A method for checking the maximum power available to members of a propulsion system of an aircraft includes first members that are sized to compensate for the failure of second members of the propulsion system by delivering a maximum power to keep the aircraft in a safe operating range. The method includes the following steps for each of the first members: placing the first member in a state that is substantially equal to a maximum power state; adjusting the power delivered by the second member working in synergy with the first member so that the first member and the second member contribute to delivering the power required for the aircraft in the flight phase; determining the power delivered by the first member placed in the maximum power state; from the determined power, deducing information relating to the maximum power available to the first member.
PROCEDE DE VERIFICATION DE LA PUISSANCE MAXIMALE DISPONIBLE DE DIFFERENTS ORGANES D' UNE CHAINE PROPULSIVE D' UN AERONEF
METHOD FOR CHECKING THE MAXIMUM POWER AVAILABLE TO DIFFERENT MEMBERS OF A PROPULSION CHAIN OF AN AIRCRAFT
VERFAHREN ZUR PRÜFUNG DER MAXIMALEN LEISTUNG, DIE VERSCHIEDENEN ELEMENTEN EINER ANTRIEBSKETTE EINES FLUGZEUGS ZUR VERFÜGUNG GESTELLT WIRD
2024-10-16
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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