Abstract:
An interconnection system for a rack of a system of an aircraft is provided. The rack includes at least one shelf with at least one frame adapted to receive an electronic device, the interconnection system comprising 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 connector, at least one interface for connecting a lateral panel consisting of an electronic circuit board, the lateral panel comprising: an interface for connecting the rear panel and 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.
Abstract:
The invention relates to optimize the use of electronic cabinets in connector technology, using simplified internal connector technology and flexibility in adapting the external connector technology to the connectors of the cabling assemblies—electronic and/or optical connector technologies—and on the structurally. To this end, according to an embodiment, an overall box-shaped electronic cabinet (1) that is fitted with at least one detachable interconnection module (6a, 6b) is provided with a bottom wall (14) including a bottom card (4) connected to a set of electronic modules (5). The rear wall (14) is extended by edges (14a, 14b) provided with connectors (C1a, C1b) that are capable of being coupled to the connectors (C6a, C6b) that are arranged on a side surface (62a, 62b) of the detachable interconnection module (6a) (6b). Devices for closing and releasably locking the at least one detachable interconnection module (6a, 6b) are provided between a handle (8a, 8b) of an interconnection module (6; 6a, 6b) and the side wall (15, 16) of the cabinet (1).