An electrical power system (100) for regenerative loads may include a DC bus (110,160) and an electrical actuator load (112,162), where back-driving the electrical actuator load (112,162) generates regenerative electrical energy, and where the electrical actuator load (112,162) is configured to transmit the regenerative electrical energy to the DC bus (110,160). The system may also include at least one additional load (114,164), where at least a portion of the regenerative electrical energy is transmitted to the at least one additional load (114,164).
POWER SYSTEM ARCHITECTURE FOR AIRCRAFT WITH ELECTRICAL ACTUATION
LEISTUNGSSYSTEMARCHITEKTUR FÜR FLUGZEUGE MIT ELEKTRISCHER BETÄTIGUNG
ARCHITECTURE DE SYSTÈME D'ALIMENTATION POUR AÉRONEF À ACTIONNEMENT ÉLECTRIQUE
2020-10-14
Patent
Elektronische Ressource
Englisch
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