Abstract: A multicore data processing system includes a set of data processing cores. At least a part of each data processing core includes a set of local data input and output interfaces for access to peripheral devices dedicated to said cores. It further includes a set of global data input and output interfaces for access to peripheral devices shared between said cores.

Abstract: A data processing system for a graphical interface includes at least one graphics processing unit (GPU) and at least one central processing unit (CPU) which communicates with the graphics processing unit, said processing unit and said central processing unit each including a group of data processing cores (C1, . . . , C6, C?1, . . . C?6). The data processing cores of the graphics processing unit are each connected to a data processing core of the central processing unit via a single dedicated bus (B1, . . . , B6) in such a way as to carry out a data transfer in parallel between said graphics processing unit and said central processing unit.

Abstract: This electric arc extinguishing device for a three-phase power distribution system comprises at least one metal strip (6) and at least one insulating support (7) on which the strip is mounted and comprising means for attaching the device between current distribution bars extending from side to side, the support comprising lateral faces (11) bearing against said bars, the strip being mounted on the support in such a way as to be internally offset relative to said lateral faces.

Abstract: This electric arc extinguishing device for a three-phase power distribution system comprises atleast one metal strip (6) and at least one insulating support (7) on which the strip is mounted and comprising means for attaching the device between current distribution bars extending from side to side, the support comprising lateral faces (11) bearing against said bars, the strip being mounted on the support in such a way as to be internally offset relative to said lateral faces.

Abstract: A method for controlling an equipment item or a function by means of a touch interface includes: displaying, on a touch screen of the interface, a first graphical object that can be manipulated to control said equipment item or said function and a second graphical object having a first configuration in which the first graphical object is disabled and a second configuration in which the first graphical object can be activated; —detecting a first gesture on the screen tending to switch the second graphical object from the first configuration to the second configuration; activating said first graphical object while the second graphical object is being manipulated; and detecting a second gesture on the screen tending to activate the first graphical object. Applicable to the activation of a protected function implemented onboard an aircraft.

Abstract: A three-phase electrical energy distribution system includes a set of current distribution bars extending side by side and clad with an insulator. The bars include opposing insulator-free zones. The electrical energy distribution system finds application to the three-phase electrical energy distribution systems embedded aboard an aircraft.

Abstract: A data processing system for a graphical interface includes at least one graphics processing unit (GPU) and at least one central processing unit (CPU) which communicates with the graphics processing unit, said processing unit and said central processing unit each including a group of data processing cores (C1, . . . , C6, C?1, . . . C?6). The data processing cores of the graphics processing unit are each connected to a data processing core of the central processing unit via a single dedicated bus (B1, . . . , B6) in such a way as to carry out a data transfer in parallel between said graphics processing unit and said central processing unit.

Abstract: A multicore data processing system includes a set of data processing cores. At least a part of each data processing core includes a set of local data input and output interfaces for access to peripheral devices dedicated to said cores. It further includes a set of global data input and output interfaces for access to peripheral devices shared between said cores.

Abstract: A three-phase electrical energy distribution system includes a set of current distribution bars extending side by side and clad with an insulator. The bars include opposing insulator-free zones. The electrical energy distribution system finds application to the three-phase electrical energy distribution systems embedded aboard an aircraft.

Abstract: A method for controlling an equipment item or a function by means of a touch interface includes: displaying, on a touch screen of the interface, a first graphical object that can be manipulated to control said equipment item or said function and a second graphical object having a first configuration in which the first graphical object is disabled and a second configuration in which the first graphical object can be activated; detecting a first gesture on the screen tending to switch the second graphical object from the first configuration to the second configuration; activating said first graphical object while the second graphical object is being manipulated; and detecting a second gesture on the screen tending to activate the first graphical object. Applicable to the activation of a protected function implemented onboard an aircraft.

Abstract: The device comprises at least one frame, a first group of infrared ray emitters and a second group of infrared ray emitters, said groups framing a touch interaction space, the scanning of this space being performed by the successive activations of the emitters of the first group then of the second group, wherein, for the first group of emitters and for the second group of emitters: each emitter is associated with a subgroup of receivers, the receivers of said subgroup being arranged facing said emitter; the scanning cycles are initiated according to set time periods, a scanning cycle comprising a complete scan of constant duration according to the first group of emitters and a complete scan of constant duration according to the second group of emitters; all of the emitted rays not received defining one or more shadow areas.

