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2022921 · 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
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
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
contact2017827 · Alloy 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
contact20071030 · 1、 Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si-0.06C(IMI 834)（ b:1050MPa） 。IMI 1984 ...
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
contactTi - 6Al - 4Sn - 3.5Zr - 0.5Mo - 0.35Si - 0.7Nb - 0.06C The niobium is added for oxidation resistance and the carbon to allow a greater temperature range over which the alloy is a
contactIMI 834 (Ti–5.8Al–4Sn–3.5Zr–0.7Nb–0.5Mo–0.35Si–0.06C) has been developed for use up to 600°C and combines the high fracture toughness and crack propagation resistance of a transformed β-structure with the typical equiaxed structure of the α + β alloys, providing good fatigue resistance and ductility. The small addition of ...
contact2015127 · These alloys include Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si alloy (IMI834), which is near-α type (an α-β alloy containing a smaller amount of β ... Hot-forging technology for titanium alloys 3.1 β-processed forging of Ti-6246 alloy disks for aircraft As described above, titanium alloy, as a light-
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
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 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,
contact2010109 · IMI834(Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5M-0.35Si) 1984 α， 600 ℃， ，，777 Trent700 ，
contact2019417 · ，Ti-5A1，Ti-5Al-2.5Sn，Ti-4Al-3Mo-1V，Ti-5.8Al-4Sn-3.5Zr-O.5Mo-O.7Nb-O.35Si-0.06C。 Ti3A1，Ti-Al，Ti-Al-Nb，Ti3A1750℃，TiAl900℃，Ti-A1-NbTiAl。
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
contact202251 · 1. Introduction. Ti-6Al-4V is the most widely used Ti alloy due to its balanced mechanical properties [[1], [2], [3]].Its tensile yield strength reaches easily the level of 1000 MPa, in combination with fairly large elongation up to 30% [4].It is also suitable for additive manufacturing [5, 6], showing high ultimate tensile strengths of 1000–1300 MPa and
contact202086 · Ti750 ， Ti–6Al–4Sn–9Zr–1.21Nb–1.6W–0.3Si，750℃。 W ， Si ， Ti750 Al ， Ti3X（X Al，Sn ）， ...
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 ...
contact2018824 · HIGH STRENGTH, HIGH TEMPERATURE, CREEP RESISTANT ALLOY TIMETAL834 is a near alpha alloy offering increased tensile strength and creep resistance up to 1110°F ... Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si-0.06C ELEMENT WEIGHT % Aluminum 5.50 6.10 Tin 3.00 5.00 Zirconium 3.00 5.00 Niobium 0.50 1.00 Molybdenum
contact1999423 · 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,
contact2015127 · These alloys include Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si alloy (IMI834), which is near-α type (an α-β alloy containing a smaller amount of β ... Hot-forging technology for titanium alloys 3.1 β-processed forging of Ti-6246 alloy disks for aircraft As described above, titanium alloy, as a light-
contact2022112 · Ti-8Al-1Mo-1V TA12 Ti-5.5Al-4Sn-2Zr-1Mo-1Nd-0.25Si TA12-1 Ti-5.5Al-4Sn-2Zr-1Mo-1Nd-0.25Si TA13 Ti-2.5Cu TA14 Ti-2.3Al-11Sn-5Zr-1Mo-0.2Si TA15 Ti-6.5Al-1Mo-1V-2Zr ...
contact2010109 · IMI834(Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5M-0.35Si) 1984 α， 600 ℃， ，，777 Trent700 ，
contactTi-5.8Al-4Sn-3.5Zr-0.7Mo-0.5Nb-1.1Ta-0.4Si-0.06C TC6 BT3-1 Ti-6Al-1.5Cr-2.5Mo-0.5Fe-0.3Si TA10 GR12 Ti-0.3Mo-0.8Ni TC8 BT8 Ti-6.5Al-3.5Mo-0.25Si TA28 Ti-3Al TB16 Ti-3Al-5V-6Cr-5Mo TC30 ~BT14 Ti-5Al-3Mo-1V TA29 Ti-5.8Al-4Sn-4Zr-0.7Nb-1.5Ta-0.4Si-0 ...
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 ...
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
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 ...
contact1999423 · 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,
contact2010109 · IMI834(Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5M-0.35Si) 1984 α， 600 ℃， ，，777 Trent700 ，
contact2017827 · Alloy 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 fatigue strength (Gogia, 2005). The alloy was aimed at replacing the Alloys 685 and 829 preferred in European jet
contact2021921 · IMI834(Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si)1984α。 β，σ b ≥930MPa，，，777Trent700。
contact2019623 · IMI834 （Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo- β，V、Cr、Mn、Fe 0.35S）i IMI829，Nb ，N、H、O， β。
contact