Safran Aircraft Engines

Alexis Thomas Chaboud

Thomas Alain De Gaillard

Alexandre Bernard Marie Boisson

Rémi Roland Robert Mercier

Alexandre Michel Henri Hasquenoph

Guillaume Maurice René Patin

A disc able to support platforms and blades of a fan, and including an external surface having a succession of grooves for receiving the fan blades and teeth interposed between the grooves to support the fan platforms, an upstream face of the disc, and a plurality of radial protrusions disposed radially around the axis of the disc on the upstream face of the disc, and able to be fastened to a fan platform retaining flange, the protrusions being offset radially toward the interior of the disc relative to the grooves of the disc, and being disposed circumferentially between two teeth of the disc.

Turbmachine fan disc

The invention relates to an assembly for a turbine engine extending about a longitudinal axis, comprising: a nose cone () comprising a conical body () extending about the longitudinal axis and a flange () comprising a first contact surface () forming an extension of an inner surface () of the conical body (); a front shroud () comprising an overall annular body () extending about the longitudinal axis and a flange () comprising a first contact surface () forming an extension of an outer surface () of the annular body (), the first contact surface () of the nose cone () being in contact with the first contact surface () of the front shroud (), the first contact surfaces () of the nose cone () and the front shroud () being tilted in the downstream direction towards the longitudinal axis, so that the flange () of the nose cone () is secured to the flange () of the front shroud (); and attachment elements () configured to clamp the first contact surface () of the flange () of the nose cone () against the first contact surface () of the flange () of the front shroud ().

Growing community of inventors

Moissy-Cramayel, France

Alexis Thomas Chaboud