首页> 美国政府科技报告 >The Use of Pins with Flats to Increase the Fatigue Life of Aluminum Alloy Lugs

【24h】

The Use of Pins with Flats to Increase the Fatigue Life of Aluminum Alloy Lugs

机译：带平头销的使用增加铝合金凸耳的疲劳寿命

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

Pins with machined flats were used to improve the fatique life of aluminium alloy lugs. A worthwhile increase in life was obtained, the magnitude of which depended on the depth of flat. The choice of optimum pin geometry is discussed. (Author)

著录项

作者
Clarke, B. C.;
展开▼
作者单位

展开▼
年度 1966
页码 p.1-2
总页数 2
原文格式 PDF
正文语种 eng
中图分类
关键词
Aluminum alloys ; Metal joints ; Fatique(Mechanics) ; Great Britain ; Rods ; Machining ; Configuration ; Stresses;

机译：铝合金;金属接头; Fatique（力学）;英国;杆;加工;配置;应力;

相似文献

外文文献
中文文献
专利

1. Improving the fatigue life of 2297-T87 aluminum-lithium alloy lugs by cold expansion, interference fitting, and their combination [J] . Huang Yongjie, Li Haitao, Yang Xu, Journal of Materials Processing Technology . 2017,第期

机译：通过冷膨胀，干涉配件及其组合提高2297-T87铝 - 锂合金凸耳的疲劳寿命
2. Fatigue life scatter of aluminum alloy helicopter lugs [J] . N.S.Xi, M.L.Xie Engineering failure analysis . 2000,第4期

机译：铝合金直升机吊耳的疲劳寿命分布
3. Crack initiation and fatigue life prediction on aluminum lug joints using statistical volume element-based multiscale modeling [J] . Jinjun Zhang, Kuang Liu, Chuntao Luo, Journal of intelligent material systems and structures . 2013,第17期

机译：基于统计体积元的多尺度建模预测铝制凸耳的裂纹萌生和疲劳寿命
4. Study on Fatigue Crack Growth Model of 7075-T7410 Aluminum Alloy Straight Attachment Lug [C] . Liming Wu, Yuting He, Xinbo Wang, International Conference on Mechanical Materials and Manufacturing Engineering . 2011

机译：7075-T7410铝合金直立凸耳疲劳裂纹增长模型研究
5. Fatigue life variability due to variations in interference fit of steel bushings in 7075-T651 aluminum lugs. [D] . Brown, Michael A. 2012

机译：7075-T651铝制凸耳中钢衬套过盈配合的变化会导致疲劳寿命变化。
6. Fatigue Life of Aluminum Alloys Based on Shear and Hydrostatic Strain [O] . Tadeusz Łagoda, Karolina Głowacka, Andrzej Kurek 2020

机译：基于剪切和静水压菌株的铝合金疲劳寿命
7. Effects of chamfering, cold expansion, bolt clamping, and their combinations on fatigue life of aluminum–lithium alloy single plate [O] . Yongjie Huang, Zhidong Guan, Haitao Li, 2018

机译：倒角，冷膨胀，螺栓钳位及其组合对铝 - 锂合金单板疲劳寿命的影响
8. Effect of Cold-Working by Hole Expansion on Fatigue Life of 7075-T7351 and 7475-T761 Aluminum Lugs with and Without Initial Flaws under Maneuver Loading Spectrum [R] . Buch, A., Berkovits, A. 1985

机译：机动载荷谱下孔扩张冷加工对7075-T7351和7475-T761铝合金凸耳疲劳寿命的影响

The Use of Pins with Flats to Increase the Fatigue Life of Aluminum Alloy Lugs

摘要

著录项

相似文献

相关主题

期刊订阅