| 摘要 |
The present invention relates to a nacelle (1) of a turbine engine (2) comprising at least one external cowling (3) defining an external aerodynamic surface and at least one internal cowling (4) defining an internal aerodynamic flow surface, these surfaces being connected upstream by a leading edge wall which forms an air inlet lip (6), said turbine engine nacelle comprising at least one heat exchanger (10) associated with at least one flow duct (13) forming at least one recirculation loop through the exchanger and comprising at least one circulation zone (13a) extending at least partially along the external cowling in contact with at least one wall of said external cowling so as to allow exchange of heat by conduction with the air outside the nacelle. |
