摘要
对开缝衬套冷挤压孔和芯棒直接冷挤压孔的工艺方法进行了比较 ,并对开缝衬套冷挤压孔工艺参数、孔挤压后铰削量与疲劳寿命的关系以及孔挤压后残余压应力释放进行了研究。
The difference between the cold worked hole with and without split _sleeve is compared . The process parameters of the cold worked with splitsleeve, the relationship of the amount of material removed by reaming and the fatigue life as well as the release of compressive residual stress after coldworking are studied.
出处
《航空制造技术》
2000年第4期46-49,共4页
Aeronautical Manufacturing Technology
关键词
开缝衬套
冷挤压孔
残余压应力
疲劳寿命
Split_sleeve Coldworking Compressive residual stress Fatigue life