Aircraft engine vibration signals carry crucial operational information, necessitating accurate monitoring and analysis to ensure flight safety. However, the detection accuracy of vibration sensors is significantly compromised in high-temperature environments, posing substantial challenges for traditional battery-powered models. Here, we present a self-powered piezoelectric vibration sensor based on a polyvinylidene fluoride-polyimide nanofiber membrane, which can effectively mitigate the performance degradation in high-temperature environments. The piezoelectric vibration sensor is capable of distinguishing the vibration signals generated by healthy gears, pitting gears, and broken gears, achieving a recognition accuracy of 96.3 % by using machine-learning algorithms. Finally, we develop a digital twin system to identify failure modes in aircraft engine gears, promising intelligent engine health management.
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