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Review Article | Open Access

Intelligent fault diagnosis methods toward gas turbine: A review

Xiaofeng LIUa( )Yingjie CHENaLiuqi XIONGaJianhua WANGbChenshuang LUOaLiming ZHANGaKehuan WANGa
School of Transportation Science and Engineering, Beihang University, Beijing 100191, China
Systems Engineering Research Institute, China State Shipbuilding Corporation, Beijing 100094, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

Fault diagnosis plays a significant role in conducting condition-based maintenance and health management for gas turbines (GTs) to improve reliability and reduce costs. Various diagnosis methods developed by modeling engine systems or certain components implement faults detection and diagnosis based on the measurement of systemic parameters deviations. However, these conventional model-based methods are hindered by limitations of inability to handle the nonlinear nature, measurement uncertainty, fault coupling and other implementing problems. Recently, the development of artificial intelligence algorithms has provided an effective solution to the above problems, triggering broad researches for data-driven fault diagnosis methods with better accuracy, dynamic performance, and universality. This paper presents a systematic review of recently proposed intelligent fault diagnosis methods for GT engines, according to the classification of shallow learning methods, deep learning methods and hybrid intelligent methods. Moreover, the principle of typical algorithms, the evolution of enhanced methods, and the assessment of pros and cons are summarized to conclude the present status and look forward to the future in the field of GT fault diagnosis. Possible directions for development in method validation, information fusion, and interpretability of intelligent diagnosis methods are concluded in the end to provide insightful concepts for scholars in related fields.

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Chinese Journal of Aeronautics
Pages 93-120

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Cite this article:
LIU X, CHEN Y, XIONG L, et al. Intelligent fault diagnosis methods toward gas turbine: A review. Chinese Journal of Aeronautics, 2024, 37(4): 93-120. https://doi.org/10.1016/j.cja.2023.09.024

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Received: 27 April 2023
Revised: 07 June 2023
Accepted: 11 September 2023
Published: 28 September 2023
© 2023 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).