The effect of duration aging temperature on fatigue strength of aluminum alloy strength of aluminum alloy
International Conference on Applications and Design in Mechanical Engineering 2012 (ICADME 2012) organized by School of Mechatronic Engineering, Universiti Malaysia Perlis (UniMAP), 27th - 28th Februari 2012 at Bayview Beach Resort, Penang, Malaysia.
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Universiti Malaysia Perlis (UniMAP)
2012
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my.unimap-194922012-05-31T13:27:54Z The effect of duration aging temperature on fatigue strength of aluminum alloy strength of aluminum alloy Ahmad Syayuthi, Abdul Rahman Haftirman Teo, Ee Lynn syayuthi@unimap.edu.my Aluminum alloy 6063 Fatigue strength Ageing heat treatment Scanning electron microscope (SEM) International Conference on Applications and Design in Mechanical Engineering 2012 (ICADME 2012) organized by School of Mechatronic Engineering, Universiti Malaysia Perlis (UniMAP), 27th - 28th Februari 2012 at Bayview Beach Resort, Penang, Malaysia. This paper present the effect of different duration aging temperature on fatigue strength of Al6063. Al 6063 alloy specimens have been solution heat treated at 520C for 2 hours. Subsequently, the artificial ageing heat treatment was carried put at 200C ageing temperature at 4, 8 and 12 hours respectively. Besides that, there are specimens that not been to heat treatment process. The hardness test was carried out where it shows that specimen at 8 hour ageing temperature have the highest hardness test result compared with other different ageing time. After that, the fatigue test was carried out. From the fatigue test, graph stress versus number of cycles was plotted. The result of S-N graph, it was found out that 8 hour ageing temperature showed the highest fatigue failure. Fractography studies via scanning electron microscopy (SEM) revealed that there is a clearly striation and crack growth appeared on the microstructure of the specimen failure. 2012-05-31T09:28:53Z 2012-05-31T09:28:53Z 2012-02-27 Working Paper http://hdl.handle.net/123456789/19492 en Proceedings of the International Conference on Applications and Design in Mechanical Engineering 2012 (ICADME 2012) Universiti Malaysia Perlis (UniMAP) Pusat Pengajian Kejuruteraan Mekatronik |
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| language |
English |
| topic |
Aluminum alloy 6063 Fatigue strength Ageing heat treatment Scanning electron microscope (SEM) |
| spellingShingle |
Aluminum alloy 6063 Fatigue strength Ageing heat treatment Scanning electron microscope (SEM) Ahmad Syayuthi, Abdul Rahman Haftirman Teo, Ee Lynn The effect of duration aging temperature on fatigue strength of aluminum alloy strength of aluminum alloy |
| description |
International Conference on Applications and Design in Mechanical Engineering 2012 (ICADME 2012) organized by School of Mechatronic Engineering, Universiti Malaysia Perlis (UniMAP), 27th - 28th Februari 2012 at Bayview Beach Resort, Penang, Malaysia. |
| author2 |
syayuthi@unimap.edu.my |
| author_facet |
syayuthi@unimap.edu.my Ahmad Syayuthi, Abdul Rahman Haftirman Teo, Ee Lynn |
| format |
Working Paper |
| author |
Ahmad Syayuthi, Abdul Rahman Haftirman Teo, Ee Lynn |
| author_sort |
Ahmad Syayuthi, Abdul Rahman |
| title |
The effect of duration aging temperature on fatigue strength of aluminum alloy strength of aluminum alloy |
| title_short |
The effect of duration aging temperature on fatigue strength of aluminum alloy strength of aluminum alloy |
| title_full |
The effect of duration aging temperature on fatigue strength of aluminum alloy strength of aluminum alloy |
| title_fullStr |
The effect of duration aging temperature on fatigue strength of aluminum alloy strength of aluminum alloy |
| title_full_unstemmed |
The effect of duration aging temperature on fatigue strength of aluminum alloy strength of aluminum alloy |
| title_sort |
effect of duration aging temperature on fatigue strength of aluminum alloy strength of aluminum alloy |
| publisher |
Universiti Malaysia Perlis (UniMAP) |
| publishDate |
2012 |
| url |
http://dspace.unimap.edu.my/xmlui/handle/123456789/19492 |
| _version_ |
1643792813045841920 |
| score |
13.222552 |