E-mail: [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.
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 -
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).
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
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 ： ：
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
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 ),
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
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
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).
contactWorkhorse general purpose high strength alloy : Ti-6Al-2Sn-4Zr-2Mo (6-2-4-2) Creep and oxidation resistant engine alloy : Ti-6Al-2Sn-4Zr-6Mo (6-2-4-6) Creep and oxidation resistant engine alloy ... Ti-4Al-4Mo-2Sn (550) Higher strength heat treatable airframe and engine alloy : Ti-5.5Al-3.5Sn-3Zr-1Nb (829) Advanced engine alloy, creep and ...
contactTitanium alloys are widely used in industry, especially (α+β)-alloys, among which Ti-6Al-4V alloy is the most popular one. Another common alloy that often appears in patents for titanium products is Ti-4Al-3Mo-1V. Here, we investigate welded joints of (α+β)-alloy Ti-4Al-3Mo-1V obtained by friction stir welding (FSW) using a working tool made of nickel
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-6AL-4V 120 830 130 895 10 Ti-4AL-4Mo-1.5Sn 125 850 170 1160 10
contactAlloys Ti-5Al-2Sn-2Zr-4Mo-4Cr and Ti-6Al-2Sn-4Zr-6Mo are designed for strength in heavy sections. Alloys Ti- 6Al-2Sn-4Zr-2Mo and Ti-6Al-5Zr-0.5Mo-0.2Si for creep resistance. Alloys Ti-6Al-2Nb-1 Ta-1Mo and Ti-6Al-4V, for resistance to stress corrosion in aqueous salt solutions and for high fracture toughness.
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 ...
contact2017615 · 1,786 74 0.3 4.8 Aluminum Alloys 2024-T4 72 330 34 1.7 27.2 7075-T651 72 503 27 0.5 8.0 7039-T651 72 338 32 1.4 22.4 Titanium Alloys Ti-6AL-4V 108 1,020 50 0.4 6.4 Ti-4Al-4Mo-2Sn-05 Si 108 945 72 0.9 14.4
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
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
contact2014111 · Fig. 1 displays the XRD profiles of the as-cast and cold-rolled Ti–7.5Nb–4Mo–2Sn alloys. It can be seen that the as-cast alloy mainly contains β phases, evidenced by the XRD pattern in Fig. 1 (a). When the alloy was subjected to cold rolling, the peaks from α″ martensites appear on the XRD patterns of the alloys, implying that the
contactWe can provide Titanium Gr 5 Threaded Bars at Dealer price which helps us to prove one of the best Importer of Grade 1 Ti. Alloy Hex Bar in South Korea. Titanium Round Bar Specification in South Korea. Specifications: ASTM B348/ ASTM SB348: Dimensions: EN, DIN, JIS, ASTM, BS, ASME, AISI: Size: ... Ti-4Al-4Mo-2Sn – Ti-5-2.5Sn ELI:
contactWorkhorse general purpose high strength alloy : Ti-6Al-2Sn-4Zr-2Mo (6-2-4-2) Creep and oxidation resistant engine alloy : Ti-6Al-2Sn-4Zr-6Mo (6-2-4-6) Creep and oxidation resistant engine alloy ... Ti-4Al-4Mo-2Sn (550) Higher strength heat treatable airframe and engine alloy : Ti-5.5Al-3.5Sn-3Zr-1Nb (829) Advanced engine alloy, creep and ...
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
contact2017615 · 1,786 74 0.3 4.8 Aluminum Alloys 2024-T4 72 330 34 1.7 27.2 7075-T651 72 503 27 0.5 8.0 7039-T651 72 338 32 1.4 22.4 Titanium Alloys Ti-6AL-4V 108 1,020 50 0.4 6.4 Ti-4Al-4Mo-2Sn-05 Si 108 945 72 0.9 14.4
contactWe can provide Titanium Gr 5 Threaded Bars at Dealer price which helps us to prove one of the best Importer of Grade 1 Ti. Alloy Hex Bar in South Korea. Titanium Round Bar Specification in South Korea. Specifications: ASTM B348/ ASTM SB348: Dimensions: EN, DIN, JIS, ASTM, BS, ASME, AISI: Size: ... Ti-4Al-4Mo-2Sn – Ti-5-2.5Sn ELI:
contact2013130 · EN 3351:2012 - This European Standard specifies the requirements relating to: ) Titanium alloy Ti-4Al-4Mo-2Sn Solution treated and aged Forgings De < or = 150 mm for aerospace application. NOTE Other designation: WL: 3.7184 Only the chemical composition of this standard must be considered.
contactWorkhorse general purpose high strength alloy : Ti-6Al-2Sn-4Zr-2Mo (6-2-4-2) Creep and oxidation resistant engine alloy : Ti-6Al-2Sn-4Zr-6Mo (6-2-4-6) Creep and oxidation resistant engine alloy ... Ti-4Al-4Mo-2Sn (550) Higher strength heat treatable airframe and engine alloy : Ti-5.5Al-3.5Sn-3Zr-1Nb (829) Advanced engine alloy, creep and ...
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
contactIn sheet form, the alloy has good superplastic properties and excellent balance of strength and toughness.Typical heat treatment for this alloy: Solution heat treatment: 900°C for 1 hr per 25 mm section, air cool. Aging treatment: 500°C for 24 hrs, air cool.Data provided by TIMET. Physical Properties.
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% ： ：TA1,TA2,TA3,TA4,TA5 ...
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
contactStep-quenching of the titanium alloy Titanium alloy Ti-4Al-4Mo-2Sn-0.5Si (IMI 550) from 900° C into salt at temperatures in the range 445 to 600° C produced tensile strength increases of up to 15% compared with the conventional heat treatment. Material quenched to 500° C or below had a different microstructure from that produced either by quenching
contact