An aircraft insulation system (10) comprises a foil (42) extending at a distance from an inner surface (44) of an aircraft outer shell (32), an air gap (50) defined between the foil (42) and the aircraft outer shell (32), and a cabin exhaust air duct (28) arranged adjacent to an inner surface (43) of the foil (42) and being adapted to be flown through with cabin exhaust air.
AIRCRAFT INSULATION SYSTEM AND AIRCRAFT AIR CONDITIONING AND INSULATION ARRANGEMENT
FLUGZEUGISOLIERUNGSSYSTEM UND FLUGZEUGKLIMATISIERUNGS- UND -ISOLIERUNGSANORDNUNG
SYSTÈME D'ISOLATION D'AÉRONEF, CLIMATISATION D'AÉRONEF ET AGENCEMENT D'ISOLATION
2019-05-01
Patent
Electronic Resource
English
AIRCRAFT INSULATION SYSTEM AND AIRCRAFT AIR CONDITIONING AND INSULATION ARRANGEMENT
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