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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).
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
contact20191127 · Ti-6Al-2Sn-4Zr-2Mo-0.1Si TA20 Ti-4Al-3V-1.5Zr TA21 Ti-1Al-1Mn TA22 Ti-3Al-1Mo-1Ni-1Zr TA22-1 Ti-3Al-1Mo-1Ni-1Zr TA23 Ti-2.5Al-2Zr-1Fe TA23-1 Ti-2.5Al
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
contact201023 · ： ：86- ：(+86)018 ： ：
contactTi-6Al-4V TA6V BT6C YATB640E Grade24 19 TC4 TiAl6V4 TiAl6V4 Ti-6Al-4V TA6V BT6 YATB640 GradeF-5 20 TC6 — — — — BT3-1 — — 21 TC9 — TiAl4Mo4Sn2 Ti-4Al-4Mo
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
contactTi-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.
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).
contactTi-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 ... Ti-4Al-4Mo-4Sn-0.5Si (551) High strength airframe alloy, very limited availability : Ti-8Al-1Mo-1V (8-1-1) Early alloy now mainly for spares and replacements ...
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 ...
contactTi-6Al-4V TA6V BT6C YATB640E Grade24 19 TC4 TiAl6V4 TiAl6V4 Ti-6Al-4V TA6V BT6 YATB640 GradeF-5 20 TC6 — — — — BT3-1 — — 21 TC9 — TiAl4Mo4Sn2 Ti-4Al-4Mo-2Sn-0.5Si — BT19(Sn) — — 22 TC10 — TiAl6V4Sn2 — — — — — 23 TC11 ...
contact20151019 · Duffy et al. [9] observed that the elongationof Ti–4Al–4Mo–2Sn–0.5Si can reach 1500% at 900 ?C.A typical a + b-alloy consists of Ti–6.5Al–3.5Mo–1.5Zr–0.3Si,which is similar to the Russia alloy BT9, and now is used in com-pressor blades and discs in aero
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
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 ...
contactTi-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.
contact201023 · Ti-4Al-4Mo-2Sn-0.5Si [Ti-550] Ti-6Al-2Sn-2Zr-2Mo-2Cr-0.1 5Si [Ti-6-22-22] Ti-4.5Al-3V-2Mo-2Fe [SP-700] *Signifies products not currently produced by RTI, but commercially available. Legend for Typical Applications
contactTi-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 ... Ti-4Al-4Mo-4Sn-0.5Si (551) High strength airframe alloy, very limited availability : Ti-8Al-1Mo-1V (8-1-1) Early alloy now mainly for spares and replacements ...
contact199621 · This 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 ...
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 ...
contactTi-6Al-4V TA6V BT6C YATB640E Grade24 19 TC4 TiAl6V4 TiAl6V4 Ti-6Al-4V TA6V BT6 YATB640 GradeF-5 20 TC6 — — — — BT3-1 — — 21 TC9 — TiAl4Mo4Sn2 Ti-4Al-4Mo-2Sn-0.5Si — BT19(Sn) — — 22 TC10 — TiAl6V4Sn2 — — — — — 23 TC11 ...
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
contact20191031 · When molybdenum was introduced as β-stabilizer, the Ti-7Al-4Mo and Ti-4Al-4Mo-2Sn-0.5Si (IMI550) alloys were developed, this latter with a particular compositional focus on improving creep resistance. The IMI550 alloy, introduced in 1958, together with the notorious and most used Ti-6Al-4V (IMI318), became the state-of-the-art reference alloys ...
contact198541 · The superplastic deformation of titanium alloy Ti-4Al-4Mo-2Sn-0.5Si (IMI 550) (where the alloy composition is given in approximate weight per cent) ha…
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 ...
contactTi-4Al-4Mo-2Sn-0.5Si [Ti-550] Heat-treatable, high strength forging alloy with good strength and creep resistance to temperatures as high as 400°C. Ingot/Bloom, Bar*, Billet GT Ti-6Al-2Sn-2Zr-2Mo-2Cr-0.15Si [Ti-6-22-22] Heat-treatable, high strength Ti alloy with strength and fracture toughness-to-strength properties superior to those of Ti ...
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 Ti-4Al-4Mn and Ti-6Al-4V. In common with other alpha-beta titanium alloys satisfactory mechanical ...
contactTi-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 ... Ti-4Al-4Mo-4Sn-0.5Si (551) High strength airframe alloy, very limited availability : Ti-8Al-1Mo-1V (8-1-1) Early alloy now mainly for spares and replacements ...
contact201023 · Ti-4Al-4Mo-2Sn-0.5Si [Ti-550] Ti-6Al-2Sn-2Zr-2Mo-2Cr-0.1 5Si [Ti-6-22-22] Ti-4.5Al-3V-2Mo-2Fe [SP-700] *Signifies products not currently produced by RTI, but commercially available. Legend for Typical Applications
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 6-4 combined with good elevated temperature tensile and creep properties up to 750°F (400°C). This alloy has applications in the aerospace industry both as aero ...
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