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Titanium Ti-4Al-4Mo-2Sn-0.5Si (IMI550), STA - MatWeb

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.

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Grade Ti-4Al-4Mo-2Sn-0.5Si Alloy -

201386 · 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).

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TIMETAL® Technical Data Sheets

TIMET TIMETAL® 3-2.5-0.05Pd Titanium Alloy. TIMET TIMETAL® 35A CP Titanium (ASTM Grade 1) TIMET TIMETAL® 367 (Ti-6Al-7Nb) Implant Grade Titanium Alloy. TIMET

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Ti–4Al–4Mo–2Sn - Titanium

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

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201493 · Ti-6Al-4V,TImetaL6-6-2(Ti-6Al-6V-2Sn),IMI550(Ti-4Al-4Mo-2Sn-0.5Si)。 GE90

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20191127 · 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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IN AIR AND -

2018414 · 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

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Ti-4Al-4Mo-2Sn-0.5Si-「」-

> 、 > > > Ti-4Al-4Mo-2Sn-0.5Si ,!

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201023 ·  : :86- :(+86)018 : :

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Total Materia -

201795 · Total Materia 、, 69 / 1000

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Sustaining an excellent strength-ductility combination of a

20221210 · Two samples of an α + β Ti-4Al-4Mo-4Sn-0.5Si (wt%) alloy, one with fine prior β grains and a heterogeneous microstructure and the other with coarse prior β grains and a homogeneous microstructure were prepared by extrusion of compacts of TiH 2 /Al/Mo/Sn/Si powder blend at 1200 and 1300 °C respectively. The heterogeneous

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Hierarchical microstructure and strain partition of a PM α

2023322 · 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

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Integ Metals | Titanium | Alpha-Beta

Ti-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.

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201493 · Ti-6Al-4V,TImetaL6-6-2(Ti-6Al-6V-2Sn),IMI550(Ti-4Al-4Mo-2Sn-0.5Si)。 GE90,,。

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Titanium For Aerospace Industries – Titanium

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

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Ti–4Al–4Mo–2Sn - Titanium

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 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).

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201023 ·  : :86- :(+86)018 : :

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IN AIR AND -

2018414 · 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

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STANDARDS FOR ALPHA-BETA TITANIUM ALLOYS

2018414 · 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 transverse microstructures (X200) of bar up to and including 100 mm diameter are presented together with proposed limits of acceptance

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Ti–4Al–4Mo–2Sn - Titanium and Special Metal Supply

Ti–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 ...

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Hierarchical microstructure and strain partition of a PM α

2023322 · 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

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A pathway to significantly improve the ductility of a high

202327 · An approach combing ball milling (BM) and thermomechanical consolidation of a TiH 2 based composite powder was used to fabricate powder metallurgy (PM) α+β Ti–4Al–4Mo–4Sn-0.5Si (wt%) alloy. Compared with the coarse-grained alloy with the same composition fabricated by the traditional blended elemental (BE-PM) method, the alloy

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Martensitic phase transformations in IMI 550 (Ti-4Al-4Mo

The 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

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Properties of Novel High Temperature Titanium Alloys for ...

202011 · 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 these alloys enables improved component performance, which is crucial to advancing jet engine performance. As a world leader in

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Titanium For Aerospace Industries – Titanium

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

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TC4【】 - ...

2018104 · TC4【】 /: ,,。 : 。

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Ti - 10V - 2Fe - 3Al - US Titanium Industry Inc.

Ti-4.5Al-3V-2Mo-2Fe & Ti-4Al-4Mo-2Sn-0.5Si September 26, 2016. Grade19; Grade20 September 26, 2016. Ti – 10V – 2Fe – 3Al. Ti-Technology. Titanium Alloy Mill Product Capabilities. Seawater General

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201553 · 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

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ALLOY INDEX

2018414 · Ti-2Al-12V-2Sn-6Zr, 535, 1567, 2339 Ti-2.5Al-115n-5Zr-1Mo-0.2Si, 2047, 2403 Ti-2.5Al-13V-75n-2Zr, 2339 Ti-3Al-2.5V, 563, 1119, 1181 Ti-3Al-3V-6Cr-4Mo-4Zr, 585, 717, 1605, 2533 Ti-3Al-9V-9Sn-3Zr, 2339 Ti-4/1.1, 2243 Ti-4Al-3Mo-1V, 625 Ti-4Al-4Mo

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Titanium metal and alloys for industries

2016926 · 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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Hierarchical microstructure and strain partition of a PM α

2023322 · 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

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Properties of Novel High Temperature Titanium Alloys for ...

202011 · 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 these alloys enables improved component performance, which is crucial to advancing jet engine performance. As a world leader in

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APPLICATIOB'S OF THE HIGH Sl'RENGTH ALLOY Ti-4Al

2017828 · 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

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Effect of micromorphology at the fatigue crack tip on the

2016825 · Request PDF | Effect of micromorphology at the fatigue crack tip on the crack growth in electron beam welded Ti-4Al-4Mo-2Sn-0.5Si joint | In this paper, we describe experiments on welded joints of ...

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Titanium For Aerospace Industries – Titanium

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

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201023 ·  : :86- :(+86)018 : :

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Ti–4Al–4Mo–2Sn - Titanium

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 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).

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Ti-4Al-4Mo-2Sn-0.5Si — BT19(Sn) — — 22 TC10 — TiAl6V4Sn2 — — — — — 23 TC11 — — — — BT11(Zr) — — ICP ...

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Ti-4Al-4Mo-2Sn-0.5Si TC11 TA9-1 ...

,Ti-4Al-4Mo-2Sn-0.5Si TC11 TA9-1 , 、、、、,!! ,,、24 ...

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Ti - 5Al - 2Zr - 2Sn - 4Mo - 4Cr - US Titanium

Ti-4.5Al-3V-2Mo-2Fe & Ti-4Al-4Mo-2Sn-0.5Si September 26, 2016. Ti – 5Al – 2Zr – 2Sn – 4Mo – 4Cr. Ti-Technology. Titanium Alloy Mill Product Capabilities. Seawater General Corrosion & Erosion. Commercial

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