Method of Using Core Shell Pre-Alloy Structure to Make Alloys in a Controlled Manner

Abstract

Disclosed herein are methods of combining at least one bulk-solidifying amorphous alloy and at least one additional metal or alloy of a metal to provide a composite preform. The composite preform then is heated to produce an alloy of the bulk-solidifying amorphous alloy and the at least one additional metal or alloy of the metal.

What is claimed is: 
     
         1 . A method of making an alloy, comprising:
 providing at least one bulk-solidifying amorphous alloy having a dimension less than or equal to its critical dimension and at least one metal or alloy of the metal that is different from the bulk-solidifying amorphous alloy;   and contacting the at least one bulk-solidifying amorphous alloy with the at least one metal or alloy of the metal to form a composite alloy preform;   heating the composite alloy preform to a temperature greater than the glass transition temperature and lower than the melting temperature of the bulk-solidifying amorphous alloy to form an alloy; and   cooling the alloy.   
     
     
         2 . The method of  claim 1 , further comprising subjecting the composite alloy preform to pressure while heating. 
     
     
         3 . The method of  claim 1 , wherein heating is carried out at a temperature of from about 100° C. to about 1,600° C. 
     
     
         4 . The method of  claim 4 , wherein heating is carried out at a temperature of from about 100° C. to about 750° C. 
     
     
         5 . The method of  claim 1 , wherein the at least one metal or alloy of the metal is a different bulk-solidifying amorphous alloy. 
     
     
         6 . The method of  claim 1 , wherein the at least one metal or alloy of the metal is selected from the group consisting of metals or alloys of aluminum, bismuth, cobalt, copper, gallium, gold, indium, iron, lead, magnesium, mercury, nickel, potassium, plutonium, rare earth alloys, rhodium, silver, titanium, tin, uranium, zinc, zirconium, and mixtures thereof. 
     
     
         7 . The method as claimed in  claim 1 , wherein the bulk-solidifying amorphous alloy is described by the following molecular formula: (Zr, Ti) a (Ni, Cu, Fe) b (Be, Al, Si, B) c , wherein “a” is in the range of from 30 to 75, “b” is in the range of from 5 to 60, and “c” is in the range of from 0 to 50 in atomic percentages. 
     
     
         8 . The method as claimed in  claim 1 , wherein the bulk-solidifying amorphous alloy is described by the following molecular formula: (Zr, Ti) a (Ni, Cu) b (Be) c , wherein “a” is in the range of from 40 to 75, “b” is in the range of from 5 to 50, and “c” is in the range of from 5 to 50 in atomic percentages. 
     
     
         9 . The method as claimed in  claim 1 , wherein the bulk solidifying amorphous alloy can sustain strains up to 1.5% or more without any permanent deformation or breakage. 
     
     
         10 . A method of making a core/shell composite alloy, comprising:
 providing at least one bulk-solidifying amorphous alloy having a dimension less than or equal to its critical dimension, providing at least one metal or alloy of the metal that is different from the bulk-solidifying amorphous alloy;   positioning the metal or alloy of the metal around at least a portion of the bulk-solidifying amorphous alloy to form a core/shell composite alloy preform;   heating the core/shell composite alloy preform to a temperature greater than the glass transition temperature and lower than the melting temperature of the bulk-solidifying amorphous alloy to form a core/shell composite alloy; and   cooling the core/shell composite alloy to form a core/shell amorphous alloyed article having at least an amorphous core.   
     
     
         11 . The method of  claim 10 , further comprising subjecting the core/shell composite alloy preform to pressure while heating. 
     
     
         12 . The method of  claim 10 , wherein heating is carried out at a temperature of from about 100° C. to about 750° C. 
     
     
         13 . The method of  claim 10 , wherein the at least one metal or alloy of the metal is a different bulk-solidifying amorphous alloy. 
     
     
         14 . The method of  claim 10 , wherein the at least one metal or alloy of the metal is selected from the group consisting of metals or alloys of aluminum, bismuth, cobalt, copper, gallium, gold, indium, iron, lead, magnesium, mercury, nickel, potassium, plutonium, rare earth alloys, rhodium, silver, titanium, tin, uranium, zinc, zirconium, and mixtures thereof. 
     
     
         15 . The method as claimed in  claim 10 , wherein the bulk-solidifying amorphous alloy is described by the following molecular formula: (Zr, Ti) a (Ni, Cu, Fe) b (Be, Al, Si, B) c , wherein “a” is in the range of from 30 to 75, “b” is in the range of from 5 to 60, and “c” is in the range of from 0 to 50 in atomic percentages. 
     
     
         16 . The method as claimed in  claim 10 , wherein the bulk-solidifying amorphous alloy is described by the following molecular formula: (Zr, Ti) a (Ni, Cu) b (Be) c , wherein “a” is in the range of from 40 to 75, “b” is in the range of from 5 to 50, and “c” is in the range of from 5 to 50 in atomic percentages. 
     
     
         17 . The method as claimed in  claim 10 , wherein the bulk solidifying amorphous alloy can sustain strains up to 1.5% or more without any permanent deformation or breakage. 
     
     
         18 . A method of making a core/shell composite alloy, comprising:
 providing at least one bulk-solidifying amorphous alloy having a dimension less than or equal to its critical dimension, providing at least one metal or alloy of the metal that is different from the bulk-solidifying amorphous alloy;   positioning the metal or alloy of the metal within at least a portion of the bulk-solidifying amorphous alloy to form a core/shell composite alloy preform;   heating the core/shell composite alloy preform to a temperature greater than the glass transition temperature and lower than the melting temperature of the bulk-solidifying amorphous alloy to form a core/shell composite alloy; and   cooling the core/shell composite alloy to form a core/shell amorphous alloyed article having at least an amorphous surface.   
     
     
         19 . A method of making an alloy comprising:
 providing at least one bulk-solidifying amorphous alloy having a dimension less than or equal to its critical dimension;   providing at least one metal or alloy of the metal that is different from the bulk-solidifying amorphous alloy;   contacting the at least one bulk-solidifying amorphous alloy with the at least one metal or alloy of the metal to form a composite alloy preform;   heating the composite alloy preform to a temperature greater than the melting temperature of the bulk-solidifying amorphous alloy to form an alloy; and   cooling the alloy in such a manner to avoid crystallization of the bulk-solidifying amorphous alloy, to form an alloy.