4.5 Article

Nonlinear Dynamic Behavior Analysis of Dual-Rotor-Bearing Systems with Looseness and Rub-Impact Faults

Journal

AIAA JOURNAL
Volume -, Issue -, Pages -

Publisher

AMER INST AERONAUTICS ASTRONAUTICS
DOI: 10.2514/1.J062967

Keywords

Finite Element Modeling; High Pressure Turbine; Model Order Reduction; Mechanical and Structural Vibrations; Aircraft Engines; Rotor Dynamics; Elastic Deformation

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This paper discusses the nonlinear dynamic behaviors of dual-rotor-bearing systems with looseness and rub-impact faults. The dual-rotor-bearing system model with looseness and rub-impact coupling faults is established using the finite element method. The component mode synthesis (CMS) and proper orthogonal decomposition (POD) methods are introduced. The efficiency of the order reduction method is verified by comparing the dynamic behaviors of the original and reduced systems. The frequency spectrum and amplitude-frequency behaviors of rotor systems are studied. The results can provide qualitative guidance for structural design optimization of large rotating machines and prior information for looseness and rub-impact coupling faults.
The nonlinear dynamic behaviors of dual-rotor-bearing systems with looseness and rub-impact faults are discussed in this paper. The dual-rotor-bearing system with looseness and rub-impact coupling faults is established by the finite element method. The component mode synthesis (CMS) and proper orthogonal decomposition (POD) methods are introduced. The CMS and POD methods are used to reduce the original rotor system model, and the efficiency of the order reduction method is verified by comparing the dynamic behaviors of the original and reduced systems. The frequency spectrum and amplitude-frequency behaviors of rotor systems are studied. The results can provide qualitative guidance to structural design optimization of large rotating machines and prior information for looseness and rub-impact coupling faults.

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