基于FSVM改良隶属度的发动机振动故障识别

白斌;白广忱;林学柱

振动与冲击 ›› 2013, Vol. 32 ›› Issue (20) : 23-28.

PDF(1176 KB)
PDF(1176 KB)
振动与冲击 ›› 2013, Vol. 32 ›› Issue (20) : 23-28.
论文

基于FSVM改良隶属度的发动机振动故障识别

  • 白斌1,白广忱1,林学柱2
作者信息 +

Improved Fuzzy Membership Method in FSVM for Aeroengine Vibration Fault Identification

  • BAIBin1,BAI Guang-chen1, LINXuezhu2
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文章历史 +

摘要

为了更好的对航空发动机整机振动进行故障诊断和识别,提出了改良的FSVM隶属度和多类隶属度与信息熵的融合定量分析方法,并且和传统的FSVM隶属度分析方法进行比较。对传统的FSVM的模糊隶属度函数改良后建立了多类模糊隶属度计算模型。通过实验实例验证了该多类模糊隶属度与信息熵相结合的技术对于航空发动机整机振动状态评估和故障诊断识别非常有效,计算出振动故障模式与故障原因之间的权值,建立了一个多参数的发动机振动状态分析模型;并对各类振动原因对发动机整体状态的影响进行定量分析,为发动机的振动抑制提供量化参考指标。

Abstract

In order to more effectively fault diagnosis and identification for aeroengine whole-body vibration, the improved Fuzzy Support Vector Machine (FSVM) and multi-class fuzzy membership with information entropy technique was proposed in this paper.And it compared with the traditional FSVM membership degree analysis methods.The calculation model of multi-class fuzzy membership function.was established based on the traditional FSVM fuzzy membership function. The experiment and examples of aircraft engine overall vibration performance and fault diagnosis and identification verify that the technology of multi-class fuzzy membership with information entropy was very effective.The relationship weights between fault modes and fault causes were determined and the multi-parameter vibration performance analysis model was developed, so that aeroengine overall vibration performance was quantitative analysis and a quantitative reference index was provided for aeroengine vibration control.



关键词

模糊支持向量机 / 信息熵 / 多类模糊隶属度 / 模糊隶属度 / 故障诊断识别

Key words

Fuzzy Support Vector Machine (FSVM) / information entropy / fuzzy membership / multi-class fuzzy membership / fuzzy membership / fault diagnosis and identification

引用本文

导出引用
白斌;白广忱;林学柱. 基于FSVM改良隶属度的发动机振动故障识别[J]. 振动与冲击, 2013, 32(20): 23-28
BAIBin;BAI Guang-chen;LINXuezhu. Improved Fuzzy Membership Method in FSVM for Aeroengine Vibration Fault Identification[J]. Journal of Vibration and Shock, 2013, 32(20): 23-28

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