| 摘要 |
The invention relates to the heating of a piece of aeronautic equipment intended to be arranged at the skin of the aircraft. The equipment 25 comprises a part 30, 31 intended to be arranged at the skin 27 of the aircraft and means for heating the part. The heating means comprise a thermodynamic loop comprising a closed circuit in which a heat transfer fluid circulates. The closed circuit comprises an evaporator 14 and a zone in which a condensation of the heat transfer fluid can occur in the appendage to heat it. Outside the evaporator 14, the circuit in which the fluid circulates is formed by a tubular channel with an empty section. At least part of the equipment is made from a material with a low heat conductivity. |
