Tank module for a structurally integrated vacuum sewage...

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 37/02 (2006.01)

Patent

CA 2614494

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).

La présente invention porte sur un module de réservoir d'un aéronef, ce module étant conçu pour s'adapter, depuis l'extérieur, au fuselage d'un aéronef. Le module de réservoir (1) comprend au moins un réceptacle (10) et une partie d'enceinte (5) qui forme une extrémité externe du module (1) et est raccordée au réceptacle (10). La section d'enceinte (5) peut être montée dans une ouverture du fuselage (8) de sorte que le réceptacle (10) soit positionné à l'intérieur (6) du fuselage (9) de l'aéronef.

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