REDUCTION GEAR HAVING AN EPICYCLIC GEAR TRAIN FOR A TURBINE ENGINE

A reduction gear having an epicyclic gear train for a turbine engine, in particular of an aircraft, comprising: a planetary shaft having an axis of rotation A; a ring gear having an axis A extending around said planetary shaft; planet gears distributed around said axis A, which mesh with said ring g...

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Hauptverfasser: Mouton, Clémentine Charlotte Marie, Lao, Jérémy Phorla, Patsouris, Emmanuel Pierre Dimitri, Nguyen Van, Thomas Julien, Belmonte, Olivier
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creator Mouton, Clémentine Charlotte Marie
Lao, Jérémy Phorla
Patsouris, Emmanuel Pierre Dimitri
Nguyen Van, Thomas Julien
Belmonte, Olivier
description A reduction gear having an epicyclic gear train for a turbine engine, in particular of an aircraft, comprising: a planetary shaft having an axis of rotation A; a ring gear having an axis A extending around said planetary shaft; planet gears distributed around said axis A, which mesh with said ring gear and the planetary shaft; and a planet carrier including members for supporting bearings of the planet gears, having axes of rotation B, which are evenly distributed around the axis A, as well as a part holding each supporting member substantially by the middle thereof along the axis B thereof, wherein said supporting members are made as a single part having means for supplying lubricating oil to said bearings. A method for assembling said reduction gear is also provided.
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subjects BLASTING
ENGINEERING ELEMENTS AND UNITS
GEARING
GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS
HEATING
LIGHTING
MECHANICAL ENGINEERING
THERMAL INSULATION IN GENERAL
WEAPONS
title REDUCTION GEAR HAVING AN EPICYCLIC GEAR TRAIN FOR A TURBINE ENGINE
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