Heat exchanger for aircraft application
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United States of America Patent
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Oct 13, 2015
Grant Date -
Oct 2, 2014
app pub date -
Apr 2, 2013
filing date -
Apr 2, 2013
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Abstract
A heat exchanger includes a plurality of mini-channel tubes. The mini-channel tubes extends for an axial length defined between two manifolds. The mini-channel tubes include a plurality of generally rectangular flow passages. The generally rectangular flow passages are aligned adjacent to each other to define a lateral dimension. A first lateral width of the generally rectangular passages is defined with a ratio of the axial length to the first lateral width being between 201.3 and 215.3. An aircraft system is also disclosed.
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