期刊文献+

某型直升机静电起火受影响铝合金蒙皮热损伤检测评估

Fire Damage Detect for Aluminum-Alloy Skin of One Type Helicopter
下载PDF
导出
摘要 针对某型直升机静电起火受影响铝合金蒙皮,采用涡流电导率测试法、维氏硬度测试法及金相检测法对其热损伤进行检测和分析评定。 In this paper, electric conductivity and hardness and metallographic inspection methods were used to fire damage detect for aluminum-alloy skin of one type Helicopter.
出处 《直升机技术》 2013年第1期40-43,共4页 Helicopter Technique
关键词 铝合金蒙皮 电导率 硬度 金相 热损伤 aluminum-alloy skin electric conductivity hardness metallographic fire damage
  • 相关文献

参考文献3

二级参考文献17

  • 1徐可北.第四专题 涡流法测量铝合金电导率[J].无损检测,1996,18(4):116-120. 被引量:7
  • 2崔忠圻.金属学与热处理[M].北京:机械工业出版社,1988.354.
  • 3Smith T J.Modeling high-temperature stress-strain behavior of cast aluminum alloys.Metallurgical and Materials Transactions,1999,3(1):57-76.
  • 4Roach D,Hamon K,Jones C,et al.Aircraft inspection validation experiments and the use of NDT validation samples[J].Materials Evaluation,1995,53 (7):803-807.
  • 5Halmshaw R.The effect of facal sport size in insdustrial radiography.Brit J NDT,1992,34(8):391.
  • 6Taleff E M.The high temperature deformation.Tensile Ductility of Al Alloys,1999,51 (1):34-36.
  • 7茹柯夫斯基 H.E.航空技术装备外场修理[M].北京:国防工业出版社,2002.1-9.
  • 8Roach D, Hamon K, Jones C, et al. Aircraft inspection validation experiments and the use of NDT validation samples [J]. Materials Evaluation, 1995, 53 (7) :803-807.
  • 9NATANM. Relationship between microstruetion hardness and electrical conductivity of 2219 aluminum [J]. Journal of Materials Science, 1983, 18(11): 3288.
  • 10Rosen M, Horouipe E. The ageing process in aluminum alloy 2024 studied by means of eddy current[J]. Materials Science and Engineering, 1982,53(2):191.

共引文献8

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部