In some examples, a structural framework component for an aerial platform comprises a body defining a cavity to receive a support system, and an arm to receive a payload, wherein the arm comprises a conduit to receive cabling linking a support system and a payload.
BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC. (USA)
Inventeur(s)
Kohl, Christopher E.
Gensler, Jeffrey A.
Hyink, Parker T.
Abrégé
Various countermeasure dispensing systems (or CMDSs) and method of use are described herein. CMDS may include a dispenser assembly operably engaged with a platform where at least one electrical connection provides electrical communication between the dispenser assembly and a sequencer. CMDS may also include a magazine assembly operably engaged with the dispenser assembly, wherein the magazine assembly comprises a magazine configured to hold at least two countermeasure expendables. CMDS may also include a breechplate assembly operably engaged with the magazine assembly and adapted to dispense the at least two countermeasure expendables. CMDS may also include at least one magazine identification switch (MIS) operably engaged with the magazine assembly and the breechplate assembly. CMDS may also include that the at least one MIS is configured to enable the sequencer and the breechplate assembly to selectively dispense at least one countermeasure expendable from the at least two countermeasure expendables.
F42B 5/15 - Cartouches, c. à d. projectile et douille avec charge propulsive formant un tout pour libérer des gaz, des vapeurs, des poudres, des particules ou des substances à réaction chimique adaptées pour créer un effet de brouillard ou de leurre, p.ex. en utilisant des paillettes anti-radar ou des corps à action infrarouge
F42B 12/70 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché pour la signalisation pour la libération de corps solides individuels pour la libération de paillettes antiradar ou de matériaux à émission infrarouge
F41A 17/06 - Sûretés électriques ou électromécaniques
H01R 31/06 - Pièces intermédiaires pour joindre deux pièces de couplage, p.ex. adaptateur
According to an aspect of the present invention there is provided a cell assembly safety system comprising: a cell; a cell enclosure configured to hold the cell; and one or more sensors for monitoring characteristics of the cell to determine a safety value of the cell; wherein one of the one or more sensors comprises one or more acoustic sensors associated with the cell assembly and configured to sense one or more acoustic signatures representing respective electrochemical reactions in the cell.
G01R 31/00 - Dispositions pour tester les propriétés électriques; Dispositions pour la localisation des pannes électriques; Dispositions pour tests électriques caractérisées par ce qui est testé, non prévues ailleurs
H01M 10/42 - Procédés ou dispositions pour assurer le fonctionnement ou l'entretien des éléments secondaires ou des demi-éléments secondaires
H01M 10/48 - Accumulateurs combinés à des dispositions pour mesurer, tester ou indiquer l'état des éléments, p.ex. le niveau ou la densité de l'électrolyte
H01M 50/569 - Connexions conductrices de courant pour les cellules ou les batteries - Détails de construction des connexions conductrices de courant pour détecter les conditions à l'intérieur des cellules ou des batteries, p.ex. détails des bornes de détection de tension
Structures are disclosed for a binned set of two or more pixels of a pixel array that share a same readout circuit. The binned pixel design provides space-saving benefits on the chip and also improves the overall image quality. According to some embodiments, each of the binned pixels includes a photodetector and its own transfer gate. The readout circuit is coupled to the transfer gates of each of the binned pixels and includes its own second transfer gate that separates the pixels from a gain mode select block. The gain mode select block may include capacitors of different sizes and one or more switches to control which capacitors are to receive the charge from any one of the binned pixels. The readout circuit may also include a potential barrier (such as a diode), which allows for pumping charge onto the one or more capacitors of the gain mode select block.
H04N 5/347 - Extraction de données de pixels provenant d'un capteur d'images en agissant sur les circuits de balayage, p.ex. en modifiant le nombre de pixels ayant été échantillonnés ou à échantillonner en combinant ou en mélangeant les pixels dans le capteur SSIS
H04N 5/372 - Capteurs à dispositif à couplage de charge [CCD]; Registres d'intégration à temps de retard [TDI] ou registres à décalage spécialement adaptés au capteur SSIS
H04N 5/3745 - Capteurs adressés, p.ex. capteurs MOS ou CMOS ayant des composants supplémentaires incorporés au sein d'un pixel ou connectés à un groupe de pixels au sein d'une matrice de capteurs, p.ex. mémoires, convertisseurs A/N, amplificateurs de pixels, circuits communs ou composants communs
H04N 5/378 - Circuits de lecture, p.ex. circuits d’échantillonnage double corrélé [CDS], amplificateurs de sortie ou convertisseurs A/N
A barrier for separating cells of a battery is described. The barrier comprises a main body comprising a thermally insulating material wherein the main body comprises a first side and a second side opposite the first side. The barrier further comprises a thermally conductive layer coating at least a part of the first side of the main body. The thermally conductive layer enables heat to be conducted across at least the part of the first side of the main body. The thermally insulating material prevents heat being conducted through the main body from the first side of the main body to the second side of the main body.
H01M 10/60 - Chauffage ou refroidissement; Commande de la température
B32B 15/04 - Produits stratifiés composés essentiellement de métal comprenant un métal comme seul composant ou comme composant principal d'une couche adjacente à une autre couche d'une substance spécifique
B32B 19/00 - Produits stratifiés composés essentiellement de fibres ou particules minérales naturelles, p.ex. d'amiante, de mica
H01M 10/653 - Moyens de commande de la température associés de façon structurelle avec les éléments caractérisés par des matériaux électriquement isolants ou thermiquement conducteurs
H01M 10/658 - Moyens de commande de la température associés de façon structurelle avec les éléments par isolation ou protection thermique
H01M 50/24 - Montures; Boîtiers secondaires ou cadres; Bâtis, modules ou blocs; Dispositifs de suspension; Amortisseurs; Dispositifs de transport ou de manutention; Supports caractérisés par les propriétés physiques des boîtiers ou des bâtis, p.ex. dimensions adaptés pour protéger les batteries de leur environnement, p.ex. de la corrosion
According to an aspect of the present invention, there is provided a cell assembly comprising: a cell; a cell enclosure configured to hold the cell; and one or more sensors for monitoring characteristics of the cell to determine a safety value of the cell; wherein one of the one or more sensors comprises a printed sensor for monitoring at least one of strain or temperature associated with the cell, wherein the printed sensor has been applied to the cell and is configured to sense the difference in at least one of strain or temperature between the cell when charged and the cell when discharged to identify the safety value.
