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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.
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 ： ：
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
contact2 · Powder metallurgy (PM) α + β Ti-4Al-4Mo-4Sn-0.5Si alloys were fabricated through thermomechanical powder consolidation of TiH 2-based powder compacts with two different processing routes: one involving blending the elemental powders (BE route) and the other involving mechanical milling a blend of elemental powders (MM route).With the MM
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
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.
contactWorkhorse general purpose high strength alloy : Ti-6Al-2Sn-4Zr-2Mo (6-2-4-2) Creep and oxidation resistant engine alloy : Ti-6Al-2Sn-4Zr-6Mo (6-2-4-6) Creep and oxidation resistant engine alloy ... 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 ...
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).
contactEN 3351 EN 3351 Aerospace series - Titanium alloy Ti-4Al-4Mo-2Sn - Solution treated and aged - Forgings - De = 150 mm - This European Standard specifies the requirements relating to: ) Titanium alloy Ti-4Al-4Mo-2Sn Solution treated and aged Forgings De or = 150 mm for aerospace application.NOTE Other designation: WL: 3.7184 Only the chemical
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 ...
contact2 · Powder metallurgy (PM) α + β Ti-4Al-4Mo-4Sn-0.5Si alloys were fabricated through thermomechanical powder consolidation of TiH 2-based powder compacts with two different processing routes: one involving blending the elemental powders (BE route) and the other involving mechanical milling a blend of elemental powders (MM route).With the MM
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
contact2021513 · Long investigated the hot deformation behavior of Ti-6Cr-5Mo-5V-4Al alloy and found that DRX and DG occurred predominantly in the (α + β) phase zone, while ... Miaoquan, L. Deformation behavior of Ti–5Al–2Sn–2Zr–4Mo–4Cr alloy with two initial microstructures during hot working. Trans. Nonferrous Met. Soc. China 2016, 26, 414–422.
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 ...
contactAlloys Ti-5Al-2Sn-2Zr-4Mo-4Cr and Ti-6Al-2Sn-4Zr-6Mo are designed for strength in heavy sections. Alloys Ti- 6Al-2Sn-4Zr-2Mo and Ti-6Al-5Zr-0.5Mo-0.2Si for creep resistance. Alloys Ti-6Al-2Nb-1 Ta-1Mo and Ti-6Al-4V, for resistance to stress corrosion in aqueous salt solutions and for high fracture toughness.
contactWorkhorse general purpose high strength alloy : Ti-6Al-2Sn-4Zr-2Mo (6-2-4-2) Creep and oxidation resistant engine alloy : Ti-6Al-2Sn-4Zr-6Mo (6-2-4-6) Creep and oxidation resistant engine alloy ... 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 ...
contact2018514 · 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, forging alloy that was developed primarily for gas turbine engine components, such as disks for fan and compressor stages. Ti-17 has strength properties superior to those of Ti-6Al-4V, and ...
contact2 · Powder metallurgy (PM) α + β Ti-4Al-4Mo-4Sn-0.5Si alloys were fabricated through thermomechanical powder consolidation of TiH 2-based powder compacts with two different processing routes: one involving blending the elemental powders (BE route) and the other involving mechanical milling a blend of elemental powders (MM route).With the MM
contact2021513 · Long investigated the hot deformation behavior of Ti-6Cr-5Mo-5V-4Al alloy and found that DRX and DG occurred predominantly in the (α + β) phase zone, while ... Miaoquan, L. Deformation behavior of Ti–5Al–2Sn–2Zr–4Mo–4Cr alloy with two initial microstructures during hot working. Trans. Nonferrous Met. Soc. China 2016, 26, 414–422.
contactWorkhorse general purpose high strength alloy : Ti-6Al-2Sn-4Zr-2Mo (6-2-4-2) Creep and oxidation resistant engine alloy : Ti-6Al-2Sn-4Zr-6Mo (6-2-4-6) Creep and oxidation resistant engine alloy ... 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 ...
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-4Al-4Mo-2Sn-0.5Si 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
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 ...
contactTitanium alloys are widely used in industry, especially (α+β)-alloys, among which Ti-6Al-4V alloy is the most popular one. Another common alloy that often appears in patents for titanium products is Ti-4Al-3Mo-1V. Here, we investigate welded joints of (α+β)-alloy Ti-4Al-3Mo-1V obtained by friction stir welding (FSW) using a working tool made of nickel
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