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采用等温压缩实验研究了具有马氏体组织的TC11合金在两相区的变形行为及微观组织演变规律.等温压缩实验在Gleeble3500热模拟实验机上进行,其中变形温度为920~980℃,应变速率为0.1~10s-1,变形量为70%.基于动态材料模型(DMM),建立了具有马氏体组织的Tcll合金两相区变形的热加工图.在低温(<940℃)区和高温(>960℃)高应变速率(>1 s-1)区域存在失稳现象,主要表现为低温时的表面开裂和高应变速率区的绝热剪切带;在塑性加工安全区域,分别对应着片层扭折和片层球化的组织机制,其中变形量70%时应变速率敏感因子在980℃,0.1 s-1时取得峰值为0.73,此时可得到完全球化的细晶组织(等轴α尺寸约为0.7μm).具有马氏体组织的TC11合金两相区变形时,为避免缺陷并得到细的等轴组织,合适的加工工艺为温度:950~980℃,应变速率0.1~1 s-1.

参考文献

[1] 王金友;葛志明;周彦邦.航空用钛合金[M].上海:上海科学技术出版社,1985
[2] Semiatin SL;Weiss I;Seetharaman V .Flow behavior and globularization kinetics during hot working of Ti-6Al-4V with a colony alpha microstructure[J].Materials Science & Engineering, A. Structural Materials: Properties, Misrostructure and Processing,1999(2):257-271.
[3] Semiatin S L;Beiler T R .Effect of texture and sllp mode on the anisotropy of plastic flow and flow softening during hot working of Ti-6Al-4V[J].Metallurgical and Materials Transactions,2000,32A:1787.
[4] Semiatin S L;Lahoti G D .Deformation and unstable flow in hot forging of Ti-6Al-2Sn-4Zr-2Mo-O.ISi[J].Metallurgical and Materials Transactions,1981,12A:1705.
[5] Scshacharyulu T;Medeiros S C;Frazier W G;Prasad Y V R K .Microstructural mechanisms during hot working of commercial grade Ti-6AI-4V with lamellar starting structure[J].Materials Science and Engineering,2002,A325:112.
[6] Scshacharyulu T;Medeirce S C;Morgan] T;Malas J C Frazie W G Prasad Y V R K .Hot deformation and microstructural damage mechanisms in extra-low interstitial (ELI) grade Ti-6Al-4V[J].Materials Science and Engineering,2000,A279:289.
[7] Shell E B;Semiatin S L .Effect of initial microstructure on plastic flow and dynamic globularization during hot working of Ti-6Al-4V[J].Metallurgical and Materials Transactions,1999,30A:3219.
[8] Semiatin S L;Thomas J F;Dadras P .Processing-micrustructure relationships for Ti-6Al-2Sn-4Zr-2Mo-O.1Si[J].Metallurgical and Materials Transactions,1983,14A:2363.
[9] Weiss I;FrcesFH;EylonD;WelschGE .Modification of Alpha Morphology in Ti-6Al-4V by thermomechnical processing[J].Metallurgical and Materials Transactions,1986,17A:1935.
[10] SemiatinSL;Seetharaman V;Wesisl.Hot working of titonium alloys-an overview[A].Minerals,Metals & Materials Society,1997:4.
[11] Korshunov AA.;Mazurski MI.;Salishchev GA.;Dmitriev OV. Muravlev AV.;Chistyakov PV.;Enikeev FU. .GRAIN-STRUCTURE REFINEMENT IN TITANIUM ALLOY UNDER DIFFERENT LOADING SCHEDULES[J].Journal of Materials Science,1996(17):4635-4639.
[12] Kaybyshev O A;Luffullin R Y;Saishcbev G A .Micostructural changes during heat treatment and hot deformation of titanium alloy VT9 with platelike micrcstructure[J].Fiz Metal Metalloyed,1985,50:578.
[13] 周军 .Ti-17钛合金片状组织球化规律研究[D].西北工业大学,2005.
[14] 李晓芹.TC11钛合金β锻造工艺、组织和性能的关系[J].机械科学与技术,2000(01):127-129.
[15] 潘雅琴,杨昭苏.TC11钛合金热压变形行为[J].稀有金属材料与工程,1992(03):18-26.
[16] 朱磊,张麦仓,董建新,庞克昌.TC11合金本构关系的建立及其在盘件等温锻造工艺设计中的应用[J].稀有金属材料与工程,2006(02):253-256.
[17] 孙新军,白秉哲,顾家琳,陈南平.TC11合金热变形行为及Z-D关系的研究[J].稀有金属,2000(03):171-177.
[18] 陈慧琴,林好转,郭灵,曹春晓.TC11钛合金高温流变行为及组织演变[J].航空材料学报,2007(03):1-5.
[19] 李鑫,赵为纲,鲁世强,王克鲁.TC11合金β相区大应变热变形行为及组织研究[J].兵器材料科学与工程,2007(03):28-33.
[20] Chen H Q;Lin H Z;Guo L;Cao C X .Hot deformation behavior and microstmcture evolution of Ti-6.5Al-1.5Zr-3.5Mo-O.3Si with equiaxed α + β starting structure[J].Materials Science Forum,2007,546-549:1383.
[21] Prasad YVRK.;Seshacharyulu T. .Processing maps for hot working of titanium alloys[J].Materials Science & Engineering, A. Structural Materials: Properties, Misrostructure and Processing,1998(1/2):82-88.
[22] Malas J C;Seetharaman V .Using material behavior model to develop process control strategies[J].Journal of the Minerals,Metals & Materials Society,1992,7:8.
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