H01M 10/42 - Procédés ou dispositions pour assurer le fonctionnement ou l'entretien des éléments secondaires ou des demi-éléments secondaires
H01M 10/48 - Accumulateurs combinés à des dispositions pour mesurer, tester ou indiquer l'état des éléments, p.ex. le niveau ou la densité de l'électrolyte
G01R 31/00 - Dispositions pour tester les propriétés électriques; Dispositions pour la localisation des pannes électriques; Dispositions pour tests électriques caractérisées par ce qui est testé, non prévues ailleurs
H01M 50/569 - Connexions conductrices de courant pour les cellules ou les batteries - Détails de construction des connexions conductrices de courant pour détecter les conditions à l'intérieur des cellules ou des batteries, p.ex. détails des bornes de détection de tension
H01M 10/0525 - Batteries du type "rocking chair" ou "fauteuil à bascule", p.ex. batteries à insertion ou intercalation de lithium dans les deux électrodes; Batteries à l'ion lithium
7.
IMPROVEMENTS IN A CELL ASSEMBLY AND AN ASSOCIATED SYSTEM
According to an aspect of the present invention there is provided a cell assembly comprising: a cell; a cell enclosure configured to substantially surround the cell; and an optical sensor deployed within the cell in a location where a chemical environment is active to monitor at least one of temperature, strain and an acoustic signature, the optical sensor configured in use to receive a pulse of light and output a signal which is detectable with an optical monitor.
G01R 31/00 - Dispositions pour tester les propriétés électriques; Dispositions pour la localisation des pannes électriques; Dispositions pour tests électriques caractérisées par ce qui est testé, non prévues ailleurs
H01M 10/42 - Procédés ou dispositions pour assurer le fonctionnement ou l'entretien des éléments secondaires ou des demi-éléments secondaires
H01M 10/48 - Accumulateurs combinés à des dispositions pour mesurer, tester ou indiquer l'état des éléments, p.ex. le niveau ou la densité de l'électrolyte
H01M 50/569 - Connexions conductrices de courant pour les cellules ou les batteries - Détails de construction des connexions conductrices de courant pour détecter les conditions à l'intérieur des cellules ou des batteries, p.ex. détails des bornes de détection de tension
A thermodynamic apparatus (10) comprising a compressor module (100), a turbine module (200), and a regenerative heat exchanger (300) centred on a central axis (12). The compressor module (100), turbine module (200) and regenerative heat exchanger (300) are arranged in series along the central axis (12) such that the regenerative heat exchanger (300) is provided between the compressor module (100) and the turbine module (200).
BAE Systems Information and Electronic Systems Integration Inc. (USA)
Inventeur(s)
Kohl, Christopher E.
Gensler, Jeffrey A.
Hyink, Parker T.
Abrégé
Various countermeasure dispensing systems (or CMDSs) and method of use are described herein. CMDS may include a dispenser assembly operably engaged with a platform where at least one electrical connection provides electrical communication between the dispenser assembly and a sequencer. CMDS may also include a magazine assembly operably engaged with the dispenser assembly, wherein the magazine assembly comprises a magazine configured to hold at least two countermeasure expendables. CMDS may also include a breechplate assembly operably engaged with the magazine assembly and adapted to dispense the at least two countermeasure expendables. CMDS may also include at least one magazine identification switch (MIS) operably engaged with the magazine assembly and the breechplate assembly. CMDS may also include that the at least one MIS is configured to enable the sequencer and the breechplate assembly to selectively dispense at least one countermeasure expendable from the at least two countermeasure expendables.
B64D 7/02 - Agencement à bord aéronefs des équipements militaires, p.ex. des armes, des accessoires d'armement ou des blindages de protection; Adaptations des installations d'armement aux aéronefs les armes étant des armes à feu
In some examples, a wing for an aircraft, the wing having a passive variable aeroelastic geometry for accommodating efficient flight at multiple aircraft speeds, comprises a wing skin comprising a composite structure comprising a lamination of multiple layers deposited for the wing skin according to a predetermined lamination profile, at least one of the layers comprising a continuous non-linear deposition of material, the wing skin comprising a stiffness distribution profile defined by the lamination profile.
B29C 70/16 - Façonnage de matières composites, c. à d. de matières plastiques comprenant des renforcements, des matières de remplissage ou des parties préformées, p.ex. des inserts comprenant uniquement des renforcements, p.ex. matières plastiques auto-renforçantes des renforcements fibreux uniquement caractérisées par la structure des renforcements fibreux utilisant des fibres de grande longueur, ou des fibres continues
B29C 70/22 - Façonnage de matières composites, c. à d. de matières plastiques comprenant des renforcements, des matières de remplissage ou des parties préformées, p.ex. des inserts comprenant uniquement des renforcements, p.ex. matières plastiques auto-renforçantes des renforcements fibreux uniquement caractérisées par la structure des renforcements fibreux utilisant des fibres de grande longueur, ou des fibres continues orientées dans au moins deux directions formant une structure bidimensionnelle
B29C 70/38 - Empilage automatisé, p.ex. utilisant des robots, par application de filaments selon des modèles prédéterminés
B29D 99/00 - Matière non prévue dans les autres groupes de la présente sous-classe
BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC. (USA)
Inventeur(s)
Thompson, David E.
Pelletier, Gerard J.
Snell, Katherine J.
