ti-5.8al-4sn-3.5zr-0.7nb alloy guatemala

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Ti-5.8Al-4.0Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si-0.06C - Titanium

15  · Ti-5.8Al-4.0Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si-0.06C. Ti 834 possesses the highest temperature capability of any commercial titanium alloy (up to 1112°F (600°C)) and is

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  • SPECIFICATIONPRODUCT FORMCP5238BarCPW534BilletDMD .sg15

    Ti-5.8Al-4.0Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si-0.06C - Titanium

    Common Name Ti-5.8Al-4.0Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si-0.06C Ti-834 UNS None assigned General Information Ti 834 possesses the highest temperature capability of any

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    TIMET TIMETAL® 834 (Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo

    Like 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

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    : TIMET

    TIMET TIMETAL® 834 (Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo

    TIMET 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

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    On the occurrence of dynamic strain aging in near-alpha

    199991 · 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

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    │ –

    2017918 · │. : 、。. ,

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    Analysis of backscattered ultrasound amplitude of

    200921 · The 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.

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    Analysis of backscattered ultrasound amplitude of

    200921 · The 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.

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    2022710 · (high temperature titanium alloy),。400~600℃。 α+β α 。

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    Creep behaviour and creep microstructures of a high ...

    : The tensile creep behaviour of the high-temperature near α-Ti alloy Ti–5.8Al–4.0Sn–3.5Zr–0.7Nb–0.35Si–0.06C (Timetal 834) with a duplex microstructure

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    [PDF]

    HIGH STRENGTH, HIGH TEMPERATURE, CREEP

    2018824 · 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

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    TIMET TIMETAL® 834 (Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo

    TIMET 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 ...

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    Tensile and creep properties of diffusion bonded titanium

    1999423 · 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,

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    2022112 · 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 ...

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    Titanium For Aerospace Industries – Titanium

    Ti-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 ...

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    αTG6_

    、,600℃TG6[2],Ti-5.8Al-4Sn-4Zr-1.5Ta-0.7Nb-0.4Si-0.06C,。,TG60.4%Si。

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    2014620 · IMI834 (Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo β , V、Cr、Mn、Fe , 、, ,,

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    - ...

    20201210 · Ti-6Al-4V,Ti-6Al-2Sn-4Zr-6Mo,Ti-5Al-2Sn-2Zr-4Cr-4MbTi-17) , Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si。,、、。

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    (,)?

    2022212 · :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

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    Linear Friction Welding of a Forged Near-α Titanium Alloy

    201211 · IMI834 (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].

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    TIMET TIMETAL® 834 (Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo

    TIMET 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 ...

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    A Study on Alpha-Case Depth in Ti-6Al-2Sn-4Zr

    2011426 · 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

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    [PDF]

    Opportunities and Issues in the Application of Titanium

    can 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

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    2022112 · 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 ...

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    [PDF]

    Materials for Gas Turbines – An Overview

    2018925 · 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

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    [PDF]

    IMI834

    2010109 · IMI834(Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5M-0.35Si) 1984 α, 600 ℃, ,,777 Trent700 ,

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    Titanium For Aerospace Industries – Titanium

    Ti-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 ...

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    αTG6_

    、,600℃TG6[2],Ti-5.8Al-4Sn-4Zr-1.5Ta-0.7Nb-0.4Si-0.06C,。,TG60.4%Si。

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    15 3620.1-2016_

    Ti-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 ...

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    High Temperature Titanium Alloy - Alloy Wiki

    Most practical alloys are near α alloys, Ti-6242 alloy composition is Ti-6Al-2Sn-4Zr-2Mo, and the operating temperature is 540℃; IMl-834 alloy composition is Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo -0.35Si, the use temperature can reach 600℃. Mainly used in the manufacture of aero-engine compressor discs and rotor blades.

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    Microstructure and texture variations in high temperature

    2020528 · Ti65 alloy (Ti-5.8Al-4.0Sn-3.5Zr-0.5Mo-0.4Si-0.3Nb-1.0Ta-0.8W-0.05C) is the newly developed high temperature titanium alloy optimized from Ti60 alloys. The long-term service temperature of the alloy is as high as 650 °C, which is unattainable with the previous high temperature titanium alloy. It has excellent strength and excellent creep ...

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    TIMET Technical Data Sheets - MatWeb

    TIMET TIMETAL® 834 (Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si-0.06C) Titanium Alloy TIMET TIMETAL® Code 12 Titanium Alloy (ASTM Grade 12) TIMET TIMETAL® EXHAUST XT™ Low Alloyed Titanium

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    [PDF]

    Oxidation Behavior of Germanium- and/or Silicon

    2017826 · Ti-1100 (Ti-6Al-2.7Sn-4Zr-0.4Mo-0.4Si) and IMI 834 (Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si-0.06C) during oxidation. The Ti 3AlN formation degraded the adher-ence of the oxide scales, although the location of the Ti 3AlN in the oxide was not clarified. [8] The oxidation kinetics of these alloys is essentially dominated by rutile TiO 2 formation ...

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    Titanium For Aerospace Industries – Titanium

    Ti-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 ...

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    201023 · Ti-5.5Al-4Sn-2Zr-1Mo-1Nd-0.25Si TA13 ©2022 Baidu | | | | |

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    High Temperature Titanium Alloy - Alloy Wiki

    Most practical alloys are near α alloys, Ti-6242 alloy composition is Ti-6Al-2Sn-4Zr-2Mo, and the operating temperature is 540℃; IMl-834 alloy composition is Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo -0.35Si, the use temperature can reach 600℃. Mainly used in the manufacture of aero-engine compressor discs and rotor blades.

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    - .pdf

    201793 ·  :2014­05­09;:2014­12­10 :,;:0731E­mail: ljm5712@ 25 2 ,: 281 、,, (HCP)α ...

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    Total Materia -

    201795 · Total Materia 、, 69 / 1000 ,、、、、、、、、、、,、、、 ...

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    Ti-5.8Al-4Sn-3.5Zr-0.5Mo-0.7Nb-0.35Si-0.06C(IMI 834),50℃。,IMI834,。

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    - ...

    20201210 · Ti-6Al-4V,Ti-6Al-2Sn-4Zr-6Mo,Ti-5Al-2Sn-2Zr-4Cr-4MbTi-17) , Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si。,、、。

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