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1998315 · Likewise for Beta-C, the lower strength age resulted in strengths and toughness less than those of Ti-62222. The Ti-10-2-3 alloy had the highest toughness,
contactThis paper is based on the FE modeling and model validation via the experimental value of turning operation in 2D on heat-treated Titanium alloy (Ti-10-2-3 is also named as Ti-10
contact202048 · Titanium 10-2-3 is a near-beta alloy developed primarily for high-strength applications in the 180 KSI (1241 MPa) UTS range, in order to provide weight savings
contactTi-10V-2Fe-3Al. USA. UNS: R56410. Composition. V. 10. Ti. Base. Al. 3. Fe. 2. Applications • Structural parts. • Helicopter rotor hubs. • Landing gear. Characteristics • Quasi-beta
contactTitanium 10-2-3 is a near-beta alloy developed primarily for high-strength applications in the 180 KSI (1241 MPa) UTS range, in order to provide weight savings over steels used in airframe forging applications.
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contactAs the first barrier for deep geological disposal of high-level nuclear waste (HLNW), HLNW containers are of great significance. Because of the superior corrosion resistance, Ti is
contact201849 · (1) 。, 。 (2) 。。
contact20221025 · For example, Fig. 2 shows a light optical micrograph of the metastable β-Ti alloy Ti-10V-2Fe-3Al (wt%) (Ti-10-2-3) after laser track melting and solidification, simulating AM.
contact20001031 · The behavior of the Ti-10-2-3 alloy was a true one way shape memory effect with no significant recovered strain obtained by simple unloading without a subsequent heating. The results of our work show clearly that superelastic behavior is possible for the β-Cez alloy with significant amount of reversible strain achievable without the necessity ...
contact2018122 · Firstly, it has been revealed f or Ti-10-2-3 alloy [7, 40] t hat when the alloy 180 solution treated below β - transus temperature and quenched in water or He gas, the athermal α˝ was
contactThe microstructure evolution of a Ti-55511 alloy deformed at high temperatures (from 1163 K to 1253 K) and wide strain rate range (from 10 s⁻¹ to 0.001 s⁻¹) is studied by isothermal ...
contact20211019 · Ti-10-2-3 （Ti10V2Fe3Al ），Fe-Mo FeV[9]。Timetal LCB ，， ，Ti-10-2-3 ，Ti-6Al-4V78%。Moβ，
contact2013314 · Ti10-2-3 alloy showed poorer machinability than Ti54M alloy in both the heat treatment conditions due to the presence of higher content of b stabilizer elements (V and Fe). Experimental setup.
contact2019730 · The hot deformation behavior of the aerospace Ti-10-2-3 alloy was investigated by isothermal compression tests at temperatures of 740 to 820 °C and strain rates of 0.0005 to 10 s−1. The results show that the studied alloy is extremely sensitive to deformation parameters, like the temperature and strain rate.
contact20211019 · Ti-10-2-3 （Ti10V2Fe3Al ），Fe-Mo FeV[9]。Timetal LCB ，， ，Ti-10-2-3 ，Ti-6Al-4V78%。Moβ，
contactTitanium 10-2-3 is a near-beta alloy developed primarily for high-strength applications in the 180 KSI (1241 MPa) UTS range, in order to provide weight savings over steels used in airframe forging applications.
contact2018414 · Application to the design of B-type alloys Ti-15-3-3-3 and Ti-10-2-3 are well-known B-type alloys with superior mechanical properties. Ti-15-3-3-3 deforms by the slip mechanism, but Ti-10-2-3 deforms by the twin mechanism. In general, the longer fracture elongation and the lower yield strength are expected in the alloy deformed
contact2019730 · The hot deformation behavior of the aerospace Ti-10-2-3 alloy was investigated by isothermal compression tests at temperatures of 740 to 820 °C and strain rates of 0.0005 to 10 s−1. The results show that the studied alloy is extremely sensitive to deformation parameters, like the temperature and strain rate.
contact2021220 · Abstract—Scanning electron microscopy, electron microprobe and X-ray diffraction analyses, and durometry are used to study changes in the structure, phase composition, and hardness of a quenched titanium Ti‒10V–2Fe–3Al alloy in the course of aging at 500°С for 2–32 h. A complex analysis of changes in the lattice parameters of the
contactTitanium 10-2-3 is a near-beta alloy developed primarily for high-strength applications in the 180 KSI (1241 MPa) UTS range, in order to provide weight savings over steels used in airframe forging applications.
contact2002130 · Titanium alloys classified by metallurgical structure. Alloy. Example. Alpha Alloys. Commercially Pure – ASTM grades 1,2,3 and 4. Ti/Pd Alloys – ASTM grades 7 and 11. Alpha + Compound. Ti-2.5%Cu – IMI 230. Near Alpha Alloys.
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