| 摘要 |
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. |
