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真空去應(yīng)力退火對(duì)TC18鈦合金殘余應(yīng)力及組織性能的影響
發(fā)布人：上海艾荔艾金屬材料有限公司bt990.com.cn
更新時(shí)間：2015-12-16
在不同溫度和時(shí)間下對(duì)TC18鈦合金進(jìn)行真空去應(yīng)力退火處理，研究TC18鈦合金真空去應(yīng)力退火前后力學(xué)性能及殘余應(yīng)力的變化規(guī)律，觀察去應(yīng)力退火后的金相組織和拉伸斷口形貌。
真空去應(yīng)力退火對(duì)TC18鈦合金殘余應(yīng)力及組織性能的影響Influence of vacuum stress relieving annealing on residual stress and microstructure properties of TC18 titanium alloy
在不同溫度和時(shí)間下對(duì)TC18鈦合金進(jìn)行真空去應(yīng)力退火處理，研究TC18鈦合金真空去應(yīng)力退火前后力學(xué)性能及殘余應(yīng)力的變化規(guī)律，觀察去應(yīng)力退火后的金相組織和拉伸斷口形貌。結(jié)果表明：經(jīng)真空去應(yīng)力退火后，TC18鈦合金的抗拉強(qiáng)度和屈服強(qiáng)度降低，沖擊韌性、斷裂韌性、伸長(zhǎng)率和斷面收縮率提高；殘余應(yīng)力消除效果顯著；隨著退火溫度的升高，合金顯微組織呈現(xiàn)規(guī)律性變化；當(dāng)溫度達(dá)到650 ℃以上時(shí)，α相明顯減少，亞穩(wěn)定β相顯著增加，導(dǎo)致其強(qiáng)度下降，與力學(xué)性能測(cè)試結(jié)果相吻合；合金塑性提高，與斷口形貌分析一致；最后，得到TC18鈦合金的真空去應(yīng)力退火制度為600~650 ℃和1~4 h。
The different temperature and time parameters were adopted in the vacuum stress relieving annealing processes of TC18 titanium alloy. The evolution of mechanical properties and residual stress was researched, the microstructures and SEM images of fracture surfaces were also observed. The results show that, after the vacuum stress relieving annealing, the tensile and yield strengths of TC18 titanium alloy decrease, while the charpy toughness, fracture toughness, elongation and area reduction increase. The removing effect of residual stress is remarkable. Along with the increases of the temperature of stress relieving annealing, the microstructure of the alloy changes regularly. When the temperature exceeds 650 ℃, α-phase decreases obviously, and the metastable β-phase increases dramatically. Thus, the strength of the alloy decreases, which coincides with the result of mechanical properties. Meanwhile, the plasticity increases, which coincides with the fracture appearance. Finally, the vacuum stress relieving annealing schedule is obtained to be 600?650 ℃ and 1?4 h.
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