Latelec

Bastien Puertolas

Jean Francois Bousquet

Vincent Banasiak

Cyrille Delame

Gerard Boucourt

Bernard Amalric

Julien Mourieras

Jean Charles Bernadac

Olivier Escalaup

Damien Morrison

Philippe Gri

Jérémy Pisanu

Martial Grimm

Damien Aguera

Yannick Marin

Jean François Bousquet

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.

Interconnection system for a rack of a system of an aircraft

A support configured to be reversibly installed on an upper part of an uncovered backrest of a seat. The support includes a plate configured to bear, completely or partly, against a rear face of the backrest, three clamping mechanisms, a Li-Fi technology data communicator connected to the plate, and a connector. Each clamping mechanism includes a bearing member and a clamping screw that are configured to cooperate with the plate so as to clamp a structural frame of the backrest between the bearing member and the plate. The connector being connected to the data communicator by a cable and being connectable an electronic equipment item.

Support for connecting a seat to a communication network

An aircraft avionics bay provided with at least one shelf () that includes: a support platform (); retention seats () for a rack-mountable electrical module () each including a module connector (); an external connection interface (); an interconnection platform () extending substantially parallel to the support platform (), on the side opposite the retention seats (), the interconnection platform () supporting conductive connection tracks (); a plurality of rear printed circuits (), each rear printed circuit () extending opposite a module connector (); the conductive connection tracks () of the interconnection platform () extending into each rear printed circuit () and to the external connection interface () via flexible conductors ().

Aircraft avionics rack with interconnection platform

A method and assembly for locking/unlocking, formed of one of several a removable module () and a mount plate (). The assembly includes a support wall () supporting each removable module (). The removable module () being provided with two lugs () through which an aperture passes. The lugs () extending out of the removable () so that they can be inserted into opening () formed in the support wall (). This assembly is equipped with a locking/unlocking system () having a lever () extending under the support wall () and provided with circular eccentric cams () arranged with offset axial symmetry in the form of an S about a central rotation axle () perpendicular to the support wall (). The lever () being fixed in terms of rotation on this central axle () at equal distances from the two openings ().

Method for locking/unlocking a removable module, and assembly for implementation

The invention relates to a structure () for housing electronic modules () provided with a system for inserting, locking and extracting such modules () including adjacent individual recesses separated by side rails and a motherboard (), each recess being intended for receiving an electronic module (). The system for inserting, locking and extracting includes one lever arm () per individual recess () provided at a distal end with a device for pivoting on the motherboard () and guiding device () capable of engaging with a circulation device (') connected to the electronic module () in order to couple connectors of the electronic module () with the connectors of the motherboard (), as well as a device for automatic locking and unlocking of a proximal end () of each lever arm ().

Method for inserting, locking and extracting an electronic module and housing structure for implementing same

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&#x2014;electronic and/or optical connector technologies&#x2014;and on the structurally. To this end, according to an embodiment, an overall box-shaped electronic cabinet () that is fitted with at least one detachable interconnection module () is provided with a bottom wall () including a bottom card () connected to a set of electronic modules (). The rear wall () is extended by edges () provided with connectors (C, C) that are capable of being coupled to the connectors (C, C) that are arranged on a side surface () of the detachable interconnection module () (). Devices for closing and releasably locking the at least one detachable interconnection module () are provided between a handle () of an interconnection module () and the side wall () of the cabinet ().

Method for integrating a detachable interconnection module in a cabinet, cabinet thus fitted, and aircraft comprising a bay consisting of such cabinets

Growing community of inventors

Castanet Toulousan, France

Bastien Puertolas