Tank module for a structurally integrated vacuum sewage system for aircraft
View Patent ↗A tank module for an aircraft is designed for being fitted into the aircraft fuselage from outside. The tank module comprises at least one receptacle and a shell section that forms an outer end of the tank module and is connected to the receptacle. The shell section can be fitted into a fuselage opening in such a way that the receptacle is positioned in the interior of the aircraft fuselage.
1. A tank module for installation into a fuselage opening of an aircraft fuselage, comprising:
at least one waste water receptacle,
a shell section forming an outer end of the tank module and connected to the at least one waste water receptacle,
at least one vacuum generator, and
a bypass line,
wherein the shell section has a contour corresponding to the fuselage opening, the tank module being configured to be fitted with the shell section thereof into the fuselage opening such that the at least one waste water receptacle is positioned in the interior of the aircraft fuselage,
wherein the shell section is configured to seal the interior of the aircraft fuselage relative to the exterior such that an equalization of pressure between the interior of the aircraft fueslage and an outside atmosphere cannot take place,
wherein the at least one waste water receptacle comprises a connector for connecting the at least one waste water receptacle to a feed pipe system in the interior of the aircraft fuselage,
wherein the at least one vacuum generator is configured for generating a suction air current from the feed pipe system into the at least one waste water receptacle via the at least one waste water receptacle, and
wherein the bypass line is configured to convey a parallel air current past the at least one vacuum generator by using a differential pressure between an outside air and the cabin air.
2. The tank module of claim 1 , wherein the shell section forms a lower end of the at least one receptacle to fit into the underside of the fuselage opening.
3. The tank module of claim 1 , wherein the at least one waste water receptacle and the shell section are formed in one piece.
4. The tank module of claim 1 , wherein the at least one waste water receptacle and the shell section are manufactured from a composite fiber material.
5. The tank module of claim 1 , wherein the shell section has such dimensions that a constructive weakening of the aircraft fuselage caused by the fuselage opening is compensated when the shell section is installed into the fuselage opening of the aircraft fuselage.
6. The tank module of claim 1 , further comprising at least one device for determining the instantaneous filling level of the at least one waste water receptacle.
7. The tank module of claim 1 , further comprising at least one device for cleaning the at least one waste water receptacle.
8. The tank module of claim 1 , further comprising at least one device for heating the at least one waste water receptacle and integrated into the walls of the at least one waste water receptacle.
9. The tank module of claim 1 , further comprising at least one drainage device for emptying the at least one waste water receptacle.
10. The tank module of claim 1 , further comprising at least one connection for connecting the tank module to an electric power supply in the interior of the aircraft fuselage.
11. An aircraft comprising a waste water receptacles, wherein the waste water receptacle comprises a tank module comprising:
the at least one waste water receptacle,
a shell section forming an outer end of the tank module and connected to the at least one waste water receptacle,
at least one vacuum generator, and
and a bypass line,
wherein the shell section has a contour corresponding to the fuselage opening, the tank module configured to be fitted with the shell section thereof into the fuselage opening such that the at least one waste water receptacle is positioned in the interior of the aircraft fuselage,
wherein the shell section is configured to seal the interior of the aircraft fuselage relative to the exterior such that an equalization of pressure between the interior of the aircraft fuselage and an outside atmosphere cannot take place,
wherein the at least one waste water receptacle comprises a connector for connecting the at least one waste water receptacle to a feed pipe system in the interior of the aircraft fuselage,
wherein the at least one vacuum generator is configured for generating a suction air current from the feed pipe system into the at least one waste water receptacle via the at least one waste water receptacle, and
wherein the bypass line is configured to convey a parallel air current past the at least one vacuum generator by using a differential pressure between an outside air and the cabin air.