A system includes a thermal engine (102) operatively connected to drive a propeller (104). An electric motor (106) is operatively connected to the thermal engine (102) to drive the propeller (104) together with the thermal engine (102). An external input system (114) is configured to accept input and output a thrust command. A protection function module (116) is configured to enforce limits on the thermal engine (102), electric motor (106), and propeller (104). A low select module (118) is operatively connected to receive input from the external input system (114) and form the protection function module (116) and to output the lower of input from the protection function module (116) and external input system (114) to the thermal engine (102), the electric motor (106), and the propeller (104).


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    Title :

    HYBRID ELECTRIC POWERPLANT (HEP) CONTROL ARCHITECTURE


    Additional title:

    STEUERUNGSARCHITEKTUR FÜR HYBRIDES ELEKTRISCHES KRAFTWERK
    ARCHITECTURE DE COMMANDE DE CENTRALE ÉLECTRIQUE HYBRIDE (HEP)


    Contributors:

    Publication date :

    2024-08-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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