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).
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
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 ： ：
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
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
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
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.
contact201023 · Ti-4Al-0.005B TA6 Ti-5Al BT5 TA7（ELI ） Ti-5Al-2.5Sn A-1、GR6 BT5-1 KS115AS-C TiAl5Sn2.5 TA8（TA8-1） Ti-0.05Pd GR16（GR17） 17（18 ...
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).
contactTo obtain maximum creep resistance and stability in the near-α alloys Ti-8Al-1 Mo-1 V and Ti-6Al-2Sn-4Zr-2Mo, a duplex annealing treatment is employed. This treatment begins with solution annealing at a temperature high in the α-β range, usually 25 to 55°C (50 to 100°F) below the β transus for Ti-8Al-1Mo-1Vand 15 to 25°C (25 to 50°F ...
contactGraபைடு நூலகம்e12 Ti-0.3Mo-0.75Ni BT9 Ti-6.5Al-3.5Mo-0.3Si TC3 Ti-4Al-4V A-1 Ti-5Al-2.5Sn BT/4 Ti-5Al-3Mo-1.5V TC4 Ti-6Al-4V A-3 Ti-6Al-2Nb-1Ta BT16 Ti-2.8Al-5Mo-5V TC6 Ti-6Al-1.5Cr-2.5Mo-0.5Fe-0.3Si ...
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 6-4 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 ...
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
contact2018824 · 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 Aluminum 3.0 5.0 Molybdenum 3.0
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).
contactGraபைடு நூலகம்e12 Ti-0.3Mo-0.75Ni BT9 Ti-6.5Al-3.5Mo-0.3Si TC3 Ti-4Al-4V A-1 Ti-5Al-2.5Sn BT/4 Ti-5Al-3Mo-1.5V TC4 Ti-6Al-4V A-3 Ti-6Al-2Nb-1Ta BT16 Ti-2.8Al-5Mo-5V TC6 Ti-6Al-1.5Cr-2.5Mo-0.5Fe-0.3Si ...
contactTo obtain maximum creep resistance and stability in the near-α alloys Ti-8Al-1 Mo-1 V and Ti-6Al-2Sn-4Zr-2Mo, a duplex annealing treatment is employed. This treatment begins with solution annealing at a temperature high in the α-β range, usually 25 to 55°C (50 to 100°F) below the β transus for Ti-8Al-1Mo-1Vand 15 to 25°C (25 to 50°F ...
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
contactTitanium Alloy Mill Product Capabilities. Seawater General Corrosion & Erosion. Commercial Titanium Alloys. Basic Titanium Metallurgy. ... Ti-4.5Al-3V-2Mo-2Fe & Ti-4Al-4Mo-2Sn-0.5Si. Ti - 10V - 2Fe - 3Al. Grade19;
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
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
contact2018414 · 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 is extended by about 100 degC (18o degF) and this improvement is
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
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:
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