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2014716 · Hot compression tests were conducted on Ti-13V-11Cr-3Al beta-Ti alloy in the temperature range of 1203 K to 1353 K (930 °C to 1080 °C) and at strain rates
contact202086 · The tensile properties of the alloys (table I), obtained from two tests of each alloy, were within the specifications frequently quoted in procurements of these alloys; for
contactThe important characteristics of this alloy are associated with its all- beta structure and the decomposition of that structure during heat treatment. In the annealed condition, it is a
contactAbstract. Ti-13V-11Cr-3Al is a high strength, meta-stable beta titanium-base alloy recommended for service in the temperature range of -65 to plus 600 F. It responds to an
contact201389 · Titanium alloys are light weight metals with excellent corrosion resistance, very high tensile strength and high toughness. Grade Ti-13V-11Cr-3Al alloy is a heat
contact23 · ERTi-6 is discontinued, 5Al-2.5Sn, Alloy A110AT. Please contact us to inquire. ... Ti 13V-11Cr-3Al is good for stuff too. Ti 8-1-1 Ti 8-1-1 (Ti-8Al-1Mo-1V) is designed for
contact13.5V -11CR-3AL Principal Design Features. This is a heat treatable, beta alloy titanium generally considered for high strength applications. It combines good fabricability with
contactTitanium alloys are light weight and have excellent corrosion resistance, very high tensile strength and toughnes. erti-13v-11cr-3al alloy mali. Home > 310.3 aluminium sae > erti
contact2015714 · A near-β Ti-13V-11Cr-3Al alloy was produced by blended elemental powder metallurgy combining warm compaction and induction sintering. Two Ti-13V-11Cr-3Al powder compacts with different oxygen content were manufactured by mixing PREP and HDH Ti powders with Cr and AlV master alloy powders, respectively. The effect of
contact2020427 · Alloy Country Nominal composition Strength level/MPa（condition） Applications B-120VCA USA Ti-13V-11Cr-3Al 1270（STA） Landing gear，beam TIMETAL 125 USA Ti-6V-6Mo-5.7Fe-2.7Al 1250（STA） Fastener β-C
contactProperties andrapplications of titanium alloys: a brief review 1 ... alloy Ti-13V-11Cr-3AlTi-11.5Mo-Ti-13V-11Cr-3Al-6Zr-4.5Sn near- alloyTi-6Al-2Sn-Ti-8Mo-8V-Ti-10V-2Fe-3AlTi-8Mn 4Zr-6Mo 2Fe-3Al
contactAB-5 B-1. Ti-3Al-2.5V Ti-3Al-13V-11Cr. ПT-3B ПT-7M. Ti-4Al-2V Ti-2Al. ：. TAD TA1 TA2 TA3 TA4 TA5 TA6 TA7 TA8 Ti-3Al Ti-4Al-0.005B Ti-5Al Ti-5Al-2.5Sn Ti-5Al-2.5Sn-3Cu-1.5Zr Grade1 Grade2 Grade3 Grade4 Grade5 Grade6 Grade7 Grade9 1 ...
contactA fatigue and creep-rupture testing program was conducted on solution-treated and aged sheet specimens of titanium alloy B-120VCA at room and elevated temperatures. Data on aged bar stock, previously tested, are also included for comparison. All tests were conducted in axial-stress machines with various combinations of alternating and mean stresses.
contact201375 · Introduction. Titanium alloys are divided into alpha alloys, near-alpha alloys, alpha and beta alloys, and beta alloys. Grade Ti 15V 3Cr 3Al 3Sn alloy is a beta alloy that can be strip-rolled and heat-treated. It is highly formable, and has good room temperature bending properties. Solution treatment of this alloy enhances its strength.
contact2018414 · Ti-13V-11Cr-3Al 3.1 13.8 11.2 .18 .018 .017 .14 .007 The beta transus of the Ti-6Al-4V alloy was determined to be 1800°F ~15°F; that of the Ti-5Al-2.5Sn alloy was 1850°F ±15°F and the alpha transus of this alloy was determined to be approximately 1675°F. Additional comparison of results2 was made with another beta
contact201995 · This Rem-Cru alloy known as B120VCA (Ti-13V-11Cr-3Al), had a low modulus ( <15 x 106 psi (103.4 GPa) elastic and <6 x 106 psi (41.4 GPa) shear) and a high fatigue strength, and could achieve yield strengths in excess of 250 ksi (1724 MPa) in wire form. In the 1960's, this combination of properties made B120VCA a logical choice as ...
contactThe manufacturing method for producing high-strength Ti-10V-2Fe-3Al alloy forgings with suitable ductility/ toughness combinations has been established. The achievable property combinations at high strengths depend critically on the billet chemistry-homogeneity, the forge heat-treat variables, and the section thickness of the forgings. The manufacturing
contact2020427 · Alloy Country Nominal composition Strength level/MPa（condition） Applications B-120VCA USA Ti-13V-11Cr-3Al 1270（STA） Landing gear，beam TIMETAL 125 USA Ti-6V-6Mo-5.7Fe-2.7Al 1250（STA） Fastener β-C
contact2005121 · Beta titanium alloys have been available since the 1950s (Ti-13V-11Cr-3Mo or B120VCA), but significant applications of these alloys, beyond the SR-71 Blackbird, have been slow in coming. The next significant usage of a β alloy did not occur until the mid-1980s on the B-1B bomber. This aircraft used Ti-15V-3Cr-3Al-3Sn sheet due to its
contact20131114 · The superplastic behavior of Ti-13V-11Cr-3Al alloy with beta single phase structure and average grain size of 220 mu m was investigated. It was found that elongation increases with temperature at ...
