On-board power supply network of an electrically propelled aircraft

A system for supplying electrical energy to at least one electrical load of an aircraft, this system including a main source of electrical energy connected to at least one electrical load through an electrical network, the system including a control device connected to the main source of electrical...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Abdellatif, Meriem, Salanne, Jean-Philippe Hervé, Petibon, Stephane, Rougier, Florent, Meunier, René
Format: Patent
Sprache:eng
Schlagworte:
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Beschreibung
Zusammenfassung:A system for supplying electrical energy to at least one electrical load of an aircraft, this system including a main source of electrical energy connected to at least one electrical load through an electrical network, the system including a control device connected to the main source of electrical energy and configured to deliver a variable voltage level on the electrical network based on a predetermined voltage variation law depending on at least one parameter characterizing the altitude of the aircraft and according to the Paschen law with a predefined margin.