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Hot deformation constitutive equation of 7059 aluminum alloy

机译:7059铝合金的热变形本构式方程

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Isothermal compression of the 7059 aluminum alloy was conducted on a Gleebe-1500D hot-simulator at the deformation temperature ranging from 330 to 450 °C and the strain rate ranging from 0.01 to 10.0 s~(-1). The influences of deformation temperature and strain rate on the stress were studied according to true stress-true strain curves, and the constitutive equation of 7059 aluminum alloy during hot deformation was established based on hyperbolic sine equations of Arrhenius type. Error analyses show that the established constitutive equation is coincident with experimental data well, and the constitutive equation provides a theory basis for determining forging technology of 7059 aluminum alloy.
机译:7059铝合金的等温压缩在Gleebe-1500D热模拟器上,变形温度范围为330至450℃,应变率范围为0.01至10.0 s〜(1)。根据真正的应力 - 真菌曲线研究了变形温度和应变率对应力的影响,并根据Arhenius型的双曲线正弦方程建立了7059铝合金的组成方程。误差分析表明,已建立的本构式方程与实验数据孔一致,本构方程为确定7059铝合金的锻造技术提供了一种理论依据。

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