| N5A飞机中翼前梁缘条LC9型材过时效工艺试验 |
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| 引用本文： | 王迪赞.N5A飞机中翼前梁缘条LC9型材过时效工艺试验[J].洪都科技,1999(4):33-43. |
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| 作者姓名： | 王迪赞 |
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| 作者单位： | 洪都航空集团理化测试中心 |
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| 摘 要： | 介绍了ＬＣ９型材过时效工艺试验和过时效及人工时效对比试验情况，从而作出了ＬＣ９型材经过时效处理可装机使用的结论。
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| 关 键 词： | LC9铝型材 过时效工艺试验 N5A飞机 中翼前梁缘条 |
Overageing Technological Tests of Edge Strip LC9 at Front Spar of N5A Mid-wing |
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| Wang Dizan.Overageing Technological Tests of Edge Strip LC9 at Front Spar of N5A Mid-wing[J].Hongdu Science and Technology,1999(4):33-43. |
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| Authors: | Wang Dizan |
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| Abstract: | This paper is to describe the overageing technological test and the over-ageing & altificial ageing comparative conditions of section LC9 so that the conclusion ismade out that the section LC9, after being ageing - treated, could be mounted on the aircraftfor servle. |
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| Keywords: | N5A-airplane LC9 aluminium section Overageing |
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