An aircraft electric actuator drive apparatus (40, 50) has an electric actuator (41, 51) and a secondary power supply device (27, 27A). The electric actuator is driven using electric power from a main power unit (21, 22) provided in an aircraft (100). The secondary power supply device can temporarily supply electric power to the electric actuator while electric power from the main power unit is applied to the electric actuator.
Aircraft electric actuator drive apparatus
Elektrische Flugzeug-Aktuatorantriebsvorrichtung
Dispositif d'entraînement d'actionneur électrique d'avion
2018-05-30
Patent
Electronic Resource
English
AIRCRAFT ACTUATOR, AIRCRAFT ACTUATOR DRIVE METHOD, AND AIRCRAFT ACTUATOR SYSTEM
European Patent Office | 2020
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