This page presents the S-N curves and fatigue limit of MS1 steel samples produced in the part of the production chamber near the inlet of the inert gas flow, then post-processed by heat treatment, machining that removed allowance of 0.5mm and shot-peening (in that order). The fatigue data were obtained using the bending tests of rotating bar with AM layers normal to the axis of rotation.
Build orientation of longitudinal axis | vertical |
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Position with respect to inert gas flow | inlet |
Post-processing | heat treatment → machining allowance 0.5mm → shot-peening |
Fatigue limit (MPa) | 511 |
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Number of cycles to failure N | N=1,71⋅1036⋅S-10,87 |
Stress amplitude S (MPa) | S=2155⋅N-0,092 |
Explanation of the terms are given at the page Fatigue strength description.
This page is a part of the section DMLS/SLM: Fatigue design rules.