Disclosed is an aircraft including ductwork (103). The ductwork includes a cabin recirculation vent (104) disposed to draw air from an aircraft cabin. The ductwork includes a riser (118) defining a return conduit disposed to convey air from the cabin recirculation vent. The ductwork includes a thermoelectric heat pump (110) having a first side and a second side, the first side in thermal contact with the return conduit that transfers heat to the second side upon application of an electrical input.
AIRCRAFT CABIN AIR THERMODYNAMIC CONTROL
THERMODYNAMISCHE STEUERUNG DER FLUGZEUGKABINENLUFT
COMMANDE THERMODYNAMIQUE DE L'AIR DANS LA CABINE D'UN AVION
2023-03-01
Patent
Elektronische Ressource
Englisch