The invention discloses an aeroengine vibration
transducer double-wire checking and detecting method and an implementation
system thereof. The implementation
system comprises a main
system which is formed by a computer, a controller, a power
amplifier, a power supply, a vibration table, a vibration
measuring instrument, a digital display No.1 and a piezoelectric accelerator No.1, and an
auxiliary system which is formed by a piezoelectric accelerator No. 2, a
charge amplifier and a digital display No.2 and is used for detecting the self errors of a vibration system. The checking and detecting method comprises that a computer is used to build a vibration test, the checking and detecting main system detects and displays the vibration
signal which is detected by a detected vibration
transducer, the
auxiliary system detects the self errors of the vibration system, and the detected vibration
transducer is checked and detected through eliminating the self errors of the detecting vibration system. By utilizing the method, the problems that a single-wire checking and detecting method of the prior art cannot reflect the vibration
system error elimination, cannot correctly judge the detected vibration transducer and the like are solved, and the method has the characteristics of high checking accuracy, high working efficiency and the like.