基于状态维护的航空发动机健康监测、诊断和预测:概述

IF 0.7 4区 工程技术 Q4 ENGINEERING, AEROSPACE International Journal of Turbo & Jet-Engines Pub Date : 2022-05-12 DOI:10.1515/tjeng-2022-0020
Narahari Rath, R. Mishra, A. Kushari
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引用次数: 12

摘要

摘要航空发动机性能退化严重影响其可靠性、可用性和寿命。因此,预测性维护是工业4.0中的一个关键数字,它保证了高可用性和减少停机时间,从而降低了军用和民用发动机的运营成本。这导致了按需维护,并需要一个有效的发动机健康监测系统。本文综述了基于气路性能参数的航空发动机健康监测、诊断和预测技术的研究进展。综述了性能监测的起源及其随时间的演变,使用发动机模型性能自适应建立高质量数据库的技术,以及计算智能技术在促进发动机故障诊断实施方面的作用。因此,生成关于发动机健康状况的可靠信息是成功实施基于状况的维护的必要条件。基于这项研究,可以尝试使用航空发动机性能数据库中的退化模式来预测关键部件的剩余寿命,这将是发动机设计者和操作员的宝贵财富。
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Aero engine health monitoring, diagnostics and prognostics for condition-based maintenance: an overview
Abstract Aero engine performance deterioration highly influences its reliability, availability and life cycle. Predictive maintenance is therefore a key figure within Industry 4.0, which guarantees high availability and reduced downtime thus reduced operational costs for both military and civil engines. This leads to maintenance on demand and needs an effective engine health monitoring system. This paper overviews the work carried out on aero engine health monitoring, diagnostic and prognostic techniques based on gas path performance parameters. The inception of performance monitoring and its evolution over time, techniques used to establish a high-quality data base using engine model performance adaptation, and effects of computationally intelligent techniques on promoting the implementation of engine fault diagnosis are reviewed. Generating dependable information about the health condition of the engine is therefore a requisite for a successful implementation of condition-based maintenance. Based on this study, further research can be attempted to predict residual life of critical components using degradation pattern from aero engine performance data bank which will be an invaluable asset for engine designers as well as for operators.
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来源期刊
International Journal of Turbo & Jet-Engines
International Journal of Turbo & Jet-Engines 工程技术-工程:宇航
CiteScore
1.90
自引率
11.10%
发文量
36
审稿时长
6 months
期刊介绍: The Main aim and scope of this Journal is to help improve each separate components R&D and superimpose separated results to get integrated systems by striving to reach the overall advanced design and benefits by integrating: (a) Physics, Aero, and Stealth Thermodynamics in simulations by flying unmanned or manned prototypes supported by integrated Computer Simulations based on: (b) Component R&D of: (i) Turbo and Jet-Engines, (ii) Airframe, (iii) Helmet-Aiming-Systems and Ammunition based on: (c) Anticipated New Programs Missions based on (d) IMPROVED RELIABILITY, DURABILITY, ECONOMICS, TACTICS, STRATEGIES and EDUCATION in both the civil and military domains of Turbo and Jet Engines. The International Journal of Turbo & Jet Engines is devoted to cutting edge research in theory and design of propagation of jet aircraft. It serves as an international publication organ for new ideas, insights and results from industry and academic research on thermodynamics, combustion, behavior of related materials at high temperatures, turbine and engine design, thrust vectoring and flight control as well as energy and environmental issues.
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