| Autor: |
CAO ZengQiang, HU ZhaoYang, GAN XueDong, ZHAO Yong, WANG Jie, HAN ChaoZhong |
| Jazyk: |
čínština |
| Rok vydání: |
2016 |
| Předmět: |
|
| Zdroj: |
Jixie qiangdu, Vol 38, Pp 1093-1098 (2016) |
| Druh dokumentu: |
article |
| ISSN: |
1001-9669 |
| DOI: |
10.16579/j.issn.1001.9669.2016.05.033 |
| Popis: |
Strengthening problem of short-edge hole of titanium lug is an important task during a new aircraft development stage,Force Mate steel bushing process has been carried out to study the fatigue life of short-edge hole. Research the interference of 0. 5% 、1. 0% 、1. 5% 、2. 0% 、2. 5% how to effect the stress and strain around the hole with FEA,and comparisons with shortedge hole and normal hole are made as well. Then apply a cycle load on the lug to predict the fatigue life and provide a theoretical guidance for the optimum technology parameter. |
| Databáze: |
Directory of Open Access Journals |
| Externí odkaz: |
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