A personal heating ventilation and air conditioning system (HVAC) for an aircraft seat, comprising at least one aircraft seat (10A, 10B, 10C), a heating/cooling device (100) disposed on the at least one aircraft seat (10A, 10B, 10C), at least one branch (101A, 101B, 101C) configured to provide at least one flow path from the heating/cooling device (100), at least one sub-branch (102A, 102B, 103A, 103B, 104A, 104B) provided within the at least one aircraft seat (10A, 10B, 10C), wherein the at least one sub-branch (102A, 102B, 103A, 103B, 104A, 104B) is configured to provide flow from the at least one branch (101A, 101B, 101C) through the at least one aircraft seat (10A, 10B, 10C), and means for expelling air from the at least one sub-branch (102A, 102B, 103A, 103B, 104A, 104B) to an interior surface of the at least one aircraft seat (10A, 10B, 10C).
PERSONAL HEATING VENTILATION AND AIR CONDITIONING SYSTEM IN AIRCRAFT SEAT
PERSÖNLICHES HEIZUNGS-, LÜFTUNGS- UND KLIMATISIERUNGSSYSTEM IM FLUGZEUGSITZ
SYSTÈME DE VENTILATION ET DE CLIMATISATION DU CHAUFFAGE INDIVIDUEL DANS LE SIÈGE D'UN AÉRONEF
2023-08-23
Patent
Electronic Resource
English
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