Abstract: The general field of the invention is that of systems for segregating audio messages in a cockpit of a first aircraft. Said system comprises: means for receiving and recording audio messages; a database of keywords for the audio messages; means for recognizing of keywords in the audio messages; means for separating the audio messages as a function of said keywords; means for ranking the messages according to an order of priority; means for processing the audio messages according to said order of priority; means for transmitting the messages processed according to said order of priority; means for listening to the audio messages.

Abstract: The general field of the invention is that of methods for using a human-machine interface device for an aircraft comprising at least one speech recognition unit, one display device with a touch interface, one graphical interface computer and one electronic computing unit, the set being designed to graphically present a plurality of commands, each command being classed in at least a first category, referred to as the critical category, and a second category, referred to as the non-critical category, each non-critical command having a plurality of options, each option having a name, said names assembled in a database called a “lexicon”. The method according to the invention comprises steps of recognizing displayed commands, activating the speech recognition unit, comparing the touch and voice information and a validation step.

Abstract: The general field of the invention is that of head viewing systems for aircraft comprising a head support, a viewing device, a detection of posture of said head support, means for detecting the current heading of an aircraft and means for graphically generating said heading. The system according to the invention comprises means of control, display and selection of headings arranged so as: to display in response to a first command, a second so-called setpoint heading and a third heading termed a “support heading” corresponding to the direction of the head support in a terrestrial reference frame, said direction given by the information arising from the detection of posture of said head support and the means for detecting the current heading; to replace, in response to a second command, said second heading by said third heading, said third heading thus becoming the new heading setpoint.

Abstract: A fiber distribution system (10) includes a fiber distribution hub (20, 300); at least one fiber distribution terminal (30, 100); and a cable (40) wrapped around a spool (110) of the fiber distribution terminal (30, 100). The fiber distribution terminal (30, 100) includes a spool (110) and a management tray (120) that rotate together. A second connectorized end (40b) of the cable (40) is held at a fiber optic adapter (125) on the tray (120). After dispensing the first connectorized end (40a) to the hub (20), an optical splitter (70, 130, 140) can be mounted to the tray (120). The splitter (26, 70, 130, 140, 306) has output adapters at which patch cords (50) can be inserted to connect subscribers to the system. The fiber distribution hub can use the same format of splitters (26, 70, 130, 140, 306). Other distributed splitter systems are provided with splicing and/or adding of splitters as needed.

Abstract: The general field of the invention is that of methods of graphic representation, modification and validation of an aeronautical flight plan for an aircraft avionics system. The system comprises means for computing and generating said flight plan, a task management system, a visualization device displaying a graphic representation of said flight plan and a man-machine interface suitable for making selections, modifications or additions to the information contained in said graphic representation, said selections, modifications and additions being taken into account by the task management system, said graphic representation containing a timeline on which feature at least the various phases of the flight plan and the information corresponding to said phases. The method according to the invention contains a step of displaying at least one item of information depending on several parameters and the graphic representation of which depends on the level of available information about said parameters.

Abstract: Able to prevent a leakage flow from a basin in a ground and to enable a filling flow from this ground, a safety anti-reversing device comprises a body comprising communicating openings for passage of the filling flow. Supported by this body, a flexible membrane comprises an annular shutter and a closing portion. The annular shutter is offset with respect to the communicating openings and swivels between a closed down position in which this annular shutter is applied in tight manner on the body, and an open position in which the annular shutter is away from the body. Distinct from the annular shutter, the closing portion covers the communicating openings so as to be able to hermetically close these communicating openings.

Abstract: The general field of the invention is that of display systems comprising a display device displaying a configuration comprising a plurality of graphical formats, a touch-sensitive surface comprising means arranged to provide a haptic sensation and means of designation of the said plurality of graphical formats. In the system according to the invention, at least one function of implementation of a first graphical format does not comprise any displayed graphical indication and is signalled solely by a haptic sensation dedicated to the said implementing function when the designation means are on the said first graphical format or in its immediate vicinity.

