Thales

Bernard Ledain

Jean-Pierre Schlotterbeck

Jacques Mandle

Jean-Philippe Pineau

Gilles Genevrier

Patrick Gremillet

Philippe Kertesz

Daniel Caban-Chastas

Dominique Henriot

A package, able to encapsulate at least one component, forming a closed cavity of Faraday cage type having side walls resting on a base and that are surmounted by a cover, wherein at least one of the side walls includes exterior electrical connection elements linked electrically to the interior of the cavity, the exterior connection elements able to interconnect with an exterior circuit such that the side wall faces the exterior circuit when the exterior connection elements are interconnected with the circuit.

Hyperfrequency housing occupying a small surface area and mounting of such a housing on a circuit

A probe system, mixed primary reference probe for an aircraft, associated aircraft and measuring method are disclosed. In one aspect, the probe system includes a base designed to be fastened on the cockpit of an aircraft, a plurality of regularly spaced static pressure taps, arranged through the base and designed to be connected to a pressure measurement device. The system includes at least one optical window transparent to laser radiation and inserted into the base.

Probe system, mixed primary reference probe for an aircraft, associated aircraft and measuring method

The invention relates to an aeronautical probe designed to be mounted on the skin of an aircraft and comprising a probe body protruding from the skin of the aircraft and a heater for de-icing an external surface of the probe body. According to the invention, the heater comprises two self-supporting electrodes and heating resistive elements. Each electrode is formed of an electrically insulating substrate and of an electrically active portion forming one face of the electrode in question. Each resistive element is in contact with the faces of the electrodes. The notable advantages of the invention are that it makes it possible to reduce the operating temperature of the resistive elements and the phenomena of fatigue in the mechanical link between the electrodes and the resistive elements due to different expansion coefficients.

Aeronautical probe with integrated heater

The invention relates to a microwave package delimiting an interior volume, comprising a Faraday cage formed by a conducting surface surrounding the interior volume, a connection point placed outside the Faraday cage, the connection point being intended to be linked electrically to an exterior circuit, an input-output passing through the Faraday cage and linked electrically to the connection point, a base forming a face of the package, the exterior surface of the base forming a mounting surface intended to be applied to the exterior circuit, the connection point being placed on the mounting surface, so that the connection point is placed between the Faraday cage and the exterior circuit when the package is mounted on the exterior circuit. The invention applies to microwave packages used in the realms of avionics, telecommunications, space.

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Sevres, France

Bernard Ledain