期刊检索

  • 2024年第32卷
  • 2023年第31卷
  • 2022年第30卷
  • 2021年第29卷
  • 2020年第28卷
  • 2019年第27卷
  • 2018年第26卷
  • 2017年第25卷
  • 2016年第24卷
  • 2015年第23卷
  • 2014年第22卷
  • 2013年第21卷
  • 2012年第20卷
  • 2011年第19卷
  • 2010年第18卷
  • 第1期
  • 第2期

主管单位 中华人民共和国
工业和信息化部
主办单位 中国材料研究学会
哈尔滨工业大学
主编 苑世剑 国际刊号ISSN 1005-0299 国内刊号CN 23-1345/TB

期刊网站二维码
微信公众号二维码
引用本文:赵小凯,徐文臣,陈宇,林恒龙,张治朋,单德彬.TA15钛合金筒-锥复合曲母线构件旋压成形工艺研究[J].材料科学与工艺,2016,24(4):10-17.DOI:10.11951/j.issn.1005-0299.20160402.
ZHAO Xiaokai,XU Wenchen,CHEN Yu,LIN Henglong,ZHANG Zhipeng,SHAN Debin.Study on the spinning process of cylinder-conical composite curved generatrix workpiece of TA15 titanium alloy[J].Materials Science and Technology,2016,24(4):10-17.DOI:10.11951/j.issn.1005-0299.20160402.
【打印本页】   【HTML】   【下载PDF全文】   查看/发表评论  下载PDF阅读器  关闭
←前一篇|后一篇→ 过刊浏览    高级检索
本文已被:浏览 2501次   下载 1059 本文二维码信息
码上扫一扫!
分享到: 微信 更多
TA15钛合金筒-锥复合曲母线构件旋压成形工艺研究
赵小凯1,2,徐文臣1,2,陈宇1,2,林恒龙3,张治朋1,2,单德彬1,2
(1.金属精密热加工国家级重点实验室(哈尔滨工业大学),哈尔滨 150001;2.哈尔滨工业大学 材料科学与工程学院, 哈尔滨 150001;3.扬州华宇管件有限公司,江苏 扬州 225800)
摘要:
TA15钛合金作为一种高比强度结构材料具有良好的室温和高温强度、热稳定性能,广泛应用于飞机、导弹和发动机等飞行器,实现关键受力构件的减重要求.本文针对钛合金筒-锥复合曲母线构件的特点,重点开展了TA15钛合金薄壁曲母线构件热旋压成形技术的研究,采用剪切旋压预成形,强力旋压/普通旋压多道次复合旋压终成形的工艺方案,获得了成形质量较好的TA15钛合金筒-锥复合曲母线旋压件.建立了多道次曲母线构件的有限元模型,结合旋压实验解释了强旋/普旋复合成形过程中出现的典型缺陷产生机制.对热旋压过程坯料的显微组织观察分析发现,剪切旋压对显微组织具有一定程度的晶粒破碎作用,多道次强旋/普旋复合旋压成形后显微组织沿构件轴向和切向都发生伸长.经历剪切旋压和多道次强旋普旋复合旋压成形后,坯料的微观组织更加细化,且均匀性得到改善.TA15钛合金旋压成形工件的单向拉伸实验结果表明,相对于原始坯料旋压件强度明显提高,塑性略有下降.
关键词:  TA15钛合金  曲母线构件  强力旋压  复合旋压  多道次成形  有限元模拟
DOI:10.11951/j.issn.1005-0299.20160402
分类号:TG146.2
文献标识码:A
基金项目:国家自然科学基金资助项目(51275131).
Study on the spinning process of cylinder-conical composite curved generatrix workpiece of TA15 titanium alloy
ZHAO Xiaokai1,2, XU Wenchen1,2, CHEN Yu1,2, LIN Henglong3, ZHANG Zhipeng1,2, SHAN Debin1,2
(1.National Key Laboratory for Precision Hot Processing of Metals(Harbin Institute of Technology), Harbin 150001,China; 2.School of Materials Science and Engineering, Harbin Institute of Technology, Harbin 150001,China; 3. Yangzhou Huayu Pipe Fitting Company, Yangzhou 225800,China)
Abstract:
As a high specific strength structural material with excellent room and elevated temperature strength and thermal stability, TA15 titanium alloy is widely used in the field of aircraft, missiles and engine for the purpose of lightweight. According to the characteristic of cylinder-conical composite curved generatrix workpiece, the forming of thin-wall curved generatrix workpiece of TA15 titanium alloy was studied using hot spinning method. Shear spinning preforming was adopted, and multi-pass power spinning and conventional spinning were used to form the final workpiece. A multi-pass spinning process of curved generatrix workpiece from the plate blank was investigated through FEM simulation and process experiment. The forming process was analyzed and the mechanisms of spinning defects were revealed. The microstructural evolution results show that the grains are crushed after shear spinning and then elongated along the axial direction and circumferential direction during multi-pass composite power spinning and conventional spinning. The microstructure was refined and the uniformity was improved after shear spinning preforming and multi-pass composite spinning process. The uniaxial tensile test results of the as-spun workpiece showed that the strength increased significantly while the peak strain decreased slightly compared with those of the initial material.
Key words:  TA15 titanium alloy  curved generatrix workpiece  shear spinning  composite spinning  multi-pass deformation  FEM simulation

友情链接LINKS