Heat exchanger assembly
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United States of America Patent
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Nov 7, 2017
Issued Date -
N/A
app pub date -
Aug 14, 2015
filing date -
Oct 21, 2014
priority date (Note) -
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status (Latency Note)
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Abstract
A heat exchanger assembly for a gas turbine engine including a frame, including a non-planar outer wall, a non-planar inner wall spaced radially inward from the non-planar outer wall to form a frame cavity therebetween, an inlet side extending between the non-planar outer wall and the non-planar inner wall, an inlet passage extending through the inlet side, an outlet side extending between the non-planar outer wall and the non-planar inner wall opposite the inlet side; an outlet passage extending through the outlet side, and a continuous non-planar core disposed within the frame cavity and in flow communication with the inlet passage and the outlet passage.
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