Abrégé
The system and method for mounting a high power laser having a coefficient of thermal expansion that is thermally matched for the gain medium and the mount. In some cases, the gain medium is clamped by the mount along longitudinal edges and has a pair of free ends not in thermal contact with the mount. A thermal interface may be present along at least a portion of the longitudinal edges.
H01S 3/091 - Procédés ou appareils pour l'excitation, p.ex. pompage utilisant le pompage optique
H01S 3/0933 - Procédés ou appareils pour l'excitation, p.ex. pompage utilisant le pompage optique par de la lumière incohérente produite par un semi-conducteur, p.ex. une diode émettrice de lumière
H01S 3/13 - Stabilisation de paramètres de sortie de laser, p.ex. fréquence ou amplitude
BAE Systems Information and Electronic Systems Integration Inc. (USA)
Inventeur(s)
Grass, Sheldon L.
Delong, Alfreda M.
Ingraham, Jonathan P
Zenga, Noel A.
Abrégé
A method for a system for security evaluation includes working one state at a time; identifying primitives of interest and systematically applying relevant attacks for the system; starting at chip level, working through states, and then expanding a system boundary and repeating; following a sequence of: chip>circuit card>subsystem>system>platform for a product solution under analysis; determining if a system definition has sufficient detail, or is too abstract; for a chip with a native secure boot protocol, determining if all players are represented; representing attacks as vectors made up of measurements of the following attributes: Dollars, days, Probability of success, Probability of destruction, technology node, and number of samples; and representing countermeasures as vectors made up of scaling factors for each of attack attributes.
G06F 21/57 - Certification ou préservation de plates-formes informatiques fiables, p.ex. démarrages ou arrêts sécurisés, suivis de version, contrôles de logiciel système, mises à jour sécurisées ou évaluation de vulnérabilité
G06Q 10/0635 - Analyse des risques liés aux activités d’entreprises ou d’organisations
G06Q 10/0637 - Gestion ou analyse stratégiques, p. ex. définition d’un objectif ou d’une cible pour une organisation; Planification des actions en fonction des objectifs; Analyse ou évaluation de l’efficacité des objectifs
G06Q 10/0639 - Analyse des performances des employés; Analyse des performances des opérations d’une entreprise ou d’une organisation
G06Q 10/067 - Modélisation d’entreprise ou d’organisation
G06Q 10/0875 - Gestion d’inventaires ou de stocks, p.ex. exécution des commandes, approvisionnement ou régularisation par rapport aux commandes Énumération ou classification des pièces, des fournitures ou des services, p.ex. nomenclatures
G06Q 10/101 - Création collaborative, p.ex. développement conjoint de produits ou de services
A given pixel of a pixel array includes various operation modes with each of the operation modes having a different conversion gain for the charge received from the photodetector of the pixel. When the modes are used in conjunction with one another, the dynamic range of the pixel can be increased. A readout circuit coupled to a photodetector within a given pixel includes a transfer gate between the photodetector and a gain mode select block that includes capacitors of different sizes and one or more switches to control which capacitors are to receive the charge from the photodetector. Depending on the state(s) of the one or more switches, different operation modes with different conversion gains can be selected to increase the dynamic range of the pixel. The adaptability of the readout circuit can allow for a high dynamic range even in extreme temperature environments by lowering the dark current.
H04N 25/59 - Commande de la gamme dynamique en commandant la quantité de charge stockable dans le pixel, p. ex. en modifiant le rapport de conversion de charge de la capacité du nœud flottant
H04N 25/63 - Traitement du bruit, p.ex. détection, correction, réduction ou élimination du bruit appliqué au courant d'obscurité
H04N 25/71 - Capteurs à dispositif à couplage de charge [CCD]; Registres de transfert de charge spécialement adaptés aux capteurs CCD
H04N 25/74 - Circuits de balayage ou d'adressage de la matrice de pixels
H04N 25/75 - Circuits pour fournir, modifier ou traiter des signaux d'image provenant de la matrice de pixels
H04N 25/77 - Circuits de pixels, p.ex. mémoires, convertisseurs A/N, amplificateurs de pixels, circuits communs ou composants communs
14.
System and method for active protection system range estimation
BAE Systems Information and Electronic Systems Integration Inc. (USA)
Inventeur(s)
Barfoot, David A.
Frank, Mark A.
Oles, David L.
Abrégé
A system and methods of an active protection system (or “APS”) for a platform. The APS has a threat cueing sensor provided at a first position on the platform where the threat cueing sensor detects a threat launched from a threat guidance system at a distance away from the platform. The APS also has a logic system operably connected to the threat cueing sensor where the logic system is adapted to determine an estimated location of the threat guidance system via a distance away from the platform. The APS also has a laser source operably connected to the logic system where the laser source emits a countermeasure beam directed at the estimated location of the threat guidance system to deter the threat away from the platform.
F41H 11/02 - Installations ou systèmes de défense anti-aérienne ou antimissiles
F41H 13/00 - Moyens d'attaque ou de défense non prévus ailleurs
G01C 21/16 - Navigation; Instruments de navigation non prévus dans les groupes en utilisant des mesures de la vitesse ou de l'accélération exécutées à bord de l'objet navigant; Navigation à l'estime en intégrant l'accélération ou la vitesse, c. à d. navigation par inertie
A computer-implemented method of modifying images of an environment for storage or transmission comprises receiving (204; 404; 604, 608) user input defining at least one selected feature of, or within, an environment. An image of a portion of the environment is captured (212; 410; 614) using an image capture device. The method can identify (216; 414; 618, 622) at least one object and/or at least one area in the image based on the at least one selected feature, and modify (218; 416; 624) the image to include or exclude the at least one identified object and/or the at least one identified area. The modified image can be stored or transmitted (220; 418, 420; 626, 628).
