Aircraft electric power distribution systems and methods 80 of operating aircraft electrical power distribution systems are provided. One such method 80 comprises determining a measure of an electrical power demand of a power and propulsion system 300 of the aircraft; setting a target operating voltage of the aircraft electrical power distribution system based at least in part on the measure of the electrical power demand; and controlling the operating voltage in accordance with the set target operating voltage. In some embodiments the measure of the electrical power is a measure of an operating parameter of a gas turbine engine 101, 201 or propulsor 204 of the aircraft. The operating parameter may include one or more of: a speed of an airflow through the gas turbine engine 101, 201 or propulsor 204; a rotational speed of a spool of the gas turbine engine 101, 201 or propulsor 204; a rate of fuel flow into a combustor of the gas turbine engine 101, 201; a pressure in the gas turbine engine 101, 201 or propulsor 204; and a temperature in the gas turbine engine 101, 201 or propulsor 204.


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    Title :

    AIRCRAFT ELECTRICAL POWER DISTRIBUTION


    Additional title:

    ELEKTRISCHE ENERGIEVERTEILUNG EINES FLUGZEUGS
    DISTRIBUTION D'ÉNERGIE ÉLECTRIQUE D'UN AÉRONEF


    Contributors:

    Publication date :

    2022-10-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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