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200291 · In the present study, an internal fatigue crack initiation (IFCI) phenomenon in metastable beta Ti–15V–3Cr–3Al–3Sn (Ti–15–3) alloys with various heat treatment
contact2018824 · production alloy that is currently used for critical applications on air and space vehicles. TIMETAL 15-3is usually acceptable for use at temperatures up to 550°F
contact202323 · Ti-15-3. Ti-15V-3Cr-3Sn-3Al. 290. ≥ 1080. With excellent cold forming properties, it can form medium and complex sheet metal parts at room temperature. It can also be superplastic in the above 700
contactWeight Calculator. Titanium Grade 15V-3Cr-3Al-3Sn | UNS# R58153 is a beta Titanium alloy that allows for strip-rolling and is heat-treatable. Highly formable, 15V-3Cr-3Al-3Sn has
contact： This investigation is aimed at revealing the deformation behavior of a β-Ti alloy, namely Ti-15V-3Cr-3Sn-3Al, under various aged conditions with an emphasis on
contactTi-15V-3Cr-3Sn-3Al alloy is mainly used to manufacture various sheet metal components, as well as fasteners. It can meet the requirements of high structural efficiency, high
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
contactIn a Ti-15V-3Cr-3Sn-3Al alloy, the internal structure of {332} deformation twins formed by weak rolling at 77 K was studied by means of transmission electron microscopy. {332}
contact2020622 · Machining chips of Ti-15V-3Cr-3Al-3Sn metastable beta titanium alloy were consolidated using back pressure-assisted equal-channel angular pressing (BP
contact202118 · In this study, the effects of various heat treatment procedures on the mechanical properties of the Ti-15V-3Al-3Sn-3Cr metastable β titanium alloy were investigated. Single-step and duplex aging treatments were applied to the alloy at low and high aging temperatures. Duplex aging treatments were carried out by selecting two
contact2020622 · Machining chips of Ti-15V-3Cr-3Al-3Sn metastable beta titanium alloy were consolidated using back pressure-assisted equal-channel angular pressing (BP-ECAP) using different processing conditions. Near fully dense specimens were obtained after multiple passes done at 500 °C with the aid of different back pressures. SEM and TEM
contact2020815 · 1. Introduction. The Ti–15V–3Cr–3Sn–3Al (Ti-15-3) alloy is a typical metastable β-type titanium alloy developed in the 1980’s and has been widely used in the aerospace field due to its high specific strength, excellent corrosion resistance and cold formability [1, 2].Although the cold formability and workability of the β-type titanium alloys
contact201991 · In the present work, a β-Ti alloy (Ti–15V–3Sn–3Cr–3Al) was unidirectionally cold rolled to 80% thickness reduction, followed by recrystallization at two temperatures: (i) 1013 K and (ii) 1053 K. The microstructural developments were studied using light optical microscopy, scanning electron microscopy X-ray peak profile analysis, and electron
contact201927 · Ti–15V–3Cr–3Sn–3Al (Ti–15–3) is a metastable β titanium alloy and is used in lightweight structures and gas storage tanks for aerospace applications. Tensile properties and fracture toughness (FT) of material are the significant inputs to the designer for finite-element analysis of structures. Fracture toughness data for Ti–15–3 alloy in different heat
contact2014825 · This paper presents the age hardening behavior of metastable beta titanium alloy Ti–15 V–3Cr–3Al–3Sn subjected to various single and duplex aging treatments.Single aging was carried out in the range 200–550 °C for times up to 150 h (h).For duplex aging first step was performed in two different ways: (i) 250 °C for 24 h (ii)
contact1996815 · Using a Ti 15V 3Cr 3Sn 3Al alloy, the process of (α + β) microstructure development was studied in heavily cold rolled (by 80%) and aged specimens and in specimens which were rolled, recovered and aged.By aging after 80% cold rolling, α phase precipitates on dislocations introduced by deformation at all aging temperatures were
contactWeight Calculator. Titanium Grade 15V-3Cr-3Al-3Sn | UNS# R58153 is a beta Titanium alloy that allows for strip-rolling and is heat-treatable. Highly formable, 15V-3Cr-3Al-3Sn has decent room temperature bending properties and solution treatment of this alloy enhances strength. This alloy is primarily found in aircraft ducting, pressure vessels ...
contact202323 · Ti-15-3. Ti-15V-3Cr-3Sn-3Al. 290. ≥ 1080. With excellent cold forming properties, it can form medium and complex sheet metal parts at room temperature. It can also be superplastic in the above 700
contact2019718 · For Ti–15V–3Sn–3Cr–3Al alloy, very few studies have been conducted on the development of deformation and recrystallization texture and its mechanism. This alloy has a potential to be used in the aerospace industries in sheet form (as fire extinguisher tank and ducting system material) [Reference Boyer 3]. It is ductile and can be cold ...
contactWeight Calculator. Titanium Grade 15V-3Cr-3Al-3Sn | UNS# R58153 is a beta Titanium alloy that allows for strip-rolling and is heat-treatable. Highly formable, 15V-3Cr-3Al-3Sn has decent room temperature bending properties and solution treatment of this alloy enhances strength. This alloy is primarily found in aircraft ducting, pressure vessels ...
