Airbus Operations (s.a.s.)

Sebastien Saletzki

Frederic Durand

Frederique Delannoy

Pierre Depape

Pierre Gruyer

Philippe Moreau

Julien Abadie

Christian Turpaud

Sebastien Delautier

A wireless high-rate communication device for a vehicle, adapted for data exchange between at least one computer system of the vehicle and at least one computer system of a structure separate from the vehicle. The device includes at least one antenna connected to at least one emitter/receiver in turn connected to the at least one computer system of the vehicle, the device adapted for exchanging data according to a point-to-point ultra-wideband communication mode, with a device of the structure including at least one antenna connected to at least one emitter/receiver in turn connected to at least one computer system of the structure when the at least one antenna of the vehicle is in a vicinity of the at least one antenna of the structure.

Devices for point-to-point wireless high-output data transmission between a parked vehicle and a fixed infrastructure

A device for communication between a portable computer system including a display screen and avionic equipment items comprises shielded walls forming at least a partial Faraday cage. The device also includes at least one wide band high output wireless transmitter-receiver arranged inside the shielded walls and adapted for carrying out a very short range point-to-point radio communication with the portable computer system when the portable computer system is placed inside the shielded walls. The device also includes at least one interface connected to the avionic equipment items and adapted for transmitting data originating from the portable computer system to the avionic equipment items and data originating from the avionic equipment items to the portable computer system, through the at least one said transmitter-receiver.

Device and method for communication between a portable computer system and items of avionics equipment

A wireless communication device for an aircraft that includes at least one antenna, for example a wide-band antenna, and a transparent multilayered substrate, for example a side glazing, a front glazing or a porthole of the aircraft, adapted for receiving the at least one antenna. At least a portion of one layer of the substrate is at least partially reflective to electromagnetic waves transmitted or received by the at least one antenna, wherein the at least one portion of the layer of the substrate is located at least partially opposite the at least one antenna. The at least one portion of the layer of the substrate can be a de-icing or defogging heating film.

Aircraft antenna

Growing community of inventors

Cornebarrieu, France

Sebastien Saletzki