Abstract: Device and method for the nondestructive testing of a part made of a composite material reinforced with fibers, the device including: a) an energizing laser beam generator and elements for producing a photoelastic stress pattern of the surface of the part, in an energizing area, using the laser beam; b) elements for generating a first detection laser beam capable of illuminating the part in a target area; c) elements for generating a second reference detection laser beam, whose characteristics can be controlled independently of those of the detection laser beam; d) a two-wave photoreactive detector including a photorefractive crystal pumped by the reference laser beam; e) elements for collecting the beam reflected by the target area of the first detection laser and conveying the beam into the photorefractive detector; and f) elements for modifying the characteristics of the reference laser so as to adjust the bandwidth of the photorefractive detector.

Abstract: Disclosed is a structural part (13) capable of dissipating energy delivered during an impact that compresses the part along an axis Z, including a web (131) having two opposite surfaces (133), characterized in that the part includes: a through-window (134) extending between the opposite surfaces of the web, dividing the web into two main portions, referred to as “first portion” (135) and “second portion” (136) respectively, arranged in series along the Z axis; and a device, referred to as an energy-dissipation device, including a cutting element (112, 122) arranged within the window and able to cut at least one of the portions of the web into strips (139) as a result of a compressive force exerted on the part along the Z axis, and an element (113, 123) for clearing away the strips thus formed.

Abstract: A method for identifying an object in a video archive including multiple images acquired in a network of cameras including a phase of characterization of the object to be identified and a phase of searching for the object in the archive, where the characterization phase consists of defining for the object at least one semantic characteristic capable of being extracted, even in low-resolution images, from the video archive.

Abstract: The invention relates to a device for monitoring the integrity and soundness of a mechanical structure, such as an aircraft. The device comprises a control unit, a radio frequency transmission means, and an electric battery. The control unit recovers data from a set of digital and/or analog sensors. The radio frequency transmission means enables the control unit to transmit the data received from the sensors to a man/machine interface. The electric battery powers the device and is rechargeable. The device further comprises a module for recovering electromagnetic energy capable of converting the recovered electromagnetic energy into electric power so as to recharge the battery and/or directly power the device.

Abstract: A ridge structural part made of laminated composite material incorporates electrically conducting cables, the structural part includes at least two structural layers including fibers held in place by a thermosetting or thermoplastic matrix, at least one conducting network layer located between two of the at least two structural layer, the at least one conducting network layer including a network of electrically conducting cables, said electrically conducting cables being arranged throughout said structural part in a substantially regular manner and being electrically insulated from said two structural layers by a dielectric material. The structural part also includes electrical connections, to which electrically conducting cables of the at least one network layer are electrically connected so as to form an electrical network by assembling several structural parts.

Abstract: To analyze an electronic component, this component is exposed to a focused laser beam. The information provided by the laser mapping relating to the position and to the depth of the sensitivity zones of the component is used as input parameter in prediction codes for quantifying the sensitivity of the mapped component to ionizing particles in the natural radioactive environment. The prediction codes are used to determine the occurrence of malfunctions in the electronic component. Determination of the risks associated with the radiative environment imposes two aspects: one, probabilistic, takes into account the particle/matter interaction and the other, electrical, takes into account the charge collection inside the electronic component.

Abstract: In order to produce a part (16) from a composite material, which is conductive at least on one of the surfaces thereof, the method consists of: the conductive overstitching (30) of a preform (20) of the part using electrically or thermally conductive threads (31, 32) with substantially parallel stitch lines (34) oriented in at least two intersecting directions. The parts obtained are adapted for the production of aircraft structures that may be subjected to lightning strikes and allow return currents from the electrical or electronic aircraft equipment and/or the discharge of heat by conduction.

Abstract: A method of controlling a group (2) of engines developing a necessary power (Wnec) for driving a rotor (3), said group (2) of engines having at least one electrical member (4), electrical energy storage means (5), and a first number n of engines (6) that is greater than or equal to two. A processor unit (10) executes instructions for evaluating a main condition as to whether the group of engines can develop the necessary power while resting one engine, and if so for resting one engine and accelerating a second number engines not at rest, and for causing the electrical member to operate in motor mode, if necessary, the electrical member operating temporarily in electricity generator mode when the storage means are discharged.

Abstract: An aircraft fuselage structure, includes a circumferential reinforcing frame (2) and a plurality of stringers (3) substantially perpendicular to the frame. The frame includes a mechanically weakened area able to cause its localized buckling under the effect of a compressive force exerted circumferentially thereon. The structure includes an energy absorbing device (5) having two effector members (52) secured to the frame respectively on either side of the weakened area, and a central core (51) maintained between the effector members such that a reduction in the distance between the effector members produces a deformation of the central core, which is able to absorb energy under the effect of the deformation.

Abstract: A method for characterizing the sensitivity of an electronic component with respect to a natural radiating environment. The safe operating area (SOA) voltage range beyond which destructive events occur is determined for the electronic component for given characteristics of a particle or incident beam. The electronic component is turned on and energized with the particle or incident beam having the given characteristics under the operating conditions that are close to the highest voltage value of the determined SOA voltage range. An efficient section of amplified transient events, which corresponds to an estimation of the destructive occurrences for the electronic component is determined. The characteristics of the particle or beam is modified and the method is repeated with the modified characteristics.

