TANK MODULE FOR A STRUCTURALLY INTEGRATED VACUUM SEWAGE SYSTEM FOR AIRCRAFT

摘要

The present invention pertains to a tank module for an aircraft. The tank module is designed for being fitted into the aircraft fuselage from outside. The tank module (1) comprises at least one receptacle (10) and a shell section (5) that forms an outer end of the tank module (1) and is connected to the receptacle (10). The shell section (5) can be fitted into a fuselage opening (8) in such a way that the receptacle (10) is positioned in the interior (6) of the aircraft fuselage (9).