An adaptive aircraft (102) electrical power distribution system includes an aircraft power source (106), a power connector (108), an aircraft power distribution bus (112), and a bidirectional power controller (114). The aircraft power source (106) is operable to generate and supply electrical power. The power connector (108) is mounted on a fuselage (104) of the aircraft (102). The aircraft power distribution bus (112) is operable to distribute electrical power to an aircraft (102) electrical load. The bidirectional power controller (114) is mounted in the aircraft (102) and is electrically coupled to the aircraft power source (106), the aircraft power connector (108), and the aircraft power distribution bus (112). The bidirectional power controller (114) is configured to:sense when the aircraft power source (106) is generating and supplying electrical power, sense when electrical power is being supplied to the power connector (108) from an external power source (202), and selectively couple at least one of the aircraft power source (106) or the power connector (108) to the aircraft (102) power distribution system.


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    Titel :

    ADAPTIVE AIRCRAFT ELECTRICAL POWER DISTRIBUTION SYSTEM


    Weitere Titelangaben:

    ADAPTIVES STROMVERTEILUNGSSYSTEM FÜR FLUGZEUGE
    SYSTÈME ADAPTATIF DE DISTRIBUTION D'ÉNERGIE ÉLECTRIQUE D'AÉRONEF


    Beteiligte:

    Erscheinungsdatum :

    11.09.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung



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