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7050-T7451鋁合金銑削加工表面材料特性與本構關系模型的建立
發(fā)布人:上海艾荔艾金屬材料有限公司bt990.com.cn
更新時間:2015-12-03
為研究7050-T7451鋁合金材料銑削后表面應力應變特征,并建立表面材料本構關系模型,采用SSM-B4000TM型應力應變顯微探針測試系統(tǒng)對鋁合金7050-T7451材料表面進行自動球壓痕(ABI)實驗測試。
7050-T7451鋁合金銑削加工表面材料特性與本構關系模型的建立Milling surface properties of 7050-T7451aluminum alloy and establishment of constitutive model
為研究7050-T7451鋁合金材料銑削后表面應力應變特征,并建立表面材料本構關系模型,采用SSM-B4000TM型應力應變顯微探針測試系統(tǒng)對鋁合金7050-T7451材料表面進行自動球壓痕(ABI)實驗測試,獲得載荷-深度曲線,據(jù)此估算本構關系模型中應變硬化指數(shù)(n)與屈服強度(σy)等未知參數(shù)。進而基于有限元建模(FEM)進行壓痕過程的有限元仿真分析,研究本構關系模型中參數(shù)n與σy的變化對載荷-深度曲線的影響規(guī)律,獲得仿真載荷-深度曲線與實驗曲線誤差最小時的參數(shù)n與σy應滿足的函數(shù)關系,驗證了基于實驗本構關系模型參數(shù)的準確性。采用該材料本構關系模型仿真的載荷-深度曲線與實驗曲線相比,平均誤差為5.2 %。
In order to investigate the stress-strain properties of milling surface for 7050-T7451 aluminum alloy, and also to establish the constitutive model, automated ball indentation (ABI) test was carried out on the SSM-B4000TM?stress-strain microprobe system. The load-depth curve was obtained. Unknown parameters such as strain hardening exponent n and yield strength σy?were obtained based on this curve. Furthermore, indentation processes were simulated based on finite element method (FEM). Accordingly, the influence rules of the changes of parameters n and σy?on load-depth curve were studied. The functional relationship between parameters n and σy?was obtained when the error of load-depth curve between the simulation result and experimental value is the lowest. At last, the validity of parameters n and σy?in constitutive model obtained from ABI test was proved. Under this constitutive model, the average error between simulation load-depth curve and the test one is 5.2%.
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