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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
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
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).
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
contactThe 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
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 =
contactTitanium Ti-4Al-4Mo-2Sn-0.5Si (IMI550), STA, Solution Treated 900ºC, Aged 500ºC. Alpha-Beta Alloy, medium strength. Applications: Aerospace - airframe and engine components.
contactFeatures: TIMETAL 550, like TIMETAL 6-4, is readily forgeable and is generally used in a heat treated condition. It has superior room and elevated temperature tensile strength
contactAerospace series - Titanium alloy Ti-4Al-4Mo-2Sn - Solution treated and aged - Forgings - De ≤ 150 mm; German and version EN 3351:2012 ... De ≤ 150 mm; German and
contactFeatures: TIMETAL 550, like TIMETAL 6-4, is readily forgeable and is generally used in a heat treated condition. It has superior room and elevated temperature tensile strength and fatigue strength compared to TIMETAL 6-4, and is creep resistant up to 400°C. It has applications in the aerospace industry, both as aeroengine and airframe components.
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.
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-4Al-4Mo-2Sn 4.60 aged ... WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim, First Edition, 2003. ... (Ti) alloys have been employed for several structural purposes due to high strength, lightweight ...
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.
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 ...
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).
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.
contact2021513 · This page cover the Ti-4AI-4Mo-2Sn Ti Alloy steel grades Mechanical Properties, Chemical Element, Cross Reference of Ti-4AI-4Mo-2Sn Ti Alloy Materials, Chinese Français; Deutsch; Italiano; Available 24/7 at . Search Post Your Request Now. Toggle menu. Post Your Request Now ...
contactTi–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).
contactAerospace series - Titanium alloy Ti-4Al-4Mo-2Sn - Solution treated and aged - Forgings - De 150 mm; German and version FprEN 3351:2012. This document specifies the requirements relating to grade 2 solution treated and aged forging in titanium alloy TI-P63001, D(Index)e> 150 mm, for aerospace applications.
contact2023120 · 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. NOTE Other common designation: Ti550, AECMA: TI-P63, ASD-STAN: TI-P63001.
contact202334 · 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.
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
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 ...
contact198541 · The superplastic deformation of titanium alloy Ti-4Al-4Mo-2Sn-0.5Si (IMI 550) (where the alloy composition is given in approximate weight per cent) ha…
contactMaterion Beryllium Copper Alloy 190 Strip; XHMS (TM08) Temper (UNS C17200) Treatment required for max strength: Mill HardenedStress Relaxation-% Stress Remaining after 1000 hrs @ 100°C: 98%Stress Relaxation after 1000 hrs
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
contactAerospace series - Titanium alloy Ti-4Al-4Mo-2Sn - Solution treated and aged - Forgings - De 150 mm; German and version FprEN 3351:2012. This document specifies the requirements relating to grade 2 solution treated and aged forging in titanium alloy TI-P63001, D(Index)e> 150 mm, for aerospace applications.
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.
contactAerospace series - Titanium alloy Ti-4Al-4Mo-2Sn - Solution treated and aged - Forgings - De ≤ 150 mm
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 ...
contact2021616 · ：（、） TAD Grade1 1 BT1-00 TA1 Grade2 2 BT1-0 TA2 Grade3 3 OT4 -0 Ti-0.8Al-0.7Sn TA3 Grade4 4 OT4 -1 Ti-2Al-1.
contactThe master alloy may be formed aluminothermically (German open application DE-OS No. 28 21 406). ... Op. Cit.), titanium alloy Ti-5Al-2Sn-2Zr-4Mo-4Cr but otherwise in accordance with AMS 4975B (1968) or AMS 4976A (1968) are produced with high purity and without any detrimental oxygen content or nitride inclusions.
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 ...
contactBuy EN 3351 : 2012 AEROSPACE SERIES - TITANIUM ALLOY TI-4AL-4MO-2SN - SOLUTION TREATED AND AGED - FORGINGS - D[E] <= 150 MM from SAI Global
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