EPICYCLIC REDUCTION GEAR FOR A TURBOMACHINE

The invention relates to an epicyclic reduction gear (15) for a turbomachine, comprising: - a sun wheel (16) that is rotatable about a first axis (A); - a ring gear (17) surrounding the sun wheel (16) and being rotatable about the first axis (A); - at least one planetary gear (18) that is rotatable...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	NIEPCERON, Clément, MORELLI, Boris
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINEERING ELEMENTS AND UNITS GAS-TURBINE PLANTS GEARING GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING THERMAL INSULATION IN GENERAL WEAPONS
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Beschreibung
Zusammenfassung:	The invention relates to an epicyclic reduction gear (15) for a turbomachine, comprising: - a sun wheel (16) that is rotatable about a first axis (A); - a ring gear (17) surrounding the sun wheel (16) and being rotatable about the first axis (A); - at least one planetary gear (18) that is rotatable about a second axis (B), the planetary gear (18) being meshed with the sun wheel (16) and the ring gear (17); - an immobile planet carrier (19), the planetary gear (18) being rotatably guided about the second axis (B) with respect to a bearing (29) of the planet carrier (19); - an item of equipment (21) comprising a rotor (22). The invention is characterized in that the item of equipment (21) is fastened to the bearing (29) of the planet carrier (19) and the rotor (22) of the item of equipment (21) is rotatably driven by the planetary gear (18). Réducteur à train épicycloïdal (15) pour une turbomachine comprenant : - un solaire (16) mobile en rotation autour d'un premier axe (A); - une couronne (17) entourant le solaire (16) et mobile en rotation autour du premier axe (A); - au moins un satellite (18) mobile en rotation autour d'un second axe (B), le satellite (18) étant engrené avec le solaire (16) et la couronne (17); - un porte-satellite (19) immobile, le satellite (18) étant guidé en rotation autour du second axe (B) par rapport à un palier (29) du porte-satellite (19); - un équipement (21) comprenant un rotor (22); caractérisé en ce que l'équipement (21) est rapporté sur le palier (29) du porte-satellite (19) et le rotor (22) de l'équipement (21) est entraîné en rotation par le satellite (18).