The invention relates to an electric propulsion unit for an aircraft comprising at least one first propulsion member, a second propulsion member and a single electric motor configured to drive the first propulsion member and the second propulsion member in a counter-rotating manner, the electric motor comprising a peripheral stator element comprising a first peripheral stage and a second peripheral stage which are offset along an axis, the first peripheral stage comprising at least a first phase, a second phase and a third phase which are alternated according to a first sequence in such a way as to allow a rotation of the first rotor element in the first direction of rotation, the second peripheral stage comprising phases which are alternated according to a second sequence in such a way as to allow a counter-rotating rotation of the second rotor element.
PROPULSEUR ÉLECTRIQUE POUR AÉRONEF ET PROCÉDÉ D'UTILISATION D'UN TEL PROPULSEUR
ELECTRIC PROPULSION UNIT FOR AN AIRCRAFT AND METHOD FOR USING SUCH A PROPULSION UNIT
ELEKTRISCHE ANTRIEBSEINHEIT FÜR EIN FLUGZEUG UND VERFAHREN ZUR VERWENDUNG EINER SOLCHEN ANTRIEBSEINHEIT
19.07.2023
Patent
Elektronische Ressource
Französisch
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