Airbus Operations (s.a.s.)

Saint-gobain Glass France

Airbus Operations Gmbh

Airbus France

Airbus Group Limited

Franck Flourens

Thomas Tondu

Eddie Gambardella

Osmin Regis Delverdier

Marie-Hélène Debrus

Hugo Canales

Catherine Unfer

Patrick Oms

Patrick Heins

Christian Donadille

Frederic Labal

Richard Mills

Joseph Rival

Jean-Francois Boissin

Matthew Cole

Matthew Jenkins

Simon Evans

Bernard Boisson

Philippe Sant-Anna

A laminated glazing includes a first and a second glass sheet that are bonded by a first interlayer adhesive layer, a peripheral zone of the laminated glazing being covered by a stepped metal element, the laminated glazing including a heating network of wires and/or a heating electrically conductive layer that is provided with busbars, a plurality of probes and other optional electrical elements that are linked to an electrical power supply via the connector of the laminated glazing, an electrical conductor linking the stepped metal element to a busbar of the heating network of wires and/or of the heating electrically conductive layer; and/or to the cap of the connector of the laminated glazing, which is linked to the ground of the structure for mounting the laminated glazing; and/or to a contact of the connector.

Suppression of electrostatic discharge noise by means of conduction between a tiered metal element and the wiring system of a glazing unit

An electrical link () configured to link a DC high-voltage power source () to a user apparatus (), and includes an electrical conductor () surrounded by an insulating cover and an electrical protection device () including: a conductive sleeve () arranged around the insulating cover, a biasing module () configured to voltage-bias the conductive sleeve (), a circuit breaker () arranged on the conductor () and configured to cut off a current transiting through the conductor (), and a detection module () connected to the conductive sleeve () and configured to detect a current leak out of the conductor () and to command the circuit breaker () on the basis of the detection. The invention also relates to a method for the secure supply of electric power.

Electrical link comprising an electrical protection device&#x2014;voltage bias

A laminated glazing includes a first and a second glass sheet that are bonded by a first interlayer adhesive layer, a peripheral zone of the laminated glazing being covered by a stepped metal element, a window press that is rigidly connected to the structure for mounting the laminated glazing making contact with the laminated glazing, so as to hold the laminated glazing secure to its mounting structure, an electrical conductor linking the stepped metal element and the structure for mounting the laminated glazing by way of the window press.

Electrostatic discharge noise suppression by conduction between a stepped metal element and the pane retainer

An on-board system for evaluating the severity of a lightning strike, intended to be installed in the interior of an airplane and connected to an avionic system of the airplane. The system comprises four devices, a master device and three slave devices, each device comprising a magnetic-field sensor. The devices are placed pairwise symmetrically about a plane of symmetry of the airplane, vertically in line with the leading edge of the wing of the airplane and vertically in line with the trailing edge of the wing, respectively. The system allows an evaluation of the severity of a lightning strike to be obtained depending on the measured magnetic fields.

On-board system for evaluating the severity of a lightning strike

A method and device is disclosed for measuring one or more physical properties of, and/or induced by, out-gassing products released from and/or trapped within a joint in response to a lightning strike or other electrical current threat. A device for measuring one or more physical properties of, and/or induced by, gases, plasma and/or particles released from a joint in response to an electrical current threat. The joint includes a fastener passing through a structure so that an end of the fastener protrudes from the structure. The device includes a containment member having a base surrounding an opening into a cavity, the containment member being arranged to be mounted over the end of the fastener to enclose the end of the fastener within the cavity and to seal the opening; and one or more sensors arranged to measure physical properties of gases, plasma and/or particles contained by the cavity.

Methods, device and apparatus for evaluating electrical current threat effects at joints

A module to test electromagnetic compatibility of at least one high speed Ethernet interface onboard an aircraft. The module includes a cable less than 1 meter long, the ends of which are fitted with two aircraft contacts, two standard connectors compatible with standard test equipment, and a mechanism simulating attenuation of a test cable.

Module for testing electromagnetic compatibility of a high-speed ethernet interface onboard an aircraft

This invention relates to a method for detection of a shielding fault in a multiwire cable forming part of a communication network, during functional operation of the said network, the said cable () transferring a multiframe signal S(t), which comprises the following steps:

Method for detection of a shielding fault in a multiwire cable

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Toulouse, France

Franck Flourens