Электронная почта: [email protected]
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.
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
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).
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
contact, Ti-4Al-2Sn-4Mo-0.5Si 、 Ti-11Sn-2.25Al-5Zr-1Mo-0.2Si(IMI879) 、 Ti-6Al-5Zr-0.5Mo-0.25Si(IMI685) ， IMI685 。
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
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).
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 ...
contact201023 · ： ：86- ：(+86)018 ： ：
contact1 · 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 +
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-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 ...
contact1 · 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 +
contact2018414 · Ti-4Al-4Mo-2Sn-0.5Si (™I 550) L.B. Duffy* and N. Ridleyt tMaterials Science Centre University of Manchester/UMIST Grosvenor Street, Manchester Ml 7HS, England *Magnesium Elektron Limited . Regal House, London Road Twickenham TWI 3QA, England Abstract .I The superplastic behaviour during uniaxial tensile deformation of
contact2018414 · (c) Ti-6Al-2Sn-4Zr-6Mo, heat-treated by air-cooling from 1143 Kand aging 8 hat 810 K. Superficially, the bonds on the Ti-6Al-4V and IMI-SSO were satisfactory. Some cracking occurred in the plate of Ti-6Al-2Sn-4Zr-6Mo, but du Pont personnel are confident that a slight modification in the technique would eliminate this feature.
contact