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. XV Sheng,REN San-yuan,LU Guo-fu.Experimental Research of Shape Selection of Composite Patch for Corroded Structure[J].Equipment Environmental Engineering,2011,8(4):104-108.
腐蚀损伤结构复合材料修补构型优选试验研究
Experimental Research of Shape Selection of Composite Patch for Corroded Structure
投稿时间:2011-04-04  修订日期:2011-08-15
DOI:
中文关键词:  腐蚀损伤  构型优选  复合材料修补  静拉伸
英文关键词:corrosion  shape selection  composite patch  static tension
基金项目:
作者单位
徐胜 海军装备部 航订部,北京 100841 
任三元 中航工业特种飞行器研究所,湖北 荆门 448035 
鲁国富 中航工业特种飞行器研究所,湖北 荆门 448035 
AuthorInstitution
XV Sheng The Aviation Equipment Ordering Department of Navy Equipment Ministry, Beijing 100841, China 
REN San-yuan Special Vehicle Research Institute of AVIC, Jingmen 448035, China 
LU Guo-fu Special Vehicle Research Institute of AVIC, Jingmen 448035, China 
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中文摘要:
      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。
英文摘要:
      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 service environment.
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