Safran Electronics & Defense

Safran Electrical & Power

Airbus Operations Gmbh

Jean-Marc Blineau

Serge Thierry Roques

Philippe Pierre Avignon

François Guillot

Franck Albero

Ismaïl Tchaaouaou

Frédéric Colin

Philippe Mairet

Francois Goge

Alexandre Fleury

François Goge

An aircraft comprising a fuselage () subdivided by a floor () into a top volume () and a bottom value () in which girders () extend supporting the floor and co-operating with the fuselage and the floor to define two lateral housings () that are of substantially triangular cross-section and that extend parallel to a longitudinal axis of the fuselage. Calculation units () are arranged in the lateral housings and each comprises a box () defining a main compartment containing calculation modules () insertable into the main compartment along an insertion axis through an opening in the compartment and connectable to the connectors () carried by a back wall () of the compartment so as to extend into the main compartment opposite from the opening, the insertion axis being substantially parallel to the longitudinal axis of the fuselage.

Aircraft having computers distributed in the fuselage

Electronic module comprising a protective casing defining an internal volume and an electronic board placed in the internal volume, the electronic module comprising: means, for detecting a predetermined environmental condition of the internal volume, means for generating a cool zone inside the internal volume, which means are arranged such that the cool zone is separated from the electronic board; a control unit that is linked to the means for detecting an environmental condition and to the means for generating a cool zone and arranged to trigger the means for generating a cool zone when the means for detecting a predetermined environmental condition in the internal volume detect an environmental condition that is liable to result in the moisture in the air contained in the internal volume condensing on the electronic board.

Electronic module with improved moisture protection

A system comprising a rack and at least one line replaceable module, the rack further comprising a primary transmission circuit comprising a primary antenna, primary emission components designed to generate an emitted power containing uplink data, and primary receiving components designed to receive downlink data, the line replaceable module comprising a secondary transmission circuit comprising a secondary antenna, secondary receiving components designed to receive the emitted power and the uplink data, and secondary emission components designed to generate the downlink data, the emitted power, the uplink data and the downlink data being transmitted via a shared coupling between the primary antenna and the secondary antenna.

System comprising a rack and a line replaceable module

An electrical power distribution assembly for an airplane, the assembly including an electric switch device for placing in a Karman fairing of the airplane.

Electrical power distribution assembly for an aircraft

An electronic unit comprising a box defining a reception compartment for receiving an electronic module along two mutually opposite directions of an insertion axis, the compartment including electrical power supply means for powering the electronic module and connection means for connecting the electronic unit to the electronic module, these means extending onto a connection face forming part of the reception compartment and extending parallel to the insertion axis. An electronic module for mounting in a compartment of an electronic unit of the invention.

Electronic unit with reversible modules

A cooling module including a first air inlet, a second air inlet, and an air discharge vent, the module having two check valves, each mounted in register with a respective inlet and arranged to allow air to pass towards the inside of the module and to oppose a flow of air in the opposite direction. An electronic unit including such a box.

Cooling module and electronic unit comprising such a module

A printed circuit board including at least one blind metal-plated hole, for receiving a pin of the printed circuit board being covered by a first layer of a protective film on which there extends a second layer of electrically insulating flexible material, the first layer and second layer are for piercing by the pins when they are engaged in the metal-plated holes, the first and second layers being for claming between a support of the pins and the printed circuit board. An electronic unit including such a device. A method of fabricating a printed circuit card for such a device.

Electronic device comprising a module connected to a PCB and electronic unit comprising such a device

A vice-type terminal block for electrically connecting a pair of lugs by clamping them together. Each lug includes a barrel extending along an axis and a radially extending flange connected to the barrel. The flange has, on the opposite side to where the barrel is located, an electrical contact surface normal to the axis. The vice-type terminal block includes two opposing plates and a clamping system. Each plate includes a slot for receiving one of the lugs such that the flange of the lug is on one side of the plate, whereas the barrel is on the other side. The pair of lugs are supported such that their electrical contact surfaces face one another and are aligned.

Growing community of inventors

Blagnac, France

Jean-Marc Blineau