Abstract

Many studies on cracked rotors developed crack breathing models that assume that the neutral axis of bending always remains horizontal for simplification. These models may generate significant discrepancies and thus there is a need to develop more sophisticated models to look into the shifting of the neutral axis for a cracked rotor. Herein, a case study on the shifting of the neutral axis for a cracked rotor is firstly performed by using a three-dimensional finite element model to confirm that the neutral axis becomes inclined as the cracked rotor rotates. In response to this finding, non-symmetric bending principles are used to develop a new crack breathing model which has the advantage of being able to numerically calculate the inclination angle of the neutral axis. When compared to an existing crack model in the literature that assumes that the neutral axis remains horizontal (HNA model), the proposed model is relatively less stiff in bending as a result of an overall lower area moment of inertia. Using the harmonic balance method, a two-dimensional finite element vibration model of a cracked rotor was devised by employing the proposed crack breathing model and the HNA model for validation. It can be found that the vibration amplitudes of the first three frequency components are similar between the two models for shallow cracks and significantly differed for deep cracks. This result highlights the potential of the proposed model for modelling and detecting mid-to-late-stage cracks in rotors.

Highlights

  • Fatigue crack propagation in a rotor shaft is an imperceptible phenomenon that occurs over tens of thousands to millions of bending cycles

  • There exists a difficulty in holistically describing the crack breathing mechanism due to its non-linear nature and so a number of studies relied on models which describe simplified behaviour [3]

  • This preliminary investigation showed that the neutral axis inclination angle increases from horizontal as the crack rotates depending on the openness of the crack

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Summary

Introduction

Fatigue crack propagation in a rotor shaft is an imperceptible phenomenon that occurs over tens of thousands to millions of bending cycles. The change in stiffness of a rotating shaft due to a transverse fatigue crack can be modelled by considering the periodic change in the area moment of inertia of the cross-section immediate to the crack location [18]. The aim was to develop a new crack breathing model which can consider the shifting of the neutral axis for cracked rotors. Model where the neutral axis is assumed to remain horizontal

Case Study of Cracked Rotor Using a Three-Dimensional Finite Element Model
Neutral
Development
U The stiffness
Conclusions
Findings
Partially
Full Text
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