| 摘要 |
The invention relates to a system ( 2 ) for deicing an aircraft turbine engine inlet cone ( 4 ) comprising air-diffusing means ( 18 ) intended to equip the inlet cone of the turbine engine so as to deliver hot air thereto. According to the invention, it also comprises a circuit ( 20 ) for removing pressurizing air from at least one bearing enclosure of the turbine engine, this circuit communicating with the air-diffusing means in order to be able to supply the latter with hot air.
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