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Structural Titanium Alloys in Modern Mechanical Engineering
by
Moiseev, V. N.
in
Aircraft
/ Alloys
/ Creep rupture strength
/ Domestic
/ Ductility
/ Spacecraft
/ Titanium alloys
/ Titanium base alloys
/ Vanadium base alloys
2004
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Do you wish to request the book?
Structural Titanium Alloys in Modern Mechanical Engineering
by
Moiseev, V. N.
in
Aircraft
/ Alloys
/ Creep rupture strength
/ Domestic
/ Ductility
/ Spacecraft
/ Titanium alloys
/ Titanium base alloys
/ Vanadium base alloys
2004
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Structural Titanium Alloys in Modern Mechanical Engineering
Journal Article
Structural Titanium Alloys in Modern Mechanical Engineering
2004
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Overview
Mechanical and process properties of widely used domestic structural titanium pseudo-alpha-alloys are studied. The Ti-Al-Mn system is chosen as a base for creating commercial titanium alloys of series OT4-0, OT4-1, OT4, etc. The developed titanium alloys guarantee ultimate rupture strength of 600 - 1100 MPa and possess satisfactory ductility in cold and hot plastic deformation. Experience in the use of alloys of this class in the aircraft and spacecraft industries is analyzed. In order to meet the international unification of titanium alloys the possibility of replacing manganese in pseudo-alpha-titanium alloys by vanadium is studied and documentation for realizing this replacement is created.
Publisher
Springer Nature B.V
Subject
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