Journal
CRYOGENICS
Volume 43, Issue 8, Pages 483-489Publisher
ELSEVIER SCI LTD
DOI: 10.1016/S0011-2275(03)00125-5
Keywords
alpha-type titanium alloy; high-cycle fatigue property; cryogenic temperature; grain sized sub-surface crack initiation
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High-cycle fatigue properties were investigated at 4, 77 and 293 K in Ti-5%Al-2.5%Sn ELI alloy which was used for liquid hydrogen turbo-pumps of Japanese-built launch vehicles. Mean grain size of specimens was controlled to be about 30 or 80 pm. In the specimens with a grain size of 30 pm, fatigue strengths at 10(6) cycles at 4 and 77 K are 1.6 and 1.5 times higher than that at 293 K, respectively. On the other hand, in the specimen with a grain size of 80 mum, fatigue strengths at 10(6) cycles at 4 and 77 K get lower to the same level as that at 293 K. Thus, it is concluded that refinement of of. grains is one of important factors to obtain the good high-cycle Fatigue properties for Ti-5%Al-2.5%Sn ELI alloy at cryogenic temperature. (C) 2003 Elsevier Ltd. All rights reserved.
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