Metal matrix composite having improved microstructure and the process for making the same
Abstract
The microstructure of a metal matrix composite comprising copper and reinforcement material is improved when the metal matrix composite comprises at least about 0.02% by weight of at least one of silver and gold. In one embodiment, the process for making a metal matrix composite comprises compacting powder particles of a reinforcement material to form a green compact, sintering the green compact to produce a porous skeletal body and infiltrating the porous skeletal body with an infiltrant comprising copper and at least about 0.1% of at least one of silver and gold, based on the weight of infiltrant. In another embodiment, the process comprises forming a mixture of particles of reinforcement material, copper and at least about 0.02% by weight of at least one of silver and gold, compacting the mixture to form a green compact, and sintering the green compact to form a near net shape metal matrix composite. The metal matrix composite has a more uniform microstructure along its cross-section and increased density, thereby providing for improved physical and thermal properties.
Claims
exact text as granted — not AI-modifiedWe claim:
1 . A process for making a metal matrix composites comprising:
compacting powder particles of reinforcement material to obtain a green compact; sintering the green compact to obtain a porous skeletal body; and infiltrating the porous skeletal body with an infiltrant comprising copper and at least about 0.1% of silver or gold, based on the weight of the infiltrant, to obtain a near net shape matrix metal composite.
2 . The process of claim 1 wherein the infiltrant comprises at least about 0.1% of silver or gold based on the weight of the infiltrant.
3 . The process of claim 1 wherein the infiltrant comprises silver and the silver is present in the form of a copper-silver alloy.
4 . The process of claim 3 wherein the copper-silver alloy comprises from about 10% to about 40% by weight copper with the remainder being substantially silver.
5 . The process of claim 3 wherein the copper-silver alloy is a copper-silver eutectic composition.
6 . The process of claim 1 wherein:
the infiltrant comprises gold and the gold is present in the form of a copper-gold alloy.
7 . The process of claim 6 wherein the copper-gold alloy comprises from about 10% to about 40% by weight copper with the remainder being substantially gold.
8 . The process of claim 6 wherein the copper-gold alloy is a copper-gold eutectic composition.
9 . The process of claim 1 wherein:
the infiltrant comprises at least about 0.3% silver present in the form of copper-silver alloy, based on the weight of infiltrant, with the remainder of the infiltrant being substantially copper.
10 . The process of claim 1 wherein the reinforcement material has a melting temperature of at least about 1180° C.
11 . The process of claim 1 wherein the reinforcement material is selected from the group consisting of tungsten, molybdenum, iron-nickel alloy, Invar®, iron-nickel-cobalt alloy, Kovar®, tantalum, chromium, osmium, ruthenium, rhenium, rhodium, hafnium, zirconium, nickel, iron, cobalt, titanium, titanium carbide, tungsten carbide, tantalum carbide, chromium carbide, silicon carbide, beryllium oxide, aluminum oxide, boron nitride, aluminum nitride, silicon nitride and mixtures thereof.
12 . The process of claim 1 wherein the reinforcement material is at least one of tungsten and molybdenum.
13 . The process of claim 1 wherein the particles of reinforcement material have a mean particle size ranging from about 2 microns to about 20 microns.
14 . The process of claim 1 wherein the particles of reinforcement material are compacted to form green compact having a density that ranges from about 50% to about 95% of theoretical density.
15 . The process of claim 1 wherein the green compact is sintered in a gas atmosphere comprising hydrogen and having a dew point of at least about 0° C.
16 . The process of claim 15 wherein the green compact is sintered at a temperature ranging from about 1400° C. to about 1500° C. for about 0.5 hours to about 2 hours.
17 . The process of claim 1 wherein the porous skeletal body produced upon sintering has a density ranging from about 50% to about 95% of theoretical density.
18 . The process of claim 1 wherein the porous skeletal body is infiltrated in a gas atmosphere having a dew point of about 10° C. or less.
19 . The process of claim 1 wherein the porous skeletal body is infiltrated at a temperature ranging from about 1100° C. to about 1500° C.
20 . The process of claim 1 wherein the near net shape metal matrix composite comprises from about 5% to about 50% copper, from about 50% to about 95% reinforcement material, and at least about 0.05% by weight of silver.
