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腐蚀损伤结构复合材料修补构型优选试验研究
引用本文:徐胜,任三元,鲁国富.腐蚀损伤结构复合材料修补构型优选试验研究[J].装备环境工程,2011,8(4):104-108.
作者姓名:徐胜  任三元  鲁国富
作者单位:1. 海军装备部航订部,北京,100841
2. 中航工业特种飞行器研究所,湖北荆门,448035
摘    要:设计了模拟含腐蚀损伤和机械损伤的铝合金结构复合材料修补试验件,开展了各种修补构型预腐蚀的静拉伸试验.通过对比分析,获得了腐蚀环境下最佳复合材料修补构型设计,为严酷腐蚀环境与载荷环境下海军飞机金属结构腐蚀损伤和机械损伤的复合材料修补设计提供了指导.

关 键 词:腐蚀损伤  构型优选  复合材料修补  静拉伸
收稿时间:4/4/2011 12:00:00 AM
修稿时间:2011/8/15 0:00:00

Experimental Research of Shape Selection of Composite Patch for Corroded Structure
XV Sheng,REN San-yuan and LU Guo-fu.Experimental Research of Shape Selection of Composite Patch for Corroded Structure[J].Equipment Environmental Engineering,2011,8(4):104-108.
Authors:XV Sheng  REN San-yuan and LU Guo-fu
Institution:XV Sheng1,REN San-yuan2,LU Guo-fu2(1.The Aviation Equipment Ordering Department of Navy Equipment Ministry,Beijing 100841,China,2.Special Vehicle Research Institute of AVIC,Jingmen 448035,China)
Abstract:Specimen repaired by composite patch which simulate the aluminum alloy structure with the mechanism and corrosion damage were designed.Uniaxial static tension test of the corroded specimen repaired by varied of patches was carried out.The optimized patch shape for specimen which subjected to corrosion was acquired by comparison and analysis of result.The purpose was to provide guidance for composite repair design of metal structure of navy's airplane with the mechanism and corrosion damage in the atrocious ...
Keywords:corrosion  shape selection  composite patch  static tension  
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