ti-4al-4mo-2sn alloy in americas

Common raw materials

Forging display

CNC processing

TIMETAL® Technical Data Sheets

TIMET TIMETAL® 550 (Ti-4Al-4Mo-2Sn) Titanium Alloy Solution Treated; TIMET TIMETAL® 550 (Ti-4Al-4Mo-2Sn) Titanium Alloy Solution Treated and Aged; TIMET

contact

TIMETAL® 407Titanium Grade 5 Sheet | Grade 2, Grade 3, Grade 4, GradeTimetal® 407: A Titanium Alloy to Enable Cost Reduction - R…Timet - TIMET HomeAll Ti Metals - A Premier Titanium Supplier•

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.

contact

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

201386 · Introduction. 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

contact
:1

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

contact

201023 ·  : :86- :(+86)018 : :

contact

_

20191127 · Ti-13Nb-13Zr ①GB/T 3620.1-2007《 》。 ,TA0~TA3TA1~TA4,ISO

contact

Material Ti-4Al-4Mo-2Sn-0.5Si : Machinig Data Sheet

Machining 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

contact

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

contact

TI–4AL–4MO–2SN – Titanium

Email Us . Call Us +65 – 6853 7424. Home; About Us; Our Products ... Ti–4Al–4Mo–2Sn : Ti-550 : UNS : None assigned : General Information : Ti 550 is a

contact

Titanium Alloys, Titanium 6AL-4V, CP (Commercially Pure)

2018514 · 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

contact

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

contact
[PDF]

HIGH-STRENGTH FORGING ALLOY - Timet

2018824 · 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

contact

FATIGUE DESIGN DATA FOR THE TITANIUM ALLOY, Ti--6Al

This 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 ...

contact

Features of Permanent Joints of Titanium

Titanium 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

contact

Titanium For Aerospace Industries – Titanium

Workhorse 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 ...

contact

Ti-4Al-4Mo-2Sn, CSN :: Total Materia

Ti-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;

contact
[PDF]

APPLICATION'S OF THE HIGH STRENGTH ALLOY Ti-4Al

2018414 · 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

contact

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).

contact

Material Ti-4Al-4Mo-2Sn-0.5Si : Machinig Data Sheet

Machining 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

contact

Grade 6Al 6V 2Sn Titanium Alloy (UNS 56620) -

2013620 · 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.

contact

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

contact

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

contact

Mechanical properties of titanium castings. [Ti-6Al-4V; Ti

This 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 ...

contact

EN 3351:2012 - Aerospace series - Titanium alloy Ti-4Al

2013130 · 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.

contact
: 4

β Ti-4Mo-6Cr-3Al-2Sn ...

20191018 · : βTi-4Mo-6Cr-3Al-2Sn(%,),。:α,α,β。

contact

Titanium For Aerospace Industries – Titanium

Workhorse 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 ...

contact
[PDF]

APPLICATION'S OF THE HIGH STRENGTH ALLOY Ti-4Al

2018414 · 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

contact

Material Ti-4Al-4Mo-2Sn-0.5Si : Machinig Data Sheet

Machining 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

contact

:|||_

2021109 · 、,,,50%,、、、,。. 40

contact

TC17,Ti-17,Ti-5Al-2Sn-2Zr-4Mo-4Cr -

2022722 · 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 ...

contact

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

contact

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

contact

Surface phase definition by microdiffractometry in ion

1991111 · X-ray microdiffraction (XRμD) was used to characterize the surface layers of a-β-Ti alloys (Ti-6Al-4V, Ti-4Al-4Mo-2Sn, Ti-5Al-2Fe and Ti-4Al-2Mn) ion

contact

Hot Deformation Behavior of a Novel Near-β Titanium

2020114 · The hot deformation behavior of a novel near-beta titanium alloy Ti-5.5Mo-6V-7Cr-4Al-2Sn-1Fe in (α+β) phase region in the temperature of 605~755°C and strain rate range of 10−3~10−1/s−1 was investigated on the Gleeble-3800 thermo-mechanical simulator. The results showed that the deformation parameters can have a significant

contact

Titanium For Aerospace Industries – Titanium

Workhorse 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 ...

contact

BS EN 3351:2012 AEROSPACE SERIES - TITANIUM ALLOY

201211 · Buy BS EN 3351:2012 AEROSPACE SERIES - TITANIUM ALLOY TI-4AL-4MO-2SN - SOLUTION TREATED AND AGED - FORGINGS - D[E] <= 150 MM from SAI Global

contact

Analysis of the Oxidation and Nitridation of Ti-17 (Ti-5Al

We investigated the oxidation and nitridation of a near β-type Ti-17 (Ti-5Al-2Sn-2Zr-4Mo-4Cr) alloy with up to 1 mass% of added Si.The alloys were heated in air at 923–1223 K for up to 518.4 ks. The mass gain was determined, and the scales and oxygen-rich α-case layer that were formed were analyzed.At temperatures below 1123 K, the primary product was

contact

Material Ti-4Al-4Mo-2Sn-0.5Si : Machinig Data Sheet

Machining 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

contact

Ti-4Al-2V Ti Alloy - Steel Grades

202334 · We can produce the Ti-4Al-2V has the following specifications: Round bar steel: 1mm to 3000mm. Square-shape steel: 1mm to 2000mm. Plate steel: 0.1mm to 2500mm. Width: 10mm to 2500mm. Lenth: We can supply any lenth based on the customer's requirement.

contact

TI–4AL–4MO–2SN – Titanium

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).

contact