Experimental investigations on dynamic in-plane compressive behavior of a plain weave composite were performed using the split Hopkinson pressure bar. A quantitative criterion for calculating the constant strain rate ...Experimental investigations on dynamic in-plane compressive behavior of a plain weave composite were performed using the split Hopkinson pressure bar. A quantitative criterion for calculating the constant strain rate of composites was established. Then the upper limit of strain rate, restricted by stress equilibrium and constant loading rate, was rationally estimated and confirmed by tests. Within the achievable range of 0.001/s-895/s, it was found that the strength increased first and subsequently decreased as the strain rate increased. This feature was also reflected by the turning point(579/s) of the bilinear model for strength prediction. The transition in failure mechanism, from local opening damage to completely splitting destruction, was mainly responsible for such strain rate effects. And three major failure modes were summarized under microscopic observations: fiber fracture, inter-fiber fracture, and interface delamination. Finally, by introducing a nonlinear damage variable, a simplified ZWT model was developed to characterize the dynamic mechanical response. Excellent agreement was shown between the experimental and simulated results.展开更多
铝反射镜在航空航天和空间遥感卫星领域中广泛应用,为了提高铝反射镜的轻量化率,降低民用商业遥感卫星的发射成本,设计了一种背部开放式、三角形孔结构和三点支撑形式的轻量化铝反射镜。在此结构基础上,首先以质量最小为优化目标,以反...铝反射镜在航空航天和空间遥感卫星领域中广泛应用,为了提高铝反射镜的轻量化率,降低民用商业遥感卫星的发射成本,设计了一种背部开放式、三角形孔结构和三点支撑形式的轻量化铝反射镜。在此结构基础上,首先以质量最小为优化目标,以反射镜背部加强筋的厚度和加强筋的布局为优化对象,以柔度最小为响应约束,应用有限元法对反射镜背部加强筋的厚度进行尺寸优化和加强筋的布局进行拓扑优化,得到的铝反射镜轻量化率超过63%;然后设计了工装夹具进行单点金刚石车削加工试验;最后使用激光干涉仪检测反射镜的面形精度。检测结果表明:反射镜的面形值PV(peak to valley)为1.48μm,能够满足民用商业遥感卫星的使用要求。展开更多
基金the National Science and Technology Major Project(Grant No.2017-VII-0011-0106)Natural Science Foundation of Heilongjiang Province(Grant No.ZD2019A001).
文摘Experimental investigations on dynamic in-plane compressive behavior of a plain weave composite were performed using the split Hopkinson pressure bar. A quantitative criterion for calculating the constant strain rate of composites was established. Then the upper limit of strain rate, restricted by stress equilibrium and constant loading rate, was rationally estimated and confirmed by tests. Within the achievable range of 0.001/s-895/s, it was found that the strength increased first and subsequently decreased as the strain rate increased. This feature was also reflected by the turning point(579/s) of the bilinear model for strength prediction. The transition in failure mechanism, from local opening damage to completely splitting destruction, was mainly responsible for such strain rate effects. And three major failure modes were summarized under microscopic observations: fiber fracture, inter-fiber fracture, and interface delamination. Finally, by introducing a nonlinear damage variable, a simplified ZWT model was developed to characterize the dynamic mechanical response. Excellent agreement was shown between the experimental and simulated results.
文摘铝反射镜在航空航天和空间遥感卫星领域中广泛应用,为了提高铝反射镜的轻量化率,降低民用商业遥感卫星的发射成本,设计了一种背部开放式、三角形孔结构和三点支撑形式的轻量化铝反射镜。在此结构基础上,首先以质量最小为优化目标,以反射镜背部加强筋的厚度和加强筋的布局为优化对象,以柔度最小为响应约束,应用有限元法对反射镜背部加强筋的厚度进行尺寸优化和加强筋的布局进行拓扑优化,得到的铝反射镜轻量化率超过63%;然后设计了工装夹具进行单点金刚石车削加工试验;最后使用激光干涉仪检测反射镜的面形精度。检测结果表明:反射镜的面形值PV(peak to valley)为1.48μm,能够满足民用商业遥感卫星的使用要求。
