在低温真空拉-压疲劳试验机上对峰时效态2A12合金的疲劳行为进行了研究,并采用扫描电镜(SEM)分析了真空对疲劳断口形貌的影响.结果表明,真空使疲劳寿命提高,疲劳曲线右移.在低循环应力时,真空环境中的疲劳断裂次数可比室温大气环境中的多2至3倍.真空和室温大气环境下的疲劳断口均为穿晶断口.在室温大气疲劳断口上可观察到轮胎花样与疲劳条纹.在低循环应力时出现疲劳条纹的区域增多.真空环境下极少出现轮胎花样与疲劳条纹.对真空影响峰时效态2A12合金疲劳行为的原因进行了讨论.
参考文献
[1] | D C Slivik;C P Blankenship;JR E A Starke .Intrinsic Fatigue Crack Growth Rates for Al-Li-Cu-Mg Alloys in Vacuum[J].Metallurgical and Materials Transactions,1993,22(03):1807-1817. |
[2] | Kichiro Endo;Kenjiro Komai .Fatigue Crack Propagalion in an Aluminum Alloy in Ultra-High Vacuum[J].Journal of the Materials Science Society of Japan,1977,26:143-148. |
[3] | D Khireddine;M H Khireddine .Low Cycle Fatigue Behavior of an Aluminium Alloy with Small Shearable Precipitates[J].Effect of Surface Coating,2000,22:585-591. |
[4] | B I Verkin;N M Grinberg .The Effect of Vacuum on the Fatigue Behavior of Metals and Alloys[J].Materials Science and Engineering,1979,41:149-181. |
[5] | R WANG;H MUGHRABI .Fatigue of Copper Single Crystals in Vacuum and in Air[J].Materials Science and Engineering,1984,65:219-243. |
[6] | N M Gringerg.The Effect of Vacuum on Fatigue Crack Growth[J].International Journal of Fatigue,1982(04):83-95. |
[7] | S Suresh.材料的疲劳[M].北京:国防工业出版社,1999:237-258. |
[8] | A Vinogadov;S Hashimoto;S Miura .Fatigue Crack lnitiation and Propagation in[210] Oriented Copper Single Crystals in Vacuum and in Air[J].Scripta Materialia,1996,34:775-779. |
上一张
下一张
上一张
下一张
计量
- 下载量()
- 访问量()
文章评分
- 您的评分:
-
10%
-
20%
-
30%
-
40%
-
50%