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含Sc航空7075合金的疲劳裂纹萌生及扩展行为

Fatigue crack initiation and propagation behavior of 7075 alloy containing Sc used for aviation

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【作者】 李向新陈律邓岚陈儒军

【Author】 Li Xiangxin;Chen Lü;Deng Lan;Chen Rujun;Department of Aviation Equipment Maintenance,Changsha Aeronautical Vocational and Technical College;School of Mechanical Engineering,Xiangtan University;

【机构】 长沙航空职业技术学院航空装备维修学院湘潭大学机械工程学院

【摘要】 对不同含量Sc微合金化的7075合金进行了疲劳裂纹萌生、疲劳裂纹扩展的对比研究,并对其作用机理进行了分析。结果表明,随着Sc含量的增加,合金的疲劳萌生寿命和强度比都呈现先增加而后降低趋势,在Sc含量为0.24wt%时,疲劳萌生寿命和强度比最大;当应力比为0.1时,在Sc含量为0.24wt%时合金具有最大的疲劳裂纹扩展阻力,而当应力比为0.5时,在Sc含量为0.48wt%时合金具有最大的疲劳裂纹扩展阻力,这可能与细小的晶粒尺寸和较多的第二相阻碍裂纹扩展有关。总而言之,在7075合金中加入0.24wt%Sc具有最佳的疲劳性能和断裂韧性。

【Abstract】 The fatigue crack initiation and propagation behavior of microalloyed 7075 alloys with different content of Sc were investigated,and its mechanism was also analyzed.The results show that with the increase of Sc content,the fatigue life and strength ratio of the alloy increase first and then decrease.The alloy gains the maximum fatigue life and the strength ratio of the alloy with 0.24wt%Sc content.When the stress ratio is 0.1,the alloy gets the maximum fatigue crack growth resistance with 0.24wt%Sc content,while the stress ratio is 0.5,the alloy gets the maximum fatigue crack growth resistance with the Sc content of 0.48wt%,which may be related to the fine grain size and more second phases block the crack propagation.In general,the 7075 alloy with 0.24wt%Sc has the best fatigue properties and fracture toughness.

【关键词】 7075合金微合金化疲劳裂纹萌生扩展
【Key words】 7075 alloymicroalloyingfatigue crackinitiationpropagation
  • 【文献出处】 金属热处理 ,Heat Treatment of Metals , 编辑部邮箱 ,2015年12期
  • 【分类号】TG146.21
  • 【被引频次】11
  • 【下载频次】205
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