contact： This investigation is aimed at revealing the deformation behavior of a β-Ti alloy, namely Ti-15V-3Cr-3Sn-3Al, under various aged conditions with an emphasis on correlating the work hardening characteristics of the alloy with its corresponding microstructure.
contactCross-ply laminate behavior of Ti-15V-3Cr-3Al-3Sn (Ti-15-3) matrix reinforced with continuous silicon-carbide fibers (SCS-6) subjected to a generic hypersonic flight profile was evaluated experimentally and analytically. Thermomechanical fatigue (TMF) test techniques were developed to conduct a simulation of a generic hypersonic flight profile. A
contact2017227 · Ti‐15V‐3Cr‐3Sn‐3Al ＊ 2.5－3.5 14.0－16.0 2.5－3.5 2.5－3.5 ≦0.25 ≦0.13 ≦0.05 ≦0.05 ST STA 689 965 703 1100 12 7 AMS4914 Super-TIX ...
contactTi-15V-3Cr-3Sn-3Al (15-3-3-3) High strength heat treatable beta sheet alloy : Ti-3Al-2.5V : Medium strength alloy used for hydraulic tubing : Ti-4Al-4Mo-2Sn (550) Higher strength heat treatable airframe and engine alloy : Ti-5.5Al-3.5Sn-3Zr-1Nb (829) Advanced engine alloy, creep and oxidation resistant ...
contact2022820 · This paper highlight the results of recent efforts to develop mechanistically based, fracture mechanics models, for the prediction of the total fatigue life in Ti-15V-3Cr-3Al-3Sn (Ti-15-3). Acoustic
contactThe scope of this study is the investigation of the effect of microstructure on fatigue behavior of Ti-15V-3Al-3Sn-3Cr (Ti 15–3) metastable beta titanium alloy. Aging treatment was applied to Ti 15–3 alloy at low and high aging temperatures. The fatigue crack initiation and propagation behavior of the alloy was determined by applying fatigue crack propagation
contact202171 · Abstract. CarTech Ti 15V-3Cr-3Sn-3Al (UNS R58153) is a metastable beta titanium alloy that offers substantial weight reduction in comparison with other engineering materials. If used in the solution heat treated condition, the alloy has excellent cold formability. In the aged condition, the alloy has high strength. It is acceptable for use up
contactIn a Ti-15V-3Cr-3Sn-3Al alloy, the internal structure of {332}〈113〉 deformation twins formed by weak rolling at 77 K was studied by means of transmission electron microscopy. {332}〈113〉 deformation twins accompany very characteristic dislocation loops attached to the twin/matrix interface in the matrix. Inside the twin, a parallel array ...
contactTi-15Vl-3Cr-2Sn-3Al is a meta stable β alloy which may be easily strip cast and cold rolled into strips. The β transus for this alloy is about 760 °C and the ingot break-down step is done in the β phase field. From: Hot Working Guide: A Compendium of Processing Maps, Second Edition. Publisher: ASM International. Published: 2015.
contactTi-15-3, a shortened designation for Ti-15V-3Cr-3Al-3Sn, is a metastable beta alloy, primarily used where cold formability and high strength are desired. Ti 15-3-3-3 is usually acceptable for use at temperatures up to 550°F (288°C). The original concept was to develop an economical sheet titanium alloy that could be fabricated by cold-forming ...
contact： This investigation is aimed at revealing the deformation behavior of a β-Ti alloy, namely Ti-15V-3Cr-3Sn-3Al, under various aged conditions with an emphasis on correlating the work hardening characteristics of the alloy with its corresponding microstructure.
contactCross-ply laminate behavior of Ti-15V-3Cr-3Al-3Sn (Ti-15-3) matrix reinforced with continuous silicon-carbide fibers (SCS-6) subjected to a generic hypersonic flight profile was evaluated experimentally and analytically. Thermomechanical fatigue (TMF) test techniques were developed to conduct a simulation of a generic hypersonic flight profile. A
contact2020728 · 20 70 ， Ti-13V-11Cr-3Al ， 70%。 ，、 β 、， Ti-15V-3Cr-3Al-3Sn Ti-3Al-8V-6Cr-4Mo-4Zr（β-C），104 GPa， ...
contactTitanium Alloys. Ti-6Al-4V. Ti-6Al-4V Sheet/Plate; Ti-6Al-4V Rod/Bar; Ti-6Al-4V Wire; Ti-5Al-2.5Sn. Ti-5Al-2.5Sn Sheet/Plate; Ti-5Al-2.5Sn Rod/Bar; Ti-5Al-2.5Sn Tube/Pipe; ... Home » Titanium Alloys » Ti-15V-3Cr-3Sn-3Al » Ti-15V-3Cr-3Sn-3Al Rod/Bar. FORMS WE CAN PROVIDE. Ti 15-3-3-3 Sheet/Plate. Ti 15-3-3-3 Rod/Bar. Request A Quote ...
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