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    A Turboshaft Aeroengine Fault Detection Method Based on One-Class Support Vector Machine and Transfer Learning

    Source: Journal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 006::page 04022085
    Author:
    Ye Zhu
    ,
    Chenglie Du
    ,
    Zhiqiang Liu
    ,
    Yao-Bin Chen
    ,
    Yong-Ping Zhao
    DOI: 10.1061/(ASCE)AS.1943-5525.0001485
    Publisher: ASCE
    Abstract: The fault detection of turboshaft engines is very important to ensure the flight safety of helicopters. Because there are few fault data in engine historical operation data, engine fault detection is often regarded as an anomaly detection problem, which is solved by the one-class classification (OCC) method. However, previous studies on fault detection usually ignored the difference between engine data caused by different engine states and operating conditions. Therefore, this paper considers the existence of these differences and introduces transfer learning to solve the problem. In this paper, based on one-class support vector machines (OC-SVM) and transfer learning (TL), an algorithm named OC-SVM-TL is proposed to detect turboshaft engine faults. In this algorithm, the hyperplane of the OC-SVM is transferred from the source domain to the target domain as a knowledge structure to help the target domain to establish a fault detection model with high accuracy. The training process is divided into two steps. The first step is to train the OC-SVM model with the data of the source domain, and the second step is to train the OC-SVM model with the data of the target domain, and the hyperplane difference between the source domain and the target domain is considered in the training process. Finally, the fault detection experiment of turboshaft engine was designed, and the fault detection of turboshaft engine was carried out under different working conditions and different engine states. The experimental results showed that the proposed algorithm has good fault detection performance when the target domain data are few or the amount of target domain data changes.
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      A Turboshaft Aeroengine Fault Detection Method Based on One-Class Support Vector Machine and Transfer Learning

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4287658
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    contributor authorYe Zhu
    contributor authorChenglie Du
    contributor authorZhiqiang Liu
    contributor authorYao-Bin Chen
    contributor authorYong-Ping Zhao
    date accessioned2022-12-27T20:36:25Z
    date available2022-12-27T20:36:25Z
    date issued2022/11/01
    identifier other(ASCE)AS.1943-5525.0001485.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4287658
    description abstractThe fault detection of turboshaft engines is very important to ensure the flight safety of helicopters. Because there are few fault data in engine historical operation data, engine fault detection is often regarded as an anomaly detection problem, which is solved by the one-class classification (OCC) method. However, previous studies on fault detection usually ignored the difference between engine data caused by different engine states and operating conditions. Therefore, this paper considers the existence of these differences and introduces transfer learning to solve the problem. In this paper, based on one-class support vector machines (OC-SVM) and transfer learning (TL), an algorithm named OC-SVM-TL is proposed to detect turboshaft engine faults. In this algorithm, the hyperplane of the OC-SVM is transferred from the source domain to the target domain as a knowledge structure to help the target domain to establish a fault detection model with high accuracy. The training process is divided into two steps. The first step is to train the OC-SVM model with the data of the source domain, and the second step is to train the OC-SVM model with the data of the target domain, and the hyperplane difference between the source domain and the target domain is considered in the training process. Finally, the fault detection experiment of turboshaft engine was designed, and the fault detection of turboshaft engine was carried out under different working conditions and different engine states. The experimental results showed that the proposed algorithm has good fault detection performance when the target domain data are few or the amount of target domain data changes.
    publisherASCE
    titleA Turboshaft Aeroengine Fault Detection Method Based on One-Class Support Vector Machine and Transfer Learning
    typeJournal Article
    journal volume35
    journal issue6
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0001485
    journal fristpage04022085
    journal lastpage04022085_15
    page15
    treeJournal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 006
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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