| 发明名称 |
NON CONDUCTING MATERIAL |
| 摘要 |
A heating of a piece of aeronautic equipment intended to be arranged at the skin of the aircraft. The equipment (25) includes a part (30, 31) intended to be arranged at the skin (27) of the aircraft and elements for heating the part. The heating element include a thermodynamic loop including a closed circuit in which a heat transfer fluid circulates, the closed circuit including 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. |
| 申请公布号 |
US2017029120(A1) |
申请公布日期 |
2017.02.02 |
| 申请号 |
US201615220417 |
申请日期 |
2016.07.27 |
| 申请人 |
THALES |
发明人 |
HODOT Romain;SARNO Claude;MARTIN Frederic;PINEAU Jean-Philippe |
| 分类号 |
B64D15/06;F28D15/04;B33Y80/00;B33Y10/00;B33Y50/02;B64F5/00;F28D15/02 |
主分类号 |
B64D15/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A piece of aeronautic equipment intended to equip an aircraft, the equipment comprising at least one part intended to be arranged at a skin of the aircraft and means for heating the part, characterized in that the heating means comprise a thermodynamic loop comprising a closed circuit in which a heat transfer fluid circulates, the closed circuit comprising an evaporator and a zone in which a condensation of the heat transfer fluid can occur in the appendage to heat it, and in that outside the evaporator, the circuit in which the fluid circulates is formed by a tubular channel with an empty section, and in that at least this part of the equipment is made from a material with a low heat conductivity. |
| 地址 |
Courbevoie FR |