21 . The process of claim 1 wherein the powder particles of the reinforcement material are mixed with powder particles of copper before being compacted to form a green compact.
22 . The process of claim 1 wherein the powder particles of the reinforcement material are mixed with powder particles of silver before being compacted to form a green compact prior to sintering the green compact.
23 . A process for making a matrix metal composites comprising:
compressing powder particles of a reinforcement material to obtain a green compact; sintering the green compact to obtain a porous skeletal body; and infiltrating the porous skeletal body with an infiltrant comprising copper and at least about 0.1% of silver or gold, based on the weight of the infiltrant, in the form of a copper-silver alloy, the silver being in form of a copper-silver alloy and the gold being in the form of a copper-gold alloy, to obtain a near net shape matrix metal composite.
24 . The process of claim 23 wherein:
the reinforcement material is selected from the group consisting of tungsten, molybdenum, iron-nickel alloy, Invar®, iron-nickel-cobalt alloy, Kovar®, tantalum, chromium, osmium, ruthenium, rhenium, rhodium, hafnium, zirconium, nickel, iron, cobalt, titanium, titanium carbide, tungsten carbide, tantalum carbide, chromium carbide, silicon carbide, beryllium oxide, aluminum oxide, boron nitride, aluminum nitride and silicon nitride and mixtures thereof;
the infiltrant comprises at least about 0.1% copper-silver alloy, based on the weight of infiltrant, with the remainder of the infiltrant being copper; and
the copper-silver alloy comprises, by weight, from about 60% to about 90% silver with the remainder being substantially copper.
25 . The process of claim 24 wherein the copper-silver alloy is the eutectic composition.
26 . The process of claim 25 wherein the reinforcement material is tungsten or molybdenum.
27 . The process of claim 23 wherein:
the reinforcement material is selected from the group consisting of tungsten, molybdenum, iron-nickel alloy, Invar®, iron-nickel-cobalt alloy, Kovar®, tantalum, chromium, osmium, ruthenium, rhenium, rhodium, hafnium, zirconium, nickel, iron, cobalt, titanium, titanium carbide, tungsten carbide, tantalum carbide, chromium carbide, silicon carbide, beryllium oxide, aluminum oxide, boron nitride, aluminum nitride, silicon nitride and mixtures thereof; and
the infiltrant comprises at least about 0.1% copper-gold alloy, based on the weight of infiltrant, with the remainder being copper; and
the copper-gold alloy comprises, by weight, from about 60% to about 90% gold with the remainder being substantially copper.
28 . The process of claim 26 wherein the copper-gold alloy is the eutectic composition.
29 . The process of claim 28 wherein the reinforcement material is tungsten or molybdenum.
30 . The process of claim 23 wherein:
the green compact is sintered in a gas atmosphere comprising hydrogen and having a dew point of at least about 0° C. to produce a porous skeletal body having a density ranging from about 50% to about 95% of theoretical density.
31 . The process of claim 23 wherein:
the porous skeletal body is infiltrated in a gas atmosphere having a dew point of about 10° C. or less.
32 . The process of claim 31 wherein the porous skeletal body is infiltrated at a temperature ranging from about 1100° C. to about 1500° C.
33 . The process of claim 31 wherein:
the infiltrant comprises at least about 0.1% silver in the form of copper-silver alloy, based on the weight of infiltrant, the copper-silver alloy comprising, by weight, from about 60% to about 90% silver and the remainder being substantially copper; and
the near net shape metal matrix composite comprises, by weight, from about 5% to about 50% copper, from about 50% to about 95% reinforcement material, and at least about 0.02% silver.
34 . The process of claim 31 wherein:
the infiltrant comprises from about 0.3% to about 20% silver in the form of copper-silver alloy, based on the weight of infiltrant, the copper-silver alloy comprising, by weight, from about 60% to about 90% silver and the remainder being substantially copper; and
the near net shape metal matrix composite comprises, by weight, from about 10% to about 20% copper, from about 70% to about 90% reinforcement material, and from about 0.03% to about 10% silver; and
the reinforcement material is tungsten or molybdenum.
