Dispersion Strengthened Cobalt-Chromium-Molybdenum Alloy Produced by Gas Atomization

1. A high strength, corrosion-resistant, high temperature stable, consolidated, biocompatible, ductile alloy having homogeneously distributed dispersed oxides and fine, equiaxed grain structure after high temperature exposure, said alloy being produced by gas atomization and consisting essentially of the following percentage composition by weight: chromium 26 to 30 molybdenum 5 to 7 manganese 0 to 1 silicon 0 to 1 iron 0 to 0.75 nickel 0 to 1.0 carbon 0 to 0.35 nitrogen 0 to 0.25 oxygen 0.003 to 0.20 oxide-forming metal 0.003 to 2.0 ______________________________________ and the balance cobalt, apart from trace amounts of incidental impurities; in which the oxide-forming metal is a metal selected from the group consisting of magnesium, calcium, aluminum, yttrium, lanthanum, titanium and zirconium, which forms high temperature-stable, non-accretive, fine oxide particles which oxide has a free energy of formation greater than the oxide of the matrix metal and is homogeneously distributed in the dispersed phase; and said alloy after fabrication by gas atomization, thermomechanical processing and further high temperature exposure has an ultimate tensile strength of 160-200 k.s.i., a 0.2% offset yield strength of 75-100 k.s.i., an elongation of 37 to 60%, and a fatigue strength at 10.sup.7 cycles (Rotating Ream) of 70-95 k.s.i.

2. An alloy according to claim 1, in which the oxide-forming metal is aluminum, lanthanum or a mixture thereof.

3. An alloy according to claim 2, in which the percentage composition by weight is: chromium 26.47-27.27 molybdenum 5.50-6.01 manganese 0.73-0.78 silicon 0.70-0.71 iron 0.066-0.520 nickel 0.002-0.187 carbon 0.09-0.11 nitrogen 0.10-0.25 oxygen 0.0035-0.016 aluminum 0.40-0.81 lanthanum 0-0.15 ______________________________________ and the balance cobalt, apart from trace amounts of incidental impurities.

4. An alloy according to claim 2, in which the percentage composition by weight is: chromium 27.24 molybdenum 5.97 manganese 0.74 silicon 0.71 iron 0.215 nickel 0.053 carbon 0.09 nitrogen 0.21 oxygen 0.0038 aluminum 0.45 lanthanum 0.022 ______________________________________ and the balance cobalt, apart from trace amounts of incidental impurities, and said alloy after fabrication by gas atomization, thermomechanical processing and further high temperature exposure has an elongation of 58.7%.

5. An alloy according to claim 2, in which the percentage composition by weight is: chromium 26.81 molybdenum 5.97 manganese 0.74 silicon 0.70 iron 0.52 nickel 0.094 carbon 0.09 nitrogen 0.22 oxygen 0.0142 aluminum 0.47 lanthanum 0.15 ______________________________________ and the balance cobalt, apart from trace amounts of incidental impurities, and said alloy after fabrication by gas atomization, thermomechanical processing and further high temperature exposure has an elongation of 51.0%.

6. A process for producing a high strength, corrosion-resistant, high temperature stable, consolidated, biocompatible, ductile alloy having homogeneously distributed dispersed oxides and fine, equiaxed grain structure after high temperature exposure, which comprises melting under an atmosphere consisting of nitrogen, an inert gas or a mixture thereof an alloy mixture consisting essentially of the following percentage composition by weight: chromium 26 to 30 molybdenum 5 to 7 manganese 0 to 1 silicon 0 to 1 iron 0 to 0.75 nickel 0 to 1.0 carbon 0 to 0.35 nitrogen 0 to 0.25 oxygen 0.003 to 0.20 oxide-forming metal 0.003 to 2.0 ______________________________________ and the balance cobalt, apart from trace amounts of incidental impurities; in which the oxide-forming metal is a metal selected from the group consisting of magnesium, calcium, aluminum, yttrium, lanthanum, titanium and zirconium, which forms high temperature-stable, non-accretive, fine oxide particles, which oxide has a free energy of formation greater than the oxide of the matrix metal and is homogeneously distributed in the dispersed phase wherein the cobalt, chromium, molybdenum and carbon are charged first, the resulting charge is flooded with nitrogen and/or inert gas and melted at a temperature within the range of 1454.degree. C. (2650.degree. F.) to 1538.degree. C. (3800.degree. F.), followed by addition of the oxide-forming metal, which acts as a getter for oxygen present in the original mixture and thus providing dispersed oxide, the nitrogen being present as nitride, derived from the nitrogenous atmosphere; immediately subjecting the molten mixture to gas atomization to produce a fine oxide dispersion homogeneously distributed throughout the alloy and thermomechanically processing the resultant alloy powder to provide a consolidated alloy having an ultimate tensile strength of 160-200 k.s.i., a 0.2% offset yield strength of 75-100 k.s.i., an elongation of 37 to 60%, and a fatigue strength at 10.sup.7 cycles (Rotating Beam) of 70-95 k.s.i.

7. A process according to claim 6, in which said oxide-forming metal is aluminum, lanthanum or a mixture thereof.

8. A process according to claim 6, in which the alloy powder after gas atomization has a percentage composition by weight of: chromium 26.47-27.27 molybdenum 5.50-6.01 manganese 0.73-0.78 silicon 0.70-0.71 nickel 0.002-0.187 iron 0.066-0.520 carbon 0.09-0.11 oxygen 0.0035-0.016 nitrogen 0.10-0.25 aluminum 0.40-0.81 lanthanum 0-0.15 ______________________________________ and the balance cobalt, apart from trace amounts of incidental impurities.