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Mode Shape Description of an Aero Engine Casing Structure Using Zernike Moment Descriptors

机译:使用Zernike矩描述符的航空发动机机壳结构的模式形状描述

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Vibration mode shape description of an aero casing structure using Zernike moment descriptor (ZMD) is introduced in this paper. The mode shapes of the aero casing structure can be decomposed as a linear combination of a series of Zernike polynomials, with the feature of each Zernike polynomial reflecting a part of characteristic of mode shapes, based on Zernike moment transformation. Meanwhile, the reconstruction of mode shapes with Zernike moment descriptor is explored and its ability to filtering the noise contaminated in the mode shapes is studied. Simulation of the aero casing structure indicates the advantage of this method to depict the mode shapes of a symmetric structure. Results demonstrate that the Zernike moment description of the mode shapes can effectively describe the double modes in the symmetric structure and also has the ability to remove or significantly reduce the influence of noise in the mode shapes. Such feature shows great practical value for further research on the correlation, model updating and model validation of the symmetric structure's FE model
机译:本文介绍了使用Zernike矩描述符(ZMD)的航空器壳体结构的振动模式形状描述。航空器壳体结构的模式形状可以分解为一系列Zernike多项式的线性组合,每个Zernike多项式的特征都可以基于Zernike矩变换反映出部分模式形状的特征。同时,探讨了用Zernike矩描述符重建模态的方法,并研究了其滤除模态中污染的噪声的能力。航空机壳结构的仿真表明,该方法的优势在于可以描绘对称结构的振型。结果表明,振型的Zernike矩描述可以有效地描述对称结构中的双振型,并且具有消除或显着降低振型中噪声影响的能力。该特征对进一步研究对称结构有限元模型的相关性,模型更新和模型验证具有重要的实用价值。

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