Method for monitoring the spark plugs of a turboshaft engine using a vibration measurement
Abstract:
A method for monitoring an aircraft turboshaft engine including a vibration sensor capable of outputting a vibration signal and a spark plug. The method includes, based on the vibration signal output by the vibration sensor, a step of determining a level of vibration of the turboshaft engine as well as a step of determining an indicator of spark plug wear.
Information query
Patent Agency Ranking
0/0