G06V 10/22 - Prétraitement de l’image par la sélection d’une région spécifique contenant ou référençant une forme; Localisation ou traitement de régions spécifiques visant à guider la détection ou la reconnaissance
Systems and methods for supplying cooled air in a vehicle, for example an aircraft, are disclosed. The system comprises: an air cycle machine (ACM) configured to compress and cool a flow of air so as to produce a flow of cooled air; an airflow path configured to direct the cooled air from the ACM to one or more parts of the vehicle; and a phase change material (PCM) heat exchanger arranged to further cool the air prior to said air reaching at least one part of the vehicle among said one or more parts, in addition to cooling provided by the ACM.
B64D 13/06 - Aménagements ou adaptations des appareils de conditionnement d'air pour équipages d'aéronefs, passagers ou pour emplacement réservé au fret l'air étant climatisé
BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC. (USA)
Inventeur(s)
Sherman, Matthew, J.
Sinha, Mritunjay
Yang, Lawrence
Abrégé
The system and method generates a pulse or a signal that is transmitted between a central processing unit or processor and an Ethernet integrated circuit card to program a trigger generator in the IC. The pulse is effectively a 1PPS signal that is provided to the IC, which may be in the form a field programmable gate array to enable timing synchronization. The trigger in the IC may also generates an interrupt to the processor so a driver in the CPU is instructed to set the next trigger. For the trigger to be accurately controlled, the control routine is implemented in the driver existing in kernel space rather than user space. A routine or protocol periodically polls the interrupt to determine when the trigger must be reset.
18.
NAVIGATION SYSTEM WITH EMBEDDED SOFTWARE DEFINED RADIO
BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC. (USA)
Inventeur(s)
Acheson, John E.
Kloos, Michael N.
James, Nathaniel L.
Dennis, Mitchell
Abrégé
Techniques are provided for employing an embedded software defined radio (SDR) in a navigation system. A navigation system implementing the techniques according to an embodiment includes a global positioning system (GPS) receiver configured to acquire and track received GPS signals. The system also includes an SDR configured to process received communication signals. The communication signals include timing data. The SDR is further configured to calculate position and navigation data based on a combination of the processed communication signals and the tracked GPS signals provided by the GPS receiver. The system further includes a system timer configured to provide a common time base for use by the GPS receiver and the SDR. The navigation system is implemented in an application specific integrated circuit (ASIC).
H04B 1/00 - TRANSMISSION - Détails des systèmes de transmission non caractérisés par le milieu utilisé pour la transmission
G01S 19/31 - Acquisition ou poursuite d'autres signaux en vue du positionnement
G01S 19/39 - Détermination d'une solution de navigation au moyen des signaux émis par un système de positionnement satellitaire à radiophares le système de positionnement satellitaire à radiophares transmettant des messages horodatés, p.ex. GPS [Système de positionnement global], GLONASS [Système mondial de satellites de navigation] ou GALILEO
19.
RADIO FREQUENCY (RF) ENVIRONMENT MONITOR AND RESPONSE SYSTEM
BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC. (USA)
Inventeur(s)
Klappert, Andrew E.
Saracino, Robert F.
Lavery, Richard J.
Ringlen, David C.
Bonino, Robert C.
Abrégé
Techniques are provided for dynamic performance enhancement of radio frequency (RF) based systems. A system implementing the techniques according to an embodiment includes a waveform decoder configured to perform message decoding operations on a received RF signal waveform and to provide a decoding validation result for the message decoding operations. The system also includes a waveform attribute analyzer configured to analyze physical characteristics of the received RF signal waveform and to provide an attribute validation result for the physical characteristics. The system further includes a statistics analyzer configured to generate a statistic based on the decoding validation results and the attribute validation results and a thresholding system configured to generate anomaly detection based on a comparison of the generated statistic to a threshold value. In some embodiments, the RF signal waveform is an Identification Friend or Foe (IFF) transponder waveform or an IFF interrogator waveform.
G01S 13/82 - Systèmes utilisant la reradiation d'ondes radio, p.ex. du type radar secondaire; Systèmes analogues dans lesquels des signaux de type continu sont transmis
G01S 13/78 - Systèmes utilisant la reradiation d'ondes radio, p.ex. du type radar secondaire; Systèmes analogues dans lesquels des signaux de type pulsé sont transmis effectuant la discrimination entre différents types de cibles, p.ex. radar pour l'identification ami–ennemi
G01S 7/28 - DÉTERMINATION DE LA DIRECTION PAR RADIO; RADIO-NAVIGATION; DÉTERMINATION DE LA DISTANCE OU DE LA VITESSE EN UTILISANT DES ONDES RADIO; LOCALISATION OU DÉTECTION DE LA PRÉSENCE EN UTILISANT LA RÉFLEXION OU LA RERADIATION D'ONDES RADIO; DISPOSITIONS ANALOGUES UTILISANT D'AUTRES ONDES - Détails des systèmes correspondant aux groupes , , de systèmes selon le groupe - Détails des systèmes à impulsions
G01S 19/46 - Détermination de position en combinant les mesures des signaux provenant du système de positionnement satellitaire à radiophares avec une mesure supplémentaire la mesure supplémentaire étant du type signal d'onde radioélectrique
G01S 5/02 - Localisation par coordination de plusieurs déterminations de direction ou de ligne de position; Localisation par coordination de plusieurs déterminations de distance utilisant les ondes radioélectriques
G01S 17/74 - Systèmes utilisant la reradiation d'ondes électromagnétiques autres que les ondes radio, p.ex. pour l'identification ami–ennemi
The present invention relates to an arrangement for feeding ammunition to a weapon (20). The weapon (20) is mounted to an elevation device (30) arranged to allow elevation movement of the weapon (20) about an elevation axis (Z1). The arrangement comprises a feeding chute (40; 140) connected at one end to the weapon (20). The feeding chute (40) comprises a set of elements (42; 142) assembled together in a stacked configuration. The set of elements (42; 142) is arranged about a shaft (44; 144) configured to be concentrically arranged relative to the elevation axis (Z1) so as to allow movement of individual elements of the set of elements (42; 142)) about said shaft (44; 144) in connection to elevation movement of the weapon (20) about the elevation axis (Z1). The invention also relates to a vehicle with an arrangement according to the present invention.
