An electronic controller (200) for an engine (100) and a propeller (120) comprises a first channel (A) and a second channel (B) independent from and redundant to the first channel (A). Each channel (A, B) having a control processor (212, 222) configured to receive first engine and propeller parameters and to output, based on the first engine and propeller parameters, at least one engine control command comprising instructions for controlling an operation of the engine (100) and at least one propeller control command comprising instructions for controlling an operation of the propeller (120). Each channel (A, B) also comprises a protection processor (214, 224) configured to receive second engine and propeller parameters and to output, based on the second engine and propeller parameters, at least one engine protection command comprising instructions for protecting the engine (100) from hazardous conditions and at least one propeller protection command comprising instructions for protecting the propeller (120) from hazardous conditions.


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    Title :

    INTEGRAL PROPELLER AND ENGINE CONTROLLER


    Additional title:

    INTEGRIERTE PROPELLER- UND MOTORSTEUERUNG
    ORGANE DE COMMANDE INTÉGRAL D'HÉLICE ET DE MOTEUR


    Contributors:
    CHAHAL JASRAJ (author) / DUKE BRANT (author) / LISIO CARMINE (author) / JARVO JIM (author) / ZINGARO GIANCARLO (author)

    Publication date :

    2021-07-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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