| 摘要 |
The invention relates to a monitoring system (22) characterized in that it comprises - detectors (30) for detecting the state of a turbojet thrust reverser, - a monitoring computer (24), - a device (26) for controlling the reverser monitored by the computer as a function of the information from the detectors provided to the computer by way of the control device, - a device (28) for regulating the turbojet monitored by the computer as a function of the information from the detectors provided to the computer by way of the control device. The invention also relates to a monitoring method applied to this monitoring system. |
