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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).
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
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
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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
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
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.
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
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
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).
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 ...
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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-2Zr-1Fe TA24 ...
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 ...
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
contactTherefore, the higher the strength of titanium alloys is, the greater the difference in yield strength is, and the more significant role the continuous α GB plays in reducing ductility. These findings are also successfully used to explain why continuous α GB leads to worse ductility in laser melting deposited Ti-5Al-5Mo-5V-1Cr-1Fe alloy ...
contactGeneral Information Machining Guidelines Equivalent Standards Chemical Composition Cutting Speeds Recommendation Recommended Carbide Grades Cutting Edge Geometry General Information for Material Ti-4Al-4Mo-2Sn-0.5Si Material Group S - Superalloys (Heat resistant and Titanium) Sub-Group Titanium alloy Hardness 35.0 HRC
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
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
contact200131 · Request PDF | Martensitic phase transformations in IMI 550 (Ti-4Al-4Mo-2Sn-0.5 Si) | The influence of solution-treatment temperature on the martensitic phase transformations observed in IMI 550 ...
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
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
contact2016926 · Heat 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: Ti-11Sn-5Zr-2.5Al-1Mo-0.2Si (679) Earlier engine alloy rarely specified in new programmes:
contact201553 · TC12 Ti-5Al-4Mo-4Cr-2Zr-2Sn-1Nb TC15(Ti-5Al-2.5Fe) Ti-5Al-2.5Fe TC16(BT16) Ti-3Al-5Mo-4.5V TC17(Ti-17) Ti-5Al-2Sn-2Zr-4Mo-4Cr ... TA5-A TI-4Al-0.005B (AL:3.7-4.5%,) TA6 (BT5) Ti-5Al TA7(Gr.7, BT5-1) Ti
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
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
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 ： ：
contact201553 · TC12 Ti-5Al-4Mo-4Cr-2Zr-2Sn-1Nb TC15(Ti-5Al-2.5Fe) Ti-5Al-2.5Fe TC16(BT16) Ti-3Al-5Mo-4.5V TC17(Ti-17) Ti-5Al-2Sn-2Zr-4Mo-4Cr ... TA5-A TI-4Al-0.005B (AL:3.7-4.5%,) TA6 (BT5) Ti-5Al TA7(Gr.7, BT5-1) Ti
contactVARIABLE AMPLITUDE FATIGUE CRACK GROWTH IN TITANIUM ALLOY Ti-4AI-4Mo-2Sn-0.5Si (IMI 550) by C.M.Ward-Close R.O.Ritchie ABSTRACT A study has been made of fatigue crack growth behaviour in the a/B titanium alloy Ti-4Ai-4Mo-2Sn-0.5Si (IMI 550), subject to single tensile overloads and the FALSTAFF fli,_t simulation loading spectrum.
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