Heat exchanger for a turbo engine
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United States of America Patent
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Jan 9, 2018
Issued Date -
N/A
app pub date -
Dec 19, 2014
filing date -
Dec 23, 2013
priority date (Note) -
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Abstract
The invention relates to a heat exchanger of an air circulation channel of a turbomachine, the heat exchanger being configured so as to have fluid to be cooled passing through it and including a plurality of fins protruding from a support surface, the heat exchanger being characterized in that each fin includes a base and a preferably continuous leading face which extends axially from the base in the air circulation direction while tapering from upstream to downstream along an axis parallel with the support surface.
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