Bifurcation studies of a bolted-joint rotor system subjected to fixed-point rubbing fault

Rotor–stator rub is a common and high-risk fault in large rotating machines. As for the aero-engine rotor system, bolted joints are widely adopted to fasten the multiple rotating parts into an integrated one. During a rubbing event, normal and tangential forces are generated by the contact and frict...

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Published inNonlinear dynamics Vol. 110; no. 4; pp. 3045 - 3073
Main Authors Li, Yuqi, Wen, Chuanmei, Luo, Zhong, Jin, Long
Format Journal Article
LanguageEnglish
Published Dordrecht Springer Netherlands 01.12.2022
Springer Nature B.V
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ISSN0924-090X
1573-269X
DOI10.1007/s11071-022-07769-w

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Abstract Rotor–stator rub is a common and high-risk fault in large rotating machines. As for the aero-engine rotor system, bolted joints are widely adopted to fasten the multiple rotating parts into an integrated one. During a rubbing event, normal and tangential forces are generated by the contact and friction at the rotor–stator contacting interface. The mechanical properties of the bolted joint change dramatically under the generated forces, which will affect the dynamics of the rotor system. However, little research has been done on the dynamic properties of the bolted joint rotor system subject to rub-impact, and the coupling effect of rubbing and bolted joint on rotor dynamics is still not understood. Thus, the dynamic model of bolted joint rotor system with fixed-point rub-impact is established based upon the proposed bolted joint element and lumped mass modeling method in this work. Then, the vibration responses of the rotor system are captured by using the Newmark- β method. Bifurcation diagrams, three-dimensional spectral plots, Poincaré maps, time-domain waveforms as well as bending stiffness plots are used to demonstrate the effect of rotor–stator rub impact on the vibration characteristics of the rotor system. After that, the influences of the radial stiffness of the stator on the mechanical properties of the bolted joint and rotor dynamics are also examined. Finally, the experimental study is carried out through a bolted joint rotor test rig with a rubbing device. The studies in the present work helped in understanding the dynamic characteristics of the bolted joint rotor system and the mechanical properties of bolted joint undergoing rub-impact force. Moreover, those study results provide insight into the diagnosis of rubbing fault.
AbstractList Rotor–stator rub is a common and high-risk fault in large rotating machines. As for the aero-engine rotor system, bolted joints are widely adopted to fasten the multiple rotating parts into an integrated one. During a rubbing event, normal and tangential forces are generated by the contact and friction at the rotor–stator contacting interface. The mechanical properties of the bolted joint change dramatically under the generated forces, which will affect the dynamics of the rotor system. However, little research has been done on the dynamic properties of the bolted joint rotor system subject to rub-impact, and the coupling effect of rubbing and bolted joint on rotor dynamics is still not understood. Thus, the dynamic model of bolted joint rotor system with fixed-point rub-impact is established based upon the proposed bolted joint element and lumped mass modeling method in this work. Then, the vibration responses of the rotor system are captured by using the Newmark-β method. Bifurcation diagrams, three-dimensional spectral plots, Poincaré maps, time-domain waveforms as well as bending stiffness plots are used to demonstrate the effect of rotor–stator rub impact on the vibration characteristics of the rotor system. After that, the influences of the radial stiffness of the stator on the mechanical properties of the bolted joint and rotor dynamics are also examined. Finally, the experimental study is carried out through a bolted joint rotor test rig with a rubbing device. The studies in the present work helped in understanding the dynamic characteristics of the bolted joint rotor system and the mechanical properties of bolted joint undergoing rub-impact force. Moreover, those study results provide insight into the diagnosis of rubbing fault.
Rotor–stator rub is a common and high-risk fault in large rotating machines. As for the aero-engine rotor system, bolted joints are widely adopted to fasten the multiple rotating parts into an integrated one. During a rubbing event, normal and tangential forces are generated by the contact and friction at the rotor–stator contacting interface. The mechanical properties of the bolted joint change dramatically under the generated forces, which will affect the dynamics of the rotor system. However, little research has been done on the dynamic properties of the bolted joint rotor system subject to rub-impact, and the coupling effect of rubbing and bolted joint on rotor dynamics is still not understood. Thus, the dynamic model of bolted joint rotor system with fixed-point rub-impact is established based upon the proposed bolted joint element and lumped mass modeling method in this work. Then, the vibration responses of the rotor system are captured by using the Newmark- β method. Bifurcation diagrams, three-dimensional spectral plots, Poincaré maps, time-domain waveforms as well as bending stiffness plots are used to demonstrate the effect of rotor–stator rub impact on the vibration characteristics of the rotor system. After that, the influences of the radial stiffness of the stator on the mechanical properties of the bolted joint and rotor dynamics are also examined. Finally, the experimental study is carried out through a bolted joint rotor test rig with a rubbing device. The studies in the present work helped in understanding the dynamic characteristics of the bolted joint rotor system and the mechanical properties of bolted joint undergoing rub-impact force. Moreover, those study results provide insight into the diagnosis of rubbing fault.
Author Luo, Zhong
Jin, Long
Li, Yuqi
Wen, Chuanmei
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Keywords Bolted joint
Rotor system
Stability analysis
Fixed-point rubbing
Dynamic modeling
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Snippet Rotor–stator rub is a common and high-risk fault in large rotating machines. As for the aero-engine rotor system, bolted joints are widely adopted to fasten...
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SubjectTerms Automotive Engineering
Bifurcations
Bolted joints
Classical Mechanics
Control
Dynamic characteristics
Dynamic models
Dynamical Systems
Engineering
Impact loads
Mechanical Engineering
Mechanical properties
Military helicopters
Original Paper
Poincare maps
Rotating machinery
Rotating machines
Rotor dynamics
Rubbing
Stators
Stiffness
Vibration
Vibration response
Waveforms
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Title Bifurcation studies of a bolted-joint rotor system subjected to fixed-point rubbing fault
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