首页 | 本学科首页   官方微博 | 高级检索  
     检索      

激光冲击强化对加力燃烧室火焰探测器焊缝的影响
引用本文:田增,王亚洲,罗思海,李国杰.激光冲击强化对加力燃烧室火焰探测器焊缝的影响[J].航空发动机,2022,48(1):97-102.
作者姓名:田增  王亚洲  罗思海  李国杰
作者单位:空军工程大学航空工程学院,西安710038;西安天瑞达光电技术股份有限公司,西安710077;西安天瑞达光电技术股份有限公司,西安710077;空军工程大学航空工程学院,西安710038
基金项目:国家重点研发计划项目(2016YFB1102600)、国家自然科学基金(52005508)、国家重大科技专项(J2019-IV-0014-0082)资助
摘    要:为了研究激光冲击强化(LSP)后加力燃烧室火焰探测器焊缝位置异常开裂原因,采用X射线衍射方法和金相方法对激光冲击强化效果进行分析,并利用扫描电子显微镜对断口进行了观察。在Abaqus有限元分析软件中建立了与观察到的焊缝缺陷相似的有限元模型,对焊缝缺陷的LSP处理及冲击波传播过程进行了模拟分析。试验结果表明:具有较好材料完整性的区域经LSP处理后,表面会预置较大残余压应力,同时表面金属晶粒得到细化,疲劳裂纹会在焊缝缺陷位置萌生和扩展。有限元分析结果表明:存在分层缺陷的焊缝经LSP强化后,冲击波会在分层缺陷处产生反射,造成分层位置发生开裂,形成裂纹源造成疲劳开裂。根据试验和仿真分析结果,为提升火焰探测器焊缝激光冲击抗疲劳效果,建议优化焊接工艺,提高焊接质量。

关 键 词:复火焰探测器  激光冲击强化  疲劳开裂  有限元仿真  加力燃烧室  航空发动机

Impact of Laser Shock Peening on Welding Seam of Flame Detector in Afterburner
Authors:TIAN Zeng  WANG Ya-zhou  LUO Si-hai  LI Guo-jie
Institution:(School of Aeronautical Engineering,Air Force Engineering University,Xi’an 710038,China;Xi’an Tyrida Optical Electric Technology Co.,Ltd,Xi’an 710077,China)
Abstract:In order to study the causes of welding seam abnormal cracking of afterburner flame detector after laser shock peening(LSP),X-ray diffraction and metallographic methods were used to analyze the effect of laser shock peening,and the fracture was observed by scanning electron microscope.A finite element model similar to the observed weld seam defects was established in Abaqus finite element analysis software,and the LSP treatment and shock wave propagation process of weld seam defects were simulated and analyzed.The test results show that the area with good material integrity treated by LSP will be reserved with large residual compressive stress on the surface,and the surface metal grains will be refined,and the fatigue cracks initiation and propagation will occured at the weld seam defect location.The finite element analysis results also show that after the weld seam with delamination defect is strengthened by LSP,the shock wave will reflect at the delamination defect,resulting in cracking at the delamination position,forming crack source and fatigue cracking.According to the test and simulation analysis results,in order to improve the fatigue resistance of flame detector weld seam by laser shock,it is suggested to improve welding process and welding quality.
Keywords:flame detector  laser shock peening  fatigue cracking  finite element simulation  afterburner  aeroengine
本文献已被 维普 万方数据 等数据库收录!
点击此处可从《航空发动机》浏览原始摘要信息
点击此处可从《航空发动机》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号