Heat exchanger of a turbomachine
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United States of America Patent
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Sep 4, 2018
Grant Date -
Jul 30, 2015
app pub date -
Jan 26, 2015
filing date -
Jan 29, 2014
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Abstract
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, is provided. The heat exchanger includes 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 includes a leading edge and a trailing edge. Each fin further includes 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.
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