IMPROVED INDUCTIVE COMPONENT FOR ELECTRIC OR HYBRID AIRCRAFT

An inductive component comprising an inductive element comprising a stack of an outer plurality of first strips of magnetic material, a central plurality of second strips of superconducting material, and an outer plurality of third strips of magnetic material, the inductive element being flexible an...

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Bibliographische Detailangaben
Hauptverfasser: GALLA, Gowtham, YBANEZ, Ludovic, SURAPANENI, Ravi Kiran, KAPAUN, Florian, STEINER, Gerhard
Format: Patent
Sprache:eng ; fre ; ger
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Beschreibung
Zusammenfassung:An inductive component comprising an inductive element comprising a stack of an outer plurality of first strips of magnetic material, a central plurality of second strips of superconducting material, and an outer plurality of third strips of magnetic material, the inductive element being flexible and configured to form at least one loop of said stack of first strips, second strips and third strips, wound on itself. Also an inductive device and an aircraft with such an inductive component or device.