REDUCTION GEAR FOR TURBOMACHINE EQUIPPED WITH AN ELECTRIC GENERATOR

A mechanical reduction gear for a turbomachine, in particular for an aircraft, including a first sun gear having a central axis forming a main axis of the reduction gear, a ring gear, planet gears, a planet carrier, and at least one electric generator, in which the electric generator has a first set...

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Bibliographische Detailangaben
Hauptverfasser: CHARPENTIER, Bernard Guy Antoine, NIEPCERON, Clément Paul René, MORELLI, Boris Pierre Marcel, RAPPAPORT, Florian
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:A mechanical reduction gear for a turbomachine, in particular for an aircraft, including a first sun gear having a central axis forming a main axis of the reduction gear, a ring gear, planet gears, a planet carrier, and at least one electric generator, in which the electric generator has a first set of electromagnetic elements and a second set of electromagnetic elements, wherein one among the first and second set of electromagnetic elements is a first set of coils, each coil of this first set of coils being wound around a direction parallel to the main axis, and in which the other among the first and second set of electromagnetic elements is configured to induce a current in the first set of coils when it is driven with a relative movement with respect to the first set of coils.