Mechanical Behavior and Microstructural Analysis of Molybdenum-TZM Alloy Subjected to Different Annealing Temperature

Pub Date : 2020-01-31 DOI:10.30650/jse.v1i1.522
M. A. M. Ghazali, M. A. Harimon, M. Mustapa
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引用次数: 4

Abstract

Mo-TZM alloy is one of the most famous economic molybdenum-based alloys. The percentage of chemical composition in mass of Mo-TZM alloy are Mo-0.5Ti-0.08Zr-0.03C. By adding some Titanium and Zirconium so that the mechanical properties and recrystallization temperature of molybdenum has been corresponding improvement. The purpose of this study is to determine the effect of different annealing temperature on mechanical properties of Mo-TZM alloy. The samples will be heated at two different temperature which are 1000 C and 1300 C in 1 hour and 40 minutes to change their microstructure behavior. The mechanical properties of the sample like hardness will be analyzed by using Vickers Micro hardness test. The force applied is 4.903 N and Vickers micro hardness number is 0.5 HVN for 10 second. Then to observe the microstructure changes, optical microscope and Scanning Electron Microscope (SEM) is be used. At annealing temperature 1000 C, it show values of hardness is 249.54 VHN and the grain boundary size is 0.0898mm. While at annealing temperature 1300 C, it show the lowest values of hardness which is 243.55 VHN and the highest grain boundary size which is 0.1068 mm. By doing annealing heat treatment it will decreases hardness values and increases the size of grain boundary.
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不同退火温度下钼- tzm合金的力学行为及显微组织分析
钼- tzm合金是最著名的经济钼基合金之一。Mo-TZM合金的化学成分占质量的百分比为Mo-0.5Ti-0.08Zr-0.03C。通过加入一定的钛和锆,使钼的力学性能和再结晶温度得到相应的改善。本研究的目的是确定不同退火温度对Mo-TZM合金力学性能的影响。将样品在1000℃和1300℃两种不同温度下加热1小时40分钟,以改变其微观结构行为。采用维氏显微硬度试验分析试样的力学性能。施加的力为4.903 N,维氏显微硬度值为0.5 HVN,持续10秒。然后利用光学显微镜和扫描电镜(SEM)观察其微观结构变化。退火温度为1000℃时,合金硬度为249.54 VHN,晶界尺寸为0.0898mm。退火温度1300℃时,合金硬度最低,为243.55 VHN,晶界尺寸最大,为0.1068 mm。退火热处理会降低硬度值,增大晶界尺寸。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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