AIRCRAFT PROVIDED WITH A HEATING SYSTEM FOR A TURBINE ENGINE PLENUM

Aircraft (1) fitted with a turbine engine (10) comprising a gas generator (15), the gas generator (15) comprising a compression assembly (20) supplying air to a combustion chamber (24) as well as a turbine assembly (25) supplied with gas by the combustion chamber (24), the aircraft (1) having a plenum (40) supplying air to the compression assembly (20). The aircraft (1) comprises a heating system (50), the heating system (50) comprising a heat exchanger (60) disposed in the plenum (40), the heating system (50) comprising a supply fluid link (70) and a discharge fluid link (80) connected to the heat exchanger (60), the supply fluid link (70) conveying hot air coming from the turbine engine (10) into the heat exchanger (60).