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孔挤压强化技术研究进展

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概述了直接、间接和复合孔挤压强化的研究现状,从残余应力与微观组织的角度总结了孔挤压强化的抗疲劳强化机理,基于孔结构的疲劳寿命和断口形貌详细分析了孔挤压强化的疲劳性能.研究结果表明,孔挤压强化的孔结构孔壁形成残余压应力,孔结构受到外加交变载荷时孔壁残余压应力能够抵消部分外加交变载荷产生的拉应力,降低了受载孔结构孔壁的应力峰值和平均应力;孔挤压强化的孔结构孔壁发生剧烈的塑性变形,孔壁微观组织发生细化,形成位错胞状结构,能够抑制晶粒的位错滑移,延缓了疲劳裂纹萌生,增大了疲劳裂纹萌生的门槛值,降低了疲劳裂纹扩展速率;在残余应力和微观组织的共同作用下,提高了孔挤压强化孔结构的疲劳寿命.最后,展望了孔挤压强化的发展趋势和研究问题.
Research progress of hole expansion strengthening technology
The research status of direct,indirect and composite hole expansion strengthening was summarized,the anti-fatigue strengthe-ning mechanism of hole expansion strengthening was summarized from the perspective of residual stress and microstructure.Based on the fatigue life and fracture morphologies of the hole structure,the fatigue performance of hole expansion strengthening was analyzed in detail.The research results show that residual compressive stress is in the hole wall of the hole expansion strengthening structure,and when the hole structure is subjected to external alternating load,the residual compressive stress on the hole wall can offset the tensile stress genera-ted by partial external alternating load,reducing the peak and average stresses on the hole wall of the loaded hole structure.In the hole expansion strengthening structure,severe plastic deformation occurs on the hole wall,and the microstructure of the hole wall is refined to form the dislocation cellular structure,which can inhibit the dislocation slip of the grains,delay the fatigue crack initiation,increase the threshold value for fatigue crack initiation,and retard the fatigue crack propagation rate.Under the combined action of residual stress and microstructure,the fatigue life of the hole structure with hole expansion strengthening is improved.Finally,the development trend and re-search issues of hole extrusion strengthening were prospected.

hole expansion strengtheningresidual stressmicrostructurefatigue life

刘飞、苏宏华、徐九华、梁勇楠、葛恩德、凡志磊

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南京航空航天大学机电学院,江苏南京 210016

中国商飞上海飞机制造有限公司,上海 200436

孔挤压强化 残余应力 微观组织 疲劳寿命

国家自然科学基金创新研究群体项目江苏省科研与实践创新计划国家商用飞机制造工程技术研究中心创新基金

51921003KYCX21_0196COMAC-SFGS-607

2024

塑性工程学报
中国机械工程学会

塑性工程学报

CSTPCD北大核心
影响因子:0.46
ISSN:1007-2012
年,卷(期):2024.31(3)
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