BAE SYSTEMS Information and Electronic Systems Integration Inc. (USA)
Inventeur(s)
Acheson, John E.
Kloos, Michael N.
James, Nathaniel L.
Dennis, Mitchell
Abrégé
Techniques are provided for employing an embedded software defined radio (SDR) in a navigation system. A navigation system implementing the techniques according to an embodiment includes a global positioning system (GPS) receiver configured to acquire and track received GPS signals. The system also includes an SDR configured to process received communication signals. The communication signals include timing data. The SDR is further configured to calculate position and navigation data based on a combination of the processed communication signals and the tracked GPS signals provided by the GPS receiver. The system further includes a system timer configured to provide a common time base for use by the GPS receiver and the SDR. The navigation system is implemented in an application specific integrated circuit (ASIC).
G01S 19/37 - Récepteurs - Détails de construction ou détails de matériel ou de logiciel de la chaîne de traitement des signaux - Détails de matériel ou de logiciel de la chaîne de traitement des signaux
22.
DUAL-POLARIZED, RIDGED WAVEGUIDE MAGIC-T FED, WIDEBAND CHEVRON SLOT PAIR ANTENNA ELEMENT FOR DIRECTION FINDING APPLICATIONS
BAE Systems Information and Electronic Systems Integration Inc. (USA)
Inventeur(s)
Kubwimana, Jean L.
Denno, Nicholas C.
St. Martin, Luke D.
Abrégé
An antenna element suited for direction finding (DF) with omni-directional radiation patterns utilizing a pair of chevron slots fed using a ridged waveguide magic tee (magic-t) and connected microstrip probes. The provided antenna element provides improved performance, power handling, and improved bandwidth compared to current monocone and/or slot antenna elements. The antenna element may be further realized utilizing additive manufacturing processes in combination with standard metal and polymer production techniques.
G01S 3/04 - Radiogoniomètres pour déterminer la direction d'où proviennent des ondes infrasonores, sonores, ultrasonores ou électromagnétiques ou des émissions de particules sans caractéristiques de direction utilisant des ondes radio - Détails
H01Q 1/42 - Enveloppes non intimement mécaniquement associées avec les éléments rayonnants, p.ex. radome
H01Q 1/48 - ANTENNES, c. à d. ANTENNES RADIO - Détails de dispositifs associés aux antennes Écrans de terre; Contrepoids
BAE SYSTEMS Information and Electronic Systems Integration Inc. (USA)
Inventeur(s)
Klappert, Andrew E.
Saracino, Robert F.
Lavery, Richard J.
Ringlen, David C.
Bonino, Robert C.
Abrégé
Techniques are provided for dynamic performance enhancement of radio frequency (RF) based systems. A system implementing the techniques according to an embodiment includes a waveform decoder configured to perform message decoding operations on a received RF signal waveform and to provide a decoding validation result for the message decoding operations. The system also includes a waveform attribute analyzer configured to analyze physical characteristics of the received RF signal waveform and to provide an attribute validation result for the physical characteristics. The system further includes a statistics analyzer configured to generate a statistic based on the decoding validation results and the attribute validation results and a thresholding system configured to generate anomaly detection based on a comparison of the generated statistic to a threshold value. In some embodiments, the RF signal waveform is an Identification Friend or Foe (IFF) transponder waveform or an IFF interrogator waveform.
G01S 7/02 - DÉTERMINATION DE LA DIRECTION PAR RADIO; RADIO-NAVIGATION; DÉTERMINATION DE LA DISTANCE OU DE LA VITESSE EN UTILISANT DES ONDES RADIO; LOCALISATION OU DÉTECTION DE LA PRÉSENCE EN UTILISANT LA RÉFLEXION OU LA RERADIATION D'ONDES RADIO; DISPOSITIONS ANALOGUES UTILISANT D'AUTRES ONDES - Détails des systèmes correspondant aux groupes , , de systèmes selon le groupe
G01S 7/28 - DÉTERMINATION DE LA DIRECTION PAR RADIO; RADIO-NAVIGATION; DÉTERMINATION DE LA DISTANCE OU DE LA VITESSE EN UTILISANT DES ONDES RADIO; LOCALISATION OU DÉTECTION DE LA PRÉSENCE EN UTILISANT LA RÉFLEXION OU LA RERADIATION D'ONDES RADIO; DISPOSITIONS ANALOGUES UTILISANT D'AUTRES ONDES - Détails des systèmes correspondant aux groupes , , de systèmes selon le groupe - Détails des systèmes à impulsions
G01S 7/292 - Récepteurs avec extraction de signaux d'échos recherchés
G01S 13/78 - Systèmes utilisant la reradiation d'ondes radio, p.ex. du type radar secondaire; Systèmes analogues dans lesquels des signaux de type pulsé sont transmis effectuant la discrimination entre différents types de cibles, p.ex. radar pour l'identification ami–ennemi
The present invention relates to a range extension device, particularly to a reversible range extension device (43), especially reversible base bleed device (47). There is provided a reversible range extension device (43), capable in use, of being reversibly engaged to a body (32) of an artillery shell, said range extension device comprising at least one energetic material (48), and an igniter, wherein the range extension device comprises a first end with an aperture (45), and second closed end (44), wherein the range extension device, in use, is selectively arranged to be in an active orientation or inert orientation, wherein in the active orientation the range extension device is arranged such that the aperture faces rearwardly away from the shell to allow the range extension device to function, and in the inert orientation the range extension device is arranged such that the aperture faces inwardly towards the shell.
