The present invention relates to auxiliary power generator systems for an aircraft. More particular, the present invention relates to an auxiliary power system with a new architecture that include an essential auxiliary power unit (APU) with dual and fully redundant starter and electrical power generation systems that can connect independently to a normal electric network or an emergency electric network of an aircraft. In addition, the present invention also relates to an aircraft comprising said auxiliary power system and a method for supplying electric power to an aircraft by means of said system.


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    Title :

    AUXILIARY POWER SYSTEM


    Additional title:

    HILFSSTROMSYSTEM
    SYSTÈME D'ALIMENTATION AUXILIAIRE



    Publication date :

    2025-07-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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