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Hot Deformation Constitutive Equation of Spray Formed Superalloy GH742y

机译:喷射成形高温合金GH742y的热变形本构方程

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Isothermal compression of spray formed superalloy GH742y has been conducted on Gleebe−1500D hot simulation at the deformation temperatures ranging from 930°C to 1020°C where the strain rates have ranged from 0.01s−1 to 10s−1, and the height reduction of 50%. The effect of deformation temperatures and strain rates on the flow stress was analyzed with the true stress-true strain curve, and the hot deformation constitutive equation of superalloy GH742y was established using Arrhenius type hyperbolic sine equations. Error analysis shown that the established constitutive equations were coincident with experimental data well, and it provided the theory basis to make forging technology of superalloy GH742y.
机译:在Gleebe -1 500D热模拟中对喷射成形的高温合金GH742y进行了等温压缩,变形温度为930°C至1020°C,应变速率为0.01s - 1 到10s -1 ,高度降低50%。用真应力-真应变曲线分析了变形温度和应变速率对流动应力的影响,并使用Arrhenius型双曲正弦方程建立了GH742y合金的热变形本构方程。误差分析表明,所建立的本构方程与实验数据吻合良好,为高温合金GH742y的锻造工艺提供了理论依据。

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