| 复合材料与金属混合结构寿命研究及验证 |
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| 引用本文： | 宁晋建,曹奇凯,隋福成,卢增威.复合材料与金属混合结构寿命研究及验证[J].飞机设计,2008,28(5):19-21. |
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| 作者姓名： | 宁晋建 曹奇凯 隋福成 卢增威 |
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| 作者单位： | 1. 沈阳飞机设计研究所,辽宁,沈阳,110035
2. 沈阳飞机工业集团有限公司,辽宁,沈阳,110034 |
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| 摘 要： | 在工程设计中常采用复合材料壁板与金属材料骨架的混合结构。本文对复合材料与金属材料混合结构的寿命展开了研究，进行了疲劳试验并用全寿命方法计算了金属结构裂纹形成寿命和裂纹扩展寿命。通过对疲劳试验件的断口反推与计算结果得到了较好的吻合。
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| 关 键 词： | 疲劳 损伤容限 全寿命 复合材料 |
The Study and Test in Mixed Structure Life of Composites and Metals |
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| NING Jin-jian,CAO Qi-kai,SUI Fu-cheng,LU Zeng-wei.The Study and Test in Mixed Structure Life of Composites and Metals[J].Aircraft Design,2008,28(5):19-21. |
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| Authors: | NING Jin-jian CAO Qi-kai SUI Fu-cheng LU Zeng-wei |
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| Institution: | 1.Shenyang Aircraft Design & Research Institute;Shenyang 110035;China;2.Shenyang Aircraft Corportion;Shenyang 110034;China |
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| Abstract: | The mixed structure of composite panels and metal beam is often adopted in the engineering design.This paper studies the fatigue life of mixed structure composites and metals,analyzes the fatigue tests,and calculates life of crack formation and crack growth with full life method.Analysis results from the cut in the fatigue test member are met with the calculation result. |
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| Keywords: | fatigue crack growth full life composite |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
