Rotor disk comprising a variable thickness web
AssigneeSafran Aircraft Engines
InventorsEmilie Pouzet, Didier Desire Rene Pasquiet
Life of this patent
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AssigneeSafran Aircraft Engines
InventorsEmilie Pouzet, Didier Desire Rene Pasquiet
Estimating the term…
A disk of a rotor including an annular radial web, a radially central hub located at the inner radial end of the web and a rim located at the outer radial end of the web, the web including an upstream face and a downstream face, and a plurality of orifices through which bolts pass for the attachment of at least one annular flange forming part of another adjacent rotor disk on either the upstream face or the downstream face of the web, or on both faces. The upstream face and/or the downstream face of the web includes a globally annular shaped indentation, with a bottom set back along the axial direction inwards into the web, and that extends radially outwards from the hub of the disk towards the rim, and that surrounds a radially inner part of each of the orifices of the web, at a distance.
A disk of a rotor comprising, relative to a principal axis of the disk:
Dependencies are inferred from the claim text.