F42B 10/40 - Dispositions pour augmenter la portée par la combustion d'une charge à vitesse de combustion lente, p.ex. projectiles du type à écoulement par le culot
F42B 10/44 - Culots spécialement adaptés pour réduire la traînée
A respirator comprising: an air supply unit arranged to deliver air at its output. A hood suitable for use with a powered air purifying respirator (PAPR), comprising a headtop with a shoulder cape extending therefrom, wherein the headtop encapsulates a user's head and neck, wherein said headtop comprises a transparent visor, and wherein the headtop comprises a resilient neck seal, said neck seal extending inwardly from the headtop to the user's neck, to create an enclosed volume, such that in use, said user's entire head moves freely therein
A62B 18/08 - Masques ou casques respiratoires, p.ex. pour assurer une protection contre les agents chimiques ou pour l'emploi à hautes altitudes - Parties constitutives des casques ou masques à gaz, p.ex. fenêtres, sangles, transmetteurs de voix, dispositifs de signalisation
A method to modify an image from a night vision camera is disclosed. The method comprises receiving at least one image from a night vision camera; modifying the at least one image, based on motion data from a tracker system and a shutter time of night vision camera, to remove smear from the image; and outputting the modified at least one image.
A method to modify an image from a night vision camera is disclosed. The method comprises receiving at least one image from a night vision camera; modifying the at least one image, based on motion data from a tracker system and a shutter time of night vision camera, to remove smear from the image; and outputting the modified at least one image.
FIG. 1 to be published with the application.
A blast attenuation device (100, 1100) for a gun tube (10). The blast attenuation device (100, 1100) has a first wall section (102, 1102) which defines a first chamber (104, 1104), which extends from an inlet end (106, 1106) having an inlet aperture (108, 1108) to an outlet end (110, 1100) having an outlet aperture (112, 1112). The blast attenuation device (100, 1100) also has a second wall section (122, 1122) which defines a second chamber (124, 1124), which extends from an inlet end (126, 1126) having an inlet aperture (128, 1128) to an outlet end (130, 1130) having an outlet aperture (132, 1132).
The present invention relates to an improved range extension device, particularly to a modular rocket assist device. A range extension device, capable in use of being reversibly engaged to a body of an artillery carrier shell, said shell comprising a payload cavity, said range extension device comprising an internal cavity comprising at least one energetic material charge, and an igniter, wherein the range extension device comprises a first region with an aperture which faces rearwardly, and second region with a closed end, wherein the closed end in use extends into the payload cavity of the carrier shell.
F42B 10/40 - Dispositions pour augmenter la portée par la combustion d'une charge à vitesse de combustion lente, p.ex. projectiles du type à écoulement par le culot
The present invention relates to the ruggedisation of electronic enclosures, particularly to the shock protection of racks, cabinets and enclosures of computers and servers.There is provided a ruggedised electronic enclosure, comprising a chassis, and a plurality of hardware components, wherein there is a reinforcement spine connected to the chassis and at least one hardware component, to prevent movement of said component during a shock-loading event.
BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC. (USA)
Inventeur(s)
Chrobak, Matthew F.
Batchelder, Jason H.
Kirsh, Samantha
Abrégé
A guidance kit for a projectile and method for suppressing a point-of-interest (POI) at a desired location away from the POI. The guidance kit includes at least one processor in the guidance kit. The guidance kit also includes a guidance protocol operatively in communication with the guidance kit and the at least one processor and having a set of angular offset modes. The guidance protocol of the guidance kit is configured to guide the projectile to at least one location relative to a desired point-of-interest (POI) upon or in response to activation of at least one angular offset mode of the set of angular offset modes.
F41G 7/36 - Systèmes de commande de guidage pour missiles autopropulsés basés sur des données prédéterminées de la position de la cible utilisant des références inertielles
31.
HIGH CAPACITY LIGHTWEIGHT VARIABLE BUOYANCY SYSTEM
BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC. (USA)
Inventeur(s)
Kemp, Mathieu P.
Romano, Christopher M.
Abrégé
Techniques and architectures are disclosed for a system capable of creating large changes in buoyancy that can be incorporated into underwater vehicles, embodiments of the system utilizing edge-welded, metal bellows disposed within a pressure vessel to balance a pressure differential across the bellows while using the bellows to displace fluid and thereby alter the buoyancy of a vehicle on which the system is disposed.
A thermal bridge for improving thermal transfer between a fuel element to a fuel block wherein there is provided a high temperature gas cooled nuclear reactor fuel block comprising a fuel channel and a coolant channel wherein the fuel channel comprises a fuel element, the fuel channel further comprising a thermal bridge thermally linking the fuel element and the fuel channel, wherein the thermal bridge comprises a melting point greater than the working temperature of the fuel block, thereby improving thermal transfer from the fuel element to the fuel block, thereby improving thermal transfer to the coolant channel.
G21C 1/07 - Réacteurs à boulets; Réacteurs à combustible granulaire
G21C 1/12 - Réacteurs hétérogènes, c. à d. dans lesquels le combustible et le modérateur sont séparés le modérateur étant hautement pressurisé, p.ex. réacteur à eau bouillante, réacteur à surchauffe intégrale, réacteur à eau pressurisée le modérateur et le réfrigérant étant différents ou séparés le modérateur étant solide, p.ex. réacteur du type Magnox
G21C 3/04 - Eléments combustibles - Détails de structure
G21C 5/02 - Structure du modérateur ou du cœur; Emploi de matériaux spécifiés comme modérateur - Détails
G21C 5/12 - Structure du modérateur ou du cœur; Emploi de matériaux spécifiés comme modérateur caractérisée par la composition, p.ex. le modérateur contenant des substances additionnelles qui assurent une meilleure résistance du modérateur
G21C 7/04 - Commande de la réaction nucléaire par utilisation des propriétés autorégulatrices des matériaux du réacteur de poisons combustibles
G21C 15/08 - Aménagement ou disposition de passages dans lesquels la chaleur est transférée au réfrigérant, p.ex. pour la circulation du réfrigérant à travers les supports des éléments combustibles provenant du matériau modérateur
A method of additive manufacturing an article from a feed material in a chamber includes evacuating at least some of a first gas from the chamber, thereby reducing a pressure therein from a first pressure to a second pressure and reducing the first gas from a first concentration to a second concentration. At least some of the first gas is then gettered from the chamber using a getter, thereby lowering the first gas concentration to a third concentration. The article is then additive manufactured from the feed material in the chamber using the getter as a substrate. The gettering comprises heating the getter at least in part using a fusion source, and the additive manufacturing comprises heating the feed material at least in part using the fusion source.
