A method for authorizing the flight of an aircraft provided with a hybrid power plant having at least one heat engine and at least one electric motor electrically connected to an electrical energy source comprising several electrical accumulators. The method comprises extracting (STP1), while on the ground, an electrical energy or an electrical power to be extracted from the electrical energy source during a predetermined time period and determining (STP2) for the electrical accumulators, respective initial values of an operating parameter, calculating (STP3) an average value from the initial values, determining (STP4) a minimum value from the measured initial values, issuing an authorization when a difference between the average value and the minimum value is less than a threshold and a prohibition when said difference between the average value and the minimum value is greater than or equal to the threshold.
PROCEDE D'AUTORISATION DE VOL D'UN AERONEF AYANT UNE INSTALLATION MOTRICE HYBRIDE MUNIE D'AU MOINS UN MOTEUR ELECTRIQUE ET D'AU MOINS UN MOTEUR THERMIQUE
METHOD FOR AUTHORIZING THE FLIGHT OF AN AIRCRAFT HAVING A HYBRID POWER PLANT PROVIDED WITH AT LEAST ONE ELECTRIC MOTOR AND AT LEAST ONE HEAT ENGINE
VERFAHREN ZUR FLUGAUTORISIERUNG EINES FLUGZEUGS MIT EINER HYBRID-ANTRIEBSANLAGE MIT MINDESTENS EINEM ELEKTROMOTOR UND MINDESTENS EINEM VERBRENNUNGSMOTOR
2025-01-15
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / G01R Messen elektrischer Größen , MEASURING ELECTRIC VARIABLES / H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY |
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