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Publishing Language: Chinese

Prediction method of blade machining deformation driven by mechanism-data hybrid

Lizhuo DONG1,2, Siqi ZHANG1,2, Zhao ZHANG1,2, Baohai WU1,2( )
Key Laboratory of High Performance Manufacturing for Aero Engine, Ministry of Industry and Information Technology, Northwestern Polytechnical University, Xi’an 710072, China
Engineering Research Center of Advanced Manufacturing Technology for Aero Engine, Ministry of Education, Northwestern Polytechnical University, Xi’an 710072, China
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Abstract

As a typical thin-walled part of aviation, blade is prone to elastic deformation and machining residual stress deformation in the process of milling, which affects the machining accuracy and quality of blade. To address the deformation mechanism modeling problem of complex machining process of blade and the data-driven model prediction problem relying on limited collected samples, a mechanism-guided Sparrow optimized Extreme Learning Machine (SSA-ELM) thin-walled blade machining deformation prediction model is established. Firstly, the machining deformation mechanism model of thin-walled blade considering elastic deformation and machining residual stress deformation is established. Secondly, the Extreme Learning Machine Neural Network (ELMNN) is designed, and the Sparrow Search Algorithm (SSA) is used to optimize the parameters of the ELMNN hidden layer network. Then, the dataset of the data-driven model is constructed, and the Monte Carlo simulation is used to enhance the processed deformation data samples to establish the data-driven model. Finally, the mechanism-guided SSA-ELM is used to predict the thin-walled blade machining deformation, and the root mean square error and correlation coefficient of the machining deformation are used as the model accuracy evaluation index. The results show that the root mean square error of the mechanism guided and SSA optimized machining deformation prediction model is reduced by 77.25% and 30.5% respectively, which proves that the model has good prediction performance.

CLC number: V261.2; TH161.6 Document code: A

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Acta Aeronautica et Astronautica Sinica
Article number: 629037

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Cite this article:
DONG L, ZHANG S, ZHANG Z, et al. Prediction method of blade machining deformation driven by mechanism-data hybrid. Acta Aeronautica et Astronautica Sinica, 2024, 45(13): 629037. https://doi.org/10.7527/S1000-6893.2023.29037

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Received: 23 May 2023
Revised: 12 June 2023
Accepted: 20 August 2023
Published: 07 October 2023
© 2024 The Journal of Acta Aeronautica et Astronautica Sinica