Effects of Cold Hole Expansion on Microstructure and Fatigue Property of 7A85 Aluminum Alloy Forging
摘 要
采用孔挤压方法对含孔的7A85铝合金锻件进行了强化, 对比分析了孔挤压前后试样的疲劳寿命; 通过扫描电镜、透射电镜以及X射线应力仪等研究了挤压前后试样的疲劳断口形貌、显微组织变化以及孔表层的残余应力场。结果表明: 采用5.3%的挤压过盈量可达到最佳强化效果, 其疲劳寿命是挤压强化前的11倍; 孔挤压强化后, 试样在强化层处产生位错缠结及残余压应力, 可有效延缓疲劳裂纹的扩展, 从而提高试样的疲劳寿命, 压应力层深度约为4.7 mm, 最大残余压应力出现在距孔边约1 mm处, 其值为-319 MPa。
Abstract
Hole expansion was employed to strengthen 7A85 aluminum alloy forging with holes. The fatigue lives of specimens before and after hole expansion were analyzed by comparison. The fatigue fracture, microstructure and residual stresses before and after hole expansion were studied by scanning electron microscopy, transmission electron microscopy and X-ray diffraction. The results show that the specimens with the shrink value of 5.3% obtained the best effect of strengthening, whose fatigue life was 11 times as long as that before hole expansion. The residual compressive stress and dislocation cell structure were found in the strengthened layer after hole expansion, which can retard the fatigue crack growth rate, and then prolongs the whole fatigue life of the specimen. The depth of strengthening layer was about 4.7 mm, and the maximum residual compressive stress of -319 MPa was observed where was 1 mm away from the border of holes.
中图分类号 TG146 DOI 10.11973/jxgccl20l506006
所属栏目 试验研究
基金项目
收稿日期 2014/10/8
修改稿日期 2014/10/27
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备注姬浩(1983—), 男, 陕西子洲人, 工程师, 硕士。
引用该论文: JI Hao,LIU Guo-guang. Effects of Cold Hole Expansion on Microstructure and Fatigue Property of 7A85 Aluminum Alloy Forging[J]. Materials for mechancial engineering, 2015, 39(6): 25~28
姬浩,刘国光. 孔挤压强化对7A85铝合金锻件组织和疲劳性能的影响[J]. 机械工程材料, 2015, 39(6): 25~28
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参考文献
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【3】张坤, 龚澎, 宋德玉, 等.孔挤压强化对超高强7055-T7751厚板组织性能的影响[J].航空材料学报, 2010, 30(5):44-47.
【4】龚澎, 郑林斌, 张坤, 等.7B50-T7451铝合金板材孔挤压工艺性能研究[J].航空材料学报, 2011, 31(4): 45-49.
【5】张洪双, 段晓飞.孔挤压强化和工艺参数研究[J].机械设计与制造, 2001, 12(11):111-113.
【6】章艳, 张兴权, 段仕伟, 等, 钻、铰工艺对铝合金紧固孔件疲劳寿命的影响[J].机械工程材料, 2014, 42(8):23-27.
【7】王强, 乔明杰, 张炜, 等. 喷丸对TC4钛合金残余压应力场及疲劳寿命的影响[J].机械工程材料, 2012, 36(12):53-57.
【8】DE MATOS P F P, MCEVILY A J.Material analysis of the effect of cold-working of rivet holes on the fatigue life of aluminum alloy[J].International Journal of Fatigue, 2007, 29(3):575-586.
【9】LIU J, SHAO X J.Effect of cold expansion on fatigue performance of open holes[J].Materials Science and Engineering, 2008, 477(5):271-276.
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