热加工工艺2024,Vol.53Issue(14) :127-129.DOI:10.14158/j.cnki.1001-3814.20193665

热处理对Ti62A钛合金显微组织及力学性能的影响

Effects of Heat Treatment on Microstructure and Mechanical Properties of Ti62A Titanium Alloy

杨晶 任晓龙 王涛 崔林林 雷锦文 李少强 陈海生
热加工工艺2024,Vol.53Issue(14) :127-129.DOI:10.14158/j.cnki.1001-3814.20193665

热处理对Ti62A钛合金显微组织及力学性能的影响

Effects of Heat Treatment on Microstructure and Mechanical Properties of Ti62A Titanium Alloy

杨晶 1任晓龙 1王涛 1崔林林 1雷锦文 1李少强 1陈海生1
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作者信息

  • 1. 西部超导材料科技股份有限公司,陕西 西安 710018
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摘要

热处理是调整钛合金组织及性能的重要手段之一.对Ti62A钛合金进行了 910~940℃/2 h、AC的热处理试验,对试样分别进行室温力学性能检测和金相组织观察,研究了不同热处理制度对Ti62A钛合金组织及力学性能的影响.结果表明:随着热处理温度的升高,Ti62A合金的冲击功呈现升高趋势,冲击功由 26J提高到 34 J,提高比较明显,而抗拉强度变化不大,屈强差略有缩小.试样经 940℃/2 h、AC热处理后,其显微组织由球状初生α相和片层状次生相组成,这种组织有利于提高材料的冲击功.因此,对Ti62A合金进行 940℃/2 h、AC热处理后,合金的强度和冲击韧性可以达到良好的匹配.

Abstract

Heat treatment is one of the important means to adjust the microstructure and properties of titanium alloy.The Ti62A titanium alloy was tested for heat treatment at 910-940℃/2 h and AC.The mechanical properties of the samples were measured at room temperature and the microstructure was observed.The effects of different heat treatment systems on the microstructure and mechanical properties of Ti62A titanium alloy were studied.The results show that the impact work of Ti62A alloy increases with the increase of heat treatment temperature,and the impact work increases from 26 J to 34 J,the improvement is obvious.The change of tensile strength is small,and the bending strength difference is slightly reduced.After heat treatment at 940℃/2 h,the microstructure of the specimen consists of spherical primary α phase and lamellar secondary phase.This kind of microstructure is beneficial to improve the impact work of the material.Therefore,the strength and impact toughness of the alloy can be well matched after 940℃/2 h,AC heat treatment.

关键词

Ti62A钛合金/组织/力学性能

Key words

Ti62A titanium alloy/microstructure/mechanical properties

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基金项目

陕西省科技计划项目(S2019-YD-CGHJ-0035)

出版年

2024
热加工工艺
中国船舶重工集团公司热加工工艺研究所 中国造船工程学会船舶材料学术委员会

热加工工艺

CSTPCD北大核心
影响因子:0.55
ISSN:1001-3814
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