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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.
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 · Beta C TB11 Ti-15Mo TC1 Ti-2Al-1.5Mn OT4-1 TC2 Ti-4Al-1.5Mn OT4 TC3 Ti-5Al-4V GB/T ASTM ΓOCT JIS DIN BS
contact201386 · 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
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
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
contactDIN EN 3351 Aerospace series - Titanium alloy Ti-4Al-4Mo-2Sn - Solution treated and aged - Forgings - De ≤ 150 mm; German and version EN 3351:2012 ... German and
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.
contact2012121 · Find the most up-to-date version of DIN EN 3351 at Engineering360. UNLIMITED FREE ACCESS TO THE WORLD'S BEST IDEAS. SIGN UP TO SEE MORE. First Name. Last Name. Email Address. Company.
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).
contactTi-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 oxidation resistant ... 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 ...
contact20221026 · DIN EN 3459-2010 .TI-P63001(Ti-4Al-4Mo-2Sn)..6 mm＜a≤50 mm.EN 3459-2010 DIN EN 3464-2010 .6mm DIN EN 3456-2010 .a≤6mmTI-P64001(Ti-6Al-4V).3456-2009
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 ...
contact2018104 · ：: Ti-1100, Ti-1023, IMI834, Timetal62S, SP-700. TC4【】 . TC4. ,。. , 90%。. , , ...
contactDIN EN 3351 Aerospace series - Titanium alloy Ti-4Al-4Mo-2Sn - Solution treated and aged - Forgings - De ≤ 150 mm; German and version EN 3351:2012 ... German and version EN 3351:2012 Luft- und Raumfahrt - Titanlegierung Ti-4Al-4Mo-2Sn - Lösungsgeglüht und ausgelagert - Schmiedestücke - De ≤ 150 mm; Deutsche und
contactDIN EN 3351:2012 Aerospace 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.
contact2018109 · Find the most up-to-date version of DIN EN 3459 at GlobalSpec. UNLIMITED FREE ACCESS TO THE WORLD'S BEST IDEAS. SIGN UP TO SEE MORE. First Name. Last Name. Email Address. Company.
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).
contactTi-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 oxidation resistant ... 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 ...
contact20221026 · DIN EN 3459-2010 .TI-P63001(Ti-4Al-4Mo-2Sn)..6 mm＜a≤50 mm.EN 3459-2010 DIN EN 3464-2010 .6mm DIN EN 3456-2010 .a≤6mmTI-P64001(Ti-6Al-4V).3456-2009
contact2018414 · 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
contact2018104 · ：: Ti-1100, Ti-1023, IMI834, Timetal62S, SP-700. TC4【】 . TC4. ,。. , 90%。. , , ...
contactBuy DIN EN 3351:2012-12 AEROSPACE SERIES - TITANIUM ALLOY TI-4AL-4MO-2SN - SOLUTION TREATED AND AGED - FORGINGS - D[E] <= 150 MM from SAI Global
contactTi-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 oxidation resistant ... 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 ...
contact20121010 · EN 3351-2012《 - Ti-4Al-4Mo-2Sn - - - De≤150 mm》 : Ti-4Al-4Mo-2Sn De <= 150mm 。 :WL:3.7184
contactDIN EN 3459:2010 DE Luft- und Raumfahrt - Titanlegierung TI-P63001 (Ti-4Al-4Mo-2Sn) - Lösungsgeglüht und ausgelagert - Platten - 6 mm a 50 mm; Deutsche und Englische Fassung EN 3459:2010 (Foreign Standard). Das Dokument legt die Anforderungen an Titanlegierung TI-P63001, lösungsgeglüht und ausgelagert, Platten 6 mm (kursiv) a 50
contact2022913 · DIN EN 3459-2010 .TI-P63001(Ti-4Al-4Mo-2Sn)..6 mm＜a≤50 mm.EN 3459-2010 DIN EN 3464-2010 .6mm DIN EN 3456-2010 .a≤6mmTI-P64001(Ti-6Al-4V).3456-2009
contact201023 · Ti-5Al-4Cr-4Mo-2Sn-2Zr [Ti-17] superior strength and Billet, exceptional hot and Plate, superplastic Sheet formability compared to Ti-6Al-4V, combined with good ductility and fatigue resistance. Heat-treatable, deep Ingot/Bloo GT section hardenable, m, Bar*, very high strength Ti Billet alloy with superior strength and creep resistance over Ti
contact197241 · DIN EN 3459 .TI-P63001（TI-4Al-4Mo-2Sn）..-6mm<a<kleiner=>50mm；EN 3459:2010 ：，，
contactDIN EN 3459 (2010) Aerospace series - Titanium alloy TI-P63001 (Ti-4Al-4Mo-2Sn) - Solution treated and aged - Plate - 6 mm a = 50 mm クロスリファレンス (40)
contact2023310 · [Offer PDF] DIN EN 3351:2012Aerospace series-Titanium alloy Ti-4Al-4Mo-2Sn-Solution treated and aged-Forgings-De,[Offer PDF] DIN EN 3351:2012 Aerospace series-Titanium alloy Ti-4Al-4Mo-2Sn-,© (Boxue58/Boxuesky) HOME SAVE. Enable Auxiliary Access Wide screen. Account: Remember me Forgot password? Password:
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