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2018824 · TIMETAL834 is a near alpha alloy offering increased tensile strength and creep resistance up to 1110°F ... NORTH AMERICA The data and other information
contactTIMET TIMETAL® 834 (Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si-0.06C) Titanium Alloy. Industry Specifications: France: T-A6EZ r4Nb. Features: TIMETAL 834 is a near alpha
contact2022921 · Titanium alloys have been used in high-temperature environments such as aerospace engines. The Ti-6Al-4V alloy, which is one of the most common titanium
contactFatigue strength of IMI 834 alloy (Ti–5.8Al–4Sn–3.5Zr–0.7Nb) depending on microstructure and specific volume of α-phase: (a) high-cycle fatigue and (b) low-cycle fatigue.
contactLike these alloys, it is weldable and has good forgeability. Major uses for TIMETAL 834 include rings, compressor discs and blades for aeroengines. It is nonmagnetic.Typical
contact2018925 · Alloy 834 (Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si-0.06C), a relatively rece nt grade, in contrast is used in D + E condition, with a 5-15% equiaxed D in the
contact199991 · Alloy Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si (IMI 834) is the most recently developed near-alpha type titanium alloy for high-temperature application up to 873 K, as
contactTIMET TIMETAL® 834 (Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si-0.06C) Titanium Alloy. Industry Specifications: France: T-A6EZ r4Nb. Features: TIMETAL 834 is a near alpha titanium alloy offering increased tensile strength and creep resistance up to 600°C together with improved fatigue strength when compared with established creep resistant alloys ...
contact2011426 · Similar studies were performed on other high-temperature Ti alloys Ti-5.8Al-4Sn-3.5Zr-0.5Mo-0.7Nb-0.35Si-0.06C (IMI 834) and Ti-6Al-2.7Sn-4Zr-0.4Mo-0.45Si (Ti-1100). Indirect measurements of α case can
contactIMI834 (Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si) is a high-tech near-α titanium alloy with improved creep resistance and mechanical property retention at temperatures up to 600°C [1]. It is used in the aerospace industry for compressor disks and blades due to its excellent balance between creep resistance and fatigue strength [2]. The linear friction welding
contact2018925 · Alloy 834 (Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si-0.06C), a relatively rece nt grade, in contrast is used in D + E condition, with a 5-15% equiaxed D in the microstructure to optimize both creep and fatigue strength (Gogia, 2005). The alloy was aimed at replacing the Alloys 685 and 829 preferred in European jet
contact20221216 · —（Rolls-Royce）Ti-5.8Al-4Sn-3.5Zr-0.5Mo-0.7Nb-0.35Si-0.06C（IMI834）α， 600℃，，、。 ...
contactTi-5.8Al-4Sn-3.5Zr-0.7Nb (834) Advanced engine alloy, creep and oxidation resistant : Ti-5Al-2Sn-4Mo-2Zr-4Cr (Ti 17) ... 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 ...
contact2022212 · ：The tensile creep behaviour of the high-temperature near #alpha#-Ti alloy Ti-5.8Al-4.0Sn-3.5Zr-0.7Nb-0.35Si-0.06C (Timetal 834) with a duplex microstructure has been extensively investigated in the temperature range from 500
contact2017514 · Ti-2.25Al-11Sn-5Zr-1Mo Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si > + A Alloys 5 Ti-6Al-4V Widely used in dental and medical industry 23 Ti-6Al-4V-ELI Widely used in dental and medical industry 24 Ti-6Al-4V, plus 0.04%-0.08% palladium 25 Ti-6Al-4V, plus 0.3%-0.8% nickel and 0.04%-0.08% palladium 29 Ti-6Al-4V-ELI, plus 0.08%-0.14%
contactNear-α Ti alloys find themselves in advanced aeroengines for applications of up to 600 °C, mainly as compressor components owing to their superior combination of ambient- and elevated-temperature mechanical properties and oxidation resistance. We evaluated, ranked, and selected near-α Ti alloys in the current literature for high-temperature
contact2022228 · High tech near-α alloy IMI834 (Ti–5·8Al–4Sn–3·5Zr–0·7Nb–0·5Mo–0·35Si) was designed to have improved creep resistance and retains its mechanical properties at temperatures up to 600°C. It balances creep resistance and fatigue strength, making it an excellent material for compressor discs and blades.
