Torque transmission device with reduced friction
AssigneeSafran Aircraft Engines
InventorsStéphane Pierre Guillaume BLANCHARD, Helene Myriam CONDAT, Nicolas Xavier TRAPPIER, Laurent Paul François PERROT
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AssigneeSafran Aircraft Engines
InventorsStéphane Pierre Guillaume BLANCHARD, Helene Myriam CONDAT, Nicolas Xavier TRAPPIER, Laurent Paul François PERROT
Estimating the term…
The invention relates to a turbomachine comprising a low-pressure shaft (27) configured to drive a fan shaft (32) in rotation by means of a coupling assembly comprising a first shaft (1) on which are formed a plurality of first axial grooves (7), a second shaft (2) on which are formed a plurality of second axial grooves (12), and a coupling device (4) including a plurality of rolling elements (13) and an annular cage (14) positioned between the first shaft (1) and the second shaft (2), the rolling elements (13) being positioned between one of the first axial grooves (7) and one of the second axial grooves (12) to couple in rotation the first and the second shaft (1, 2), each first and second groove (7, 12) having a first (16) and a second (17) substantially planar surface inclined with respect to one another and extending along the axis.
-11. (canceled)
A turbomachine including a casing (35), a low-pressure shaft (27) mounted in rotation in the casing (35), a fan shaft (32) mounted in rotation relative to the casing (35) and a coupling assembly, the low-pressure shaft (27) being configured to drive the fan shaft (32) in rotation by means of the coupling assembly, the coupling assembly including:
Dependencies are inferred from the claim text.