| 修理问题中层压板特性的工程估算方法 |
| |
| 引用本文： | 童谷生%章钢.修理问题中层压板特性的工程估算方法[J].宇航材料工艺,2007,37(2):58-61. |
| |
| 作者姓名： | 童谷生%章钢 |
| |
| 作者单位： | 1. 华东交通大学土木建筑学院,南昌,330013
2. 洪都航空集团科技开发部,南昌,330024 |
| |
| 摘 要： | 研究了层压板修理中对无损、开孔以及具冲击损伤情况下力学性能的简便工程计算方法。根据自行设计的试验及其相关文献的试验结果,采用Heslehurst关于层压板弹性常数及强度的估算方法时数据进行了分析,同时把其对开孔板得到剩余强度的估算方法推广到合冲击损伤在内的损伤结构剩余强度。多种材料体系和铺层方式组成的层压板的试验和计算对比表明,该工程算法给出的精度大都在20%以内。因此可以用该算法来确定结构的修理容限的下限。
|
| 关 键 词： | 层压板 冲击损伤 修理容限 剩余强度 |
| 修稿时间： | 2005-11-21 |
An Engineering Approach to Evaluation of Mechanical Properties of Composite Laminate |
| |
| Tong Gusheng,Zhang Gang.An Engineering Approach to Evaluation of Mechanical Properties of Composite Laminate[J].Aerospace Materials & Technology,2007,37(2):58-61. |
| |
| Authors: | Tong Gusheng Zhang Gang |
| |
| Institution: | 1 East China Jiaotong University, Nanchang 330013;2 Hongdu Aviation Industry Group,Nachang 330024 |
| |
| Abstract: | An engineering method evaluating mechanical properties of composite laminate with impact damage, hole and undamaged sample is presented.Experiment results of the strength and equivalent elastic eharacteristie of different material system and layer up' s laminate are analyzed by using Heslehurt' s formula.At the same time,resid- ual strength of a laminate after impact can be estimated by using the method for damaged hole with the errors within 20%.By using the engineering method,it can be easily determined whether the damaged area of a laminate is within repair tolerance. |
| |
| Keywords: | Laminate Impact damage Repair tolerance Residual strength |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
| 点击此处可从《宇航材料工艺》浏览原始摘要信息 |
| 点击此处可从《宇航材料工艺》下载免费的PDF全文 |
