System for deicing an aircraft turbine engine inlet cone
The invention relates to a system for deicing an aircraft turbine engine inlet cone comprising air-diffusing means 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 for removing pressurizing air from at le...
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| Format: | Patent |
| Sprache: | eng |
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| Zusammenfassung: | The invention relates to a system for deicing an aircraft turbine engine inlet cone comprising air-diffusing means 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 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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