A method of operating a reverse thrust system of an aircraft engine includes receiving a status signal indicative that the aircraft is on-ground or in-flight, and upon detecting that the aircraft is on-ground, overriding a protection module such that the reverse thrust system is operable regardless of the protection module being in an active state or in a disabled state. The protection module causes, absent the overriding, the reverse thrust system to be inoperable when in the active state. An aircraft includes an engine with a reverse thrust system, a thrust control input device configured for generating an input signal indicative of a reverse thrust demand. A sensor is configured for generating at least one status signal indicative of the aircraft being in-flight or on-ground. A control system is electronically connected with the at least one sensor, the thrust control input device and the reverse thrust system.


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    Title :

    REVERSE THRUST SYSTEM AND METHOD


    Additional title:

    SYSTEME ET METHODE D~INVERSION DE POUSSEE


    Contributors:

    Publication date :

    2024-06-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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