首页 | 本学科首页   官方微博 | 高级检索  
     

DZ125定向凝固合金的喷丸工艺
引用本文:王欣,杨清,于鹏,马世成. DZ125定向凝固合金的喷丸工艺[J]. 金属热处理, 2021, 46(1): 149-153. DOI: 10.13251/j.issn.0254-6051.2021.01.028
作者姓名:王欣  杨清  于鹏  马世成
作者单位:1.中国航发北京航空材料研究院 表面工程研究所,北京 100095; 2.中国航发北京航空材料研究院 航空材料先进腐蚀与防护重点实验室,北京 100095; 3.中国航发沈阳黎明航空发动机有限公司 盘轴加工分厂,辽宁 沈阳 110043
摘    要:针对DZ125合金开展铸钢丸喷丸强化研究,分析了多种喷丸强度、覆盖率条件下合金700℃旋弯疲劳性能、表面残余应力和硬度梯度.结果表明:随喷丸强度的增大,中值疲劳寿命估计量逐渐增大,高喷丸强度时,700℃/500 MPa中值疲劳寿命估计量是原始试样的2倍;随表面覆盖率的增大,中值疲劳寿命估计量呈现先增大后稳定的趋势,当覆...

关 键 词:DZ125合金  喷丸强度  表面覆盖率  疲劳  应力松弛
收稿时间:2020-11-05

Shot peening process of directionally solidified DZ125 alloy
Wang Xin,Yang Qing,Yu Peng,Ma Shicheng. Shot peening process of directionally solidified DZ125 alloy[J]. Heat Treatment of Metals, 2021, 46(1): 149-153. DOI: 10.13251/j.issn.0254-6051.2021.01.028
Authors:Wang Xin  Yang Qing  Yu Peng  Ma Shicheng
Affiliation:1. Surface Engineering Institution,AECC Beijing Institute of Aeronautical Materials,Beijing 100095,China; 2. Aviation Key Laboratory of Advanced Corrosion and Protection on Aviation Materials,AECC Beijing Institute of Aeronautical Materials,Beijing 100095,China; 3. Disk and Shaft Machining Branch,AECC Shenyang Liming Aero-engine Co.,Ltd.,Shenyang Liaoning 110043,China
Abstract:Cast-steel shot peening was employed on directionally solidified alloy DZ125 to analyze the fatigue property,surface residual stress and microhardness profile under various shot peening intensity and coverage conditions.The results show that with the increase of shot peening intensity,the estimated median fatigue life increases gradually.At high intensity,the estimated median fatigue life at 700℃/500 MPa is2 times that of the original specimen.Moreover,with the increase of surface coverage,the estimated median fatigue life increases first and then stabilizes,and when the coverage reaches 400%,the estimated median fatigue life is stable.When the shot peening intensity is high and at the coverage rate of 400%,the fatigue limit is 480 MPa,which is 20% higher than the original value(400 MPa).Residual stress and microstructure strengthening mechanism are the strengthening factors of shot peening for DZ125 alloy.With the increase of shot peening intensity,the residual compressive stress decreases slightly,but it is still obviously larger than the original state.When the shot peening intensity is high and at the coverage rate of 400%,the surface hardness field of DZ125 alloy exceeds 200μm in depth,and the surface hardness is 37% higher than that of the matrix(430 HV0.1).When the actual load at the notch is greater than the yield strength,the residual stress and hardness are relaxed obviously during fatigue process;the surface residual stress of the fractured specimen decreases by 54% and the surface hardness decreases by 14% after 700℃/600 MPa/1.5×105 cycles.
Keywords:DZ125 alloy  shot peening intensity  surface coverage  fatigue  stress relaxation
本文献已被 CNKI 维普 万方数据 等数据库收录!
点击此处可从《金属热处理》浏览原始摘要信息
点击此处可从《金属热处理》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