Abstract

The established linear fatigue life prediction model based on the Miner rule has been widely applied to fatigue life prediction under constant amplitude uniaxial and multiaxial loading. Considering the physical significance of crack formation and propagation, a multiaxial equivalent linear fatigue life prediction model is put forward based on Miner rule and critical plane method under constant amplitude loading. The essence of this approach is that the equivalent strain, which consists of the shear strain and normal strain on the critical plane, replaces the relevant parameter of uniaxial nonlinear fatigue damage model. The principal axes of stress/strain rotate under non-proportional loading. Meanwhile, the microstructure of material and slip systems change, which lead to additional hardening effect. The ratio of cyclic yield stress to static yield stress is used to represent the cyclic hardening capacity of material, and the influence of phase difference and loading condition on the non-proportional hardening effect is considered. The multiaxial fatigue life is predicted using equivalent stain approach, maximum shear stain amplitude model, CXH model, and equivalent multiaxial liner model under proportional and/or non-proportional loading. The smooth and notched fatigue specimens of four kinds of materials (Q235B steel, titanium alloy TC4, Haynes 188, and Mod.9Cr-1Mo steel) are used in the multiaxial fatigue experiments to verify the proposed model. The predicted results of these materials are compared with the test results, and the results show that these four models can achieve good effect under proportional loading, but the proposed model performs better than the other three models under non-proportional loading. Meanwhile, it also verifies that the proposed enhancement factor can reflect the influence of phase difference and material properties on additional hardening.

Highlights

  • Most of the components in engineering work under alternating loading, and the loading form may be uniaxial or multiaxial

  • A multiaxial equivalent linear fatigue damage accumulation model by combining Miner rule with the critical plane method is proposed under constant amplitude loading in this article

  • In the multiaxial fatigue life prediction model, the equivalent strain method, the maximum shear strain amplitude model, and CXH model can better predict the fatigue life of most metal materials, and it is convenient for engineering application

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Summary

Introduction

Most of the components in engineering work under alternating loading, and the loading form may be uniaxial or multiaxial. A multiaxial equivalent linear fatigue damage accumulation model by combining Miner rule with the critical plane method is proposed under constant amplitude loading in this article. The normal stress amplitude on the critical surface is used as the fatigue damage parameter to reflect the effect of additional hardening on the fatigue life of multiaxial fatigue. Because there is no additional hardening effect under proportional loading, the predicted results of the maximum shear strain amplitude model and the multiaxial equivalent linear prediction model agree well with the experimental results

Analysis and discussion
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