固溶温度对TC16钛合金显微组织与冲击韧性的影响
Effect of Solution Temperature on Microstructure and Impact Toughness of TC16 Titanium Alloy
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摘要: 分别在两相区温度(840,860 ℃)与单相区温度(880 ℃)下对TC16钛合金进行2 h固溶处理,再进行560 ℃×8 h时效处理,研究了固溶温度对固溶态和时效态合金显微组织、物相组成和冲击韧性的影响。结果表明:经固溶处理后TC16钛合金组织主要由α相与α"相组成,再经时效处理后,主要由α相和β相组成;固溶温度的升高使固溶态合金中的初生α相含量降低,等轴化程度增加,针状α相和α"相含量增加,当固溶温度升高到880 ℃时,初生α相完全消失;再经时效处理后,组织中形成大量针状次生α相,且次生α相含量随固溶温度的升高而增加,而初生α相含量和尺寸与固溶态相比无明显变化。随着固溶温度的升高,固溶处理后合金的冲击吸收能量和冲击韧性值增加;经时效处理后,二者相比于固溶态均减小,且随固溶温度升高而不断降低;随着固溶温度的升高,冲击断口中韧窝数量减少,当固溶温度为880 ℃时,冲击断口主要由解理面组成;再经时效处理后,断口中出现较多二次裂纹,随着固溶温度的升高,二次裂纹数量增加。Abstract: TC16 titanium alloy was treated by solution at two-phase region temperature (840, 860 ℃) and single-phase region temperature (880 ℃) for 2 h, and then aging at 560 ℃ for 8 h. The effects of solution temperature on the microstructure, phase composition and impact toughness of alloy in the solution state and in the aging state were studied. The results show that the microstructure of TC16 titanium alloy after solution was mainly composed of α phase and α" phase, and after aging was mainly composed of α phase and β phase. With the increase of solution temperature, the content of primary α phase in the soluted alloy decreased, the equiaxialization degree increased, and the content of acicular α phase and α" phase increased. When the solution temperature increased to 880 ℃, the primary α phase disappeared completely. After aging, a large number of needle-like secondary α phase was formed in the microstructure, and the content of secondary α phase increased with the increase of solution temperature, while the content and size of primary α phases had no obvious change compared with those in the solution state. With the increase of solution temperature, the impact absorbed energy and impact toughness value of the alloy after solution increased. After aging, both of them decreased comparing with those in solution state, and decreased with the increase of solution temperature. With the increase of solution temperature, the number of dimples in the impact fracture decreased. When the solution temperature was 880 ℃, the impact fracture was mainly cleavage plane. After aging, more secondary cracks appeared in the fracture. With the increase of solution temperature, the number of secondary cracks increased.