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2018824 · HIGH STRENGTH, HIGH TEMPERATURE, CREEP RESISTANT ALLOY TIMETAL834 is a near alpha alloy offering increased tensile strength and creep
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
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
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
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 ...
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
contact199971 · 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-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（-0.15Si ... AB-3 TC11 Ti-6.5Al-3.5Mo-1.5Zr-0.3Si GB/T ASTM ΓOCT JIS ...
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 ...
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。
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 mixture of α+β, in order to facilitate thermomechanical processing.
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.
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-
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
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 ...
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 ...
contact201023 · 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（-0.15Si ... AB-3 TC11 Ti-6.5Al-3.5Mo-1.5Zr-0.3Si GB/T ASTM ΓOCT JIS ...
contact2022217 · α ，Ti-6242Ti-6Al-2Sn-4Zr-2Mo，540℃；IMl-834Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si，600℃。 。
contact2022125 · 2. BAO Ti Group Co., Ltd., Baoji , Shaanxi, China. . : GB/T 3620.1-2016，、、，。. ，，、、 ...
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。
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 ...
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.
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
contactTitanium alloys are used in the manufacture of gas turbine aircraft engine compressor section components, which in use are exposed to high temperatures and corrosive environments. ... Ti-5.8Al-4Sn-3.5Zr-0.7Nb
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 ...
contactThe amplitudes of backscattered ultrasound were measured at 10 MHz on different samples of the near-α titanium alloy Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.3Si. Orientation imaging maps (OIMs) of these samples were also determined by electron backscatter diffraction. The
contactTIMET TIMETAL® 3-2.5-0.05Pd Titanium Alloy. TIMET TIMETAL® 35A CP Titanium (ASTM Grade 1) TIMET TIMETAL® 367 (Ti-6Al-7Nb) Implant Grade Titanium Alloy. TIMET TIMETAL® 50A CP Titanium (ASTM Grade 2) TIMET TIMETAL® 5111 Titanium Alloy (Ti-5Al-1Sn-1Zr-1V-0.8Mo; ASTM Grade 32)
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 ...
contact1 なa＋b の． 1 (エンジンはターボファンエンジン)にいられるチタン(4)(7) (20)．Al ではをしてい ないが，によるものやプロセスのでを0.1～0.2 mass する，それぞれ1～2 をす
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