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202021 · Fig. 1 shows the XRD patterns for the surface and different depths (100 μm, 200 μm and 350 μm) of Ti-10-2-3 specimens with solution treatment in vacuum. The
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
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.
contact202086 · and Ti-10-2-3 and alpha-beta alloys Ti-62222, Ti-6242S, Timetal 550, Ti-62S, SP-700, and Corona-X. The emphasis is on properties of rolled sheet product form
contact201023 · ： ：86- ：(+86)018 ： ：
contact202334 · We can produce the Ti 10-2-3 has the following specifications: Round bar steel: 1mm to 3000mm. Square-shape steel: 1mm to 2000mm. Plate steel: 0.1mm to
contact2023323 · In this stuy, a new high-throughput heat treatment method was applied to rapidly optimize the microstructure of metastable β titanium alloy Ti-6.8Mo-3.9Al-2.8Cr
contact2020427 · β-Ti alloys have been used in many military/commercial aircraft since 1950s. Their high specific strength, good corrosion resistance, and high formability meet
contact202021 · Fig. 1 shows the XRD patterns for the surface and different depths (100 μm, 200 μm and 350 μm) of Ti-10-2-3 specimens with solution treatment in vacuum. The surface region is composed of dominant β phase and a few α″ phase, and the volume fraction of α″ phase increases significantly with increasing corrosion depths from surface to 100 μm,
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.
contact2019116 · Fig. 2 shows typical TEM microstructure in the undeformed pillar of β Ti-10-2-3 at the solution-treated condition. It is revealed that no α″ plate was observed in the undeformed β matrix (Fig. 2 a).The selected area electron diffraction (SAED) pattern analysis along the <011> β zone axis of the β matrix shows that the primary components
contact2020527 · There also were other Ti alloy landing gear parts (mostly Ti-10-2-3) besides the truck beam as can be seen in Figure 7. Later, Airbus also used Ti-10-2-3 for the landing gear of the A380 aircraft. This alloy, as well as Ti-6-4, has been used for quite some time in rotor components by helicopter manufacturers to replace steel for weight savings.
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 ...
contactChrist H J, Decker M, Zeitler S. Hydrogen diffusion coefficients in the titanium alloys IMI 834, Ti 10-2-3, Ti 21 S, and alloy C [J]. Metall. Mater. Trans., 2000, 31A: 1507 [43] Miyoshi T, Naito S, Yamamoto M, et al. Diffusion of hydrogen in titanium, Ti 88 Al 12 3
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
contact2023323 · In this stuy, a new high-throughput heat treatment method was applied to rapidly optimize the microstructure of metastable β titanium alloy Ti-6.8Mo-3.9Al-2.8Cr-2Nb-1.2V-1Zr-1Sn to obtain high strength and ductility. Continuous temperature gradient solution treatment was created in a tubular furnace at 746–909 ° C (the β-transus temperature
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.
contact2020621 · However, studies on the effect of Cr content on the Ti-10-2-3 alloy have been less reported. In the present study, a novel Ti 20 V 20 Al 20 Fe 20 Cr 20 equiatomic HEAs is developed using plasma spark sintering methods, which are accompanied by thorough characterization of synthesized alloys for property profiles and performance
contactAbout 10-2-3 Titanium Alloy. 10-2-3 Titanium Alloy, or Ti-10V-2Fe-3Al, is a high-strength titanium-based forging alloy consisting of 10% vanadium, 3% aluminum, and 2% iron typically used in aerospace and automotive components. American Elements manufactures alloy products are in various forms such as powder, bar, ingot, sheet, plate, and other ...
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.
contact201023 · ： ：86- ：(+86)018 ： ：
contact202323 · Ti 10-2-3 alloy application. Ti-1023 alloy has been widely used in aerospace industry because of its excellent strength, toughness and high cycle fatigue performance. Meanwhile, the Ti-1023 alloy can also be
contact201023 · Ti-6.5Al-3.5Mo-2.5Sn-0.3Si TC10 Ti-6Al-6V-2Sn-0.5Cu-0.5Fe AB-3 TC11 Ti-6.5Al-3.5Mo-1.5Zr-0.3Si GB/T ASTM ΓOCT JIS DIN BS TA1（ELI） Ti GR1
contact2012518 · This 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 V-2Fe-3Al).
contact2019710 · BOBBILI R, RAMUDU B V, MADHU V. A physically-based constitutive model for hot deformation of Ti-10-2-3 alloy [J]. Journal of Alloys and Compounds, 2016, 696: 295–303. DOI: 10.1016/j.jallcom.2016.11.208. Article Google Scholar GANDIN C A, RAPPAZ M. A coupled finite element-cellular automaton model for the prediction of
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
contactAbout 10-2-3 Titanium Alloy. 10-2-3 Titanium Alloy, or Ti-10V-2Fe-3Al, is a high-strength titanium-based forging alloy consisting of 10% vanadium, 3% aluminum, and 2% iron typically used in aerospace and automotive components. American Elements manufactures alloy products are in various forms such as powder, bar, ingot, sheet, plate, and other ...
contact201793 · .doc,GB/T ASTM ΓOCT JIS DIN BS TA1（ELI） Ti GR1 BT1-00 JIS 1Ti1 2TA 1 TA2（ELI） Ti GR2 BT1-0 JIS 2Ti3 2TA2 TA3（ELI） Ti GR3 BT1-0 JIS 3Ti4 2TA2 TA4 ...
contact2023323 · In this stuy, a new high-throughput heat treatment method was applied to rapidly optimize the microstructure of metastable β titanium alloy Ti-6.8Mo-3.9Al-2.8Cr-2Nb-1.2V-1Zr-1Sn to obtain high strength and ductility. Continuous temperature gradient solution treatment was created in a tubular furnace at 746–909 ° C (the β-transus temperature
contactThe TCS alloy also had an improved homogeneous elongation compared to TA6V and Ti-10-2-3. Yield and ultimate tensile stresses (YS and UTS) as well as hardening and elongation to fracture are summarized in Table 1. The reduction of area to fracture, evidencing the ultimate ductility, is also indicated in this table, when available. Fig. 1: a ...
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