066C22C 26/00B01J 2203/068B01J 2203/0685B24D 3/08B24D 99/005B01J 2203/062B01J 2203/066
60
PatentIndex Score
0
Cited by
0
References
0
Claims

Abstract

Superabrasive tools and methods for the making thereof are disclosed and described. In one aspect, superabrasive particles are chemically bonded to a matrix support material according to a predetermined pattern by a braze alloy. The brazing alloy may be provided as a powder, thin sheet, or sheet of amorphous alloy. A template having a plurality of apertures arranged in a predetermined pattern may be used to place the superabrasive particles on a given substrate or matrix support material.

Claims

exact text as granted — not AI-modified
1 . A method of making a superabrasive tool, comprising the steps of:
 a) providing a substrate; and   b) brazing a plurality of superabrasive particles directly to an exposed surface of the substrate in accordance with a predetermined pattern with a brazing alloy.   
     
     
         2 . The method of  claim 1 , wherein the brazing is accomplished using a brazing alloy that includes a material selected from the group consisting of titanium, vanadium, chromium, zirconium, molybdenum, tungsten, manganese, iron, silicon, aluminum and mixtures or alloys thereof. 
     
     
         3 . The method of  claim 2 , wherein the brazing alloy includes between about 2% and about 50% by weight of a material selected from the group consisting of chromium, manganese, titanium, silicon and aluminum. 
     
     
         4 . The method of  claim 3 , wherein the material is chromium. 
     
     
         5 . The method of  claim 1 , wherein the step of brazing includes heating the brazing alloy and substrate to a temperature of less than about 1,100° C. which is sufficient to braze the superabrasive particles directly to the substrate. 
     
     
         6 . The method of  claim 1 , wherein the braze alloy is a sheet of amorphous braze alloy. 
     
     
         7 . The method of  claim 1 , wherein prior to the step of brazing, the method further comprises the steps of:
 a) affixing the superabrasive particles in a predetermined pattern on an exposed surface of the substrate; and   b) applying the braze alloy to the substrate and the superabrasive particles.   
     
     
         8 . The method of  claim 1 , wherein prior to the step of brazing, the method further comprises the steps of:
 a) affixing the superabrasive particles in a predetermined pattern on a transfer sheet of amorphous braze alloy; and   b) applying the transfer sheet to the substrate.   
     
     
         9 . The method of  claim 1 , wherein the superabrasive particles are placed in a predetermined pattern. 
     
     
         10 . The method of  claim 9 , wherein the predetermined pattern is a uniform grid. 
     
     
         11 . A superabrasive tool comprising:
 a) a solid metal substrate;   b) a plurality of superabrasive particles; and   c) a layer of amorphous braze alloy chemically bonding the plurality of superabrasive particles to the solid metal substrate.   
     
     
         12 . The superabrasive tool of  claim 11 , wherein the brazing alloy includes a material selected from the group consisting of titanium, vanadium, chromium, zirconium, molybdenum, tungsten, manganese, iron, silicon and aluminum. 
     
     
         13 . The superabrasive tool of  claim 11 , wherein the brazing alloy includes between about 2% and 50% by weight of a material selected from the group consisting of chromium, manganese, titanium, silicon and aluminum. 
     
     
         14 . The superabrasive tool of  claim 11 , wherein bonding of the superabrasive particles avoids damage to the superabrasive particles. 
     
     
         15 . The superabrasive tool of  claim 11 , wherein superabrasive particles are oriented in a predetermined pattern. 
     
     
         16 . The superabrasive tool of  claim 15 , wherein the predetermined pattern consists of superabrasive particles positioned substantially along an exterior edge of the superabrasive tool. 
     
     
         17 . The superabrasive tool of  claim 15 , wherein the predetermined pattern comprises an exterior portion concentration of superabrasive particles that is higher than an interior portion concentration of superabrasive particles. 
     
     
         18 . The superabrasive tool of  claim 15 , wherein the predetermined pattern is a uniform grid. 
     
     
         19 . The super abrasive tool of  claim 11 , further comprising a layer of overlay material affixed to a working surface of the brazing alloy to create a smooth working surface. 
     
     
         20 . A superabrasive tool precursor comprising:
 a) a metal support matrix;   b) a plurality of superabrasive particles placed on the metal support matrix; and   c) a layer of amorphous braze alloy placed in contact with either the plurality of superabrasive particles or the metal support matrix.

Join the waitlist — get patent alerts

Track US2012192499A1 — get alerts on status changes and closely related new filings.

We store only your email — no account needed. See our privacy policy.