超塑性板料的成形极限<sup>*</sup>

杜志孝; 李淼泉; 刘马宝; 吴诗惇

超塑性板料的成形极限^*

西北工业大学402教研室西安 710072

基金项目: * 国家自然科学基金;航空科学基金

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出版历程
- 收稿日期: 1994-10-24
- 修回日期: 1995-03-07
- 刊出日期: 1996-02-15

Forming Limit during Superglatic Deformation of Sheet Metals

Faculty 402 of Northwestern Polytechnical University, Xi'an 710072, P. R. China

摘要

摘要: 根据超塑变形过程中的损伤演变方程和超塑性变形的特点,本文将基于粘塑性势的热粘塑性损伤势函数与Hill描述板料变形的各向异性材料屈服行为有机地结合起来,考虑了起塑变形过程中损伤与失稳的交互作用.将起塑变形全过程分为稳定变形.准稳定变形、应变路径飘移和集中性失稳发展四个阶段,用数值方法建立了超塑性板料的损伤失稳模型.然后在此基础上,以集中性失稳发生(dε₂=0)或临界空洞体积分数(f_c)作为破坏判据,预测了板料超塑变形时的成形极限.
- 超塑性 /
- 损伤失 /
- 稳成形极限
Abstract: In the present paper, a thermo-viscoplastic damage potential and Hill's normal anisolropy(isotropy in plane).yield criterion to be quadratic in the stress components are combined to describe the interaction process of damage and instability during superplastic deformation, based on the kinetic equation for damoge during superplastic deformation and the deformation features of superplastic materials. The superplastic deformation process is devided into four Slages, namely, Stable, quasistable, Strain path drift to plane Strain and piane strain stages, and a damageinstability model during superplastic deformation of sheet metals is developed through numerical method. On the basis of the above results and taking the occurrence of localized inslability(dε₂=0) or the cavity volume fraction reaching the critical value(f_c) as a fracture criterion. the forming limit during superplastic deformation of sheet metals is predicted.
- superplasticity /
- damage-intability /
- forming limit

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参考文献(10)

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