| 摘要 |
The invention pertains to a method for monitoring an aircraft engine retractable doors thrust reverser, the thrust reverser being a reverser having hydraulic actuators and being provided with contactors (3a, 4a, 5a, 3B, 4b, 5b, Sa, Sb) arranged so as to each return an item of information about the position of the doors, the engine comprising a computer (3) configured to carry out measurements (E1) of a parameter representative of the position of the contactors on the basis of the information returned by the contactors, characterized in that it comprises a calculation (E2) of one or more statistical indicators of the parameter measured and an analysis (E3) of the temporal evolution of the statistical indicator or indicators calculated. The invention extends also to a computer program for the implementation of this method. |
