AIRCRAFT TURBOMACHINE COMPRISING A BEARING SUPPORT HAVING AN IMPROVED DESIGN

Abstract: an assembly for aircraft turbomachine, including a stator part, a first bearing, a second bearing and a support part in an oil enclosure delimited by an outer enclosure delimiting portion integral with the stator part, the support part including a first axial end portion forming an outer ring of the first bearing, or supporting such a ring; a second axial end portion forming an outer ring of the second bearing or supporting such a ring, a compression damping oil film being arranged between the second portion and the stator part; an intermediate ring, arranged axially between the first and second portions, and forming a flexible connection as well as an oil-spray protection element.

Inventor(s): Alexandre DEBAT, Antoine Bernard CHRISTOPHE, Olivier ROBERT, Sébastien Mathieu COMBEBIAS

CPC Classification: F01D25/164 ({Flexible supports; Vibration damping means associated with the bearing})

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