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Variability in Fatigue Life of Near-α Titanium Alloy IMI 834
Most aero-engine components and structures are subjected to life critical fatigue loads during service. Near- α titanium alloy IMI 834 is one candidate aero-engine material that is used as high-pressure compressor discs due to its superior fatigue strength and creep resistance. The effect of heat tr...
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Published in: | Transactions of the Indian Institute of Metals 2021-04, Vol.74 (4), p.979-989 |
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Main Authors: | , , , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
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Summary: | Most aero-engine components and structures are subjected to life critical fatigue loads during service. Near-
α
titanium alloy IMI 834 is one candidate aero-engine material that is used as high-pressure compressor discs due to its superior fatigue strength and creep resistance. The effect of heat treatment on the microstructure and high-cycle fatigue behaviour of the material has been studied and reported here. The alloy was solution-heat-treated at 1060 °C and subsequently quenched in different media. A strong effect of quench media (cooling rate) on high-cycle fatigue life has been observed. Fractographic investigations were performed to correlate the fracture micro-mechanism with heat treatment. Further, a generalized stress-life model has been deduced from the fatigue data and integrated with finite element analysis to develop a fatigue model for the alloy. |
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ISSN: | 0972-2815 0975-1645 |
DOI: | 10.1007/s12666-021-02210-z |