Near-beta titanium alloy for high strength applications and methods for manufacturing the same
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United States of America Patent
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Jun 4, 2013
Grant Date -
Jul 19, 2012
app pub date -
Mar 29, 2012
filing date -
May 29, 2009
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Abstract
A high strength near-beta titanium alloy including, in weight %, 5.3 to 5.7% aluminum, 4.8 to 5.2% vanadium, 0.7 to 0.9% iron, 4.6 to 5.3% molybdenum, 2.0 to 2.5% chromium, and 0.12 to 0.16% oxygen with balance titanium and incidental impurities is provided. An aviation system component comprising the high strength near-beta titanium alloy, and a method for the manufacture of a titanium alloy for use in high strength, deep hardenability, and excellent ductility applications are also provided.
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