| 选择性加强结构在飞机结构设计中的应用 |
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| 引用本文： | 沈培良.选择性加强结构在飞机结构设计中的应用[J].科学技术与工程,2012,12(21):5404-5407,5411. |
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| 作者姓名： | 沈培良 |
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| 作者单位： | 上海飞机设计研究院,上海,200232 |
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| 摘 要： | 针对如何满足民用飞机高寿命低重量的设计指标问题,引入一种在原铝合金飞机结构上固化GLARE条带的新型结构,以提高疲劳和损伤容限性能。并对其疲劳和损伤容限性能以及湿热环境敏感性进行阐述,提出适航符合性思路。
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| 关 键 词： | 疲劳 损伤容限 选择性加强结构 GLARE |
| 收稿时间： | 3/17/2012 3:52:25 PM |
| 修稿时间： | 4/22/2012 9:45:06 PM |
Selective reinforcement structure application in aircraft structural design |
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| shenpeiliang.Selective reinforcement structure application in aircraft structural design[J].Science Technology and Engineering,2012,12(21):5404-5407,5411. |
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| Authors: | shenpeiliang |
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| Institution: | SHEN Pei-liang(Shanghai Aircraft Design and Research Institute,Shanghai 200232,P.R.China) |
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| Abstract: | For meeting the design objective about long life and low weight civil aircraft, this paper introduce a new kind of structure, which is advanced in damage tolerance & fatigue with GLARE strip solidified onto original aluminum aircraft structure, and expatiate its damage tolerance & fatigue capability, and susceptivity to high humidity & high temperature environment. In the end this paper gives a means of certification compliance. |
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| Keywords: | fatigue damage tolerance selective reinforcement structure glare |
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