Abstract: A two-pilot multifunction display system and an aircraft equipped with the system, the system comprising: at least three screens, at least two of the at least three screens being suitable for displaying a page of symbologies referred to as the “FND page” comprising predetermined symbols and information relating to the flight and to the navigation of the aircraft; and detectors for detecting at least one failed screen among the at least three screens.

Abstract: The display device comprises a display screen comprising a bonding surface and a mechanical structure. The display device also comprises a glass protective casing consisting of two sheets of glass and inserts. This protective casing is bonded to the structure beneath the second sheet of glass. The screen is bonded to the inside of the protective casing on only one of the two sheets. The invention proposes a compact protective device for a flat screen which is applied essentially to liquid crystal matrix screens comprising light-emitting diode light. The preferred field of application is that of screens used for aviation.

Abstract: The field of the invention is that of the discharge of heat from electronic cards in operation and more specifically from electronic devices comprising at least one heat pipe. The electronic package according to the invention comprises at least a mechanical structure comprising at least one housing, an electronic card, and means for mechanically attaching the electronic card in the housing of the structure, the electronic card comprising at least one electronic component and a device of high thermal conductivity joined to the electronic card and comprising two ends, the first end being in thermal contact with the electronic component and the second end of the device of high thermal conductivity being mechanically arranged so as to ensure good thermal contact with the walls of the housing of the structure.