Identification of bearing dynamic parameters and unbalance states in a flexible rotor system fully levitated on active magnetic bearings

Mechatronics ◽  
2014 ◽  
Vol 24 (3) ◽  
pp. 274-286 ◽  
Author(s):  
Rajiv Tiwari ◽  
Avinash Chougale
Keyword(s):  
Rotor System ◽  
Magnetic Bearings ◽  
Dynamic Parameters ◽  
Active Magnetic Bearings ◽  
Flexible Rotor

Identification of dynamic parameters of active magnetic bearings in a flexible rotor system considering residual unbalances

Mechatronics ◽  
2018 ◽  
Vol 49 ◽  
pp. 46-55 ◽  
Author(s):  
Yuanping Xu ◽  
Jin Zhou ◽  
Zongli Lin ◽  
Chaowu Jin
Keyword(s):  
Rotor System ◽  
Magnetic Bearings ◽  
Dynamic Parameters ◽  
Active Magnetic Bearings ◽  
Flexible Rotor

Estimation of Active Magnetic Bearings (AMB) Dynamic Parameters and Residual Mass Imbalance Using FEM With PID Controller and Identification Algorithm of a Flexible Rotor System Fully Levitated on AMB

2019 ◽  
Author(s):  
Bala Murugan S. ◽  
R. K. Behera
Keyword(s):  
Pid Controller ◽  
Rotor System ◽  
Magnetic Bearings ◽  
Identification Algorithm ◽  
Dynamic Parameters ◽  
Active Magnetic Bearings ◽  
Flexible Rotor ◽  
Residual Mass ◽  
Mass Imbalance ◽  
Least Squares Fit

Abstract The dynamic analyses of rotating systems are always a testing task to obtain the definite results. This paper carries the dynamic modelling, analysis and identification of coupled flexible rotor system supported by an auxiliary Active Magnetic Bearings (AMBs). An identification algorithm is used to estimate the dynamic parameters of AMB, and rotor residual mass imbalance. The proposed algorithm is a right method for the analysis of fully levitated rotor on AMBs. Finite element method is used to model the dynamic flexible rotor system with PID controller. A conventional dynamic condensation technique is implemented in the development of identification algorithm to overcome the difficulty in numerical simulation. The least-squares fit technique is deployed to estimate the dynamic parameters in frequency domain. Then the algorithm is extended to find the misalignment forces and moments at the coupling point. Numerical study is carried to check the correctness of the algorithm. The proposed algorithm is yet to be tested to experimental results from a fully levitated rotor test rig supported with AMBs.

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