Issue |
J. Phys. IV France
Volume 134, August 2006
EURODYMAT 2006 - 8th International Conference on Mechanical and Physical Behaviour of Materials under Dynamic Loading
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Page(s) | 269 - 274 | |
DOI | https://doi.org/10.1051/jp4:2006134041 | |
Published online | 26 July 2006 |
J. Cirne, R. Dormeval, et al.
J. Phys. IV France 134 (2006) 269-274
DOI: 10.1051/jp4:2006134041
High strain rate and high temperature behaviour of metallic materials for jet engine turbine containment
F. Gálvez, D. Cendón, A. Enfedaque and V. Sánchez-GálvezDepartment of Materials Science, Polytechnic University of Madrid, c/ Profesor Aranguren s/n, 28040 Madrid, Spain
Published online: 26 July 2006
Abstract
This work presents a study on the mechanical
characterisation of the materials involved in air jet engine turbines. The
final objective is to analyse the phenomenon of a turbine blade off failure,
to verify the requirements of the case containment. The materials in the
turbine are under high temperatures, ranging from 400C to 800
C
and when the fail of the blade occurs if impacts against the case, reaching
strain rates up to 103 s - 1. To obtain the behaviour of the
materials, testing at high strain rate and high temperature at one time is
necessary. The experimental set-up used was a split Hopkinson pressure bar,
with a high temperature furnace adapted. The bars used on the device were
high strength nickel alloys with a cooling system to decrease the
temperature of the measurement devices. The effect of wave dispersion due to
the temperature gradient has been also studied to correct the measurements
if necessary. The material tested has been the FV535 stainless steel used on
the case. The full stress-strain curves at different temperatures and at
strain rates up to 103 s-1 have been obtained. The experimental
results show a marked influence of the strain rate and the temperature that
cannot be neglected. The Johnson-Cook material model has been used to fit
the results of the material tests.
© EDP Sciences 2006