The application discloses an aero-engine bearing inner ring passive
temperature measurement system and method, and relates to the technical field of aero-engine
temperature measurement.The application uses a high-temperature-resistant composite
piezoelectric quartz crystal resonator as a passive resonant temperature-sensitive unit, combines a non-contact
coupling reading antenna and an advanced
signal demodulation and temperature calculation module, and realizes high-precision, high-reliability and real-time measurement of the temperature of the bearing inner ring under all working conditions.The application not only overcomes the limitations of traditional
temperature measurement methods, but also significantly improves the accuracy and reliability of temperature measurement data, provides strong support for the health management of aero-engines, and has the advantages of compact structure, convenient installation, long service life and the like, and has wide
engineering application prospects and important economic value.