Email: [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.
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
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
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
contact2022722 · TC17， ：Ti-17 ：Ti-5Al-2Sn-2Zr-4Mo-4Cr ： Al：4.5%~5.5% Mo：3.5%~4.5% Sn：1.5%~2.5% Zr：1.5%~2.5%
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
contact2018824 · high performance automotive engines. 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
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.
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 ...
contact201023 · Ti-5Al-4Mo-4Cr-2Zr-2Sn-1Nb TC15 Ti-5Al-2.5Fe TC16 Ti-3Al-5Mo-4.5V BT16 TC17 Ti-5Al-2Sn-2Zr-4Mo-4Cr TC18 Ti-5Al-4.75Mo-4.75V-1Cr-1Fe BT22 TC19 Ti-6Al-2Sn-4Zr-6Mo ...
contact2023120 · NOTE Other common designation: Ti550, AECMA: TI-P63, ASD-STAN: TI-P63001. SIST EN 3351:2014 - This European Standard specifies the requirements relating to: 1) Titanium alloy Ti-4Al-4Mo-2Sn Solution treated and aged Forgings De ≤ 150 mm for aerospace applications.
contact2023131 · Ti-17 Titanium Alloy, also known as Ti-5Al-2Sn-2Zr-4Cr-4Mo alloy (UNS R58650), is used as a high strength deep hardening alloy for compressor discs and other large components. Ti-17 Titanium Alloy is a ‘β-rich’ α-β type titanium alloy. This alloy has high strength, good fracture toughness, high hardenability, and wide forging temperature.
contactTitanium alloys can be divided into three main groups: corrosion resistant alloys, high strength alloys, and high temperature alloys. Titanium is a light metal (4.5 g/cm 3 ), strong and highly resistant to corrosion. Titanium is highly resistant to heat with a melting temperature as high as 1668°C; its melting point is higher than that of steel.
contact2013620 · Beta-phase titanium alloys are more ductile. The third category of alpha-beta-phase titanium alloys strikes a balance between the other two categories with its mechanical properties. Grade 6Al 6V 2Sn titanium alloy is an alpha-beta alloy that can be heat treated to higher strengths and heavier section sizes than titanium alloy 6AL-4V.
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
contactAbstract. Plates of a novel metastable β -Ti alloy Ti-4Mo-6Cr-3Al-2Sn (mass fraction,%) were solid solution treated at different temperatures for 0.5 h and subsequently aging treated at 400℃ for 4 h. Then the microstructure and room temperature tensile properties of the treated plates were examined by means of SEM, TEM and electronic ...
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
contact2020114 · The paper presents the analysis of hot deformation behavior of Ti-6Al-2Sn-4Zr-6Mo (Ti-6246) alloy using the theory of dynamic material modeling (DMM) based on hot compression tests performed to a total true strain of 1 at the strain rates from 0.01 to 100 s−1 and at the temperatures within the range between 800 and 1100 °C. The processing
contactEffects of cold rolling deformation and annealing temperature on texture and superelasticity of Ti-7.5Nb-4Mo-2Sn alloy CHEN Wang 1, SUN Hong-ji 1, GONG Lun-jun 1, ZHANG De-chuang 1,2, LIN Jian-guo 1,2 1. School of Materials Science and Engineering 2. ...
contactHighly creep-resistant, non-ageable, weldable, and high-strength Ti alloy for use up to 455°C exhibiting the lowest density and highest modulus of all commercial Ti alloys. Ti-6Al-2Sn-4Zr-2Mo-0.1Si [Ti-6-2-4-2-S] Weldable and high strength Ti alloy offering excellent strength, stability, and creep resistance to temperatures as high as 550°C.
contact2018514 · Ti-17 is a near beta, high strength alloy used primarily for gas turbine applications. Ti-5Al-2Sn-4Mo-2Zr-4Cr (Ti-17) is a high-strength, deep hardenable, forging alloy that was developed primarily for gas turbine engine components, such as disks for fan and compressor stages. Ti-17 has strength properties superior to those of Ti-6Al-4V, and ...
contactTitanium alloys can be divided into three main groups: corrosion resistant alloys, high strength alloys, and high temperature alloys. Titanium is a light metal (4.5 g/cm 3 ), strong and highly resistant to corrosion. Titanium is highly resistant to heat with a melting temperature as high as 1668°C; its melting point is higher than that of steel.
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;
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
contact2020101 · 1. Introduction. Due to their high specific strength, excellent fracture toughness, good creep and corrosion resistance, titanium alloys are widely used in aerospace applications [1, 2].Ti-5Al-2Sn-2Zr-4Mo-4Cr (Ti-17) as a high strength (can be heat treated to yield strength of 1030 to 1130 MPa), deep hardenable and high creep
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
contactTi-5Al-2Sn-4Mo-2Zr-4Cr is known as Ti-17 alloy and is a beta-rich material for large aerospace components. 5Al-2Sn-4Mo-2Zr-4Cr is an advanced engine alloy, creep and oxidation resistant. Ti-17 is a near beta, high strength alloy used primarily for gas turbine applications. Ti-5Al-2Sn-4Mo-2Zr-4Cr (Ti-17) is a high-strength, deep hardenable ...
contactTi-4Al-4Mo-2Sn, CSN, CSN EN 3351, Aerospace series. Titanium alloy Ti-4Al-4Mo-2Sn. Solution treated and aged. Forgings. De ≤ 150 mm, CSN EN 3459, Aerospace series - Titanium alloy TI-P63001 (Ti-4Al-4Mo-2Sn) - Solution treated and aged - Plate - 6 mm < a = 50 mm. The world’s most comprehensive materials database. ; Español;
contact2014101 · Ti-17 Ti-5Al-2Sn-2Zr-4Mo-4Cr 890 400 112 1050 1100-1250 8-15 30-80 Metastable β Titanium Alloys SP 700 Ti-4.5Al-3V-2Mo-2Fe 900 300-500 110 900 960 8-20 60-90
contactMost resistant Ti alloy to corrosion in reducing acids and localized attack in hot halide media, with physical, mechanical, formability properties equivalent to Gr. 1 Ti (soft grade) and excellent weldability. ... Ti-4Al-4Mo-2Sn-0.5Si [Ti-550] Heat-treatable, high strength forging alloy with good strength and creep resistance to temperatures as ...
contact