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Titanium Ti-4Al-4Mo-2Sn-0.5Si (IMI550), STA, Solution Treated 900ºC, Aged 500ºC. Alpha-Beta Alloy, medium strength. Applications: Aerospace - airframe and engine components.
contactThis Item presents constant amplitude data on the fatigue strength of the wrought titanium alloys Ti-6Al-6V-2Sn and Ti-4-Al-4Mo-2Sn-0.5Si, in both plain and notched specimen
contactTi-4Al-4Mo-2Sn-0.5Si Titanium Alloy has very limited weldability . ... Ti-4Al-4Mo-2Sn-0.5Si Titanium is not best suited to machining. The best results are achieved using slow
contact201386 · Grade Ti-4Al-4Mo-2Sn-0.5Si alloy is an alpha-beta alloy with medium strength. This alloy can be solution treated at 900ºC (1652°F) and aged 500ºC (932°F).
contactMechanical Property Data TIMET TIMETAL® 10-2-3 Titanium Alloy (Ti-10V-2Fe-3Al), Solution Treated and Aged 950°F (510°C), TIMET TIMETAL® 1100 Titanium Alloy (Ti
contactCommon Name; Ti–4Al–4Mo–2Sn: Ti-550: UNS; None assigned: General Information; Ti 550 is a high strength, forgeable alpha beta alloy. In the solution treated and aged
contact201023 · ： ：86- ：(+86)018 ： ：
contactMachining Material Ti-4Al-4Mo-2Sn-0.5Si. Material Ti-4Al-4Mo-2Sn-0.5Si is a titanium alloy with a hardness of 35 HRC and a machinability rating of 18%.. Titanium alloys such as Ti
contactTi–4Al–4Mo–2Sn. Ti 550 is a high strength, forgeable alpha beta alloy. In the solution treated and aged condition it has superior tensile and fatigue properties compared to Ti 6
contact1991111 · X-ray microdiffraction (XRμD) was used to characterize the surface layers of a-β-Ti alloys (Ti-6Al-4V, Ti-4Al-4Mo-2Sn, Ti-5Al-2Fe and Ti-4Al-2Mn) ion
contactAbstract. Plates of a novel metastable β -Ti alloy Ti-4Mo-6Cr-3Al-2Sn (mass fraction,%) were solid solution treated at different temperatures for 0.5 h and subsequently aging treated at 400℃ for 4 h. Then the microstructure and room temperature tensile properties of the treated plates were examined by means of SEM, TEM and electronic ...
contactTi-4Al-4Mo-2Sn-0.5Si Titanium Alloy has very limited weldability . ... Ti-4Al-4Mo-2Sn-0.5Si Titanium is not best suited to machining. The best results are achieved using slow speeds, accurate cooling flow and high feed rates. Contact us now for more info and pricing. Back to Top. Ti-6Al-2Sn-2Zr-2Mo-2Cr-0.15Si.
contact2017828 · Ti-4Al-4Mo-2Sn-0.5Si was developed in 1956 by Jessop-Saville Limited, in response to a demand from gas-turbine designers for an alloy with higher elevated-temperature properties than were then available from compositions such as
contactCommon Name; Ti–4Al–4Mo–2Sn: Ti-550: UNS; None assigned: General Information; Ti 550 is a high strength, forgeable alpha beta alloy. In the solution treated and aged condition it has superior tensile and fatigue properties compared to Ti 6-4 combined with good elevated temperature tensile and creep properties up to 750°F (400°C).
contact2013620 · Beta-phase titanium alloys are more ductile. The third category of alpha-beta-phase titanium alloys strikes a balance between the other two categories with its mechanical properties. Grade 6Al 6V 2Sn titanium alloy is an alpha-beta alloy that can be heat treated to higher strengths and heavier section sizes than titanium alloy 6AL-4V.
contact2022722 · TC17， ：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 ...
contactThis Item presents constant amplitude data on the fatigue strength of the wrought titanium alloys Ti-6Al-6V-2Sn and Ti-4-Al-4Mo-2Sn-0.5Si, in both plain and notched specimen form. The fatigue strength of these alloys is affected by the microstructure which is largely dependent upon the degree of working and heat treatment of the original bar ...