contactTitanium alloys display low density, high mechanical strength and good corrosion resistance, being ideal structural materials for aerospace engineering. In this paper, the effects of nitrogen on the anelastic properties of the bcc alloy Ti-13V-11Cr-3Al were investigated. The results show an asymmetric thermally activated relaxation structure in the high
contactSecondary current density increases were observed for all the alloys at potentials above + 1.0v. For the 13V‐11Cr‐3Al alloy such behavior was attributed to transpassivity. For the other alloys the phenomena was attributed to pitting or localized corrosion. The commercially pure metal remained passive in this potential range.
contact@article{osti_, title = {Recrystallisation and x-ray diffraction investigation of age-hardening in a metastable Ti--13V--11Cr--3Al alloy}, author = {Seilstorfer, H}, abstractNote = {Three recrystallization diagrams for the metastable titanium alloy, Ti-- 13 V-- 11Cr-- 3Al, were established, based on grain size determinations. . Qualitative as well as quantitative
contactAbstract. Ti-13V-11Cr-3Al is a high strength, meta-stable beta titanium-base alloy recommended for service in the temperature range of -65 to plus 600 F. It responds to an age-hardening heat treatment. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information
contact23 · ERTi-6 is discontinued, 5Al-2.5Sn, Alloy A110AT. Please contact us to inquire. ... Ti 13V-11Cr-3Al is good for stuff too. Ti 8-1-1 Ti 8-1-1 (Ti-8Al-1Mo-1V) is designed for creep resistance up to 450°C, used primarily in engine applications such as forged compressor blades and disks. This alloy has a relatively high tensile modulus to density ...
contactしたTi-13V-11Cr-3Al のにぼすとの 6 1 3 いほどでのにれている.650Kで300 ks したもは, さ2.05GPa, り4.1%に した.750Kで したものは, がせずの みがしている.
contact2018414 · Ti-13V-11Cr-3Al 3.1 13.8 11.2 .18 .018 .017 .14 .007 The beta transus of the Ti-6Al-4V alloy was determined to be 1800°F ~15°F; that of the Ti-5Al-2.5Sn alloy was 1850°F ±15°F and the alpha transus of this alloy was determined to be approximately 1675°F. Additional comparison of results2 was made with another beta
contact20161128 · Flow softening behavior of Ti–13V–11Cr–3Al beta Ti alloy in double-hit hot compression tests - Volume 31 Issue 24
contact2020427 · Alloy Country Nominal composition Strength level/MPa（condition） Applications B-120VCA USA Ti-13V-11Cr-3Al 1270（STA） Landing gear，beam TIMETAL 125 USA Ti-6V-6Mo-5.7Fe-2.7Al 1250（STA） Fastener β-C
contact@article{osti_, title = {Recrystallisation and x-ray diffraction investigation of age-hardening in a metastable Ti--13V--11Cr--3Al alloy}, author = {Seilstorfer, H}, abstractNote = {Three recrystallization diagrams for the metastable titanium alloy, Ti-- 13 V-- 11Cr-- 3Al, were established, based on grain size determinations. . Qualitative as well as quantitative
contactAbstract. Ti-13V-11Cr-3Al is a high strength, meta-stable beta titanium-base alloy recommended for service in the temperature range of -65 to plus 600 F. It responds to an age-hardening heat treatment. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information
contactA fatigue and creep-rupture testing program was conducted on solution-treated and aged sheet specimens of titanium alloy B-120VCA at room and elevated temperatures. Data on aged bar stock, previously tested, are also included for comparison. All tests were conducted in axial-stress machines with various combinations of alternating and mean stresses.
contact23 · ERTi-6 is discontinued, 5Al-2.5Sn, Alloy A110AT. Please contact us to inquire. ... Ti 13V-11Cr-3Al is good for stuff too. Ti 8-1-1 Ti 8-1-1 (Ti-8Al-1Mo-1V) is designed for creep resistance up to 450°C, used primarily in engine applications such as forged compressor blades and disks. This alloy has a relatively high tensile modulus to density ...
contactThe Ti-6Al-4V alloy was only slightly embrittled, while the Ti-13V-11Cr-3Al alloy was severely embrittled. An investigation concerning the titanium-LOX reaction was conducted by using high-pressure gaseous O. The study established that a fresh Ti surface would react with gaseous O under about 100-psig pressure between -250 F and room temperature.
contact200091 · Alloys. Nickel. Also known as: SAE AMS 4633 ... Titanium Alloy Bars, Forgings and Forging Stock 13V - 11Cr - 3Al Solution Heat Treated and Aged. AMS6926C. View Details. STANDARD Aluminum Bronze, Centrifugal and Chill Castings 85Cu - 11Al - 3.6Fe Solution Heat Treated and Tempered.
contactMACHINABILITY OF Ti-13V-11Cr-3Al MATERIAL. Material Ti-13V-11Cr-3Al is a titanium alloy with a hardness of 40 HRC and a machinability rating of 15%. Titanium alloys such as Ti-13V-11Cr-3Al are used in mechanical components for two main reasons: It has an excellent strength-to-weight ratio. On the one hand, it is almost as light as aluminum, and ...
contactしたTi-13V-11Cr-3Al のにぼすとの 6 1 3 いほどでのにれている.650Kで300 ks したもは, さ2.05GPa, り4.1%に した.750Kで したものは, がせずの みがしている.
contact