| 摘要 |
A device (44) for controlling an exhaust nozzle (32) with variable cross-section of a turbojet engine (20) nacelle (10) of an aircraft, the device (44) comprising a computer (46) suitable for determining a position setpoint of the nozzle (32). The device comprises means for managing the servo control of the position of the variable nozzle (32) as a function of the flow rate of fuel supplying the turbojet engine (20), said management means comprising an instantaneous fuel flow sensor (48) and a management unit (50) which compares the flow rate measured by the flow sensor (48) with a theoretical flow rate, determines a correction value for the nozzle position (32), and corrects the position setpoint of the nozzle (32). |