Abstract: An aircraft includes a cabin in which at least part of the space is demarcated by trim panels and the cabin is provided with a system for the active control of ambient noise. Each trim panel is either an active panel including actuators powered by the active noise control system or a passive panel without such actuators. In addition, the trim panels of the cabin of the one type, either active or passive, are mechanically interchangeable with a panel of the other type, either passive or active, respectively. Power supply wiring for active panels is installed in the aircraft, this wiring being capable of powering all active panels which could be installed, whether said active panels are actually installed or whether interchangeable passive panels are installed. Finally, a power supply system for the active panels is installed in the aircraft and connected to the power supply wiring of the active panels.

Abstract: The behavior of a component subjected to pulsed laser radiation is measured. The polarization value, frequency, and temperature (or other operating conditions) to which the component is sensitive are determined by detecting a temporary or permanent fault in the operation of the component. If necessary, the parasitic currents generated are prevented from destroying the tested component at the time of testing. A susceptibility of the component to energetic interactions and the preferred operating conditions for the component are deduced.

Abstract: A lightning protection device (25) for an antenna receiver, includes a shield (40, 70) for a coaxial cable (35, 65) connected to the antenna, and a high-pass filter mounted in series relative to the shield and capable of limiting the low-frequency power flowing in the coaxial cable, including a capacitor (30, 50, 55) and an inductor lower than 1 ohm at the lowest frequency used by the receiver, the capacitor including at least one layer of a conductive material embedded in a printed circuit. In some embodiments, the capacitor is made of a printed circuit (30) including at least two floor plans (50, 55), each of which is connected to the ground of a connector (80, 85) of the coaxial cable. The printed circuit may e.g. include at least one layer of a highly pervious material sandwiched between two layers of a conductive material.

Abstract: The invention relates to a device for testing an integrated circuit. The device comprises a plate for receiving and subjecting the integrated circuit to a test. The plate comprises a component for powering and operating the integrated circuit and another component for measuring the operation of the integrated circuit during the test. The device also comprises an irradiation device for subjecting the circuit to a proton bombardment and a mask with a variable thickness provided between a bombardment access region on the integrated circuit and an established zone of the integrated circuit.

Abstract: To analyze an electronic component, this component is exposed to a focused laser beam. The information provided by the laser mapping relating to the position and to the depth of the sensitivity zones of the component is used as input parameter in prediction codes for quantifying the sensitivity of the mapped component to ionizing particles in the natural radioactive environment. The prediction codes are used to determine the occurrence of malfunctions in the electronic component. Determination of the risks associated with the radiative environment imposes two aspects: one, probabilistic, takes into account the particle/matter interaction and the other, electrical, takes into account the charge collection inside the electronic component.

Abstract: To solve a leakage problem in a box, it is proposed to provide the box with an electronic circuit for measurement of its specific humidity. It is shown that by comparing this current specific humidity to an initial specific humidity and by evaluating the difference found in relation thereto, one has a reliable tool for measuring the permanence of tightness.

Abstract: According to the invention, one or more thermoplastic sheets (NdT: “feuilles thermoplastique” in the original) (2) are applied on a flat or curved tool (13), and strips (NdT: “des bande” in the original) of a polymer are applied and pressed onto the sheets (2). They are maintained by suction pumps (8), the orifices (4) of which open into a closed volume or one substantially delimited by a sealing joint (3) and occupied by a draining fabric (7). The heating treatment concomitant to the deposition to harden or consolidate the prepreg softens the sheets (2), distorts them to the curvature of the tool (13) and incorporates them in the structure of the prepreg. Application to methods of draping parts with composite material.

Abstract: A strain gauge includes a substrate (2) for mounting an element (3) to be reversibly lengthened by a force applied while displaying a variation in the resistance thereof, the element (3) lengthening itself along an axis for measurement by the gauge. The gauge includes at least one contrast target (5, 6) capable of reflecting an incident light beam, the at least one contrast target (5, 6) being placed on the gauge in a predetermined position that makes it possible to predetermine the center of the axis (4), for measurement by the strain gauge (1), by detecting the position of the at least one contrast target (5, 6).

Abstract: A monitoring device of environmental parameter values of an environment surrounding a system. The device includes a sensor to these parameters, and includes a capability to transmit, in real time, each measurement to a processing unit. The processing unit is installed in the system and includes a capability to filter the transmitted measurements. This processing unit comprises a capability to determine cycles from the measurements thus simplified as well as a capability to calculate, in real time, of a percentage of length of consumed life of the system, from the thus determined cycles.

Abstract: A part (1) includes a structural portion made of an electrically insulating or low-conductive composite material (2) and includes, on a surface (11) of the structural portion likely to be subjected to lightning impacts (10), a metallization layer (30) covered with an electrically insulating protection paint (4). The metallization layer includes a layer of a first electrically conductive metal material (31), referred to as HVT material, and includes at least one second electrically conductive metal material (32), referred to as LVT material, having a vaporization temperature ?l substantially lower than the vaporization temperature ?h of the first electrically conductive HVT metal material. A lightning impact results in the vaporization of the LVT material and the removal of the paint on a surface larger than that in which the HVT material is vaporized, and therefore exposes or lifts a portion of the metallization around the lightning impact point, thereby promoting the anchoring of the lightning arc base.