35 . A process for making a metal matrix composites comprising:
forming a mixture comprising, by weight, from about 5% to about 50% copper, from about 50% to about 95% reinforcement material, and at least about 0.02% of at least one of silver in the form of a copper-silver alloy or gold in the form of a copper-gold alloy, to form a mixture; compressing the mixture to obtain a green compact; and sintering the green compact to obtain a near net shape matrix metal composite.
36 . The process of claim 35 wherein:
the mixture comprises from about 0.03% to about 10% by weight silver in the form of a copper-silver alloy composition, wherein copper-silver alloy composition comprises from about 10% to about 40% copper and from about 60% to about 90% silver;
the reinforcement material is selected from the group consisting of tungsten, molybdenum, iron-nickel alloy, Invar®, iron-nickel-cobalt alloy, Kovar®, tantalum, chromium, osmium, ruthenium, rhenium, rhodium, hafiium, zirconium, nickel, iron, cobalt, titanium, titanium carbide, tungsten carbide, tantalum carbide, chromium carbide, silicon carbide, beryllium oxide, aluminum oxide, boron nitride, aluminum nitride, silicon nitride and mixtures thereof; and
the green compact is sintered in a gas atmosphere comprising hydrogen and having a dew point of at least about 0° C.
37 . The process of claim 35 wherein:
the mixture comprises from about 0.03% to about 10% by weight gold in the form of a copper-gold alloy composition, wherein the copper-gold alloy composition comprises from about 10% to about 40% copper and from about 90% to about 60% gold;
the reinforcement material is selected from the group consisting of tungsten, molybdenum, iron-nickel alloy, Invar®, iron-nickel-cobalt alloy, Kovar®, tantalum, chromium, osmium, ruthenium, rhenium, rhodium, hafnium, zirconium, nickel, iron, cobalt, titanium, titanium carbide, tungsten carbide, tantalum carbide, chromium carbide, silicon carbide, beryllium oxide, aluminum oxide, boron nitride, aluminum nitride, silicon nitride and mixtures thereof; and
the green compact is sintered in a gas atmosphere comprising hydrogen and having a dew point of at least about 0° C.
38 . A metal matrix composite comprising, by weight:
at least about 0.03% silver or gold; from about 5% to about 50% copper; and from about 50% to about 95% reinforcement material.
39 . The metal matrix composite of claim 38 wherein the metal matrix composite comprises from about 0.03% to about 10% by weight silver.
40 . The metal matrix composite of claim 38 wherein the metal matrix composite comprises from about 0.03% to about 10% by weight gold.
41 . The metal matrix composite of claim 38 wherein the reinforcement material has a melting point of at least about 100° C. greater than the melting point of copper.
42 . The metal matrix composite of claim 38 wherein the reinforcement material is selected from the group consisting of:
tungsten, molybdenum, iron-nickel alloy, Invar®, iron-nickel-cobalt alloy, Kovar®, tantalum, chromium, osmium, ruthenium, rhenium, rhodium, hafnium, zirconium, nickel, iron, cobalt, titanium, titanium carbide, tungsten carbide, tantalum carbide, chromium carbide, silicon carbide, beryllium oxide, aluminum oxide, boron nitride, aluminum nitride, silicon nitride and mixtures thereof.
43 . The metal matrix composite of claim 38 wherein the metal matrix composite comprises from about 0.05% to about 5% by weight silver.
44 . The metal matrix composite of claim 38 wherein the metal matrix composite comprises from about 0.05% to about 5% by weight gold.
45 . The metal matrix composite of claim 38 wherein the metal matrix composite comprises by weight:
from about 0.05% to about 5% silver;
from about 10% to about 30% copper; and
from about 70% to about 90% reinforcement material.
46 . The metal matrix composite of claim 38 wherein the metal matrix composite comprises by weight:
from about 0.05% to about 5% gold;
from about 10% to about 30% copper; and
from about 70% to about 90% reinforcement material.
47 . The metal matrix composite of claim 45 wherein the reinforcement material comprises at least one of tungsten and molybdenum.
48 . The metal matrix composite of claim 46 wherein the reinf orcement material comprises at least one of tungsten and molybdenum.
49 . The metal matrix composite of claim 45 further comprising gold.
50 . The metal matrix composite of claim 46 further comprising silver.Join the waitlist — get patent alerts
Track US2003217828A1 — get alerts on status changes and closely related new filings.
We store only your email — no account needed. See our privacy policy.