Titanium-based alloy having high mechanical strength

Specialized metallurgical processes – compositions for use therei – Processes – Free metal or alloy reductant contains magnesium

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148 325, 148133, C22C 1400, C22F 118

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042538734

ABSTRACT:
A titanium-based alloy of a high mechanical strength, which provides an excellent material of, particularly turbine blades, comprising 2.0 to 5.0% by weight of aluminum, 1.0 to 9.0% by weight of molybdenum, 6.1 to 9.0% by weight of chromium, traces of impurities, and titanium constituting the balance. The alloy may further contain 0.05 to 0.2% by weight of silicon and/or 0.001 to 0.05% by weight of boron, as required.

REFERENCES:
patent: 2892706 (1959-06-01), Jaffee et al.
patent: 3666453 (1972-05-01), Goosey
patent: 3833363 (1974-09-01), Bomberger, Jr. et al.

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