Turbomachine comprising an alternator between two counter-rotating elements

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United States of America Patent

PATENT NO 11041400
APP PUB NO 20200191010A1
SERIAL NO

16709990

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Abstract

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A geared turbomachine includes: a fan, a low pressure shaft which drives the fan rotationally around the main axis of the turbomachine, a speed reducer interposed between the fan and the low pressure shaft, and an alternator driven by the low pressure shaft. The alternator includes an inductor and an armature of which one of the inductor and the armature is integral with the fan and the other of the inductor and the armature is integral with the low pressure shaft.

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Patent Owner(s)

Patent OwnerAddress
SAFRAN AIRCRAFT ENGINESPARIS

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Becoulet, Julien Fabien Patrick Moissy-Cramayel, FR 39 88
Tan-Kim, Alexandre Jean-Marie Moissy-Cramayel, FR 13 24

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