Turbomachine output bearing support
AssigneeSafran Aircraft Engines
InventorsNicolas Ovaere, Fabien Stéphane Garnier, Arnaud Lasantha Genilier, Pierre Jean-Baptiste Metge
Life of this patent
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Abstract
Turbomachine output bearing support extending according to an axial direction, said support being formed by one and the same piece and comprising an annular inner wall having an inner side and an outer side, an annular outer wall and a twist support.
Claims8
A turbomachine output bearing support extending according to an axial direction, said support being formed by one and the same piece and comprising an annular inner wall and having an inner side and an outer side, an annular outer wall arranged to the outer side of the inner wall, and a twist support, the inner wall comprising a first section having a first substantially frustoconical form extending according to the axial direction and having the inner side and the outer side, the first section having a first axial end provided with a first attachment flange and a second axial end opposite according to the axial direction to the first axial end, provided with a bearing support section, the first section carrying on the inner side an inner section forming a second attachment flange, the twist support being carried by the inner wall on the outer side.
Dependencies are inferred from the claim text.