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2015215 · The Ti–5Al–2Sn–2Zr–4Mo–4Cr shows pronounced change in microstructure following compression at different conditions (Fig. 2) comparing to the as
contact202078 · The high-speed finish turning tests of Ti-17 titanium alloy (Ti-5Al-2Sn-2Zr-4Mo-4Cr) were carried out by using PVD cemented carbide tools with TiAlN coating. The
contact2015215 · Journal of Alloys and Compounds. Volume 622, 15 February 2015, Pages 174-183, 15 February 2015, Pages 174-183
contact201211 · ATI Ti-5Al-2Sn-2Zr-4Cr-4Mo is known as Ti-17 alloy and is a beta-rich material for large aerospace components. This datasheet provides information on
contact2020227 · ATI Ti-5Al-2Sn-2Zr-4Cr-4Mo Alloy (UNS R58650), also known as Ti-17, was developed by General Electric as a high strength, deep hardening alloy for fan and
contact2013730 · Grade Ti 5AI 2Sn 2Zr 4Mo 4Cr alloy is an alpha-beta wrought alloy that has high tensile strength, good fracture toughness, and good crack growth/fatigue
contact201553 · TC17(Ti-17) Ti-5Al-2Sn-2Zr-4Mo-4Cr TC18(BT22) Ti-5Al-5Mo-5V-1Cr-1Fe TC19(Ti-6246) Ti-6Al-2Sn-4Zr-6Mo TC20(IMI367) Ti-6Al-7Nb TC21(Ti-62222S) Ti-6Al
contact2016129 · Ti−5Al−2Sn−2Zr−4Mo−4Cr alloy (a “β-rich” α+β titanium alloy) is characterized by high strength, excellent corrosion resistance, superior fracture
contact20211021 · The microstructure evolution characteristics and the shear strength of bond and base alloys were investigated during the press bonding of the Ti–5Al–2Sn–2Zr–4Mo–4Cr alloy. The quantitative detection of the interfacial void shows that the interfacial voids shrunk gradually with time and a bond free of voids could be
contact202078 · The high-speed finish turning tests of Ti-17 titanium alloy (Ti-5Al-2Sn-2Zr-4Mo-4Cr) were carried out by using PVD cemented carbide tools with TiAlN coating. The machinability behaviors in terms of cutting forces, cutting temperatures, surface roughness, and tool service life were measured and evaluated under different machining parameter
contactWe investigated the oxidation and nitridation of a near β-type Ti-17 (Ti-5Al-2Sn-2Zr-4Mo-4Cr) alloy with up to 1 mass% of added Si.The alloys were heated in air at 923–1223 K for up to 518.4 ks. The mass gain was determined, and the scales and oxygen-rich α-case layer that were formed were analyzed.At temperatures below 1123 K, the primary product was
contact2010218 · The microstructural evolution, microhardness, tensile properties and impact toughness of Ti-5Al-2Sn-2Zr-4Mo-4Cr (Ti17) alloy joints welded by linear friction welding (LFW) are investigated. A narrow, sound weld is formed, consisting of a superfine α + β structure in the weld center.
contactTi-5Al-2Sn-2Zr-4Mo-4Cr , 2015,25(9),2893-2900 ,DOI:, ISSN:1003-6326 132. , 1997,14(4),1 ,DOI:, ISSN:1000-4939 133.
contactR58650. General Information. This near-beta, high strength, deep hardenable forging alloy was developed primarily for gas turbine applications such as discs for fan and compressor stages. In addition to offering superior strength properties over Ti-6Al-4V, the alloy also provides higher creep resistance in the intermediate temperature ranges.
contact2023131 · Ti-17 Titanium Alloy, also known as Ti-5Al-2Sn-2Zr-4Cr-4Mo alloy (UNS R58650), is used as a high strength deep hardening alloy for compressor discs and other large components. Ti-17 Titanium Alloy is a ‘β-rich’ α-β type titanium alloy. This alloy has high strength, good fracture toughness, high hardenability, and wide forging temperature.
contactTi 15Mo 2.7Nb 3Al 0.2Si(Beta21S) b 12.8 3 4.93 ナセル，プラグ，エンジンノズル エンジン Ti 5Al 2Sn 2Zr 4Mo 4Cr(Ti 17)ニアb 5.4 6.0 4.65 ファンディスク，コンプレッサーディスク (MUT: 673 K)
contactTitanium alloys have been used not only in air frames for commercial aircrafts, but also in its jet engine components such as fans and compressor disks, which have a function at relatively low temperatures up to 673 K. Near β-type Ti-5Al-2Sn-2Zr-4Cr-4Mo (Ti-17) exhibits greater strength, crack propagation resistance, and creep resistance at intermediate
contact201553 · TC17(Ti-17) Ti-5Al-2Sn-2Zr-4Mo-4Cr TC18(BT22) Ti-5Al-5Mo-5V-1Cr-1Fe TC19(Ti-6246) Ti-6Al-2Sn-4Zr-6Mo TC20(IMI367) Ti-6Al-7Nb TC21(Ti-62222S) Ti-6Al-2Zr-2Mo-2Sn-2Cr-0.25Si —αα TA4 Ti-3Al
contact2019411 · TC17 (Ti–5Al–2Sn–2Zr–4Mo–4Cr) is a dual-phase (α + β) titanium alloy that is rich in β-stabilizing elements. Owing to a series of advantages, such as high strength, good fracture toughness, high
contact2015621 · The true stress-strain relationships of Ti-5Al-2Sn-2Zr-4Mo-4Cr(TC17) alloy with a wide range of strain rates were investigated by uniaxial quasi-static and dynamic compression tests, respectively. Quasistatic compression tests were carried out with Instron 8874 test machine, while dynamic compression tests were performed with the split
contact20131112 · The effect of process variables on flow response and microstructure evolution during hot working of Ti-17 (Ti–5Al–2Sn–2Zr–4Mo–4Cr) alloy with lamellar microstructure was established using isothermal hot compression tests at strain rates of 0·001–10 s −1, test temperature between 780 and 860°C, and height reductions of
contactR58650. General Information. This near-beta, high strength, deep hardenable forging alloy was developed primarily for gas turbine applications such as discs for fan and compressor stages. In addition to offering superior strength properties over Ti-6Al-4V, the alloy also provides higher creep resistance in the intermediate temperature ranges.
