ti-5.8al-4sn-3.5zr-.7nb-.5mo-.35si-.06c alloy brazil

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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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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

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: M. Humbert, A. Moreau, E. Uta, N. Gey, Philippe Bocher, C. Bescond

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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[PDF]

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

201613 · TIMET TIMETAL® 834 (Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si-0.06C) Titanium Alloy Category : Metal , Nonferrous Metal , Titanium Alloy , Alpha/Near Alpha

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20221216 · —(Rolls-Royce)Ti-5.8Al-4Sn-3.5Zr-0.5Mo-0.7Nb-0.35Si-0.06C(IMI834)α,

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600℃——IMI 834_Ti_ ...

20071030 · 1、 Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si-0.06C(IMI 834)( b:1050MPa) 。IMI 1984 ...

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: : 10

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2017918 · │. : 、。. ,

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

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Review on the Creep Resistance of High-Temperature

2021111 · The composition of IMI834 is Ti–5.8A1–4Sn–3.5Zr–0.7Nb–0.5Mo–0.35Si–0.06C. The addition of trace β-stabilizing elements Mo and Nb greatly improves the thermal strength and thermal stability (increase the strength while maintaining good thermal stability). ... et al. studied the tensile creep

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600℃——IMI 834_Ti_ ...

20071030 · 1、 Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si-0.06C(IMI 834)( b:1050MPa) 。IMI 1984 ...

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: : 10

Microstructure evolution and mechanical properties of a

202121 · Ti-5.8Al–4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si-0.06C alloy (Ti834) is a typical near-α high-temperature titanium alloy, which used in jet engines as compressor discs and blades [18, 19]. Our previous work found that LSP is an effective method to improve the mechanical properties of the Ti834 alloy with bimodal microstructure [ 17 ].

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[PDF]

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

201613 · TIMET TIMETAL® 834 (Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si-0.06C) Titanium Alloy Category : Metal , Nonferrous Metal , Titanium Alloy , Alpha/Near Alpha Titanium Alloy Material Notes: High-Strength, High Temperature, Creep Resistant AlloyIndustry Specifications: France: T-A6EZ r4Nb.Features: TIMETAL 834 is a near

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Automobile applications of titanium - ScienceDirect

201911 · Therefore, since the 1980s, high-temperature near-α titanium alloys, specifically Ti-5.8Al-4Sn-3.5Zr-0.5Mo-0.7Nb-0.35Si-0.06C (IMI834) [10] and Ti-6Al-2.7Sn-4Zr-0.4Mo-0.45Si (Ti-1100) [11], have been developed by IMI and TIMET. In the 1990s, moreover, a large number of high-temperature α-titanium alloys were developed for

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[PDF]

Materials for Gas Turbines An Overview - IntechOpen

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 engines.

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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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20221216 · —(Rolls-Royce)Ti-5.8Al-4Sn-3.5Zr-0.5Mo-0.7Nb-0.35Si-0.06C(IMI834)α,600℃,,、

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20161119 · ,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。

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A Study of the High-Temperature Strength of Titanium

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 alloys, has also been applied to fan and cooler parts of compressors. [] Near α-Ti alloys, such as Ti-6242S (Ti-6Al-2Sn-4Zr-2Mo-0.1Si) and IMI-834 (Ti-5.8Al-4Sn-3.5Zr-0.5Mo-0.7Nb

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A Study of the High-Temperature Strength of Titanium

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 alloys, has also been applied to fan and cooler parts of compressors. [] Near α-Ti alloys, such as Ti-6242S (Ti-6Al-2Sn-4Zr-2Mo-0.1Si) and IMI-834 (Ti-5.8Al-4Sn-3.5Zr-0.5Mo-0.7Nb

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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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201023 · 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 ...

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Microstructural stability of the ({alpha} + {beta}) solution

1995101 · 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.

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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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[PDF]

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

201613 · TIMET TIMETAL® 834 (Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si-0.06C) Titanium Alloy Category : Metal , Nonferrous Metal , Titanium Alloy , Alpha/Near Alpha Titanium Alloy Material Notes: High-Strength, High Temperature, Creep Resistant AlloyIndustry Specifications: France: T-A6EZ r4Nb.Features: TIMETAL 834 is a near

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2021916 · 、. ㈠、. 71% , 、,, 。. ,3.5% ,,

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- .pdf

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

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2016524 · . 1275 0. 。. ,,。. ,。. ,

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Creep behaviour and creep microstructures of a high

200151 · 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 has been extensively ...

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

3.0 - 5.0 % Some of the values displayed above may have been converted from their original units and/or rounded in order to display the information in a consistent format. Users requiring more precise data for scientific or engineering calculations can click on the property value to see the original value as well as raw conversions to ...

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Platinum Aluminide Coatings for Oxidation

Recent results on bare IMI 834 alloy at different temperatures have revealed that the thickness of oxide scale and depth of alpha case are proportional to the temperature to which they ... Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si

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Creep behaviour and creep microstructures of a high

200151 · 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 has been extensively ...

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[PDF]

IMI834

2010109 · Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5M-0.35Si-0.06C(,%), , 12 g 。10×10 , 100 ,220 ,1 。1

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20221020 · (4)Ti-5.8Al-4Sn-3.5Zr-0.5Mo-0.7Nb-0.35Si-0.06C(IMI834)。IMI834(Rolls-Royce,),600℃。,α。

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Alloying elements characterization in a Ti-5.6Al-4.8Sn-2Zr ...

International Journal of Minerals, Metallurgy and Materials (IJMMM, ISSN 1674-4799, CN 11-5787/TF, monthly, started in 1994, formerly known as Journal of University of Science and Technology Beijing) is an international journal devoted to publishing original ...

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600℃|||nb_

202086 · Ti750 , Ti–6Al–4Sn–9Zr–1.21Nb–1.6W–0.3Si,750℃。 W , Si , Ti750 Al , Ti3X(X Al,Sn ), ...

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201023 ·  : :86- :(+86)018 : :

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2016818 · ,。. , (、、) (Al+SiO2),。.

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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 commercial titanium alloy (up to 1112°F (600°C)) and is primarily used in aircraft engine applications. This “near alpha” alloy is weldable and possesses a fine grained alpha/beta

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