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冶金质量对铝合金疲劳性能影响的探讨 被引量:3

Influence of metallurgical quality on the fatigue properties of aluminum alloy
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摘要 评述铝合金疲劳裂纹萌生研究现状及机制,阐述了典型铝合金及其合金元素对疲劳性能的影响规律,非金属夹杂、气孔、疏松及粗大第二相等对疲劳裂纹萌生的影响,得出通过控制合金元素含量、减少杂质、提高洁净度、改善变质效果和改进热处理等可有效改善铝合金的断裂韧性。 This review summarizes research status and mechanism of fatigue crack initia- tion in aluminum alloy, the influence of typical aluminum alloy and alloy elements on fatigue properties and the influence of non-metallic inclusion, pore, loose and coarse second phases on fatigue crack initiation. The results show that controlling of alloy elements, reducing impu- rities, improving cleanliness, modification effect and heat treatment can effectively improve the fracture toughness of high strength aluminum alloys.
出处 《轻合金加工技术》 CAS 北大核心 2015年第11期19-23,共5页 Light Alloy Fabrication Technology
关键词 铝合金 冶金质量 疲劳性能 裂纹萌生 aluminum alloy metallurgical quality fatigue properties crack initiation
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  • 1WILLIAMS J C, STARKE E A. Progress in structural materials for aerospace systems [ J 1. Acta Materialia, 2003,51 (19) : 5775 -5799. 被引量:1
  • 2杨守杰,戴圣龙.航空铝合金的发展回顾与展望[J].材料导报,2005,19(2):76-80. 被引量:204
  • 3DUMONT D, DESCHAMPS A,BRECHET Y. On the relationship between microstructure,strength and tough- ness in AA7050 aluminum alloy[ J]. Materials Science and Engineering A,2003, A356(3) : 326 -336. 被引量:1
  • 4SRIVATSAN T S, KOLAR D, MAGNUSEN P. The cyclic fatigue and final fracture behavior of aluminum alloy 2524[J]. Materials Design,2002,23(2) : 129 - 139. 被引量:1
  • 5陈文.先进铝合金在A380上的应用[J].航空维修与工程,2005(2):40-41. 被引量:40
  • 6RODRIGES E M, MATIAS A, GODERFROID L B, BASTIAN F L, RUBAIE K S. Fatigue crack growth resist- ance and crack closure behavior in two aluminum alloys for aeronautical applications [ J ]. Materials Research, 2005,8(3) : 287 -291. 被引量:1
  • 7VRATNICA M, CUROVIC J, BURZIC Z. Fatigue properties of high strength A1-Zn-Mg-Cu alloys with different levels impurity [ J ]. Materials and Technology ,2002,36 ( 1/2 ) : 11 - 14. 被引量:1
  • 8PAYNE J, WELSH G. Observations of fatigue crack initiation in 7075-T651 [ J ]. International Journal of Fa- tigue,2010,32(2) :247 -255. 被引量:1
  • 9韩剑,戴起勋,赵玉涛,李桂荣.7075-T651铝合金疲劳特性研究[J].航空材料学报,2010,30(4):92-96. 被引量:21
  • 10郑子樵,陈圆圆,钟利萍,佘玲娟,翟同广.2524-T34合金疲劳裂纹的萌生和扩展行为[J].中国有色金属学报,2010,20(1):37-42. 被引量:19

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