The invention belongs to the technical field of
aviation engineering design, and discloses an aircraft hidden fault indication
recording system and an alarm
database design method.The aircraft hidden fault indication
recording system comprises a plurality of sensors used for feeding back state parameters of an aircraft in real time, and the state parameters comprise
voltage, current, vibration, frequency, Hall, displacement, temperature and
humidity; the at least one
processing unit is used for receiving the state parameters of the sensor and external
system data so as to realize a
system design expected function; the at least one resident application is used for synthesizing the abnormal state of the whole aircraft based on the feedback data of each
processing unit and the sensor data, then giving out comprehensive judgment and feeding back possible hidden faults; wherein the
system is composed of the sensor, the
processing unit and the resident application according to the complexity of cross-linking of the aircraft system. According to the invention, the problem that the existing hidden fault of the
airplane is difficult to position and troubleshoot is solved, so that the hidden fault of the
airplane is quickly positioned and troubleshot.