Interconnection system for a rack of a system of an aircraft

An interconnection system for a rack of a system of an aircraft, the interconnection system comprising:

• at least one shelf comprising at least one frame, each frame being adapted to receive an electronic device, each frame comprising a connector allowing, on a first side, a connection of said electronic device, and, on a second side, a connection to the system of the aircraft,
• a rear panel, consisting of a printed circuit, the rear panel comprising:
• as many coupling fittings as connectors of the shelf, each coupling fitting being connected to a second side of a corresponding connector,
• at least one interface for connecting a lateral panel,
• the lateral panel, consisting of an electronic circuit board, the lateral panel comprising:
• at least one interface for connecting the rear panel,
• a plurality of connectors allowing a connection to the system of the aircraft, the printed circuit of the rear panel allowing a set of predefined electrical links between the connectors and the interface, the electronic circuit board of the lateral panel allowing a set of electrical links to be set up between the interface and the connectors to the system of the aircraft, the interconnection system being characterized in that:
• each second side of each connector of the shelf comprises a flexible part configured to bear flexibly on a coupling fitting of the rear panel, each flexible part comprising integrated electrical links,
• each coupling fitting of the rear panel comprising a plurality of electrical contacts, and each second side of the connectors coming to bear flexibly on a coupling fitting of the rear panel when the rear panel is securely fixed to the shelf.