In accordance with at least one aspect of this disclosure, an emergency power unit system for an aircraft includes, a fuel cell system (102) configured to generate power using a fuel and an oxidizer and to supply electrical power to an aircraft electrical bus in at least a fuel cell operational mode. An electrical storage (130) is operatively connected to the aircraft electrical bus (110) and directly connected to the fuel cell system to provide electrical power to the aircraft electrical bus and to the fuel cell system in a fuel cell start up mode.
EMERGENCY POWER UNITS
NOTSTROMVERSORGUNGSEINHEITEN
UNITÉS D'ALIMENTATION DE SECOURS
2024-07-31
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |