A heat exchange device to be positioned in an aircraft pylon and including a heat exchanger and an obturator to adopt a closed state where it prevents flow of air from flowing through the heat exchanger, and more- or less-permissive states where it allows flow of air to flow with a higher or lower flow rate. The obturator includes slats each including a pivot axis, the pivot axes of the various slats being mutually parallel and intersecting the direction of the flow of air, the slats being simultaneously mobile in rotation about their pivot axis between a closed position in which the slats are contiguous, which corresponds to the closed state of the obturator, and an open position in which the slats are spread apart, which corresponds to the permissive state of the obturator.
DISPOSITIF D'ECHANGE THERMIQUE COMPACT INCORPORE DANS UN MAT D'AERONEF
COMPACT HEAT-EXCHANGE DEVICE INCORPORATED IN AN AIRCRAFT STRUT
KOMPAKTE WÄRMEAUSTAUSCHVORRICHTUNG, DIE IN EINEN MAST EINES LUFTFAHRZEUGS INTEGRIERT IST
2020-01-22
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
DISPOSITIF D'ECHANGE THERMIQUE COMPACT INCORPORE DANS UN MAT D'AERONEF
European Patent Office | 2019
|DISPOSITIF THERMIQUE AVEC ELEMENT D'ECHANGE THERMIQUE TUBULAIRE
European Patent Office | 2018
|European Patent Office | 2019
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