Airliner, has hydrophilic manifold connected with hot gas source through connector, and outlet arranged at end of hydrophilic manifold, where end of manifold is turned away from connector of hot gas source

摘要

The airliner has a drainage device for discharging condensed water within a fuselage (1), and hydrophilic spacers (8) extended between an insulation part and an airliner outer skin (2) and opened into a covered hydrophilic manifold (9). The manifold is connected with a hot gas source (23) i.e. engine, through a connector (22), and an outlet (24) is arranged at an end of the manifold, where the end is turned away from the connector of the source. The manifold is designed as a pipe (25) that is lined with hydrophilic material. The fuselage comprises fiber reinforced plastic composite panels.