Abstract:Titanium alloy obtained lamellar microstructure (LM) and bimodal microstructure (BM) microstructures by the controlling of heat treatment parameters. Moreover, the tensile deformation behavior and effects of microstructure type on low cycle fatigue (LCF) behavior were investigated. The results indicate that TC21 alloy with coarse LM microstructure occur ductile rupture, since the annealing twins change the crystal orientation of part lamellar, and increase the plastic deformation degree before rupture. Dislocation multiplication and movement in αp phase and lathlike second α phase is the dominant factor for the deformation behavior of TC21 alloy with BM microstructure. The αp phase in BM microstructure can hinder the LCF crack propagation direction. Moreover, the absorbed energy of crack propagation can be increased by the αp phase. Therefore, the LCF lives were enhanced because of αp phase. The resistance for LCF crack propagation of αp phase in BM microstructure can be increased by the precipitation of α2 phase, since the harder α2 phase precipitated in the αp phase during thermal exposure (TE). For the BM+TE specimens, the crack mainly passes through the αp phase with “bypass”, while, for the BM specimens, the crack passes through the αp phase with “cutting”. Therefore, the LCF lives of Ti600 alloy after thermal exposure become longer because that the α2 phase precipitated in αp phase.
刘晓斌,翟羽佳,于腾. 显微组织对钛合金强韧性的影响[J]. , 2018, 25(3): 25-30.
LIU Xiao- bin,ZHAI Yu- jia,YU Teng. Effects of microstructure on strengthening- toughening of titanium alloys. , 2018, 25(3): 25-30.
[1] 莱茵斯C,皮特尔斯M编,陈振华等译. 钛与钛合金[M],北京:化学工业出版社,2005.[2] 陶春虎,刘庆瑔,曹春晓等著. 航空用钛合金的失效及其预防[M],北京:国防工业出版社,2002.[3] 曲恒磊,赵永庆,朱知寿等. 1种高强韧钛合金及其加工方法[P],中国国防专利:0310596511, 2003. [4] 张振祺,罗国珍,洪权等. Ti600合金的性能与显微组织的研究[J],航空材料学报,1999, 19(4): 6-10.[5] 蔡建明,李臻熙,马济民等. 航空发动机用600℃高温钛合金的研究与发展[J],材料导报,2005, (1): 50-53.[6] 李士凯,熊柏青,惠松骁. 热处理制度对TA15合金组织与性能的影响[J],材料热处理学报,2008, 29(6): 82-85.[7] Lee D H, Nam S W, Choe S J. Effect of microstructure and relaxation behavior on the high temperature low cycle fatigue of near-α-Ti-1100 [J], Materials Science and Engineering A, 2000, 291: 60-67.[8] 刘杨,王磊,丁扬等. 电场处理对GH4199合金组织与变形行为的影响[J],中国有色金属学报,2006, 16(10): 1749-1755.[9] Singh N, Gouthama, Singh V. Low cycle fatigue behavior of Ti alloy IMI 834 at room temperature [J], Materials Science and Engineering A, 2002, 325: 324-332.[10] Cui, W F, Liu C M, Zhou L, et al. Characteristics of microstructures and second-phase particles in Y-bearing Ti-1100 alloy [J], Materials Science and Engineering A, 2002, 323: 192-197. [11] 张廷杰. 钛合金相变的电子显微研究(Ⅶ)—耐热钛合金中的有序相Ti3Al沉淀[J],稀有金属材料与工程,1992, (2): 74-78.