摘要
利用SEM及EBSD技术,研究热变形参数(变形方式、变形温度、变形量、应变速率、保温时间)对TC18钛合金β相组织及织构演变规律的影响。结果表明,TC18钛合金在热压缩及两相区热拉伸时,β相均以动态回复为主。在热压缩后,主要形成{100}及{111}织构,在热拉伸后,主要形成{110}织构;在单相区压缩时,随着变形温度升高、变形量提高、应变速率降低,{100}织构比例提高、{111}织构比例降低;在两相区压缩时,随着变形温度升高、变形量提高,{100}织构比例提高、{111}织构比例降低;在两相区拉伸时,随着变形量提高,{110}织构比例逐渐提高。
Titanium alloys have the advantages of high specific strength, fatigue resistance, and corrosion resistance. Also, they are widely used in the aviation, aerospace, weapons, petroleum, and chemical industries and other fields. The use of large-scale and integrated aviation forgings, which are an important development in titanium alloy manufacturing technology, can increase the service life, safety and reliability of aircraft structures and engines, and simultaneously reduce their structural weight and shorten their manufacturing cycle. However, problems such as a decline in mechanical properties and the presence of abnormal low-magnification structures due to the strong β phase texture have gradually been revealed. For example, large-size near-β titanium alloy bars often have the problem of coarse and uneven macrostructures, and the center layer of these bars tend to form a strong {100} β phase texture. These defects are easily inherited in the forgings, which adversely affect their performance and threaten their safe use. In this work, 300 mm diameter TC18 titanium alloy bars were used as the research material.The SEM and EBSD techniques were used to study the microstructure and texture characteristics of theβ phase after thermal deformation, respectively. This work compared the influence of the thermal deformation parameters(compression/stretching, deformation temperature, reduction, strain rate, and holding time) on the evolution of the β phase microstructure and texture in the TC18 titanium alloy. Also, the deformation, dynamic recovery, dynamic recrystallization, and grain growth behavior of the β phase were investigated. The results showed that when the TC18 titanium alloy was compressed and stretched in the twophase region, the β phase was mainly dynamic recovery. After thermal compression, the {100} and the{111} textures were mainly formed, while after thermal stretching, the {110} texture was mainly formed.When it was compressed in the β phase region, as the deformation temperature increased, the reduction increased, the strain rate decreased, the strength of the {100} texture increased and the {111} texture decreased. When it was compressed in the two-phase region, as the deformation temperature increased and the reduction increased, the strength of the {100} texture increased and the {111} texture decreased.When it was stretched in the two-phase region, as the reduction increased, the strength of the {110} texture gradually increased.
作者
颜孟奇
陈立全
杨平
黄利军
佟健博
李焕峰
郭鹏达
YAN Mengqi;CHEN Liquan;YANG Ping;HUANG Lijun;TONG Jianbo;LI Huanfeng;GUO Pengda(AECC Beijing Institute of Aeronautical Materials,Beijing 100095,China;School of Materials Science and Engineering,University of Science and Technology Beijing,Beijing 100083,China)
出处
《金属学报》
SCIE
EI
CAS
CSCD
北大核心
2021年第7期880-890,共11页
Acta Metallurgica Sinica
关键词
TC18钛合金
热变形
组织
织构
Β相
TC18 titanium alloy
hot deformation
microstructure
texture
βphase