MATEC Web of Conferences
Volume 12, 2014FDMD II - JIP 2014 - Fatigue Design & Material Defects
|Number of page(s)||3|
|Section||Session 10.1: Very High Cycle Fatigue|
|Published online||09 June 2014|
Influence of defects on the very high cycle fatigue behaviour of forged aeronautic titanium alloy
1 LEME, U. Paris Ouest Nanterre La Defense, 50 rue de Sèvres, 92410 Ville-d'Avray, France
2 Arts et Métiers ParisTech, I2M, CNRS, Université Bordeaux 1, Esplanade des Arts et Métiers, 33405 Talence, France
3 SCCAFS, Air. Sheremetevo-1, PO Box 54, Moscow reg., Chimkinskiy State 141426, Russia
a Corresponding author: e-mail: firstname.lastname@example.org
This paper is focused on fatigue failure of forged aeronautic titanium alloy Ti-6Al-4Mo under VHCF loading. Continuous fatigue tests were carried out in gigacycle fatigue regime (up to on 1010 cycles) on specimens machined from real aircraft compressor disk produced by forging. It has been shown, that crack initiation site shifts from surface to subsurface location with stress amplitude decreasing and fatigue life increasing. Microstructural inhomogeneities so that “hard” alpha particles, borders of large alpha lamella clusters and TiN particles are the cause of fatigue crack nucleation in forged Ti-6Al-4Mo titanium alloy under VHCF loading.
© Owned by the authors, published by EDP Sciences, 2014
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.
Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.
Initial download of the metrics may take a while.