Disclosed herein is a humidification system (1) for aircrafts comprising:- a first duct (6, 6') configured to guide a first air stream;- a second duct (10, 10') configured to guide a second air stream, said second duct (10, 10') comprising a humidifier (28, 28') for humidifying the air in the second duct (10, 10'),The humidification system further comprises a:- a first conduit (8, 8') for directing a part of the second air stream to the first duct (6, 6'), said first conduit (8, 8') comprising a first conduit inlet (20, 20') leading into the first duct (6, 6') and a first conduit outlet (22, 22') from the second duct (10, 10');- a second conduit (12, 12') for directing a part of the first air stream to the second duct (10, 10'), said second conduit (12, 12') comprising a second conduit inlet (34, 34') leading into the second duct (10, 10') and a second conduit outlet (36, 36') from the first duct (6, 6'), wherein the first conduit outlet (22, 22') is arranged downstream of the humidifier (28, 28'), the second conduit inlet (34, 34') is arranged downstream of the first conduit outlet (22, 22') and wherein the first conduit inlet (20, 20') is arranged downstream the second conduit outlet (36, 36').
HUMIDIFICATION SYSTEM FOR AIRCRAFT
BEFEUCHTUNGSSYSTEM FÜR FLUGZEUGE
SYSTÈME D'HUMIDIFICATION POUR AÉRONEF
2024-07-03
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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