Systems and methods are disclosed for providing flexible, scalable, and controllable electrical power to an aircraft. In some embodiments, a modular power unit comprises a container containing a power generation unit, a control system, a conditioning system, and an environmental control system. The power generation unit produces a generated power. The control system provides control signals to the power generation unit and controls at least one parameter of the generated power. The conditioning system receives and conditions the generated power and provides an output power to the power bus of the aircraft. The environmental control system provides a temperature regulating fluid to the power generation unit.


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    Titel :

    Modular power units for aircraft


    Beteiligte:
    LONG STEPHEN (Autor:in) / BEVIS DWAYNE (Autor:in) / GUITAR SEAN (Autor:in)

    Erscheinungsdatum :

    18.04.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02B BOARDS, SUBSTATIONS, OR SWITCHING ARRANGEMENTS FOR THE SUPPLY OR DISTRIBUTION OF ELECTRIC POWER , Schalttafeln, Unterstationen oder Schaltanordnungen für die Abgabe oder Verteilung elektrischer Energie



    MODULAR POWER UNITS FOR AIRCRAFT

    LONG STEPHEN / BEVIS DWAYNE / GUITAR SEAN | Europäisches Patentamt | 2020

    Freier Zugriff

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    Aircraft Power Transfer Units

    Wise, C. | Emerald Group Publishing | 1975


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    Wise, C. | Tema Archiv | 1975


    Power units for future aircraft

    Banks, F.R. | Engineering Index Backfile | 1946