Turbine engine with epicyclic reduction gear train
AssigneeSafran Aircraft Engines
InventorsGwenolé Yann Le Pache, Augustin Curlier, Clément Dupays
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AssigneeSafran Aircraft Engines
InventorsGwenolé Yann Le Pache, Augustin Curlier, Clément Dupays
Estimating the term…
A turbine engine, comprising at least one drive shaft having an axis of rotation A and configured to drive a fan wheel by means of an epicyclic reduction gear train, said reduction gear having: a sun gear configured to be driven by said drive shaft about said axis A, a ring gear surrounding the sun gear and configured to drive a fan shaft about said axis A, and an annular row of planet gears interposed between the sun gear and the ring gear and held by a planet carrier fixed to a stator housing of the turbine engine, said turbine engine also having an electrical apparatus with rotor, wherein the stator of the electrical apparatus is fixed to the stator housing by means of an annular member for apparatus support, the annular member comprising legs of an elongated shape that axially traverse the reduction gear, the annular member comprising at longitudinal extremities of the legs a first annular element for fixing to an annular flange integral with the stator housing, and wherein the stator of the apparatus comprises a first annular fixing flange connected integrally to opposed longitudinal extremities of the legs of the annular member.
A turbine engine comprising at least one drive shaft having an axis of rotation A and configured to drive a fan wheel by means of an epicyclic reduction gear train, said reduction gear train having:
Dependencies are inferred from the claim text.