Transient gas path fault diagnosis of aero-engine based on domain adaptive offline reinforcement learning

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2024-11-12 DOI:10.1016/j.ast.2024.109701
Jinghui Xu, Ye Wang, Zepeng Wang, Xizhen Wang, Yongjun Zhao
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Abstract

Real-time measurement parameters are crucial for diagnosing faults in aero-engine gas path performance, ensuring engine reliability, and mitigating potential economic losses. Traditional aero-engines performance diagnosis was mainly based on the measurements of steady-state condition and lacked the utilization of data under transient conditions. Gas path diagnosis of aero-engines under transient conditions is crucial for early fault detection and safety of flight within the envelope. The challenge lies in the inconsistent distribution of performance deviations caused by variable operating conditions, especially with complex fault types, which can undermine diagnostic credibility. To improve reliability of gas path diagnosis under transient conditions, an offline reinforcement learning fault diagnosis framework based on a transient aero-engine performance model is proposed. To address the issue of variable operating conditions during transient states, a domain adaptive approach is utilized to reconstruct the measurement baseline and facilitate the transfer of different performance deviation distributions. Additionally, by adding spool acceleration as a measurement parameter, the multi-component fault coupling is solved. Finally, validation with actual operating data simulates fault cases, demonstrating the proposed method's efficacy in quantitatively detecting gradual, sudden, and multiple component faults under transient conditions with high accuracy and efficiency. The method proposed in this study achieves a computational speed improvement by 64% compared to the conventional method, achieving a time of 0.13 seconds, with an average error of less than 0.00389%. Additionally, it demonstrates strong robustness in the presence of noise, with an average error of less than 0.03125%. This proposed method improves real-time fault detection under transient conditions for its higher accuracy and efficiency, and therefore significantly enhance gas path health monitoring and diagnosis capability.
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基于域自适应离线强化学习的航空发动机瞬态气路故障诊断
实时测量参数对于诊断航空发动机气路性能故障、确保发动机可靠性和减少潜在经济损失至关重要。传统的航空发动机性能诊断主要基于稳态条件下的测量,缺乏对瞬态条件下数据的利用。瞬态条件下的航空发动机气路诊断对早期故障检测和包络线内的飞行安全至关重要。面临的挑战在于,不同的运行条件会导致性能偏差分布不一致,尤其是复杂的故障类型,这会影响诊断的可信度。为了提高瞬态条件下气路诊断的可靠性,提出了一种基于瞬态航空发动机性能模型的离线强化学习故障诊断框架。为解决瞬态期间工作条件多变的问题,采用了域自适应方法来重建测量基线,并促进不同性能偏差分布的转移。此外,通过添加阀芯加速度作为测量参数,解决了多组件故障耦合问题。最后,利用实际运行数据对故障案例进行了模拟验证,证明了所提出的方法在定量检测瞬态条件下的渐变、突变和多组件故障方面具有很高的准确性和效率。与传统方法相比,本研究提出的方法计算速度提高了 64%,耗时仅为 0.13 秒,平均误差小于 0.00389%。此外,该方法在存在噪声的情况下也表现出很强的鲁棒性,平均误差小于 0.03125%。该方法提高了瞬态条件下的实时故障检测精度和效率,从而显著增强了气体路径健康监测和诊断能力。
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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