Abstract: The general field of the invention is that of methods for determining safety zones surrounding an aircraft travelling or taking off from an airport zone, the safety zone being calculated at a determined instant that may be the present instant or the future instant. The method according to the invention comprises at least the following steps: Step 0: Establishment of a convex safety envelope surrounding the aircraft on the basis of reference points taken on the aircraft; Step 1: Establishment of a first convex envelope safety zone surrounding the aircraft on the basis of reference circles taken on the aircraft, each circle having as center one of the reference points and as radius the value of the uncertainty in the exact position of the aircraft. Other steps of the method make it possible to refine this first safety zone depending on whether the aircraft is in a taxiing or takeoff phase and depending on whether it is calculated at the present instant or at the future instant.

Abstract: The general field of the invention is that of systems for aiding the guidance of a first aircraft travelling around an airport zone. The system according to the invention comprises: a set of databases comprising bulkiness and performance characteristics of the said first aircraft, geometric and technical characteristics of the airport zone and information about the air traffic in the immediate environment of the said first aircraft; calculation means making it possible to firstly determine a safety zone around the said first aircraft taking into account at least the position of the said aircraft, its size and the uncertainty in the measurement of its position; and then a taxiing indication on the basis of the information arising from the databases and the characteristics of the safety zone; viewing means displaying at least one view of the airport one in which the first aircraft is situated and a representation of the said taxiing indication.

Abstract: The present invention relates to the preparation of food compositions capable of improving the bone status of the consumer by promoting bone tissue formation. In particular, it relates to the use of milk protein proteolysates for the preparation of these compositions.

Abstract: The general field of the invention is that of methods for determining a taxiing path of an aircraft over an airport area. The method is implemented by the avionics system of the aircraft. It comprises the following steps: Determining the “nodes” of a connectivity graph, said nodes representing the junction points between the traffic lanes of said airport area; Determining the useful arcs joining said nodes and representing the network of traffic lanes that can be taken by the aircraft; Attributing a “weight” to each useful arc; Determining the optimal path by an algorithm of Dijkstra type starting from the present position of the aircraft up to its destination position and passing through datum points; Computing, and displaying a graphical representation including a representation of the airport area, of the aircraft and of the optimal path.

Abstract: The general field of the invention is that of systems for aiding the guidance of a first aircraft travelling around an airport zone. The system according to the invention comprises: a set of databases comprising bulkiness and performance characteristics of the said first aircraft, geometric and technical characteristics of the airport zone and information about the air traffic in the immediate environment of the said first aircraft; calculation means making it possible to firstly determine a safety zone around the said first aircraft taking into account at least the position of the said aircraft, its size and the uncertainty in the measurement of its position; and then a taxiing indication on the basis of the information arising from the databases and the characteristics of the safety zone; viewing means displaying at least one view of the airport zone in which the first aircraft is situated and a representation of the said taxiing indication.

Abstract: The general field of the invention is that of methods for determining safety zones surrounding an aircraft travelling or taking off from an airport zone, the safety zone being calculated at a determined instant that may be the present instant or the future instant. The method according to the invention comprises at least the following steps: Step 0: Establishment of a convex safety envelope surrounding the aircraft on the basis of reference points taken on the aircraft; Step 1: Establishment of a first convex envelope safety zone surrounding the aircraft on the basis of reference circles taken on the aircraft, each circle having as centre one of the reference points and as radius the value of the uncertainty in the exact position of the aircraft. Other steps of the method make it possible to refine this first safety zone depending on whether the aircraft is in a taxiing or takeoff phase and depending on whether it is calculated at the present instant or at the future instant.

