A method for controlling power in an aircraft (10) includes monitoring an electric energy storage module (112) electrically connected to an electrical bus (110) for an exceedance of a first current limit and monitoring a generator module (108) connected to the electrical bus (110) for an exceedance of a second current limit. If the current limit of either of the electric energy storage module (112) or the generator module (108) is exceeded by a predetermined exceedance amount, the method includes reducing a power consumption for an electric machine (104) by a predetermined bias until the exceedance of the electrical energy storage module (112) and the exceedance of the generator module (108) are both less than or equal to zero.


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    Title :

    NESTED CONTROL LOOP STRUCTURE FOR HYBRID PROPULSION SYSTEM


    Additional title:

    VERSCHACHTELTE REGELKREISSTRUKTUR FÜR HYBRIDANTRIEBSSYSTEM
    STRUCTURE DE BOUCLE DE CONTRÔLE IMBRIQUÉE POUR SYSTÈME DE PROPULSION HYBRIDE


    Contributors:

    Publication date :

    2023-02-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / B60W CONJOINT CONTROL OF VEHICLE SUB-UNITS OF DIFFERENT TYPE OR DIFFERENT FUNCTION , Gemeinsame Steuerung oder Regelung von Fahrzeug-Unteraggregaten verschiedenen Typs oder verschiedener Funktion / B64U



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