The present invention provides an alignment device for aligning a corner-casting during installation. The alignment device comprises a body adapted to fit within a corner-casting aperture and to engage with the edges of the aperture with a friction fit, wherein the upper surface of the body comprises a visual guide. A kit and method of installing a corner-casting are also provided.
B63B 25/24 - Moyens pour prévenir les déplacements indésirables de la cargaison, p.ex. fardage
B63B 25/28 - Installations de chargement, p.ex. pour le rangement ou l'arrimage; Navires spécialisés à cet effet pour charges sur le pont
B63B 73/60 - Construction ou assemblage de navires ou de structures marines, p.ex. coques ou plateformes en pleine mer caractérisés par l’automatisation, p.ex. l’utilisation de robots
B63B 73/20 - Construction ou assemblage de modules de navires préfabriqués ou de pièces autres que les sous-ensembles de coque, p.ex. de salles des moteurs, de gouvernails, d'hélices, de superstructures, de couchettes, de casiers ou de soutes
Air data estimation involves determining values of air data parameters such as airspeed, altitude, angle of attack and angle of sideslip. Accurate determination of air data parameter values is crucial to enable accurate control of an aircraft. An aircraft has an air data estimator comprising a machine learning model having been trained to predict air data parameter values from input values. The air data estimator is operable in real time on input values, where the input values are sensor data only from sensors internal to the aircraft or data derived from such sensor data
G01P 5/00 - Mesure de la vitesse des fluides, p.ex. d'un courant atmosphérique; Mesure de la vitesse de corps, p.ex. navires, aéronefs, par rapport à des fluides
G01P 13/02 - Indication de la direction uniquement, p.ex. par une girouette
B64D 43/02 - Aménagements ou adaptations des instruments pour indiquer la vitesse des aéronefs ou les conditions de décrochage
G01C 23/00 - Instruments combinés indiquant plus d’une valeur de navigation, p.ex. pour l’aviation; Dispositifs de mesure combinés pour mesurer plusieurs variables du mouvement, p.ex. la distance, la vitesse ou l’accélération
G06N 3/042 - Réseaux neuronaux fondés sur la connaissance; Représentations logiques de réseaux neuronaux
BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC. (USA)
Inventeur(s)
Lavely, Eugene M.
Weichman, Peter B.
Abrégé
An underwater sensing system includes a cable structure, a water surface mount coupled to the cable structure, and a processor. The cable structure is configured to be deployed in a vertical orientation underwater and includes one or more sensors along a length of the cable structure. The one or more sensors are configured to detect maritime data associated with one or more marine-based parameters in an underwater maritime region around the cable structure. The water surface mount is configured to be at least partially exposed above a surface of the underwater maritime region and includes a transmitter configured to transmit the maritime data. The processor is configured to access a maritime model comprising parameters associated with the maritime region and update the maritime model based on the maritime data. The maritime model can be used as an input, or otherwise made accessible, to a navigation system of an underwater vehicle.
A computer-implemented method of computing training data for training an air data estimator (106) to predict values of air data parameters (120) of an aircraft (100) comprises: selecting ground truth values of the air data parameters (120) according to a flight envelope of the aircraft (100). The method involves simulating corresponding values from avionics in the aircraft (100) by using stored empirical data about engines of the aircraft (100) and empirical data about the aircraft (100) obtained from wind tunnel testing, and rules of computational fluid dynamics.
G01C 23/00 - Instruments combinés indiquant plus d’une valeur de navigation, p.ex. pour l’aviation; Dispositifs de mesure combinés pour mesurer plusieurs variables du mouvement, p.ex. la distance, la vitesse ou l’accélération
A fuel delivery device for air-to-air refuelling, the device comprising: a fuel outlet; and an optical transceiver, wherein the optical transceiver is configured to: illuminate the fuel delivery device to provide visual indication to an aircraft receiving fuel; and, transmit and receive data via optical wireless communication to the aircraft receiving fuel from the fuel delivery device.
A rake assembly (100) for measuring fluid flow parameters in a fluid flow rig (10), the rake assembly (100) comprising: a housing (102) comprising a wall (104) which defines a flow passage (110), with a flow inlet (112) and a flow outlet (114), the flow passage (110) extending from the flow inlet (112) to the flow outlet (114). The housing wall (104) defines an access aperture (106). The housing (102) is configured to define an Aerodynamic Instrument Plane (AIP) at, or part of the way downstream of, the flow inlet (112). There is provided an instrumentation arm (120) which extends from a leading edge end (122) to a trailing edge end (124) and configured to be removably mounted to the housing (102). The instrumentation arm (120) is operable such that, when mounted to the housing wall (104) the instrumentation arm (120) extends through the access aperture (106) to extend at least part of the way across the flow passage (110), the access aperture (106) and instrumentation arm (120) sized so that: the instrumentation arm (120) can be removed from the casing wall (104) by drawing the instrumentation arm (120) through the access aperture (106); and the instrumentation arm (120) can be installed on the casing wall (104) by inserting the instrumentation arm (120) through the access aperture (106).