Abstract: The invention relates to a device (1) for the vision correction of an eye (6), comprising: a converter (3, 3A, 3B, 5A, 5B) which can generate an electrical and/or magnetic and/or electromagnetic signal in response to the mechanical energy generated by a movement of the eye; and a soft lens (2) intended to be aligned with the eye. The converter is positioned in relation to the lens such that the electrical and/or magnetic and/or electromagnetic signal generated during the movement of the eye causes the optical properties of the lens to change. The invention is characterised in that the lens (2) includes a polymer material (7) containing a material (4) having a refractive index that can vary under the action of the electrical and/or magnetic and/or electromagnetic signal generated during a movement of the eye.

Abstract: The general field of the invention is that of methods of graphic representation, modification and validation of an aeronautical flight plan for an aircraft avionics system. The system comprises means for computing and generating said flight plan, a task management system, a visualization device displaying a graphic representation of said flight plan and a man-machine interface suitable for making selections, modifications or additions to the information contained in said graphic representation, said selections, modifications and additions being taken into account by the task management system, said graphic representation containing a timeline on which feature at least the various phases of the flight plan and the information corresponding to said phases. The method according to the invention contains a step of displaying at least one item of information depending on several parameters and the graphic representation of which depends on the level of available information about said parameters.

Abstract: The general area of the invention is that of methods for managing flight plans by an avionic system comprising a visualization device and a touch-sensitive interface. The visualization device displays a cartographic representation of the terrain flown over, aeronautical data and a flight plan composed of a set of segments connecting together certain aeronautical waypoints. The management method contains several steps, a first editing step activated by touch-sensitive designating of any point of the flight plan, a second modification of the flight plan step activated by a touch-sensitive movement, the end of the touch-sensitive movement triggering a movement or an addition or the removal of a waypoint. The method also makes it possible to easily manage the airways in order to incorporate them into a flight plan during modification.

Abstract: A device for aiding the following of an airport route by an aircraft includes: an onboard system of optical sensors; means providing the current position of the aircraft; a database having topological information for the airport; a recognition system providing, on the basis of the video images arising from the system of optical sensors, data characteristics of the airport route portion, making it possible to identify a simple primitive representative of the route portion followed; and a processing computer. The processing computer extracts, from the database, a succession of simple geometric shapes representing the airport route and of the same nature as the primitives arising from the recognition system, compares the succession of shapes with the primitives, and validates or invalidates the route followed by the aircraft as a function of the result of the comparison.

Abstract: Connector (1) for flexible printed circuit (FPC) (3) comprising a connector housing (5) including an insertion slot (4) adapted to receive the FPC (3). The connector comprises a shield (18) adapted to be electrically connected to a ground path (2a) of a circuit substrate (2) on which the connector (1) is to be mounted. Said insertion slot (4) comprises a signal side corresponding to conductive tracks (29) of the FPC and a ground side (26a) opposite to said signal side. The shield comprises at least one electrically conductive tooth (25), movable from a retracted position outside the insertion slot (4), to a protruding position where said tooth (25) protrudes from the ground side (26a) to the inside of the insertion slot (4).

Abstract: Systems and of the methods for allowing a taxiing route to be established over an airport area are described. In one embodiment, the method comprises input of an instruction representative of a succession of names of passing points representing the taxiing route to be created, each passing point name being composed of alphanumeric characters, the succession of the names of passing points not comprising separators allowing them to be identified one by one. The method also comprises decomposition of the instruction by a lexical analysis device into at least one succession of credible names of passing points. The method further comprises verification for each succession that the corresponding route is compatible with the connectivities existing between the various airport elements of the taxiing clearance corresponding to the succession, in the case where there exists one and only one credible route, display of the said route on a display device.

Abstract: Able to prevent a leakage flow from a basin in a ground and to enable a filling flow from this ground, a safety anti-reversing device comprises a body comprising communicating openings for passage of the filling flow. Supported by this body, a flexible membrane comprises an annular shutter and a closing portion. The annular shutter is offset with respect to the communicating openings and swivels between a closed down position in which this annular shutter is applied in tight manner on the body, and an open position in which the annular shutter is away from the body. Distinct from the annular shutter, the closing portion covers the communicating openings so as to be able to hermetically close these communicating openings.