Электронная почта: info@cjmetals.com.cn
20061125 · The α. + β type Ti–5Al–2Sn–2Zr–4Mo–4Cr (Ti-17) alloy, can be subjected to different thermal treatments of solution and aging.. During the solution treatment,
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
contact201441 · Dissimilar linear friction welding of Ti–5Al–2Sn–2Zr–4Mo–4Cr with bimodal and lamellar microstructures was produced. The microstructure evolution of the joint was
contact2020319 · Mechanical properties, such as residual stress, micro-hardness and fatigue performance, of the Ti-5Al-4Mo-4Cr-2Sn-2Zr titanium alloy were improved via the laser
contactCommon Name. Ti-5Al-2Zr-2Sn-4Mo-4Cr. UNS. R58650. General Information. This near-beta, high strength, deep hardenable forging alloy was developed primarily for gas
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
contact201023 · ： ：86- ：(+86)018 ： ：
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
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.
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
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
contactTi-5Al-2Sn-2Zr-4Mo-4Cr (Ti-17) as a high strength (can be heat treated to yield strength of 1030 to 1130MPa), deep hardenable and high creep resistance near β
contact2020918 · TC17 (Ti-5Al-2Sn-2Zr-4Mo-4Cr) with the size of 100 mm in length, 10 mm in width, and 40 mm in height. More detailed deposition processing can be found in our previous study [9] .
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
contactCommon Name. Ti-5Al-2Zr-2Sn-4Mo-4Cr. UNS. R58650. 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 ...
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.
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 ...
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.
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
contact2020918 · TC17 (Ti-5Al-2Sn-2Zr-4Mo-4Cr) with the size of 100 mm in length, 10 mm in width, and 40 mm in height. More detailed deposition processing can be found in our previous study [9] .
contact201721 · Semantic Scholar extracted view of "Ti-5Al-2Sn-2Zr-4Cr-4Mo（Ti-17）ののおよび" by et al. ... Static globularization kinetics for Ti-17 alloy with initial lamellar microstructure. Jianwei Xu, W. Zeng, Z. Jia, Xinnan Sun, Jianhua Zhou; Materials Science. 2014; 43. Save. Alert ...
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
contactCommon Name. Ti-5Al-2Zr-2Sn-4Mo-4Cr. UNS. R58650. 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 ...
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)
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-5Al-2Sn-4Mo-2Zr-4Cr is known as Ti-17 alloy and is a beta-rich material for large aerospace components. 5Al-2Sn-4Mo-2Zr-4Cr is an advanced engine alloy, creep and oxidation resistant. Ti-17 is a near beta, high strength alloy used primarily for gas turbine applications. Ti-5Al-2Sn-4Mo-2Zr-4Cr (Ti-17) is a high-strength, deep hardenable ...
contact201023 · ： ：86- ：(+86)018 ： ：
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
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
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
contactMicrostructural conversion mechanisms under hot forging process (at temperatures ranging from 750 °C to 1050 °C and strain rates ranging from 10–3 s–1 to 1 s–1) of a Ti-5Al-2Sn-2Zr-4Mo-4Cr (Ti-17) alloy with a lamellar starting microstructure were
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
contactCommon Name. Ti-5Al-2Zr-2Sn-4Mo-4Cr. UNS. R58650. 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 ...
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
contactTi-5Al-2Sn-4Mo-2Zr-4Cr is known as Ti-17 alloy and is a beta-rich material for large aerospace components. 5Al-2Sn-4Mo-2Zr-4Cr is an advanced engine alloy, creep and oxidation resistant. Ti-17 is a near beta, high strength alloy used primarily for gas turbine applications. Ti-5Al-2Sn-4Mo-2Zr-4Cr (Ti-17) is a high-strength, deep hardenable ...
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.
contactGleeble-1500DTi-6Al-3Nb-2Zr-1Mo,850~1050℃,0.010~1.000 s-1,60%;Q786.609 kJ·m-1,,;(OM)(TEM ...
contact