Dynamic parametric modeling-based model updating strategy of aeroengine casings

•Propose parametric modeling-based model updating strategy (PM-MUS) for structural dynamic modeling and updating.•Deal with uncorrelated mode shapes by introducing an objective function.•The proposed model updating method can correctly identify CMPs in dynamic model updating.•Finish accurately FE mo...

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Veröffentlicht in:Chinese journal of aeronautics 2021-12, Vol.34 (12), p.145-157
Hauptverfasser: FEI, Chengwei, LIU, Haotian, LI, Shaolin, LI, Huan, AN, Liqiang, LU, Cheng
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Sprache:eng
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Zusammenfassung:•Propose parametric modeling-based model updating strategy (PM-MUS) for structural dynamic modeling and updating.•Deal with uncorrelated mode shapes by introducing an objective function.•The proposed model updating method can correctly identify CMPs in dynamic model updating.•Finish accurately FE model updating of the casings by advanced parametric modeling and model updating technology.•Offer a useful insight and a perfect model updating strategy for establishing reliable FE model for complex structures. For accurate Finite Element (FE) modeling for the structural dynamics of aeroengine casings, Parametric Modeling-based Model Updating Strategy (PM-MUS) is proposed based on efficient FE parametric modeling and model updating techniques regarding uncorrelated/correlated mode shapes. Casings structure is parametrically modeled by simplifying initial structural FE model and equivalently simulating mechanical characteristics. Uncorrelated modes between FE model and experiment are reasonably handled by adopting an objective function to recognize correct correlated modes pairs. The parametrized FE model is updated to effectively describe structural dynamic characteristics in respect of testing data. The model updating technology is firstly validated by the detailed FE model updating of one fixed–fixed beam structure in light of correlated/uncorrelated mode shapes and measured mode data. The PM-MUS is applied to the FE parametrized model updating of an aeroengine stator system (casings) which is constructed by the proposed parametric modeling approach. As revealed in this study, (A) the updated models by the proposed updating strategy and dynamic test data is accurate, and (B) the uncorrelated modes like close modes can be effectively handled and precisely identify the FE model mode associated the corresponding experimental mode, and (C) parametric modeling can enhance the dynamic modeling updating of complex structure in the accuracy of mode matching. The efforts of this study provide an efficient dynamic model updating strategy (PM-MUS) for aeroengine casings by parametric modeling and experimental test data regarding uncorrelated modes.
ISSN:1000-9361
DOI:10.1016/j.cja.2020.10.036