Predicting the effects of material properties gradient and residual stresses on the bending fatigue strength of induction hardened aeronautical gears
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文摘

Microstructure, hardness and residual stress effects on fatigue are studied.

The bending fatigue endurance limit of induction hardened gears is predicted.

Model predictions are compared to experimental single tooth bending fatigue tests.

The proposed model provides reasonable predictions of the bending endurance limit.

The crack initiation location is more challenging to predict with such model.

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