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202021 · A Ti-10-2-3 alloy forging bar (~100 mm diameter) provided by Beijing Institute of Aeronautical Materials was used in the present study. The β-transus
contact2023313 · Danard, Y. et al. Microstructure design and in-situ investigation of TRIP/TWIP effects in a forged dual-phase Ti–10V–2Fe–3Al alloy. Materialia 8 ,
contact2011825 · Fig. 2. (a) Effect of master alloy type and powder size on the sintered density of Ti–10V–2Fe–3Al at 1300 °C for 120 min. The figures in parentheses are real
contact202071 · Titanium alloys have been widely used in the aerospace industries as replacements for aluminum alloys and steel because of their attractive properties
contact201161 · In turning β-titanium Ti–10V–2Fe–3Al the results presented in Fig. 8, Fig. 9 prove that the development of notch wear depends on the cutting length while cooling
contact2022215 · A relatively low β-transus temperature (∼795±5 °C) of Ti-10V-2Fe-3Al alloy, compared to those of α+β alloys such as Ti-6Al-4 V (∼995±5 °C), allows manufacturing of near net shape parts by forging at comparatively low temperatures using low cost tools and dies.
contact201351 · The alloy Ti–10V–2Fe–3Al was developed by Timet in 1970. It has capability to replace precipitation-hardening steels because of its deep hardenability and
contact201791 · Conducted researches allowed to determine the aging impact on near-beta Ti-10V-2Fe-3Al titanium alloy properties. Studies revealed that exposure of examined
contact20061121 · Ti-10V-2Fe-3Al alloy was developed specifically for aerospace applications. Samples were produced by mixing of initial metallic powders followed by
contact2019111 · These alloys undergo ductile failure which is governed by void nucleation, growth and coalescence (Lütjering and Williams, 2007; Peters et al., 2003; Xie et al., 2018). Difference in ductility of various solution treated and aged conditions of Ti-10V-2Fe-3Al alloy was presented by the Terlinde et al. (1980).
contact201351 · The alloy Ti–10V–2Fe–3Al was developed by Timet in 1970. It has capability to replace precipitation-hardening steels because of its deep hardenability and good ductility. It received a major breakthrough in aerospace applications when it was used as landing gear in Boeing 777 , . While the initial cost of the alloy was higher than 4340 ...
contact202021 · A Ti-10-2-3 alloy forging bar (~100 mm diameter) provided by Beijing Institute of Aeronautical Materials was used in the present study. The β-transus temperature of the Ti–10V–2Fe–3Al alloy was metallographically measured to be 1068 K. The detailed chemical compositions (wt%) of the forging bar are presented in Table 1.
contact201791 · Abstract. Microstructural evolution in Ti-10V-2Fe-3Al after specified heat treatment conditions has been the basis of performed analysis. The schedule involves prior heating at the temperature of ...
contactAbstract Two different types of titanium alloy, near α Ti–8Al–1Mo–1V and near β Ti–10V–2Fe–3Al, were studied in this work. They were thermochemically treated in a pure nitrogen atmosphere in order to Expand
contact20221122 · ：Ti-10V-2Fe-3Al ： ： ： 15:00 ：334 、 、：
contact20191127 · Ti-4Al-7Mo-10V-2Fe-1Zr TB5 Ti-15V-3Al-3Cr-3Sn TB6 Ti-10V-2Fe-3Al TB7 Ti-32Mo TB8 Ti-15Mo-3Al-2.7Nb-0.25Si TB9 Ti-3Al-8V-6Cr-4Mo-4Zr TB10 Ti-5Mo-5V-2Cr-3Al TB11 Ti-15Mo TC1 Ti-2Al-1.5Mn TC2 Ti-4Al-1.5Mn TC3 Ti-5Al-4V TC4 Ti-6Al-4V TC4ELI Ti-6Al ...
contact202338 · Commercially Pure (CP) Ti Ti-6Al-4V Alloy Ti-10V-2Fe-3Al Titanium Aluminides (TiAl) Others . By Application/End Use: ... Latin America (Brazil, Rest of LA)
contact200355 · Chemical Formula: Ti 10 V 2 Fe 3 Al. Background: T his near beta alloy was developed primarily for high strength applications in the 1241 MPa (180ksi) UTS range, in order to provide weight savings over steels in airframe forging operations.. The alloy also possesses the best hot die forgability of any commercial titanium alloy and is suitable for
contact201023 · Ti-8823 BT32 TB4 Ti-4Al-7Mo-10V-2Fe-1Zr Ti-47121 TB5 Ti-15V-3Al-3Cr-3Sn Ti-15333 BTຫໍສະໝຸດ Baidu35 TiAl6V4 Ti-6Al-4V TC6 Ti-6Al-1.5Cr-2.5Mo-0.5Fe-0.3Si BT3-1 TC8 Ti-6.5Al-3.5Mo-0.25Si BT8 TC9 ...
contact10V-2Fe-3Al SPEC SHEET. Ti-10V-2Fe-3Al is a near beta alloy developed as a high strength forging alloy. This grade provides the best combination of strength and toughness of the commercially available titanium alloys. Its strength permits about a 27% weight savings when compared to Ti-6Al-4V. At the 180 ksi tensile strength level, the K1c value ...
