Instability Threshold and Stability Boundaries of Rotor-Bearing SystemsSource: Journal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 001::page 115Author:W. J. Chen
DOI: 10.1115/1.2816526Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A direct numerical method for the determination of instability threshold and stability boundaries of flexible rotor-bearing systems is presented. The proposed procedure can also be used to improve the system stability by considering the design variables as operating parameters. The finite element method is utilized in the formulation of system equations of motion. The numerical algorithm is based on nonlinear optimization techniques. Two examples are presented to illustrate the feasibility, desirability, and ability of the proposed algorithm. A simple journal bearing system is used for the parametric study. An industrial high-speed compressor is employed to demonstrate the ability of this algorithm to deal with practical applications. The stability boundaries calculated from this algorithm are in agreement with the experimental results.
keyword(s): Stability , Bearings , Rotors , Algorithms , Journal bearings , Design , Numerical analysis , Optimization , Compressors , Equations of motion AND Finite element methods ,
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| contributor author | W. J. Chen | |
| date accessioned | 2017-05-08T23:50:11Z | |
| date available | 2017-05-08T23:50:11Z | |
| date copyright | January, 1996 | |
| date issued | 1996 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26747#115_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/116980 | |
| description abstract | A direct numerical method for the determination of instability threshold and stability boundaries of flexible rotor-bearing systems is presented. The proposed procedure can also be used to improve the system stability by considering the design variables as operating parameters. The finite element method is utilized in the formulation of system equations of motion. The numerical algorithm is based on nonlinear optimization techniques. Two examples are presented to illustrate the feasibility, desirability, and ability of the proposed algorithm. A simple journal bearing system is used for the parametric study. An industrial high-speed compressor is employed to demonstrate the ability of this algorithm to deal with practical applications. The stability boundaries calculated from this algorithm are in agreement with the experimental results. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Instability Threshold and Stability Boundaries of Rotor-Bearing Systems | |
| type | Journal Paper | |
| journal volume | 118 | |
| journal issue | 1 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.2816526 | |
| journal fristpage | 115 | |
| journal lastpage | 121 | |
| identifier eissn | 0742-4795 | |
| keywords | Stability | |
| keywords | Bearings | |
| keywords | Rotors | |
| keywords | Algorithms | |
| keywords | Journal bearings | |
| keywords | Design | |
| keywords | Numerical analysis | |
| keywords | Optimization | |
| keywords | Compressors | |
| keywords | Equations of motion AND Finite element methods | |
| tree | Journal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 001 | |
| contenttype | Fulltext |