Aircraft comprising at least one deflector configured to divert a gas exhaust cone exiting a propulsion assembly away from a trailing edge of a wing

An aircraft comprising:

• a wing,
• at least one propulsion assembly, and
• for each propulsion assembly, a pylon connecting the propulsion assembly and the wing, each propulsion assembly comprising a thrust reversal device, an engine axis and at least one nozzle which has a trailing edge and an inner face extending to the trailing edge and inclined with respect to the engine axis, the pylon comprising at least right and left lateral fairings positioned on either side of a median plane and at least one secondary rear fairing comprising, offset rearward with respect to the trailing edge of the nozzle, a lower face, an upper face and at least one edge connecting the lower and upper faces, which has a rear end and a point spaced apart from the median plane and aligned with the trailing edge of the nozzle,
• wherein the lower face of the at least one secondary rear fairing forms, with the inner face of the nozzle, an angle of between 2 and 20°, the lower face of the at least one secondary rear fairing and the engine axis forming an angle greater than an angle formed between the inner face of the nozzle and the engine axis, and
• wherein each secondary rear fairing is configured to house at least one piece of equipment of the thrust reversal device and forms a deflector which diverts a gas exhaust cone exiting the at least one propulsion assembly away from a trailing edge of the wing.