Heat exchanger for aircraft engine
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United States of America Patent
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Aug 15, 2017
Grant Date -
Sep 24, 2015
app pub date -
Jun 9, 2015
filing date -
Jun 26, 2013
priority date (Note) -
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Abstract
A heat exchanger for an aircraft engine includes: a body including a plate-like first member and a plate-like second member that are stacked in a thickness direction of the first and second members and joined together, and a channel which is defined in the body and in which the cooling target fluid flows; and a corrugated fin plate disposed in the channel in the body. The body is bent along a curved surface to which the heat exchanger is attached. A plurality of heat dissipation fins stand on an outer surface of at least one of the first member or the second member.
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