变形—损伤耦合的超塑性恒压轴对称充模胀形的有限元模拟

采用大变形刚粘塑性有限元法模拟超塑性恒压轴对称充模胀形过程，分析了模具几何参数及材料参数对胀形过程中材料的流变行为、胀形制件厚度分布和成形时间的影响规律，给出了质点的流动轨迹，不同时刻制件的剖面形状及应力、应变分布；基于修正的Ｇｕｒｓｏｎ粘塑性势推导了内部空洞体积分数累积增大模型并据此进行了变形－损伤耦合计算。     

ANALYSIS OF SURFACE CRACK ON FORWARD EXTRUDING BAR DURING AXISYMMETRIC CUP-BAR COMBINED EXTRUSION PROCESS

In this paper,the kinematically admissible velocity field with surface crack on forwardextruding bar is put forward during the axisymmetric cup-bar combined extrusion process,in accordance with the results of model experiments.On the basis of velocity field,the necessary condition for surface crack formation onthe forward extruding bar is derived,with the help of upper bound theorem and theminimum energy principle.Meanwhile,the relationships between surface crack formationand combination of reduction in area for the part of forward and backward extursions(εb,εf),relative residual thickness of billet(T/R_0),frictional factor(m)or relativeland length of ram and chamber(l_b/R_0,l_f/R_0)are calculated during the extrusion process.Therefore,whether the surface crack on forward exturding bar occurs can be predictedbefore extruding the lower-plasticity metals for axisymmetric cup-bar combined extrusionprocess.The analytical results agree very well with experimental results of aluminium alloyLY12 (ASTM2024)an     

超塑性恒压充模胀形过程各力学量场的影响因素及影响规律

采用刚粘塑性有限元法模拟了超塑性恒压充模胀形过程，分析了应变速率敏感性指数ｍ、厚向异性系数Ｒ、初始板厚、界面摩擦等因素对应力、应变和应变速率等力学量场的影响；通过对铝合金ＬＹ１２ＣＺ板料的相应实验对模拟结果进行了验证     

Forming limit during superplastic deformation of sheet metals

ＦＯＲＭＩＮＧＬＩＭＩＴＤＵＲＩＮＧＳＵＰＥＲＰＬＡＳＴＩＣＤＥＦＯＲＭＡＴＩＯＮＯＦＳＨＥＥＴＭＥＴＡＬＳＤｕＺｈｉｘｉａｏ（杜志孝）;ＬｉＭｉａｏｑｕａｎ（李淼泉）;ＬｉｕＭａｂａｏ（刘马宝）;ＷｕＳｈｉｃｈｕｎ（吴诗惇）（Ｆａｃｕｌｔｙ４０２ｏ...     

变形-损伤耦合的起塑性恒压轴对称充模胀形的有限元模拟

采用大变形刚粘塑性有限元法模拟超塑性恒压轴对称充模胀形过程、分析了模具几何参数及材料参数对胀形过程中材料的流变行为、胀形制许厚度分布和成形时间的影响规律。给出了质点的流动轨迹、不同时刻制件的剖面形状及应力、应变分布；基于修正的Gurson粘塑性势推导了内部空洞体积分数累积增大模型并据此进行了变形-损伤耦合计算．     

Analysis of surface crack on forward extruding bar during axisymmetric cup-bar combined extrusion process

In this paper, the kinematically admissible velocity field with surface crack on forward extruding bar is put forward during the axisymmetric cup-bar combined extrusion process, in accordance with the results of model experiments.On the basis of velocity field, the necessary condition for surface crack formation on the forward extruding bar is derived, with the help of upper bound theorem and the minimum energy principle. Meanwhile, the relationships between surface crack formation and combination of reduction in area for the part of forward and backward extursions (ε_b,ε_f) relative residual thickness of billet (T/R₀),frictional factor (m) or relative land length of ram and chamber (l_b|R₀,l_f|R₀) are calculated during the extrusion process. Therefore, whether the surface crack on forward exturding bar occurs can be predicted before extruding the lower-plasticity metals for axisymmetric cup-bar combined extrusion process.The analytical results agree very well with experimental results of aluminium alloy LY12 (ASTM 2024) and LC4 (ASTM 7075).     

超塑性板料的成形极限

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（ｆｃ）作为破坏判据，预测了板料超塑变形时的成形极限。     

复合挤压时的杆部表面裂纹分析

本文依据实验结果拟定了轴对称杯杆型复合挤压出现杆部表面裂纹时的金属流动速度场,以此为基础,并藉助于上限原理和最小能量原理,获得了此类复合挤压时杆部表面裂纹形成的必要条件。同时,研究了此类复合挤压杆部变形开裂区与正挤,反挤部分变形程度(εf,εb)组合、坯料相对余厚(T/R_0)、摩擦因数m值以及模具工作带相对长度(l_f/R_0,l_b/R_0)的关系.从而可以估测低塑性材料在进行此类复合挤压时杆部是否形成表面裂纹.LY12和LC4材料的试验结果与本文的分析结果具有很好的一致性.