Turbofan Engine Remaining Useful Life Prediction based on Physics-aware Hybrid Framework and Fatigue Cycles

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Published May 18, 2026
Slawomir Szrama

Abstract

Accurate remaining useful life (RUL) prognostics for turbofan engines are critical for advancing aviation safety and optimizing condition-based maintenance. While conventional methods rely on static service intervals or purely data-driven models, this study introduces a physics-aware hybrid framework that synergizes low-cycle fatigue (LCF) dynamics with a multi-architecture neural network. The framework addresses two fundamental limitations in existing approaches: (1) the omission of material fatigue mechanisms in purely data-driven models, and (2) the limited generalizability of simulated training data to real-world operational variability. The proposed model achieves superior degradation tracking by integrating fatigue cycle analytics, derived from engine operational stress profiles, with a hybrid neural architecture comprising Long Short-Term Memory (LSTM) networks for temporal dependencies, Temporal Convolutional Networks (TCN) for local feature extraction, and Multi-Head Self-Attention (MHSA) layers for dynamic weighting of critical sensor inputs. Comprehensive evaluation on both a 12-year real-world fleet dataset (53 F100-PW-229 engines) and the NASA C-MAPSS benchmark demonstrates significant improvements in predictive performance, with RMSE reductions of 29-48% compared to state-of-the-art hybrid models. The results underscore the potential of physics-aware deep learning to revolutionize predictive maintenance practices in aviation.

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Keywords

physics-informed neural networks, fatigue-driven prognostics, operational degradation analytics, multi-modal sensor fusion, turbofan health management, low-cycle fatigue

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