Stability Analysis of Rotor-Bearing Systems Using Component Mode Synthesis

1980 ◽  
Vol 102 (2) ◽  
pp. 352-359 ◽  
Author(s):  
D. A. Glasgow ◽  
H. D. Nelson

A method of component mode synthesis is presented for the analysis of multishaft rotor-bearings systems. The motion of each component of the system is described as the superposition of constraint modes associated with boundary coordinates and constrained precessional modes associated with internal coordinates. The constrained precessional modes for each component are truncated and the reduced component equations are assembled to yield a set of system equations. The nonsymmetric nature of the general problem requires the utilization of biorthogonality relations between right and left vector sets in order to decouple the component precessional modes. The method is developed for damped whirl speed/stability analysis and comparative results are presented for various levels of mode truncation for two example systems.

Author(s):  
H. D. Nelson ◽  
W. L. Meacham

A method of component mode synthesis is utilized to determine the forced response of linear multi-shaft rotor-bearing systems. The formulation allows for simulation of system response due to blade loss, base shock, maneuver loads, and specified fixed frame forces. The motion of each rotating component of the system is described by superposing constraint modes associated with boundary coordinates and constrained precessional modes associated with internal coordinates. The precessional modes are truncated for each component and the reduced component equations are assembled to obtain a set of complex system equations of reduced order. The method allows for nonsymmetric effects and comparative results are presented for various levels of mode truncation for two example cases.


1983 ◽  
Vol 105 (3) ◽  
pp. 606-614 ◽  
Author(s):  
H. D. Nelson ◽  
W. L. Meacham ◽  
D. P. Fleming ◽  
A. F. Kascak

The method of component mode synthesis is developed to determine the forced response of nonlinear, multishaft, rotor-bearing systems. The formulation allows for simulation of system response due to blade loss, distributed unbalance, base shock, maneuver loads, and specified fixed frame forces. The motion of each rotating component of the system is described by superposing constraint modes associated with boundary coordinates and constrained precessional modes associated with internal coordinates. The precessional modes are truncated for each component and the reduced component equations are assembled with the nonlinear supports and interconnections to form a set of nonlinear system equations of reduced order. These equations are then numerically integrated to obtain the system response. A computer program, which is presently restricted to single shaft systems has been written and results are presented for transient system response associated with blade loss dynamics, with squeeze film dampers, and with interference rubs.


Author(s):  
Nur Alyani Nadhiya ◽  
Fitri Yakub ◽  
Hatta Ariff ◽  
Azizul Azizan ◽  
Zainuddin A. Rasit ◽  
...  

1996 ◽  
Author(s):  
Christopher Tarpley ◽  
Darryll Pines ◽  
Ajay Kothari

Sign in / Sign up

Export Citation Format

Share Document