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Title:Study on properties of heat deformation and heat treatment for Ti alloy TC8M-1
Authors: Li Yafei  Fang Bo Wang Guan Ma Wen'ge Zhang Pinghui 
Unit: Guizhou Aero-Engineer Institute of AVIC  Shenyang Liming Aero-Engineer Company  West Super-Conduction Technology Company Limited Baoji Titanium Alloy Group 
KeyWords: Ti alloy TC8M-1  forging  heat treatment  microstructure 
ClassificationCode:TG166.5;TG319
year,vol(issue):pagenumber:2015,40(2):127-132
Abstract:
Ti alloy TC8M-1 under the deformation rates of 5%,15%,30%,50% and 70% at 910 ℃ was forged respectively for testing its properties of heat deformation and heat treatment. Microstructure was observed and compared with the ones which were observed under the deformation rate of 40% at 890℃ and 930 ℃ respectively. Finally heat treatment experiments were carried out. The results show that TC8M-1 alloy is of good plastic deformation properties and wide forging temperature range. When the forging temperature is at 910 ℃, the deformation rate shoots up to 70% at once heat treatment. However, fine microstructure areas are found when the deformation rate exceeds 50%. Under the condition of deformation rate 40%,primary α phase is spheroidized at 930 ℃, and primary α phase is kept plastic deformation at 890 ℃. Thus, suitable heat treatment condition of Ti alloy TC8M-1 is under cooling for two hours at 930 ℃ or cooling for an hour at 590 ℃ to meet the tensile strength at room temperature and enduring strength at 450 ℃.
Funds:
江苏省自然科学基金资助项目(BK2005128)
AuthorIntro:
李亚非(1986-),男,硕士,工程师
Reference:

 
[1]Donachie M J. Titanium: A Technical Guide [M]. 2nd Edition. USA: ASM International, 2000.
[2]蔡建明,曹春晓.新一代600 ℃高温钛合金材料的合金设计及应用展望[J].航空材料学报,2014,(4):27-36.Cai J M, Cao C X. Alloy design and application expectation of a new generation 600 ℃ high temperature titanium alloy[J].Journal of Aeronautical Material,2014,(4):27-36.
[3]蔡建明,郝孟一,李学明,等.BT36高温钛合金的成分特点及组织研究[J]. 材料工程,2000,(2):10-14.Cai J M, Hao M Y, Li X M, et al. Study of composition character and microstructure of BT36 high temperature Ti alloy[J].Journal of Materials Engineering, 2000,(2):10-14.
[4]廖明夫,谭大力,耿建明,等.航空发动机高压转子的结构动力学设计[J].航空动力学报,2014,29(7):1505-1519.Liao M F, Tan D L, Geng J M, et al. Structure dynamics design method of aero-engine high pressure rotor[J].Journal of Aerospace Power,2014,29(7):1505-1519.
[5]樊东黎,徐跃明,佟晓辉.热处理工程师手册 [M]. 北京:机械工业出版社,2005.Fan D L, Xu Y M, Tong X H. Manual of Treatment [M]. Beijing: China Machine Press, 2005.
[6]GB/T 228.1—2010,金属材料 拉伸试验 第1部分:室温试验方法[S]. GB/T 228.1—2010,Metallic materials—Tensile testing—Part l: Method of test at room temperature[S].
[7]GB/T 2039—2012, 金属材料 单轴拉伸蠕变试验方法[S].GB/T 2039—2012, Metallic materials—Uniaxial creep testing method in tension[S].
[8]朱知寿,王庆如,郑永灵.准β锻造钛合金的组织和性能研究[J].金属学报,2002,38(Zl):382-384.Zhu Z S, Wang Q R, Zheng Y L. Quasi-β forging processing of titanium alloys [J].Acta Metallurgica Sinica, 2002,38(Zl):382-384.
[9]童路,朱知寿,俞汉清.TC4-DT钛合金自由锻件组织与性能的影响因素[J].中国有色金属学报,2010,20(10):87-91.Tong L, Zhu Z S, Yu H Q. Influence factors of microstructure and property of TC4-DT titanium alloy free forgings [J]. The Chinese Journal of Nonferrous Metals, 2010,20(10):87-91.
[10]金哲,张万明.生物医用Ti-6Al-7Nb合金高温变形行为的研究[J].稀有金属,2012,36(2):218-223.Jin Z, Zhang W M. High temperature deformation behaviors of biomedical titanium alloy Ti-6Al-7Nb [J].Chinese Journal of Rare Metals,2012,36(2):218-223.
[11]费玉环,周廉,曲恒磊,等.两相区热处理对TC21钛合金显微组织的影响[J]. 稀有金属材料与工程,2007,36(11):1028-1034. Feng Y H, Zhou L, Qu H L, et al. Effects of heat-treatment on microstructure of TC21 titanium alloy[J].Rare Metal Material and Engineering, 2007,36(11):1028-1034.
[12]段锐,张华,蔡建明,等.显微组织对近α型TG6钛合金高温蠕变变形行为的影响[J].中国有色金属学报,2010,20(10):11-17. Duan R, Zhang H, Cai J M, et al. Effects of microstructure on creep deformation behavior of near-alpha titanium alloy TG6 [J]. The Chinese Journal of Nonferrous Metals, 2010,20(10):11-17.
[13]张俊善.材料的高温变形与断裂[M].北京:科学出版社,2006.Zhang J S. High Temperature and Fracture of Materials[M].Beijing: Science Press, 2006.
[14]吴崇周,李兴无,黄旭,等.TA15钛合金疲劳裂纹扩展与微观组织的关系[J]. 稀有金属材料与工程,2007,36(12):2128-2132.Wu C Z, Li X W, Huang X, et al. Relationship of fatigue crack propagation and microstructure for TA15 alloy [J]. Rare Metal Material and Engineering, 2007,36(12):2128-2132.

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