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Fatigue Behaviour of Ti-6Al-4V Alloy in Vacuum and at Low Temperature

Journal Advanced Materials Research (Volumes 41 - 42)
Volume Structural Integrity and Failure
Edited by Xiaozhi Hu, Brent Fillery, Tarek Qasim and Kai Duan
Pages 83-90
DOI 10.4028/www.scientific.net/AMR.41-42.83
Online since April, 2008
Authors J.H. Zuo, Z.G. Wang, En Hou Han
Keywords Coupling Function, Fatigue Behaviour, Low Temperature, Ti6Al4V Alloy, Vacuum
Abstract Investigations have been conducted on the fatigue behavior of Ti-6Al-4V alloy with the bimodal microstructure in air at room temperature, in vacuum at room temperature and in vacuum at low temperature (100K), respectively. The results show that the fatigue life of this alloy is longer in vacuum and/or at low temperature than that in air at room temperature. The combination of vacuum and low temperature can much improve the fatigue properties of this alloy because of their purifying effect on fatigue cracks propagation. SEM observation of fatigue fracture surface indicates that all the fatigue cracks initiate in the sample surface when Nf ≦106 cycles. The above three testing conditions lead to different modes of fatigue crack propagation and therefore much different morphology of fatigue fracture.
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