A method for assisting piloting beyond an altitude that can be reached with only the capabilities of a thermal power plant of a rotorcraft, by supplying power from an electrical power plant. After defining a take-off point of the rotorcraft and a target point, and their respective altitudes, a determination of a first maximum altitude that can be reached by the rotorcraft using only the thermal power plant is carried out according to a first altitude law. Then, an estimate of a second maximum altitude that can be reached by the rotorcraft using the thermal power plant and the electrical power plant jointly driving each rotor of the rotorcraft is made according to a second altitude law. If the second maximum altitude is higher than the altitude of the target point, the rotorcraft can fly to the target point.
PROCEDE D AIDE AU PILOTAGE D'UN GIRAVION EN HAUTES ALTITUDES GRACE A L'APPORT D'UNE PUISSANCE MECANIQUE PROVENANT D'UNE INSTALLATION MOTRICE ELECTRIQUE
METHOD FOR ASSISTED PILOTING OF A ROTORCRAFT AT HIGH ALTITUDES THROUGH DELIVERY OF MECHANICAL POWER FROM AN ELECTRIC POWER PLANT
VERFAHREN ZUR UNTERSTÜTZUNG DER STEUERUNG EINES DREHFLÜGELFLUGZEUGS IN HOHEN HÖHEN DANK EINER MECHANISCHEN LEISTUNG, DIE AUS EINER ELEKTRISCHEN MOTORANLAGE STAMMT
2023-09-06
Patent
Electronic Resource
French
IPC: | G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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