HEAT EXCHANGER OF A TURBOMACHINE

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...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	GHAZLANE IMANE, SZYDLOWSKI JULIEN, PHILIPPART GABRIELA
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OFGENERAL APPLICATION HEAT EXCHANGE IN GENERAL HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS,IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	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.