| 摘要 |
<p>The invention relates to a heat exchanger for an air circulation channel of a turbomachine, with the heat exchanger being configured to be passed through by a fluid to be cooled and comprises a plurality of fins protruding with respect to a support surface, each fin extends axially over a length in the direction of the circulation of air and comprises a leading edge and a trailing edge, with the heat exchanger characterised in that each fin further comprises a central body, between the leading edge and the trailing edge, with the central body having in a plane parallel to the support surface a curved central profile.</p> |
