不同热成形工艺下TA32钛合金的流变性能及组织演变
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Study on Rheological Properties and Microstructure Evolution of TA32 Titanium Alloy under Different Thermoforming Processes
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    摘要:

    针对随炉成形及到温成形2种主要的热成形工艺,通过高温拉伸试验,从TA32钛合金热成形流变性能及组织演变的角度出发,首先研究温度、变形速率、应变量等共性因素的影响,再对比分析2种热成形工艺下不同升温速率和冷却方式等特性因素的影响。设计两因素两水平工艺试验,分析不同高温润滑剂及热成形条件下TA32钛合金的氧化行为。结果表明:温度为800℃、应变速率为0.001 s~(-1)、保温时间为30 min、应变量为0.45~0.6,且选用到温热成形(升温速率为800℃/5 min,空冷)时,TA32钛合金的变形抗力较低,塑性较好,晶粒较为均匀,β相等轴晶粒较多,综合成形性能较好;到温成形条件下,选用立方氮化硼(CBN)作为高温润滑剂时,成形件的氧化程度最低。综合考虑,TA32钛合金板材最优高温成形方案为到温成形工艺并采用CBN作为高温润滑剂。

    Abstract:

    In order to study the two main thermoforming processes of thermoforming with furnace and temperaturereached thermoforming,through the analysis of thermoforming rheological properties and microstructure evolution of TA32 titanium alloy,the effects of common influence factors such as temperature,deformation rate and strain were studied firstly,and then the effects of heating rates and cooling methods under two thermoforming processes were compared.The oxidation behavior of TA32 titanium alloy under different high temperature lubricants and thermoforming conditions was also researched by two-factor two-level orthogonal test.The best formability and properties of TA32titanium alloy present during temperature-reached thermoforming with these process parameters:the temperature 800℃,strain rate 0.001 s~(-1),holding time 30 min,strain between 0.45 and 0.6,heating rate 800℃/5 min and air-cooling.Under this condition,TA32 titanium alloy has better plasticity,lower deformation resistance,uniform grains,and the moreβequiaxed grains.The lowest oxidation degree is found that the sample with the lubricant of cubic boron nitride(CBN)during the temperature-reached thermoforming.Finally,the temperature-reached thermoforming with the lubricant of CBN is the best process for TA32 titanium alloy sheets thermoforming.

    参考文献
    [1]Liu Z G,Li P J,Geng L L,et al.Microstructure and texture evolution of TA32 titanium alloy during superplastic deformation[J].Materials Science and Engineering A,2017,699:71-80.
    [2]王德林.传导加热法在复杂钛薄板件成形中的应用[J].钛工业进展,1996,13(1):21-22.
    [3]吴全兴.钛合金在航空产业中的应用及加工方法(连载Ⅱ)[J].钛工业进展,2013,30(3):44.
    [4]尚建勤.航空发动机钛合金钣金零件热成形[J].航空工程与维修,1999(2):28-29.
    [5]Liu J L,Zeng W D,Shu Y,et al.Hot working parameters optimization of TC4-DT titanium alloy based on processing maps considering true strain[J].Rare Metal Materials and Engineering,2016,45(7):1647-1653.
    [6]王小芳,陈明和,陈伟,等.TC4-DT钛合金高温热变形行为研究[J].航空材料学报,2012,32(1):30-34.
    [7]肖宁斌.BTi-6431S钛合金板材热成形性能评价研究[D].南京:南京航空航天大学,2012.
    [8]贾蔚菊,曾卫东,刘建荣,等.Ti60高温钛合金氧化行为研究[J].稀有金属材料与工程,2010,39(5):781-786.
    [9]梁锡梅,陈明和,苏楠,等.TA32钛合金高温连续氧化行为研究[J].钛工业进展,2019,36(2):12-19.
    [10]赵爱玲,王大月,王燕,等.钛及钛合金热氧化行为研究[J].钛工业进展,2013,30(1):16-19.
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苏楠;陈明和;梁锡梅;罗峰.不同热成形工艺下TA32钛合金的流变性能及组织演变[J].钛工业进展,2020,37(1):1-8.

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  • 在线发布日期: 2024-02-22