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BT9 Ti-6.5Al-3.5Mo-0.3Si TC3 Ti-4Al-4V A-1 Ti-5Al-2.5Sn BT/4 Ti-5Al-3Mo-1.5V TC4 Ti-6Al-4V A-3 Ti-6Al-2Nb-1Ta BT16 Ti-2.8Al-5Mo-5V ... BT22 Ti-5.5Al-5V-5Mo-1.5Cr-1.0Fe A-4
contact201023 · Beta C TB11 Ti-15Mo TC1 Ti-2Al-1.5Mn OT4-1 TC2 Ti-4Al-1.5Mn OT4 TC3 Ti-5Al-4V GB/T ASTM ΓOCT JIS DIN BS
contact201023 · Ti-4Al-1.5Mn OT4 TC3 Ti-5Al-4V TC4 （ TC4ELI ） Ti-6Al-4V GR5 （ GR23 ） BT6 （ BT6C ） 60 （ 60E ） TiAl6V4 Ti-6Al-4V TC6 Ti-6Al-1.5Cr-2.5Mo
contactDownload scientific diagram | True stress-true strain curves of Ti-4Al-1Sn-2Zr-5Mo-8V-2.5Cr alloy at (a) 780 C, (b) 830 C, (c) 880 C and (d) 930 C. from publication: Investigation of
contact20191127 · Ti-4Al-1.5Mn TC3 Ti-5Al-4V TC4 Ti-6Al-4V TC4ELI Ti-6Al-4VELI TC6 Ti-6Al-1.5Cr-2.5Mo-0.5Fe-0.3Si TC8 Ti-6.5Al-3.5Mo-0.25Si TC9 Ti-6.5Al-3.5Mo-2.5Sn
contact2022822 · Ti-4Al-5Mo-5V-5Cr-1Nb (wt.%) is a new type of high-strength (~1300 MPa) titanium (Ti) alloy developed for aerospace applications. Until now, the research on its welding and subsequent heat treatment is barren. Herein, we employed electron beam welding (EBW) to a solutionized Ti-4Al-5Mo-5V-5Cr-1Nb with a phase constituent of α +
contact2022511 · But the preparation of solid-to-liquid diffusion couples can be accelerated with the aid of higher diffusion ability in melts In this paper, a new damascene-structure diffusion couple composed of pure iron and T20C (Ti-4.5Mo–5Al-1.8Zr-2.5Cr-1.1Sn) titanium alloy was designed by taking advantage of the fact that the diffusion ability of metal ...
contact202291 · Here, we report a hierarchical microstructure tailoring strategy to achieve an excellent strength-ductility combination in Ti-4Al-5Mo-5V-5Cr-1Nb (Ti-45551) alloy. It was revealed that high density ...
contact2021616 · ：（、） TAD Grade1 1 BT1-00 TA1 Grade2 2 BT1-0 TA2 Grade3 3 OT4 -0 Ti-0.8Al-0.7Sn TA3 Grade4 4 OT4 -1 Ti-2Al-1.
contact2021223 · The 5Cr-0.5Mo steel is a member of the heat-resistant chromium-molybdenum (Cr-Mo) alloy steel family. Piping materials made of 5Cr-0.5Mo are widely used for a variety of high pressure and high temperature services such as petroleum cracking facility, coking unit, fertilizer production system, steam facility, and other petrochemical &
contactSuperplastic forming and diffusion bonding (SPF/DB) is a near-net-shape forming and joining process used with alloys having superplastic properties in order to make manufact which should have light weight and high stiffness. The aerospace is one of those sectors in which such technology is mainly used. This process allows to reduce the buy-to-fly ratio
contact2022725 · TA5 ：Ti-4Al-0.005B ： Al：3.3%~4.7% B：0.005% GB/T2965-2007 ：≥685(MPa) ...
