南京航空航天大学学报2012，Vol.44Issue(z1)：52-55,4.
自动钻铆连接件疲劳性能分析
Fatigue Analysis of Components Produced by Automatic Drilling and Riveting
王宇波 1余路 2洪华舟 2蒋红宇 3陈福玉2
作者信息
- 1. 上海交通大学机械与动力工程学院,上海,200240
- 2. 上海飞机制造有限公司航空制造技术研究所,上海,200436
- 3. 南京航空航天大学机电学院,南京,210016
- 折叠
摘要
Abstract
Automatic drilling and riveting technique is an advanced joint technology commonly used in the aircraft assembly process. In view of the inadequacy of the technology accumulation in domestic, the riveting components produced by two automatic drilling and riveting equipments and manual drilling and riveting are fatigue tested respectively. The test results show that the fatigue lifes of the riveting components produced by automatic drilling and riveting are improved, compared with those produced by manual drilling and riveting when the process parameters are appropriate. The different squeezing forces and speeds influence the fatigue life of the structure, and the parameter control precision using automatic drilling and riveting is higher than that using manual drilling and riveting.关键词
自动钻铆/工艺规范/疲劳试验Key words
automatic drilling and riveting/ process standard/ fatigue test分类
航空航天引用本文复制引用
王宇波,余路,洪华舟,蒋红宇,陈福玉..自动钻铆连接件疲劳性能分析[J].南京航空航天大学学报,2012,44(z1):52-55,4.
