Abstract
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Highlights
The titanium alloy Ti – 10V – 2Fe – 3Al has been developed for the manufacture of Selection and Peer-review under the responsibility of The Ural school-seminar of metal scientists-young researchers Conference Committee.high-strength elements to replace steel, which gives a significant weight gain
Hardening heat treatment of the Ti–10V–2Fe–3Al alloy is used to obtain the final complex of mechanical properties
The investigation of five Ti–10V–2Fe–3Al alloy compositions with different carbon content, aluminum and molybdenum structural equivalents, calculated by the formulas from the handbook [12], which are presented in Table 1, was carried out
Summary
The titanium alloy Ti – 10V – 2Fe – 3Al has been developed for the manufacture of Selection and Peer-review under the responsibility of The Ural school-seminar of metal scientists-young researchers Conference Committee. High-strength elements to replace steel, which gives a significant weight gain. Since 1980s the alloy has been widely used in aircraft industry for manufacture of landing gear assemblies and loaded airframe elements [1]. Hardening heat treatment of the Ti–10V–2Fe–3Al alloy is used to obtain the final complex of mechanical properties. The alloy strength can be changed in a wide range from 1000 to 1350 MPa by changing the temperature of aging [3]. The mechanical properties of the alloy, in addition, are influenced by a large number
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