초록

The present invention is directed to a method of joining an amorphous material to a non-amorphous material including, forming a cast mechanical joint between the bulk solidifying amorphous alloy and the non-amorphous material.

대표청구항 ▼

1. A method of joining a bulk-solidifying amorphous alloy material to a non-amorphous metal material wherein the melting temperature of the bulk-solidifying amorphous alloy material is higher than the melting temperature of the non-amorphous material, comprising:providing a pre-formed piece, wherein

1. A method of joining a bulk-solidifying amorphous alloy material to a non-amorphous metal material wherein the melting temperature of the bulk-solidifying amorphous alloy material is higher than the melting temperature of the non-amorphous material, comprising:providing a pre-formed piece, wherein the pre-formed piece is made of the bulk-solidifying amorphous alloy material;casting a second piece at a casting temperature in a joining relationship with said pre-formed piece to form a single integral article, wherein the second piece is made of the non-amorphous metal material, and wherein the casting temperature is greater than the melting temperature of the non-amorphous metal material; andcooling the single integral article at a rate sufficient to ensure that the bulk-solidifying amorphous alloy material remains substantially amorphous. 2. The method as described in claim 1, wherein a heat sink is further provided to maintain the temperature of the preformed piece below the glass transition temperature of the bulk-solidifying amorphous alloy. 3. A method of joining a bulk-solidifying amorphous alloy material to a non-amorphous metal material, comprising:providing a pre-farmed piece, wherein the pre-formed piece is made of a bulk-solidifying amorphous alloy material;casting a second piece from a non-amorphous material at a casting temperature above the melting temperature of the non-amorphous material in a joining relationship with said pro-formed piece; andcooling the second piece at a rate at least about the critical cooling rate of the bulk-solidifying amorphous alloy material to form a single integral article. 4. The method as described in claim 3 wherein the bulk-solidifying amorphous alloy material is described by the equation: a (Ni,Cu,Fe) b (Be,Al,Si,B) c where a is in the range of from about 30 to about 75, b is in the range of from about 5 to about 60, and c is in the range of from 0 to about 50, in atomic percentages. 5. The method as described in claim 4, wherein the bulk-solidifying amorphous alloy material includes up to about 20 atomic percent of at least one additional transition metal. 6. The method as described in claim 3, wherein the bulk-solidifying amorphous alloy material is described by the equation: d (Ni, Cu) e (Be) f where d is in the range of from about 40 to about 75, e is in the range of from about 5 to about 60, and f is in the range of from about 5 to about 50, in atomic percentages. 7. The method as described in claim 3, wherein the bulk-solidifying amorphous alloy material is described by the equation: a (Nb,Ti) b (Ni,Cu) c (Al) d ,where a is in the range of from 45 to 65, b is in the range of from 0 to 10, c is in the range of from 20 to 40 and d in the range of from 7.5 to 15 in atomic percentages. 8. The method as described in claim 3, wherein the non-amorphous material is selected from the group consisting at aluminum alloys, magnesium alloys, and copper alloys. 9. The method as described in claim 3, wherein the non-amorphous material is selected from the group consisting of: steels, nickel alloys, titanium alloys, and copper alloys. 10. The method as described in claim 3, wherein the pre-formed and second pieces are designed to mechanical interlock in the single integral article. 11. The method as described in claim 3, wherein the preformed piece is cooled at a rate at least about twice the critical cooling rate of the bulk-solidifying amorphous alloy material. 12. The method as described in claim 3, wherein the step of cooling includes actively quenching both the preformed and second pieces. 13. The method as described in claim 3, wherein the rate of cooling is about 500 K/sec or less. 14. The method as described in claim 3, wherein the step of casting is selected from the group consisting of: injection casting, die casting, and mold casting. 15. The method as described in claim 3, wherein the melting temperature of the material being cast is less than the melting temperature of the material in the preformed piece. 16. An article made in accordance with the method described in claim 3. 17. The article as described in claim 16, wherein the preformed and second pieces mechanically interlock to form a single integral piece.