A turbine engine heat exchanger has: a manifold having a first face and a second face opposite the first face; a plurality of first plates along the first face, each first plate having an interior passageway; and a plurality of second plates along the second face, each second plate having an interior passageway. A first flowpath passing through the interior passageways of the first plates, the manifold, and the interior passageways of the second plates.
Aircraft Heat Exchangers
2021-07-22
Patent
Electronic Resource
English
Improving the Efficiency of Aircraft Heat Exchangers
Springer Verlag | 2020
|Repair and overhaul of aircraft heat exchangers
Online Contents | 1996
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