contactTitanium Ti-10V-2Fe-3Al Titanium alloy This titanium alloy has a better fatigue resistance than the average and an excellent hot forgeability. This metal is ideal for the landing gear components. Key benefits Fatigue resistance Forgeability Technical Information More info on Ti-10V-2Fe-3Al Titanium alloy Contact us + 33 (0)4 72 14 55 00 Industrial
contact202323 · Ti-10-2-3. Ti-10V-2Fe-3Al. 320. ≥ 1105. It belongs to high strength and high toughness titanium alloy. It can be used for isothermal forging.It can be used for aircraft fuselage, wing and
contact200355 · Chemical Formula Ti 10 V 2 Fe 3 Al Background T his near beta alloy was developed primarily for high strength applications in the 1241 MPa (180ksi) UTS range, in order to provide weight savings over steels in airframe forging operations.
contactPhysical and mechanical properties for this high strength titanium alloy. Fabrication and alternative designations for Ti10V2Fe3Al are also provided. ... Ti/10V/2Fe/3Al: Property Minimum Value (S.I.) Maximum Value (S.I.) Units (S.I.) Minimum Value (Imp.) Maximum Value (Imp.) Units (Imp.) Atomic Volume (average) 0.01: 0.011: m 3 /kmol:
contact201815 · The detailed chemical compositions (wt%) of the Ti-10V-2Al-3Fe alloy are presented in Table 1. The β - transus temperature of the alloy was determined to be 795 ℃ approximately by a metallographic method [1]. Specimens were β solution treated at 820 ℃ for 0.5 h, then water quenched to acquire a single-phase β structure [24]. Table 1.
contact201197 · The microstructural evolution and grain refinement mechanisms of a Ti-10V-2Fe-3Al alloy, β-solution quenched and cold forged (CF) to strains of 0.1, 0.35, and 1.2 have been investigated using optical microscopy (OM), X-ray diffraction (XRD), and transmission electron microscopy (TEM). The results showed that the stress-induced martensitic
contact202338 · Commercially Pure (CP) Ti Ti-6Al-4V Alloy Ti-10V-2Fe-3Al Titanium Aluminides (TiAl) Others . By Application/End Use: ... Latin America (Brazil, Rest of LA)
contact201351 · The alloy Ti–10V–2Fe–3Al was developed by Timet in 1970. It has capability to replace precipitation-hardening steels because of its deep hardenability and good ductility. It received a major breakthrough in aerospace applications when it was used as landing gear in Boeing 777 [2], [4].
contact2023313 · Danard, Y. et al. Microstructure design and in-situ investigation of TRIP/TWIP effects in a forged dual-phase Ti–10V–2Fe–3Al alloy. Materialia 8 , (2019). Article CAS Google Scholar
contact2015519 · Although alloys such as Ti-15V-3Al-3Sn-3Cr, Ti-10V-2Fe-3Al and Ti-3AI-8V-6Cr-4Mo-4Zr (Beta C) were commercialized into well-known airframe systems by the 1980s, Ti-13V-11Cr-3Al was
contact2017222 · Strong and ductile powder metallurgy (PM) Ti-10V-2Fe-3Al alloy has been fabricated by spark plasma sintering (SPS) of titanium and V-Fe-Al master alloy powder blends at 1100°C for 30 min under 30 MPa. The homogenization of vanadium, which dictates the realization of a uniform microstructure of the Ti-10V-2Fe-3Al alloy, was
contact20061121 · Ti-10V-2Fe-3Al alloy was developed specifically for aerospace applications. Samples were produced by mixing of initial metallic powders followed by cold uniaxial and isostatic pressing with subsequent densification by sintering at 1200 °C and 1400° in vacuum.
contactTi–10V–2Fe–3Al alloy, also called TB6 alloy, has inspired broad interests in the academic community and industry. It was firstly developed by TIMET Company in
contactAbstract Beta alloys, such as Ti-10V-2Fe-3Al, can be processed and heat treated to provide a wide range in mechanical and fracture properties. A systematic study of the effect of processing and heat treatment variations on the properties combinations achievable was
contactAbstract Two different types of titanium alloy, near α Ti–8Al–1Mo–1V and near β Ti–10V–2Fe–3Al, were studied in this work. They were thermochemically treated in a pure nitrogen atmosphere in order to Expand
contact202338 · Commercially Pure (CP) Ti Ti-6Al-4V Alloy Ti-10V-2Fe-3Al Titanium Aluminides (TiAl) Others . By Application/End Use: ... Latin America (Brazil, Rest of LA)
contact2020924 · Ti-10V-2Fe-3Alth120 GPa[26]，Ti-6Al-4Vth65~153 GPa，eff0.33 [27]，，，2(th=115 GPa，eff=0.33) ...
contact201911 · A welding of dissimilar alloy gives an optimum combination of high strength of Ti-10V-2Fe- 3Al (Ti1023) and low cost of Ti-6Al-4V (Ti64). Three different fusion ratios of Ti1023 and Ti64 were resulting in a similar width size of the fusion zone (FZ) and heat affected zones (HAZ) whereas a thicker sample with the same fusion ratio generated a
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