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Common 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).
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
contactFeatures: TIMETAL 551 has high strength and is creep resistant up to 400°C. It has a similar composition to TIMETAL 550, apart from an increase in tin content, which gives
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
contactTitanium Ti-4Al-4Mo-2Sn-0.5Si (IMI550), STA, Solution Treated 900ºC, Aged 500ºC. Alpha-Beta Alloy, medium strength. Applications: Aerospace - airframe and engine components.
contact201023 · ： ：86- ：(+86)018 ： ：
contact2018414 · are based on Ti-6Al-4V but should be equally applicable to other a+~ titanium alloys such as Ti-6Al-6V-2Sn and Ti-4Al-4Mo-2Sn-0.5Si. In the first part
contact2023322 · 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
contact2Cr, 0.25Si Ti-4Al-4Mo-2Sn-0.5Si 4 2 4 – 0.5Si β alloys Ti-10V-2Fe-3Al 3 – – ...
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). The following sections will discuss in detail about grade
contact2018414 · Ti-4Al-4Mo-2Sn-0.5Si (™I 550) L.B. Duffy* and N. Ridleyt tMaterials Science Centre University of Manchester/UMIST ... 0.5%Si (IMI 550)(6). This alloy has been shown to exhibit creep and elevated temperature tensile properties superior to those of Ti-6%Al-4% V(7). Published work on SPF of IMI 550
contactHeat treatable sheet alloy : 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 : Ti-6-6-2 : High strength alloy with specific earlier applications
contact201023 · ： ：86- ：(+86)018 ： ：
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).
contact2018414 · The Ti-4Al-4Mo-2Sn-o.5Si alloy (IMI 550) rolled plate (835 mm x 364 mm x 43 mm) was tested in the solution treated and aged condition (STA). The chemical analysis is given in Table 1. Table 1 Chemical Analysis Element Al Fe Mo Sn Si H2 N2 02 Percentage by 4.11 0.02 4.09 2.01 0.44 0.001 0.01 0.17 Weight
contact2023322 · 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
contact202011 · Legacy titanium alloys for elevated temperature jet engine applications include Ti-5Al-2Sn-2Zr-4Mo-4Cr, Ti-6Al-2Sn-4Zr-2Mo-0.1Si and Ti-4Al-4Mo-2Sn-0.5Si. Improving the mechanical behavior of ...
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 ...
contactHeat treatable sheet alloy : 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 : Ti-6-6-2 : High strength alloy with specific earlier applications
contact201023 · ： ：86- ：(+86)018 ： ：
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] ... (Grade 20) A Pd-containing version of the m, Bar*, 4Mo-0.05Pd Ti-38644 alloy Billet, [Ti Beta-C/Pd] (Beta
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 ...
contact2023322 · 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
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…
contact2017828 · Ti-4Al-4Mo-2Sn-0.5Si and Ti-6Al-4V are compared in Figure 1 and the specific elevated-temperature tensile properties in Figure 2, and it is evident that the Ti-4Al-4Mo-2Sn-0.5Si alloy represents a sub stantial improvement over Ti-6Al-4V. The service-temperature range
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 results in
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).
contactHeat treatable sheet alloy : 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 : Ti-6-6-2 : High strength alloy with specific earlier applications
contact2018717 · Titanium Alloys and their classification: There are several titanium alloys that have been developed for use in the past four decades. These alloys include Ti-6Al-4V (an alloy of titanium, aluminum and vanadium), the most highly used alloy of titanium and Ti-4Al-4Mo-2Sn-0.5Si (an alloy of titanium, aluminum, molybdenum, tin, and silicon), which
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