摘要
通过试验,研究了干涉配合铆接试件相对于普通铆接试件疲劳强度的增益,估算了冠状铆钉干涉配合的填充作用。研究结果表明:在中寿命区,干涉配合铆接的疲劳强度比普通铆接的疲劳强度提高约25%。通过理论计算与试验结果的对比,建议冠状铆钉干涉配合的填充系数可取为0.474。
In this paper,the gain of fatigue strength of interference-fit riveting components compared with conventional riveting components is studied through tests, and the interference-fit filling effect of coronary rivet is estimated. Results show that in the middle life range the fatigue strength of interference-fit riveting increases by about 25% compared with that of conventional riveting. Based on the comparison between theoretical calculation and test results, this paper suggests that the filling coefficient of coronary rivet should be at 0.474.
出处
《中国民航学院学报》
2006年第4期9-10,15,共3页
Journal of Civil Aviation University of China
基金
中国民用航空总局科技基金项目(20030802)
关键词
铆接件
疲劳寿命
干涉铆接
填充系数
riveting components
fatigue life
intervening concerted riveting
filling coefficient
