An Approximate Modal Method for Rotordynamic Stability Prediction of Flexible Rotors
The prediction of rotordynamic stability is important in the design and diagnosis of high-performance turbomachinery. An approximate method using the mode shape and natural frequency of the first undamped vibration mode of the rotor-bearing system is developed and verified to be accurate for practical cases. The assumption that the damping does not significantly affect the first mode modal parameters can be relaxed if the damped mode shape is available. It confirms previous findings that the mode deflection at the bearing position is most critical to rotor-bearing system stability. The modal method, despite its simplicity, is superior to the lumped parameter method since it can easily account for the distributed shaft parameters and the effective modal contribution of other component properties including the aerodynamic excitation. When provided with the results of the undamped vibration analysis (i.e. only one eigensolution for a specified system configuration), the method predicts a linear relationship between stability measured in terms of logarithmic decrement and system (bearing) damping. The method allows very efficient parameter studies for the effect of bearing damping and aerodynamic cross-coupling on system stability.