contact201721 · The details of the melting procedure of four experimental alloys with nominal compositions Ti-5Al-5Mo-5V-3Cr, Ti-5Al-3.5Mo-7.2V-3Cr, Ti-5Al-5Mo-8.6V-1.5Cr and Ti-5Al-3.5Mo-5V-3.94Cr designated as A1, A2, A3 and A4, respectively are given elsewhere (Manda et al., 2015).The chemical composition of alloy A1 is same as the Ti-5553, while
contact2021722 · In this work, a near-beta Ti-5Al-5Mo-5V-1Cr-1Fe titanium alloy was fabricated by selective laser melting (SLM), and the microstructure evolution together with the mechanical properties was studied. The as-fabricated alloy showed columnar β grains spreading over multiple layers and paralleling to the building direction. The distinct
contactTi-4Al-5Mo-6Cr-5V-1Nb. ,Ti-4Al-5Mo-6Cr-5V-1Nb700~900℃、0.001~1.000 s;。. -,
contactLow cycle fatigue (LCF) behaviour of the near α titanium alloy, Ti-6Al-5Zr-0.5Mo-0.25Si (LT26A), was investigated in the (a + β) as well as β treated conditions at room temperature. LCF tests were carried out under total strain controlled mode in the range of Δεt/2: from ±0.60% to ±1.40%. The alloy shows cyclic softening in both the conditions. Also it
contact20211025 · 1.25Cr0.5Mo，、1.25Cr-0.5Mo（），ASMESA387/SA387M Gr11 class 2。1.25Cr-0.5Mo、，
contactTC10、TC11、TC17、TC18、TC21、TC25, BaoJi Fitow Metal Co., LTD. Tel : 86 . Email: Add:Tai Cheng Road ,WeiBin Bistrict,Baoji City ...
contactIn general, metastable β-Ti-alloys exhibit low ductility at room temperature, which restricts its workability and critical applications. Here, we report a... DOAJ is a unique and extensive index of diverse open access journals from around the world, driven by a growing community, committed to ensuring quality content is freely available online ...
contact20141219 · The synthesis of CORONA 5 (Ti-4.5Al-5Mo-1.5Cr) is described from the viewpoints of alloy chemistry and microstructure. Lenticular alpha is shown to maximize fracture resistance parameters, while a globular alpha optimizes hightemperature flow characteristics. The processing and application of CORONA 5 as forging, plate, sheet
contactThe Ti-4.5Al-5Mo-1.5Cr alloy has an increased fatigue life under higher strain when heat treated at higher temperatures in the α-β region. Comparison of the fatigue lives of the Ti-6Al-4V and Ti-4.5Al-5Mo-1.5Cr alloys in the mill-annealed condition shows that Ti-4.5Al-5Mo-1.5Cr has improved fatigue behavior in the high-cycle region, but Ti ...
contact@article{osti_, title = {Effect of microstructure and yield strength on the void nucleation, growth, and fracture of. alpha. /. beta. Ti-4. 5Al-5Mo-1. 5Cr alloy (CORONA-5)}, author = {Vijayaraghavan, T V}, abstractNote = {The objective was to investigate the effect of varying plastic interaction between particle and matrix in a two-ductile-phase system,
contactTi6Al4V is an alpha-beta alloy and the most widely used of all the titanium alloys. Ti6Al4V ELI is also briefly described. We use cookies to enhance your experience.
contact202151 · In order to study the aging hardening characteristics and isothermal aging process of Ti-6Cr-5V-5Mo-4Al-1Nb alloy the time-temperature-transformation (TTT) curve of the alloy was measured by aging hardness method, and the microstructure changes during isothermal process were analyzed by XRD and SEM. It was found that the alloy had a
contact201758 · The metastable titanium Ti-5Al-5Mo-5V-3Cr (Ti-5553) (wt.%) alloy has been developed recently to replace the alloy Ti-10V-2Fe-3Al (Ti-1023) in some of the structural components of the aircraft. The microstructure, texture and mechanical prop-erties of the alloy Ti-5553 and similar Mo equivalent (8.15)
contactThe dynamic mechanical properties and failure behavior of rolled and heat treated Ti-4.5Mo-5.1Al-1.8Zr-1.1Sn-2.5Cr-2.9Zn alloys were studied.The results show that after multi-pass rolling at 880℃,a duplex microstructure consisting ofβmatrix and non-uniformly distributed"equiaxed+strip"αphase is obtained,and the microstructure is composed ...
contactTi-4Al-5Mo-6Cr-5V-1Nb. ,Ti-4Al-5Mo-6Cr-5V-1Nb700~900℃、0.001~1.000 s;。. -,
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