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TiB_2颗粒增强ZA-8锌合金的显微组织与疲劳裂纹扩展行为的关系 被引量:3

RELATIONSHIP BETWEEN MICROSTRUCTURE AND FATIGUE CRACK PROPAGATION BEHAVIOUR IN TiB_2 PARTICULATE REINFORCED ZA-8 Zn ALLOY
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摘要 研究了TiB2颗粒增强ZA-8锌合金复合材料和基体材料的疲劳裂纹扩展行为与显微组织、断口的关系。结果表明:所研究复合材料的抗疲劳裂纹扩展能力优于基体材料,尤其在小裂纹阶段.其原因为:增强粒子与裂纹尖端的相互作用降低了裂纹尖端的应力强度;增强粒子与基体良好的界面结合力;增强粒子的加入,导致了基体微观组织结构的变化和细化以及增强粒子的桥接(Bridging)作用。最后,探讨了在两种材料中不同的裂纹扩展机理。 The relationships between microstructure, fracture surface and propagation behaviour of fatigue crack in TiB2 particulate reinforced ZA-8 Zn alloy and in the corresponding constitute matrix materials were studied. The present results indicate that the resistance to fatigue crack growth of the employed composite is in general superior to that of constitute matrix materials, especially for the short crack behaviour. This is attributed to (1) the interaction between particle and crack tip decreased the stress intensity ahead of the crack tip,(2) owing to the excellent interface strength,(3) the addition of reinforcement caused the change of matrix microstructure and refined the structure and (4) the bridging function of reinforcement. Finally, the mechanism for the difference in fatigue crack growth behaviour of the two materials was discussed.
出处 《金属学报》 SCIE EI CAS CSCD 北大核心 1996年第3期254-260,共7页 Acta Metallurgica Sinica
关键词 锌合金 疲劳裂纹 扩展 显微组织 硼化钛 fatigue crack propagation, interface strength, microstructure
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参考文献3

  • 1王执锐,Mater Sci Eng,1993年,171卷,85页
  • 2Shang Jianku,Metal Matrix Composites Mechanisms and Properties,1991年
  • 3Chin C S,Int J Fatigue,1985年,7卷,2期,87页

同被引文献16

  • 1王坤茜,徐人平,林捷晖.考虑应力比的疲劳裂纹扩展概率模型[J].航空动力学报,2009,24(9):2012-2018. 被引量:11
  • 2赵荣国,罗希延,蒋永洲,李红超,李秀娟,刘学晖.航空发动机涡轮盘用GH4133B合金疲劳损伤与断口分析[J].机械工程学报,2011,47(6):92-100. 被引量:18
  • 3KUNZ L, LUKAS P, KONECNA R. Initiation and pro- pagation of fatigue cracks in cast IN 713LC superalloy[J]. Engineering Fracture Mechanics, 2010, 77(11) : 2008-2015.
  • 4MANN T. The influence of mean stress on fatigue crack propagation in aluminium alloys[J]. Internatinal Journal of Fatigue, 2007,29(8). 1393-1401.
  • 5HU D, WANG R. Experimental study of creep-fatigue interaction behavior of GH4133B superalloy[J]. Materials Scienee and Engineering A, 2009, 515(1-2): 183 - 189.
  • 6ULLOCH J H. Near threshold fatigue crack propagation behaviour of CrMoV turbine steel[J]. Theoretical and Applied Fracture Mechanics, 1995, 23(1): 89-101.
  • 7LAWSON L, CHEN E Y, MESHII M. Near-threshold fatigue: A review[J]. International Journal of Fatigue, 1999, 21(Suppl. 1). 15-34.
  • 8KUJAWSKI D. A fatigue crack driving fore parameter with load ratio effect[J]. International Journal of Fatigue, 2001, 23(Suppl. 1): 239-246.
  • 9吴崇周,李兴无,黄旭,马济民,曹春晓.TA15钛合金疲劳裂纹扩展与显微组织的关系[J].稀有金属材料与工程,2007,36(12):2128-2131. 被引量:14
  • 10王一飞,王燕舞,吴晓源,崔维成,黄小平.有效应力强度因子范围门槛值与载荷比关系的研究(英文)[J].船舶力学,2008,12(3):440-453. 被引量:7

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