Abstract: A process for routing virtual links in a frame-switching network including a plurality of source and/or destination terminals of the frames, in which frame switches are connected to one another by physical connections, with each virtual link being defined, for a point-to-point type, by a path through the network between a source terminal and a destination terminal, and, for a multipoint type, by a plurality of paths through the network between a source terminal and a plurality of destination terminals. The process performs the routing of links by minimizing at least one cost function on a set of solutions satisfying at least one predetermined topological constraint.

Abstract: A method for routing virtual links in a frame switching network including a plurality of source terminals and/or destination of the frames, frame switches being connected together through physical connections, each virtual link being defined, for a point-to-point type, by a path through the network between a source terminal and a destination terminal and, for a multipoint type, by a plurality of paths through the network between a source terminal and a plurality of destination terminals. The method carries out routing of the links while observing a segregation constraint with regard to triplets of consecutive switches belonging to the oriented loops, so as to allow verification of determinism of the network.

Abstract: Embodiments of the invention enable the integrity of data processed by a switch to be guaranteed better than 10?9 undetected erroneous frames per flight hour. To do this, rules for disabling ports are included in the switch management program. These rules include a maximum absolute admissible number of erroneous frames, to a maximum relative rate of admissible erroneous frames and a minimum number of erroneous frames constituting a significance threshold. Random errors are detected at the level of each frame due to the insertion of a CRC. Deterministic or data-dependent errors able to deceive systematically the CRC check are made random by means of a frame index.

Abstract: A data integrity checking system in a frame-switched on-board network, including at least first and second asynchronous transmitter terminals, with the second transmitter terminal being in charge of monitoring the first transmitter terminal, and at least first and second receiving terminals, with the second receiving terminal being in charge of monitoring the first receiving terminal. The system includes a first multicast virtual link connecting the first transmitter terminal to the receiving terminals, a second virtual link connecting the first receiving terminal to the second transmitter terminal, the second virtual link not passing through any of the switches that are common to the branches of the first virtual link, a third virtual link connecting the second transmitter to the first receiving terminal in order to transmit thereto the result of an integrity check on the data received by the first receiving terminal.

Abstract: A method for routing virtual links in a frame switching network including a plurality of source terminals and/or destination of the frames, frame switches being connected together through physical connections, each virtual link being defined, for a point-to-point type, by a path through the network between a source terminal and a destination terminal and, for a multipoint type, by a plurality of paths through the network between a source terminal and a plurality of destination terminals. The method carries out routing of the links while observing a segregation constraint with regard to triplets of consecutive switches belonging to the oriented loops, so as to allow verification of determinism of the network.

Abstract: A process for routing virtual links in a frame-switching network including a plurality of source and/or destination terminals of the frames, in which frame switches are connected to one another by physical connections, with each virtual link being defined, for a point-to-point type, by a path through the network between a source terminal and a destination terminal, and, for a multipoint type, by a plurality of paths through the network between a source terminal and a plurality of destination terminals. The process performs the routing of links by minimizing at least one cost function on a set of solutions satisfying at least one predetermined topological constraint.

Abstract: Embodiments of the invention enable the integrity of data processed by a switch to be guaranteed better than 10?9 undetected erroneous frames per flight hour. To do this, rules for disabling ports are included in the switch management program. These rules include a maximum absolute admissible number of erroneous frames, to a maximum relative rate of admissible erroneous frames and a minimum number of erroneous frames constituting a significance threshold. Random errors are detected at the level of each frame due to the insertion of a CRC. Deterministic or data-dependent errors able to deceive systematically the CRC check are made random by means of a frame index.

Abstract: The invention relates to a data integrity checking system in a frame-switched on-board network, comprising at least first and second asynchronous transmitter terminals, with the second (202) being in charge of monitoring the first (201), and at least first and second receiving terminals, with the second (204) being in charge of monitoring the first (203).

Abstract: A method and device for monitoring the validity of a parameter calculated by an anemometric unit of an aircraft may employ a first section for taking into account n first data, each dependent on the parameter being monitored and n being greater than or equal to 1. A second section takes into account p second data that each depends on a value obtained from a data source external to the anemometric unit, where P is greater than or equal to 2. A calculator calculates, for each of the second data, a difference between this second datum and a first datum of the same type. A comparator compares the absolute value of each of the calculated differences with a threshold value. A deducing section deduces from the comparisons that the monitored parameter is invalid if the absolute values of two of the various differences are greater than the corresponding threshold values.