The invention relates to an inductive element (100) characterized in that it comprises a stack of at least one first strip (107a) of magnetic material, at least one second strip (105) of superconducting material, and at least one third strip (107b) of magnetic material.It is thus advantageously possible to obtain an increased ratio between the weight of an aircraft comprising inductive elements such said inductive element (100) and the electrical power available on board for the aircraft systems.
IMPROVED INDUCTIVE COMPONENT FOR ELECTRIC OR HYBRID AIRCRAFT
VERBESSERTE INDUKTIVE KOMPONENTE FÜR ELEKTRO- ODER HYBRIDFLUGZEUG
COMPOSANT INDUCTIF AMÉLIORÉ POUR AÉRONEF ÉLECTRIQUES OU HYBRIDE
2024-01-03
Patent
Electronic Resource
English