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
22.07.2021
Patent
Elektronische Ressource
Englisch
Repair and overhaul of aircraft heat exchangers
Online Contents | 1996
|Repair and overhaul of aircraft heat exchangers
Emerald Group Publishing | 1996
|