Patent ID: 11959400
Assignee: SAFRAN AIRCRAFT ENGINES
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC B  F  Y | IPC F

Claim 10:
11. The fan rotor according to claim 1, wherein the cell is provided with flanks, wherein the flanks of the cell comprise an downstream end provided with two downstream slots, wherein a downstream axial retention lock of the blade root, formed from a plate, is inserted into the two downstream slots provided at the downstream end of the flanks of said cell for receiving the blade root, these two downstream slots being arranged in a V, wherein the downstream lock is drilled with an orifice for receiving a downstream end of said wedge and wherein the downstream retention lock has, on the inner face of the downstream retention lock, a surface forming an axial abutment for a downstream end of said stressing rod.