An electrical power system for regenerative loads can include a DC bus and an electrical actuator load, wherein back-driving the electrical actuator load generates regenerative electrical energy. The electrical actuator load is configured to transmit the regenerative electrical energy to the DC bus. The system can also include at least one additional load, wherein at least a part of the regenerative electrical energy is transmitted to at least one additional load.

    재생 부하들을 위한 전력 시스템은, DC 버스, 및, 전기 작동 부하를 포함할 수 있고, 이 경우 전기 작동 부하를 역구동하는 것은 재생 전기 에너지를 발생시키고, 전기 작동 부하는 재생 전기 에너지를 DC 버스에게 전송하도록 구성된다. 상기 시스템은 또한 적어도 하나의 추가 부하를 포함할 수 있고, 이 경우 재생 전기 에너지의 적어도 일부가 적어도 하나의 추가 부하에 전송된다.


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    Titel :

    POWER SYSTEM ARCHITECTURE FOR AIRCRAFT WITH ELECTRICAL ACTUATION


    Weitere Titelangaben:

    전기 작동기를 갖는 항공기를 위한 전력 시스템 아키텍쳐


    Beteiligte:

    Erscheinungsdatum :

    17.06.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung / H02P CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS , Steuern oder Regeln von elektrischen Motoren, elektrischen Generatoren, dynamoelektrischen Umformern



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