A previously published model that separates surface from subsurface survival is adapted for high temperature bearing steels and it is applied in life calculations for aircraft gas turbine mainshaft rolling bearings. This approach shows more realistic calculated life than current practices with the use of the
method. Besides this, the proposed approach incorporates the effects of high temperature in the reduction of the fatigue limit, which is reflected in the life calculations, this can discriminate among steels working at high temperatures. As shown previously, with the separation of surface from subsurface, the effects from fatigue are quantified in the two separated zones and they can be compared, showing the zone of higher fatigue risk. Therefore, the proposed approach shows advantages in comparison with the current life calculation method used in the aircraft industry.
method. Besides this, the proposed approach incorporates the effects of high temperature in the reduction of the fatigue limit, which is reflected in the life calculations, this can discriminate among steels working at high temperatures. As shown previously, with the separation of surface from subsurface, the effects from fatigue are quantified in the two separated zones and they can be compared, showing the zone of higher fatigue risk. Therefore, the proposed approach shows advantages in comparison with the current life calculation method used in the aircraft industry.
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