The invention relates to a method for checking vibration fault of a
fan blade of an aerial engine. The method comprises the following steps of: measuring torsion vibration of the aerial engine by utilizing a speed measuring fluted disc, an
eddy current displacement sensor, a
signal conditioner, a
data acquisition card and a computer, and carrying out real-time monitoring on the torsion vibration under the conditions of aerial engine ground
bench test drive, vehicle-mounted ground test drive and maneuver flight. The reliability and maintenance of the engine are improved by detecting the
fan blade vibration characteristic frequency contained in a rotor torsion vibration
signal, judging an aeroelectric state of the
fan blade and diagnosing the vibration fault of the blade of the aerial engine. According to the method for checking the vibration fault of the fan blade of the aerial engine, disclosed by the invention, a torsion vibration
signal is measured directly from an aerial engine shaft
system so that the fault information of vibration can be clearly reflected, the elements of the torsion vibration signal obtained through measurement are simple and are convenient to analyze, the
engineering limitation of a current conventional measurement method is overcome, and the real-time monitoring of the vibration of the fan blade is ensured to be carried out under various conditions, such as the engine ground
bench test drive, the vehicle-mounted ground test drive, the maneuver flight and the like.