采用恒应变速率热压缩模拟实验,对Ti-5Mo-5V-1Cr-3A1(简称1Cr)钛合金在应变速率0.001~1s-1、变形温度700~900℃条件下进行研究.结果表明:该材料的流变应力对温度与应变速率敏感:当变形温度为700~800℃时,真应力-真应变曲线呈现动态再结晶单曲线特征;当变形温度为800~900℃时,低应变速率(0.001s-1)的真应力-真应变曲线呈现动态再结晶多应力峰值曲线特征,高应变速率(0.01~1s-1)的真应力-真应变曲线呈现动态回复曲线特征.1Cr合金在等温压缩变形时的流变行为可用包含Zener-Holomon参数的Arrhenius本构方程描述,变形激活能为456kJ/mol.金相结果显示,材料在热压缩过程中的动态行为除了与变形速率、变形温度等加工参数相关外,也与相应温度、变形速率下材料的组织及相结构有关.合金在低应变速率0.001s 1下热压缩变形时,在接近相变点或以上(800~900℃)温度范围内仍呈现动态再结晶行为,这与材料在此阶段发生的应变诱发马氏体转变密切相关,马氏体相的析出促使材料在热变形时趋向于发生动态再结晶行为.
参考文献
[1] | Weiss I.;Semiatin SL. .Thermomechanical processing of beta titanium alloys - an overview[J].Materials Science & Engineering, A. Structural Materials: Properties, Misrostructure and Processing,1998(1/2):46-65. |
[2] | BOYER R R .An over view on use of titanium in aerospace industry[J].MATERIALS SCIENCE & ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING,1996,213(1-2):103-114. |
[3] | 赵永庆,奚正平,曲恒磊.我国航空用钛合金材料研究现状[J].航空材料学报,2003(z1):215-219. |
[4] | 付艳艳,宋月清,惠松骁,米绪军.航空用钛合金的研究与应用进展[J].稀有金属,2006(06):850-856. |
[5] | 张翥,惠松骁,刘伟.高强高韧TB10钛合金棒材研究[J].稀有金属,2006(02):221-225. |
[6] | 毛柏平,郭胜利,沈健.Ti-5523钛合金热变形流变行为的研究[J].稀有金属,2008(05):674-678. |
[7] | 余永宁.金属学原理[M].北京:冶金工业出版社,2003:464-465. |
[8] | ZENER C;HOLLOM J H .Effect of strain-rate upon the plastic flow of steel[J].Journal of Applied Physics,1944,15(01):22-32. |
[9] | SHI H;MALAREN A J;SELLARS C M et al.Constitutive equations for high temperature flow stress of aluminum alloys[J].Material Science and Engineering,1997,13(03):210-216. |
[10] | 沈健.AA7005铝合金的热加工变形特性[J].中国有色金属学报,2001(04):593-597. |
[11] | SELLARS C M;TEGART W J M .On the mechanism of hot deformation[J].ACTA METALLURGICA,1966,14(09):1136-1139. |
[12] | MCQUEEM H J;YUE S;RYAN N D et al.Hot working characteristics of steels in austenitic state[J].Journal of Materi als Processing Technology,1995,53(1-2):293-310. |
[13] | H.J. McQueen;E. Fry;J. Belling .Comparative Constitutive Constants for Hot Working of Al-4.4Mg-0.7Mn (AA5083)[J].Journal of Materials Engineering and Performance,2001(2):164-172. |
[14] | POIRIER J P;关德林.晶体的高温塑性变形[M].大连:大连理工出版社,1989:52-54. |
[15] | JONAS J J;SELLARS C M;MCG W J .Strength and structure under hot working conditions[J].Tegart Int Metall Reviews,1969,130(14):1-24. |
[16] | SHEPPARD T;PARSON N C;ZAIDI M A .Dynamic recrystallization in Al-7Mg alloy[J].Metal Science Journal,1983,17(10):481-490. |
[17] | 林启权,张辉,彭大暑,林高用,杨立斌.2519铝合金热压缩变形流变应力行为[J].热加工工艺,2002(03):3-5. |
[18] | 蒋树农,刘楚明,李慧中,张新明.99.992%高纯多晶铝热压缩流变应力特征[J].热加工工艺,2004(09):17-19. |
[19] | LEYENSC;PETERSM;陈振华.钛与钛合金[M].北京:化学工业出版社,2005:4-5. |
[20] | 沈桂琴.Ti-10V-2Fe-3Al合金的应力诱发马氏体转变[J].航空材料学报,1997(02):26. |
[21] | DUERIG T W;ALBRECHT J;RICHTER D et al.Formation and reversion of stress induced martensite inTi-10V-2Fe-3Al[J].ACTA METALLURGICA,1980,30:2161-2172. |
[22] | 陈威,孙巧艳,肖林,佘文博,孙军,葛鹏.应变速率对β固溶Ti-10V-2Fe-3Al合金应力诱发马氏体相变的影响[J].中国有色金属学报,2010(11):2124-2129. |
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