contactZ.L. Zhao, h.z. guo, z.k. yao. microstructure and properties of ti-17 powder compact prepared through powder sintering and isothermal forging, powder metallurgy, 2012, 55: 368~373 (sci、ei) Z.L. Zhao, h.z. guo, x.c. wang, z.k. yao. deformation behavior of isothermally forged ti-5al-2sn-2zr-4mo-4cr powder compact. journal of materials
contactIn this paper, the microstructure and hardness of Ti-5Al-2Sn-2Zr-4Mo-4Cr titanium alloy with and without laser shock peening (LSP) were examined and compared. The titanium alloy samples were laser shock peened with
contact2022820 · ：Ti−5Al−2Sn−2Zr−4Mo−4Cr 4. Wire-based Laser Metal Deposition for Additive Manufacturing of TiA16V4: Basic Investigations of Microstructure and Mechanical Properties from Build-up
contactFor alpha-beta alloys, the cooling such as Ti-6Al-2Sn-4Zr-6Mo Quench delay, s cooled rate has an important effect on and Ti-5Al-2Sn-2Zr-4Mo-4Cr, strength. Appreciable diffusion can in which fan or air cooling develops Fig. 3 — Effect of quench delay on the tensile occur if the rate is too low, affecting properties of Ti-6Al-4V alpha-beta alloy.
contact2022722 · ：Ti-17 ：Ti-5Al-2Sn-2Zr-4Mo-4Cr ： Al：4.5%~5.5% Mo：3.5%~4.5% Sn：1.5%~2.5% Zr：1.5%~2.5% ： ：TA1,TA2,TA3,TA4,TA5,TA6,TA8,TA9,TA10,TA15(BT20),TA18,TB5(Ti ...
contact2020227 · ATI Ti-5Al-2Sn-2Zr-4Cr-4Mo Alloy (UNS R58650), also known as Ti-17, was developed by General Electric as a high strength, deep hardening alloy for fan and compressor discs and for other large components. It has been classified as a “beta-rich” alpha-beta alloy. The alloy may be processed in the beta region, or in the alpha plus beta
contact201791 · The microstructural evolution and special flow behavior of Ti-5Al-2Sn-2Zr-4Mo-4Cr during isothermal compression at a strain rate of 0.0001 s −1 were investigated. The dislocation climbs in elongated α grains resulted in the formation of low-angle boundaries that transform into high-angle boundaries with greater deformation, and the
contact2023210 · Wire arc additive manufacture (WAAM) technology was employed to repair Ti–5Al–2Sn–2Zr–4Mo–4Cr (TC17) titanium alloy, which is widely used as compressor blades and blisk. The microstructure evolution and mechanical properties of the repaired specimen were investigated.
contact2015621 · The true stress-strain relationships of Ti-5Al-2Sn-2Zr-4Mo-4Cr(TC17) alloy with a wide range of strain rates were investigated by uniaxial quasi-static and dynamic compression tests, respectively. Quasistatic compression tests were carried out with Instron 8874 test machine, while dynamic compression tests were performed with the split
contactTi-5Al-2Sn-2Zr-4Mo-4Cr , 2015,25(9),2893-2900 ,DOI:, ISSN:1003-6326 132. , 1997,14(4),1 ,DOI:, ISSN:1000-4939 133.
contact201775 · Ti-5Al-2Sn-2Zr-4Mo-4Cr titanium alloy was nanocrystallized with supersonic fine particles bombarding (SFPB). The microstructure features of nanocrystalline layer were determined by XRD, TEM, and microhardness tester. The electrochemical corrosion properties of the surface of original sample and the nanocrystallized sample surface were
contactStatic Globularization and Grain Growth Behavior of Ti-5Al-2Sn-2Zr-4Cr-4Mo（Ti-17） Alloy Under Static Heat Treatment Process Gen Yamane* and Hiroaki Matsumoto Department of Advanced Materials Science, Faculty of Engineering, Kagawa University
contactR58650. General Information. This near-beta, high strength, deep hardenable forging alloy was developed primarily for gas turbine applications such as discs for fan and compressor stages. In addition to offering superior strength properties over Ti-6Al-4V, the alloy also provides higher creep resistance in the intermediate temperature ranges.
contactIn this paper, the microstructure and hardness of Ti-5Al-2Sn-2Zr-4Mo-4Cr titanium alloy with and without laser shock peening (LSP) were examined and compared. The titanium alloy samples were laser shock peened with
contactIn this study, the temperature increase of the Ti-17 alloy (Ti–5Al–2Sn–2Zr–4Cr–4Mo, wt.%) during isothermal forging in the (α + β) dual-phase region was investigated using large-size workpieces forged between hot dies in a 1500-ton forging press. The temperature increase was predicted using finite element analysis (FEA). The tip of a thermocouple was
contact2022722 · ：Ti-17 ：Ti-5Al-2Sn-2Zr-4Mo-4Cr ： Al：4.5%~5.5% Mo：3.5%~4.5% Sn：1.5%~2.5% Zr：1.5%~2.5% ： ：TA1,TA2,TA3,TA4,TA5,TA6,TA8,TA9,TA10,TA15(BT20),TA18,TB5(Ti ...
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