Abstract: The present invention relates to an aircraft comprising a cooling system integrated into the fuselage, and at least one propeller driven by an electric motor adapted to propel the aircraft, the cooling system comprising: at least one cooling duct (or air duct), installed inside the fuselage of the aircraft, provided with an air inlet and an air outlet, the cooling duct being designed to allow air to flow between the air inlet and the air outlet; at least one heat exchanger positioned inside the cooling duct, the heat exchanger being designed to transfer thermal energy to the air flowing in the cooling duct; wherein the air inlet is positioned in an area of overpressure generated by the air accelerated by the rotation of the propeller, and the air outlet is strategically positioned on an outer surface of the fuselage passed over by the air flow accelerated by the rotation of the propeller, generating an area of lower pressure facilitating the flow of air through the cooling duct, thereby allowing efficient

Abstract: The invention relates to a piece of equipment (1) of a system for transmitting data remotely in accordance with a wireless communication standard, comprising a processing unit (50) coupled to a radio front-end unit (20) which provides bi-directional radio frequency communication with a piece of remote equipment, the radio front-end unit comprising an analogue block (30) and a digital block (40) which exchange digital waveform samples. The processing unit (50) includes a synchronisation module (52) configured to initiate the exchange with the remote equipment of synchronisation messages selected from messages of the wireless communication standard. The digital block (40) comprises 10 an identification module (43) configured to detect and date the synchronisation messages exchanged with the remote equipment.