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

Common raw materials

Forging display

CNC processing

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

(PDF) Titanium and its Alloy - ResearchGate

2014101 · Ti-4Al-4Mo-2Sn 4.60 aged ... above 400℃ and have outstanding characteristics that enable their application in gas turbines

contact
:2

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).

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

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

contact

201023 ·  : :86- :(+86)018 : :

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

Titanium Alloys and Their Characteristics: Part One

Ti - 6Al - 2Sn - 4Zr - 2Mo. where the Zr and Sn give solid solution strengthening. Ti-5Al-2.5Sn is an α alloy which is available commercially in many forms. Because it is stable in

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 -

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

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

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

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

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

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

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
[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

Shape memory effect and aging behavior of Bi-added

2023324 · Metastable β Ti alloys can also provide more functions such as low Young's modulus and shape memory effect (SME) (Niinomi, 2008; Biesiekierski et al., 2012; Zhang and Chen, 2019). For advanced biomedical applications, new metastable β Ti alloys composed only of non-toxic elements are needed, and these properties should be

contact

Stress relaxation induced morphological evolution and

A uniform, fine-grained microstructure is attained by stress relaxation (SRT) method in Ti-6Al-4V alloy subsequent to hot compression (HC) executed at the temperature of 900 °C and a strain rate of 10 −3 s −1 to a 50% height reduction. The pronounced SRT-induced α grain spheroidization and texture weakening is proposed.

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

TIMET TIMETAL® 550 (Ti-4Al-4Mo-2Sn) Titanium Alloy

In 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.

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

EN 3351 : 2012 AEROSPACE SERIES - TITANIUM ALLOY TI

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

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
[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

Guide to Titanium Grades- TNTI

Most 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

Titanium Alloys and Their Characteristics: Part One

Ti - 6Al - 2Sn - 4Zr - 2Mo. where the Zr and Sn give solid solution strengthening. Ti-5Al-2.5Sn is an α alloy which is available commercially in many forms. Because it is stable in the α condition, it cannot be hardened by heat treatment. It is therefore not particularly strong, but can easily be welded.

contact

βTi-4Mo-6Cr-3Al-2Sn ...

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

contact

Ti-4Al-6Mo-2V-5Cr-2Zr

20211026 · β(Ti-4Al-6Mo-2V-5Cr-2Zr)。,αβ,α。β ...

contact

Characterization of the hot deformation behavior of a

201211 · Such discontinuous yielding behavior has been observed in Ti–4Al–4Mo–2Sn–0.5Si alloy in the α + β field [17], which is suggested that the discontinuous yielding was attributed to the rapid generation of mobile dislocations from grain boundary sources during hot deformation of some β titanium alloys [20], [21]. Thus,

contact

Opportunities and Issues in the Application of

2020527 · Other α + β alloys include, Ti-6Al-6V-2Sn (Ti-662) and IMI550 (Ti-4Al-2Sn-4Mo-0.5Si). All of the α + β alloys are considered weldable in an inert environment, although special precautions such as

contact
[PDF]

HIGH-STRENGTH FORGING ALLOY

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 Aluminum 3 ...

contact

β Ti-4Mo-6Cr-3Al-2Sn ...

20191018 · 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

contact
[PDF]

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

2017828 · 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

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

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

Shape memory effect and aging behavior of Bi-added

2023324 · Metastable β Ti alloys can also provide more functions such as low Young's modulus and shape memory effect (SME) (Niinomi, 2008; Biesiekierski et al., 2012; Zhang and Chen, 2019). For advanced biomedical applications, new metastable β Ti alloys composed only of non-toxic elements are needed, and these properties should be

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

Influence of continuous grain boundary α on ductility of

Therefore, the higher the strength of titanium alloys is, the greater the difference in yield strength is, and the more significant role the continuous α GB plays in reducing ductility. These findings are also successfully used to explain why continuous α GB leads to worse ductility in laser melting deposited Ti-5Al-5Mo-5V-1Cr-1Fe alloy ...

contact