An Efficient Approach for the Frequency Analysis of Nonaxisymmetric Rotating Structures: Application to a Coupled Bladed Birotor System

Author:

Dumartineix Cécile12,Chouvion Benjamin3,Thouverez Fabrice3,Parent Marie-Océane4

Affiliation:

1. École Centrale de Lyon, Laboratoire de Tribologie et Dynamique des Systèmes, UMR-CNRS 5513, Écully cedex 69134, France;

2. Safran Aircraft Engines, Rond Point René Ravaud—Réau, Moissy-Cramayel 77550, France e-mail:

3. École Centrale de Lyon, Laboratoire de Tribologie et Dynamique des Systèmes, UMR-CNRS 5513, Écully cedex 69134, France

4. Safran Aircraft Engines, Rond Point René Ravaud—Réau, Moissy-Cramayel 77550, France

Abstract

The improvement of efficiency in the design of turbomachines requires a reliable prediction of the vibrating behavior of the whole structure. The simulation of blades vibrations is decisive and this is usually based on elaborated finite element model restricted to the bladed-disk. However, the blades dynamic behavior can be strongly affected by interactions with other parts of the engine. Global dynamic studies that consider these other parts are required but usually come with a high numerical cost. In the case of a birotor architecture, two coaxial rotors with different rotating speeds can be coupled with a bearing system. The mechanical coupling between the shafts generates energy exchange that alters the dynamic behavior of the blades. The equations of motion of the whole structure that take into account the coupling contain periodic time-dependent coefficients due to the difference of rotational speed between both rotors. Equations of this kind, with variable coefficients, are typically difficult to solve. This study presents a preprocessing method to guarantee the elimination of time-dependent coefficients in the birotor equations of motion. This method is tested with a simplified finite element model of two bladed-disks coupled with linear stiffnesses. We obtain accurate results when comparing frequency analysis of preprocessed equations with time-integration resolution of the initial set of equations. The developed methodology also offers a substantial time saving.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference21 articles.

1. Two-Dimensional Modeling of an Aircraft Engine Structural Bladed Disk-Casing Modal Interaction;J. Sound Vib.,2009

2. Dynamics of Rotationally Periodic Structures;Int. J. Numer. Methods Eng.

3. Dynamical Analysis of Multi-Stage Cyclic Structures;Mech. Res. Commun.,2007

4. Reduced Order Modeling for Multi-Stage Coupling of Cyclic Symmetric Structures;Proc. ISMA,2016

Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Probabilistic analysis of maximum mode shape for mistuned blisk;International Journal of Turbo & Jet-Engines;2022-07-18

2. Influence of Blade Flexibility on the Dynamic Response Simulation of a Turbomolecular Pump on Magnetic Bearings;Journal of Engineering for Gas Turbines and Power;2020-01-29

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