contactcan be used up to about 540 °C maximum, and IMI 834 (Ti-5.8Al-4Sn-3.5Zr-0.5Mo-0.7Nb-0.35Si- 0.06C) which is used up to about 600 °C. Today, IMI834 is generally considered the highest
contactIMI834 (Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si) is a high-tech near-α titanium alloy with improved creep resistance and mechanical property retention at temperatures up to 600°C [1]. It is used in the aerospace industry for compressor disks and blades due to its excellent balance between creep resistance and fatigue strength [2]. The linear friction welding
contactOn the occurrence of dynamic strain aging in near-alpha alloy Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si. Nidhi Singh 1, Nishtala Prasad 1 & Vakil Singh 1 Metallurgical and Materials Transactions A volume 30, pages 2547–2549 (1999)Cite this article
contact2010109 · IMI834(Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5M-0.35Si) 1984 α， 600 ℃， ，，777 Trent700 ，
contact2018925 · Alloy 834 (Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si-0.06C), a relatively rece nt grade, in contrast is used in D + E condition, with a 5-15% equiaxed D in the microstructure to optimize both creep and fatigue strength (Gogia, 2005). The alloy was aimed at replacing the Alloys 685 and 829 preferred in European jet
contactAlloy 834 (Ti-5.8Al-4Sn-3.5Zr-0.7Nb- 0.5Mo-0.35Si-0.06C), a relatively recent grade, in contrast is used in + condition, with a 5- 15% equiaxed in the microstructure to optimize both creep and ...
contact201023 · Ti-6.5Al-3.5Mo-1.5Zr-0.3Si BT9 TC12 Ti-5Al-4Mo-4Cr-2Zr-2Sn-1Nb TC15 Ti-5Al-2.5Fe TC16 Ti-3Al-5Mo-4.5V BT16 TC17 Ti-5Al-2Sn-2Zr-4Mo-4Cr TC18 Ti-5Al-4.75Mo-4.75V-1Cr-1Fe BT22 TC19 Ti-6Al-2Sn-4Zr-6Mo BS TA21 ...
contact201023 · Ti-0.3Mo-0.8Ni GR12 Ti Ni0.8Mo0.3 TA11 Ti-8Al-1Mo-1V A-4 （ Ti-811 ） Ti-811 Ti-811 Ti-811 Ti-811 TA12 （ TA12-1 ） Ti-5.5Al-4Sn-2Zr-1Mo-1Nd-0.25Si TA13 Ti-2.5Cu ...
contact202086 · Ti750 ， Ti–6Al–4Sn–9Zr–1.21Nb–1.6W–0.3Si，750℃。 W ， Si ， Ti750 Al ， Ti3X（X Al，Sn ）， ...
contact20221122 · 2 Ti 3(Al,Sn) phase [1]. For instance, Ti{834 (Ti{5.8Al{4Sn{3.5Zr{0.7Nb{0.5Mo{0.35Si{0.06C) produces a ne dispersion of 2 precipitates after 24h at 700°C [2]. This ordered phase promotes slip localisation that increases the risk of dwell fatigue crack nucleation in critical rotating parts of jet engines. Under stress cor-
contact2022228 · High tech near-α alloy IMI834 (Ti–5·8Al–4Sn–3·5Zr–0·7Nb–0·5Mo–0·35Si) was designed to have improved creep resistance and retains its mechanical properties at temperatures up to 600°C. It balances creep resistance and fatigue strength, making it an excellent material for compressor discs and blades.
contact202114 · IMI834(Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si)1984α。 β，σ b ≥930MPa，，，777Trent700。
contact2010109 · IMI834(Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5M-0.35Si) 1984 α， 600 ℃， ，，777 Trent700 ，
contact20221216 · —（Rolls-Royce）Ti-5.8Al-4Sn-3.5Zr-0.5Mo-0.7Nb-0.35Si-0.06C（IMI834）α， 600℃，，、。 ...
contactIMI834 (Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si) is a high-tech near-α titanium alloy with improved creep resistance and mechanical property retention at temperatures up to 600°C [1]. It is used in the aerospace industry for compressor disks and blades due to its excellent balance between creep resistance and fatigue strength [2]. The linear friction welding
contactTi-5.8Al-4Sn-3.5Zr-0.7Nb (834) Advanced engine alloy, creep and oxidation resistant : Ti-5Al-2Sn-4Mo-2Zr-4Cr (Ti 17) ... 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 ...
contact1995101 · Alloy Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si (IMI 834) is the most recently developed near-alpha type titanium alloy for high-temperature application up to 873 K, as discs and blades in the high pressure part of compressors, in advanced jet engines. It possesses a good combination of creep and fatigue resistance at elevated temperature,
contact201023 · Ti-0.3Mo-0.8Ni GR12 Ti Ni0.8Mo0.3 TA11 Ti-8Al-1Mo-1V A-4 （ Ti-811 ） Ti-811 Ti-811 Ti-811 Ti-811 TA12 （ TA12-1 ） Ti-5.5Al-4Sn-2Zr-1Mo-1Nd-0.25Si TA13 Ti-2.5Cu ...
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