Design properties of a high-strength titanium alloy, Ti-10V-2Fe-3Al

Journal Article · Fri Feb 29 23:00:00 EST 1980 · J. Met.; (United States)

DOI:https://doi.org/10.1007/BF03354557· OSTI ID:5550839

Boyer, R R

The new titanium alloy Ti-10V-2Fe-3Al is shown to have adequate fracture toughness and stress corrosion resistance at the 180 ksi tensile strength level. This alloy has higher strength and fatigue resistance than other commercially available titanium alloys, and a considerable strength-to-weight advantage over comparable-strength steels. Detailed fracture toughness and fatigue data are presented and compared to commercially available titanium alloys. The special combination of properties and fabricability characteristics is likely to lead to use of this alloy in aerospace, commercial, and marine applications.

• Research Organization: Boeing Commercial Airplane Co., Seattle, WA
• OSTI ID: 5550839
• Journal Information: J. Met.; (United States), Journal Name: J. Met.; (United States) Vol. 32:3; ISSN JOMTA
• Country of Publication: United States
• Language: English

Related Subjects

36 MATERIALS SCIENCE
360103 -- Metals & Alloys-- Mechanical Properties
360105* -- Metals & Alloys-- Corrosion & Erosion
AIRCRAFT
ALLOYS
ALUMINIUM ALLOYS
CHEMICAL REACTIONS
CORROSION
CORROSION RESISTANCE
FATIGUE
FRACTURE PROPERTIES
IRON ALLOYS
MECHANICAL PROPERTIES
STRESS CORROSION
TITANIUM ALLOYS
TITANIUM BASE ALLOYS
VANADIUM ALLOYS
WEIGHT