A1 Refereed original research article in a scientific journal

Fatigue behavior of low-temperature hot isostatic pressed electron beam powder bed fusion manufactured Ti-6Al-4 V




AuthorsPandian K, Neikter M, Bahbou F, Ganvir A, Hansson T, Pederson R

PublisherElsevier Science

Publication year2023

JournalJournal of Alloys and Compounds

Journal name in sourceJOURNAL OF ALLOYS AND COMPOUNDS

Journal acronymJ ALLOY COMPD

Article number 171086

Volume962

Number of pages10

ISSN0925-8388

eISSN1873-4669

DOIhttps://doi.org/10.1016/j.jallcom.2023.171086

Web address https://doi.org/10.1016/j.jallcom.2023.171086

Self-archived copy’s web addresshttps://research.utu.fi/converis/portal/detail/Publication/180540575


Abstract
Ti-6Al-4 V finds application in the fan and compressor modules of gas turbine engines due to its high specific strength. Ti-6Al-4 V components manufactured using one of the additive manufacturing (AM) techniques, the electron beam powder bed fusion (PBF-EB) process, has been an active area of research in the past decade. The fatigue life of such PBF-EB built Ti-6Al-4 V components is improved by hot isostatic pressing (HIP) treatment typically performed at about 920 C. The HIP treatment at 920 C results in coarsening of & alpha; laths and reduced static strength and therefore a low-temperature HIP treatment is performed at about 800 C to limit the impact on static mechanical properties. In the present work, the low cycle fatigue and fatigue crack growth behavior of such a modified HIP (low-temperature HIP) treated material is assessed and compared with the respective data for the standard HIP-treated material. The modified HIP-treated material has fatigue performance comparable to the standard HIP-treated material. This work suggests that the modified HIP treatment improves the static mechanical properties without significantly impacting the fatigue performance. Also, fatigue life predictions were made from the measured defect size at the crack initiation site using a linear elastic fracture mechanics tool. The life predictions show good agreement with the experimental values for defects greater than the intrinsic crack length, where life is well predicted by large-crack growth methodology.

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Last updated on 2024-26-11 at 14:45