TURBOJET INCLUDING A CURRENT GENERATOR MOUNTED IN THE FAN AND A PROCESS FOR MOUNTING THE SAID GENERATOR IN THE FAN

摘要

The invention relates to a turbojet engine with double-body gas turbine, comprising a high pressure rotor (1) and a low pressure rotor, the low rotor shaft pressure (2) being connected, at its upstream end, to a fan (10) housed in a fan casing (14), characterized in that it comprises, upstream of the blower (10), a fixed hood member (12) centered on the motor shaft (X3), on which is mounted an electric power generator (20) arranged for take the mechanical power of the low pressure rotor shaft (2) and the convert to electrical power.