Chinese Journal of Mechanical Engineering

, Volume 27, Issue 6, pp 1178–1185 | Cite as

Fatigue life prediction under service load considering strengthening effect of loads below fatigue limit

Article

Abstract

Lightweight design requires an accurate life prediction for structures and components under service loading histories. However, predicted life with the existing methods seems too conservative in some cases, leading to a heavy structure. Because these methods are established on the basis that load cycles would only cause fatigue damage, ignore the strengthening effect of loads. Based on Palmgren-Miner Rule (PMR), this paper introduces a new method for fatigue life prediction under service loadings by taking into account the strengthening effect of loads below the fatigue limit. In this method, the service loadings are classified into three categories: damaging load, strengthening load and none-effect load, and the process for fatigue life prediction is divided into two stages: stage I and stage II, according to the best strengthening number of cycles. During stage I, fatigue damage is calculated considering both the strengthening and damaging effect of load cycles. While during stage II, only the damaging effect is considered. To validate this method, fatigue lives of automobile half shaft and torsion beam rear axle are calculated based on the new method and traditional methods, such as PMR and Modified Miner Rule (MMR), and fatigue tests of the two components are conducted under service loading histories. The tests results show that the percentage errors of the predicted life with the new method to mean life of tests for the two components are −3.78% and −1.76% separately, much lesser than that with PMR and MMR. By considering the strengthening effect of loads below the fatigue limit, the new method can significantly improve the accuracy for fatigue life prediction. Thus lightweight design can be fully realized in the design stage.

Keywords

fatigue life fatigue damage service loading strengthening effect load below the fatigue limit 

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Copyright information

© Chinese Mechanical Engineering Society and Springer-Verlag Berlin Heidelberg 2014

Authors and Affiliations

  1. 1.College of Mechanical EngineeringUniversity of Shanghai for Science and TechnologyShanghaiChina
  2. 2.College of Automobile EngineeringShanghai University of Engineering ScienceShanghaiChina
  3. 3.Machinery Industry Key Laboratory for Mechanical Strength & Reliability Evaluation of Auto Chassis ComponentsUniversity of Shanghai for Science and TechnologyShanghaiChina

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