Bypass turbine engine comprising at least one accessory or equipment

A bypass turbine engine comprising, from upstream to downstream in an axial direction of gas flow, a fan and a splitter nose from which originate a primary stream flow channel, called primary flow path, and a secondary stream flow channel, called secondary flow path, which surrounds the primary flow path, the turbine engine further comprising:

• a fixed casing comprising an arm which extends radially, relative to the longitudinal axis, in the secondary flow path,
• a first shaft, called low pressure shaft, designed to rotate relative to the casing about a longitudinal axis oriented in the axial direction of gas flow,
• a second shaft, called high pressure shaft, designed to rotate relative to the casing around the low pressure shaft, the high pressure and low pressure shafts being concentric,
• at least one accessory designed to be driven by a motor powered with electrical energy,
• an upper portion via which the turbine engine is intended to be attached to an aircraft,
• an opposite lower portion in a vertical direction orthogonal to the longitudinal axis, the arm extending generally vertically, in the lower portion, in the secondary flow path,
• the turbine engine being characterised in that it further comprises:
• a first intermediate shaft designed to draw mechanical power from the low pressure shaft,
• a second intermediate shaft designed to draw mechanical power from the high pressure shaft,
• an electrical energy generator assembly housed in the arm and coupled, on the one hand, to the first intermediate shaft and, on the other hand, to the second intermediate shaft, so as to receive mechanical power from the first intermediate shaft, on the one hand, and from the second intermediate shaft, on the other hand, the generator assembly being further designed to convert the mechanical power received from the first and second intermediate shafts into electrical energy in order to power the motor(s) driving the accessory or accessories, the electrical energy powering the motor(s) driving the accessory or accessories thus originating simultaneously from the mechanical power drawn from the low pressure shaft and the mechanical power drawn from the high pressure shaft.