doi: 10.52899/24141437_2026_01_63
UDK: 621.82:004.94, 534.1:62-1/-9

Effect of Support Rigidity on Modal Parameters of Multi-Supported Rotors

Изотов Н. В., Портнова О. С., Плаксин Р. А., Васютина А. А., Нестеренко И. А.

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Citation Link: Izotov NV, Portnova OS, Plaksin RA, Vasyutina AA, Nesterenko IA. Effect of Support Rigidity on Modal Parameters of Multi-Supported Rotors. Transactions of the Saint Petersburg State Marine Technical University. 2026;5(1):63–68. DOI: 10.52899/24141437_2026_01_63 EDN: WSMXZF

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BACKGROUND: The study on the effect of support rigidity on modal parameters of multi-supported rotors is relevant as scientific and technical publications mainly analyze data for two-support rotor systems. The findings should be considered when balancing multi-supported rotor systems on their supports. AIM: To study the effect of variable support rigidity on the modal parameters of a multi-supported rotor; to determine the relationship between the natural vibration frequency and the ratio of the support and rotor rigidity, and to identify relationships between changes in the natural vibration mode shapes and the support rigidity. METHODS: The study used the Fidesys software suite. The method involved creating a digital model of a four-support rotor, followed by changing their rigidity in the range of 10⁻⁶–10⁸ N/mm. The rotor modal parameters were investigated at each rigidity value. RESULTS: It is shown that the higher the rigidity of the supports, the higher the natural vibration frequency of the rotor following a nonlinear law. The study identified the following patterns: at Kc >105, the modal parameters are identical to the values obtained for a structure with absolutely rigid supports; in the range of Kc from 10-6 to 105 , a nonlinear frequency change occurs; at Kc
Keywords: rotor; rigidity; modal analysis; natural frequencies; natural mode shape.

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