Method to produce metal matrix composite articles from rich metastable-beta titanium alloys
AssigneeThe United States of America as represented by the Secretary of the Air Force
InventorsDaniel Eylon, Francis H. Froes
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Abstract
A method for fabricating an improved titanium alloy composite consisting of at least one high strength/high stiffness filament or fiber embedded in an alpha-beta titanium alloy matrix which comprises the steps of providing a rapidly-solidified foil made of a rich metastable beta titanium alloy, fabricating a preform consisting of alternating layers of the rapidly-solidified foil and the filamentary material, and applying heat and pressure to consolidate the preform, wherein consolidation is carried out at a temperature below the beta-transus temperature of the alloy.
Claims6
A method for fabricating a titanium alloy composite consisting of at least one filamentary material selected from the group consisting of silicon carbide, silicon carbide-coated boron, boron carbide-coated boron, and silicon-coated silicon carbide, and a rich metastable beta titanium alloy which comprises the steps of:
- (a) providing a rapidly solidified foil of said alloy;
- (b) fabricating a preform consisting of alternating layers of at least one of said filamentary materials and said foil;
- and
- (c) applying heat at a level about 1% to 10% below the beta transus temperature of said alloy and pressure of about 1.5 to 15 ksi for about 0.25 to 24 hours to consolidate said preform.
Dependencies are inferred from the claim text.