An aircraft pylon including a heat exchange device having a heat exchanger which includes a first circuit portion ducting a flow of hot air tapped off an engine of the aircraft and a second circuit portion ducting a flow of cold air, the first and second circuit portions of the heat exchanger being coaxial, separated by at least one partition forming an exchange surface, and positioned, at least partially, in the primary structure of the pylon.
AIRCRAFT PYLON COMPRISING A COAXIAL HEAT EXCHANGER
2019-07-25
Patent
Elektronische Ressource
Englisch