Method to produce high temperature oxidation resistant metal matrix composites by fiber density grading
AssigneeThe United States of America as represented by the Secretary of the Air Force
InventorsDaniel Eylon, Stephen W. Schwenker
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Abstract
A method to produce high temperature oxidation resistant metal matrix composites by fiber diameter grading, which comprises the steps of (a) laying up an alloy/fiber preform consisting of a plurality of alternating layers of metal alloy and fibers and (b) consolidating the preform under suitable conditions, wherein the layers of fibers in the preform are graduated so that fiber density is lower nearer what will become the exposed surface of the composite and higher toward the interior of the composite. The difference in fiber density is achieved by spacing the near-surface fibers further apart than the interior fibers.
Claims4
A method to produce high temperature oxidation resistant metal matrix composites which comprises the steps of (a) laying up an alloy/fiber preform consisting of a plurality of alternating layers of metal alloy and fibers and (b) consolidating the preform by heating the alloy-fiber preform to a temperature below the beta-transus temperature of the alloy while applying a pressure of at least 10 Ksi for a time sufficient to effect consolidation, wherein the layers of fibers in the preform are graduated so that fiber density is lower nearer what will become the surface of the composite exposed to high temperature, oxidizing conditions, and fiber density is higher toward the interior of the composite.
A method to produce high temperature oxidation resistant metal matrix composites which comprises the steps of (a) laying up an alloy/fiber preform consisting of a plurality of layers of metal alloy and fibers and (b) consolidating the preform by heating the alloy-fiber preform to a temperature below the beta-transus temperature of the alloy while applying a pressure of at least 10 Ksi for a time sufficient to effect consolidation;
- wherein the layers of fibers in the preform are graduated so that fiber density is lower nearer what will become the surface of the composite exposed to high temperature, oxidizing conditions, and fiber density is higher toward the interior of the composite;
- and wherein said layers of metal alloy and fibers are fabricated by depositing a layer of metal alloy on a plurality of fibers laid in parallel relation to provide a sheet-like material.
The method of claims wherein said alloy is a titanium alloy.
Dependencies are inferred from the claim text.