2018
DOI: 10.1016/j.msea.2018.01.113
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Tensile properties of a newly developed high-temperature titanium alloy at room temperature and 650 °C

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Cited by 79 publications
(19 citation statements)
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“…In recent years, as the flight speed and distance of air vehicles increase significantly, traditional titanium alloys such as TC4, TA15 cannot cover the operating requirements. High-temperature titanium alloys possess excellent mechanical properties at high temperature, and the service temperature of these alloys is increased to above 873 K [5][6][7]. Due to these excellent performances, high-temperature titanium alloys have become advanced materials in aerospace applications, such as the components of aircraft engines, wings and rudders [8].…”
Section: Introductionmentioning
confidence: 99%
“…In recent years, as the flight speed and distance of air vehicles increase significantly, traditional titanium alloys such as TC4, TA15 cannot cover the operating requirements. High-temperature titanium alloys possess excellent mechanical properties at high temperature, and the service temperature of these alloys is increased to above 873 K [5][6][7]. Due to these excellent performances, high-temperature titanium alloys have become advanced materials in aerospace applications, such as the components of aircraft engines, wings and rudders [8].…”
Section: Introductionmentioning
confidence: 99%
“…Titanium alloys with exceptional properties of specific strength, creep strength, thermal resistance, corrosion resistance and workability have been developed for high-temperature applications up to 600 • C, such as in compressor disks and the blades of gas turbines in advanced jet engines [1,2]. With increases in the service temperature, the Al equivalent ([Al]eq) of common high-temperature titanium alloys, such as Ti-1100 [3], IMI834 [4] and Ti600 [5], reach the critical value, and the contents of the α stabilizing element and the neutral element have no room to adjust.…”
Section: Introductionmentioning
confidence: 99%
“…Conventional near-alpha Ti alloys are strengthened by fine alpha2 phase with DO 19 structure and intermetallic silicides [7][8]. Up to now, numerous works were focused on the influence of alpha stabilizing alloying elements such as Ga, Sn, Hf and Zr on the high temperature mechanical properties of the near-alphaa titanium alloys [9][10]12]. These studies demonstrated that the solid solution strengthening and the formation of a 2 phase are effective in improving high temperature strength, but degrade the ductility of the material [10][11] probably due to the lower symmetry of its DO 19 crystal structure.…”
Section: Introductionmentioning
confidence: 99%