The transfer matrix–component mode synthesis has been developed for the analysis of critical speed, response to imbalance and rotordynamic optimal design of multi–spool rotor system. This method adopted the advantages of the transfer matrix method for the train structure and the component mode synthesis for reducing degrees of freedom. In this method, the whole system is divided into several subsystems at the boundary coordinates. The constrained vibration modes and the static deflection curves of the constrained rotor subsystems are analysed by the improved transfer matrix method. The whole system is connected together by the component mode synthesis in accordance with the coordinate transformation. Numerical examples show that this method is superior to the traditional transfer matrix method and the component mode synthesis by FEM. This method has been successfully used for the rotordynamic analysis and optimal design of the compressors and the gas turbine aeroengines.
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ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition
June 10–13, 1996
Birmingham, UK
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7876-7
PROCEEDINGS PAPER
The Transfer Matrix–Component Mode Synthesis for Rotordynamic Analysis
Huang Taiping
Huang Taiping
Nanjing University of Aeronautics and Astronautics, Nanjing, China
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Huang Taiping
Nanjing University of Aeronautics and Astronautics, Nanjing, China
Paper No:
96-GT-079, V005T14A010; 6 pages
Published Online:
February 6, 2015
Citation
Taiping, H. "The Transfer Matrix–Component Mode Synthesis for Rotordynamic Analysis." Proceedings of the ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition. Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; General. Birmingham, UK. June 10–13, 1996. V005T14A010. ASME. https://doi.org/10.1115/96-GT-079
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