简介概要

Vibration reliability analysis for aeroengine compressor blade based on support vector machine response surface method

来源期刊:中南大学学报(英文版)2015年第5期

论文作者:GAO Hai-feng BAI Guang-chen

文章页码:1685 - 1694

Key words:vibration; reliability analysis; compressor blade; support vector machine response surface method; natural frequency

Abstract: To ameliorate reliability analysis efficiency for aeroengine components, such as compressor blade, support vector machine response surface method (SRSM) is proposed. SRSM integrates the advantages of support vector machine (SVM) and traditional response surface method (RSM), and utilizes experimental samples to construct a suitable response surface function (RSF) to replace the complicated and abstract finite element model. Moreover, the randomness of material parameters, structural dimension and operating condition are considered during extracting data so that the response surface function is more agreeable to the practical model. The results indicate that based on the same experimental data, SRSM has come closer than RSM reliability to approximating Monte Carlo method (MCM); while SRSM (17.296 s) needs far less running time than MCM (10958 s) and RSM (9840 s). Therefore, under the same simulation conditions, SRSM has the largest analysis efficiency, and can be considered a feasible and valid method to analyze structural reliability.

详情信息展示

Vibration reliability analysis for aeroengine compressor blade based on support vector machine response surface method

GAO Hai-feng(高海峰), BAI Guang-chen(白广忱)

(School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics,
Beijing 100191, China)

Abstract:To ameliorate reliability analysis efficiency for aeroengine components, such as compressor blade, support vector machine response surface method (SRSM) is proposed. SRSM integrates the advantages of support vector machine (SVM) and traditional response surface method (RSM), and utilizes experimental samples to construct a suitable response surface function (RSF) to replace the complicated and abstract finite element model. Moreover, the randomness of material parameters, structural dimension and operating condition are considered during extracting data so that the response surface function is more agreeable to the practical model. The results indicate that based on the same experimental data, SRSM has come closer than RSM reliability to approximating Monte Carlo method (MCM); while SRSM (17.296 s) needs far less running time than MCM (10958 s) and RSM (9840 s). Therefore, under the same simulation conditions, SRSM has the largest analysis efficiency, and can be considered a feasible and valid method to analyze structural reliability.

Key words:vibration; reliability analysis; compressor blade; support vector machine response surface method; natural frequency

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