contact2020101 · 1. Introduction. Due to their high specific strength, excellent fracture toughness, good creep and corrosion resistance, titanium alloys are widely used in aerospace applications [1, 2].Ti-5Al-2Sn-2Zr-4Mo-4Cr (Ti-17) as a high strength (can be heat treated to yield strength of 1030 to 1130 MPa), deep hardenable and high creep
contact2018824 · high performance automotive engines. The alloy may be welded using controlled electron beam or laser welding techniques. Slow welding speeds and low cooling rates are necessary to achieve adequate weld properties. In sheet form, the alloy has good superplastic properties and excellent balance of strength and toughness. Ti-4Al-4Mo-2Sn
contactThe influence of solution-treatment temperature on the martensitic phase transformations observed in IMI 550 (Ti−4Al−4Mo−2Sn−0.5Si) has been investigated. When solution treatment is conducted at temperatures above 1233 K, a hexagonal martensite α′ is formed on rapid cooling. However solution treatment at temperatures between 1233 and 1123 K
contact2017828 · Ti-4Al-4Mo-2Sn-0.5Si was developed in 1956 by Jessop-Saville Limited, in response to a demand from gas-turbine designers for an alloy with higher elevated-temperature properties than were then available from compositions such as
contact2013620 · Beta-phase titanium alloys are more ductile. The third category of alpha-beta-phase titanium alloys strikes a balance between the other two categories with its mechanical properties. Grade 6Al 6V 2Sn titanium alloy is an alpha-beta alloy that can be heat treated to higher strengths and heavier section sizes than titanium alloy 6AL-4V.
contact201263 · to Titanium alpha-beta alloys to Properties of titanium alloys titanium_alpha-beta_alloy_ti-4al-4mo-2sn.txt · Last modified: 2012/06/03 by dmitri_kopeliovich Except where otherwise noted, this work is licensed under a Creative Commons Attribution-Noncommercial-Share Alike 3.0 License
contact2022722 · TC17， ：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 ...
contactThis Item presents constant amplitude data on the fatigue strength of the wrought titanium alloys Ti-6Al-6V-2Sn and Ti-4-Al-4Mo-2Sn-0.5Si, in both plain and notched specimen form. The fatigue strength of these alloys is affected by the microstructure which is largely dependent upon the degree of working and heat treatment of the original bar ...
contact2014101 · Ti-4Al-4Mo-2Sn 4.60 aged ... above 400℃ and have outstanding characteristics that enable their application in gas turbines for a compressor disc alloy. Ti-6Al-5Zr-0.5Mo-0.25Si is a typical ...
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-6AL-4V 120 830 130 895 10 Ti-4AL-4Mo-1.5Sn 125 850 170 1160 10
contactIn sheet form, the alloy has good superplastic properties and excellent balance of strength and toughness.Typical heat treatment for this alloy: Solution heat treatment: 900°C for 1 hr per 25 mm section, air cool. Aging treatment: 500°C for 24 hrs, air cool.Data provided by TIMET. Physical Properties.
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.
contact201495 · TiC particles and equiaxed Ti 5 Si 3 C 1−x phase, while, in the layer close to the substrate, dendritic TiC phase and eutectic phases of Ti 3 SiC 2 +βTi form. The hardness of the top layer is up to 1262HV 0.2， which is
contact201582 · for elevated temperature’s (350–400°C) application. IMI 550 (Ti-4Al-2Sn-4Mo-0.5Si) and especially Ti-6Al-4V.which is one of the most commonly used titanium alloys in industry belong to this group [8]. During machining these alloys metallurgy influences the some properties as per many researchers observation at very high-speed dry
contact201263 · to Titanium alpha-beta alloys to Properties of titanium alloys titanium_alpha-beta_alloy_ti-4al-4mo-2sn.txt · Last modified: 2012/06/03 by dmitri_kopeliovich Except where otherwise noted, this work is licensed under a Creative Commons Attribution-Noncommercial-Share Alike 3.0 License
contact2020114 · The hot deformation behavior of a novel near-beta titanium alloy Ti-5.5Mo-6V-7Cr-4Al-2Sn-1Fe in (α+β) phase region in the temperature of 605~755°C and strain rate range of 10−3~10−1/s−1 was investigated on the Gleeble-3800 thermo-mechanical simulator. The results showed that the deformation parameters can have a significant
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