G01F 15/18 - Supports ou moyens de raccordement pour les compteurs
G01F 15/14 - Revêtements, p.ex. avec un matériau spécial
G01P 5/165 - Agencement ou structure des tubes de Pitot
F01D 21/00 - Arrêt des "machines" ou machines motrices, p.ex. dispositifs d'urgence; Dispositifs de régulation, de commande ou de sécurité non prévus ailleurs
F01D 17/08 - Aménagement des éléments sensibles sensibles aux conditions de fonctionnement du fluide énergétique, p.ex. à la pression
A rake assembly (100) for measuring fluid flow parameters in a fluid flow rig (10), the rake assembly (100) comprising : a rake assembly support frame (500); a housing (102) mounted on the rake assembly support frame (500); the housing (102) comprising a wall (104) which defines a flow passage (110), with a flow inlet (112) and a flow outlet (114), the flow passage (110) extending from the flow inlet (112) to the flow outlet (114). The housing (102) is cylindrical and is centred on a longitudinal axis (130). An instrumentation arm (120) extends from a leading edge end (122) to a trailing edge end (124), and the instrumentation arm (120) extends from the housing wall (104) to extend at least part of the way across the flow passage (110), the leading edge end (122) located in an Aerodynamic Instrument Plane (AIR); the housing (102) being rotatably mounted to the rake assembly support frame (500); such that the housing (102) and instrumentation arm (120) are operable to rotate at least part of the way around the longitudinal axis (130).
G01F 15/18 - Supports ou moyens de raccordement pour les compteurs
G01F 15/14 - Revêtements, p.ex. avec un matériau spécial
G01P 5/165 - Agencement ou structure des tubes de Pitot
G01M 9/06 - Dispositions pour la mesure spécialement adaptées aux tests aérodynamiques
F01D 17/08 - Aménagement des éléments sensibles sensibles aux conditions de fonctionnement du fluide énergétique, p.ex. à la pression
F01D 21/00 - Arrêt des "machines" ou machines motrices, p.ex. dispositifs d'urgence; Dispositifs de régulation, de commande ou de sécurité non prévus ailleurs
F01D 25/28 - Dispositions pour le support ou le montage, p.ex. pour les carters de turbines
G01L 15/00 - Dispositifs ou appareils pour la mesure simultanée de plusieurs valeurs de la pression des fluides
G01M 15/14 - Test des moteurs à turbine à gaz ou des moteurs de propulsion par réaction
An undercarriage unit is provided. The undercarriage unit comprises: a rotatable wheel; at least one electromagnet for releasably coupling the undercarriage unit to the aircraft; a switch for selectively activating and deactivating the at least one electromagnet; and a controller arranged to actuate the switch. An aircraft having the undercarriage unit is also provided.
A flow body unit (600) for a fluid flow rig (10) for simulating fluid flow patterns; the flow body unit (600) comprising: a flow body support frame (700); a core member (800) extending from the flow body support frame (700) along a flow body unit longitudinal axis (630); the core member (800) having a leading edge end (822) and a trailing edge end (824), the core member (800) mounted to the flow body support frame (700) at its trailing edge end (824) such that it extends away from the flow body support frame (700) to terminate at a free end (834) defined by the leading edge end (822).
B63B 49/00 - Aménagements relatifs aux instruments nautiques ou d'aide à la navigation
B64D 43/00 - Aménagements ou adaptations des instruments
B64F 5/60 - Test ou inspection des composants ou des systèmes d'aéronefs
F03B 11/00 - "MACHINES" OU MACHINES MOTRICES À LIQUIDES - Parties constitutives ou détails non couverts par les groupes ou présentant un intérêt autre que celui visé par ces groupes
G01L 5/13 - Appareils ou procédés pour la mesure des forces, du travail, de la puissance mécanique ou du couple, spécialement adaptés à des fins spécifiques pour la mesure de la puissance de traction ou propulsive des véhicules
G01P 5/165 - Agencement ou structure des tubes de Pitot
According to some examples, an energy harvesting assembly for a projectile comprises an inlet provided at the tip of a casing of the projectile, multiple outlets provided circumferentially around an outer surface of the casing proximate the tip, and an airflow channel structure extending from the inlet in a generally axial direction through a turbine to the multiple outlets.
F42C 15/295 - Dispositifs d'armement des fusées; Dispositifs de sécurité pour empêcher l'explosion prématurée des fusées ou des charges actionnés par l'écoulement d'un matériau fluent, p.ex. du plomb, un fluide actionnés par une turbine ou une hélice; Moyens de montage pour celles-ci
F42B 12/38 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché pour la signalisation du type traçant
According to the present disclosure, there is provided a fuze system for attaching to a munition body, the fuze system comprising: a body comprising a foremost section; a fuze located in the body; a power generator, attached to the body, for generating electrical power and providing it to the fuze system, the power generator configured to generate electrical power by interacting with an airstream around the fuze system, wherein at least a part of the power generator is located behind the foremost section, the at least a part of the power generator being arranged to rotate relative to the foremost section of the body.
The present disclosure relates to a modular muzzle brake assembly for an artillery weapon or cannon. The modular muzzle brake assembly comprises a plurality of modules configured to be releasably coupled together to define a passage for a projectile such that, when the artillery weapon or cannon is fired, propellant gas urges the projectile to pass through the passage. The plurality of modules include a plurality of baffles configured to divert at least a portion of the propellant gas in the passage. The present disclosure also relates to a kit of parts for a modular muzzle brake assembly.
The invention relates to a method for the flow synthesis manufacture of RDX, comprising the steps of preparing input flow reagent A, comprising hexamine dissolved in nitric acid with a concentration less than 92%, preparing input flow reagent B comprising 99% concentration nitric acid, causing the input flow reagents A and B to enter a flow reactor at a flow rate, so as to cause a total nitric acid concentration of greater than 93%, in said flow reactor, cooling the reaction chamber to less than 30° C., causing the output mixed flow to be quenched.
C07D 251/06 - Composés hétérocycliques contenant des cycles triazine-1, 3, 5 non condensés avec d'autres cycles ne comportant pas de liaisons doubles entre chaînons cycliques ou entre chaînons cycliques et chaînons non cycliques avec des hétéro-atomes liés directement aux atomes d'azote du cycle
C06B 25/34 - Compositions contenant un composé organique nitré le composé étant une amine nitrée acyclique, cyclanique ou hétérocyclique
In some example, a method for regulating a trajectory of a projectile comprises adjusting the position of a mass within a cavity defined by a jacket of the projectile, whereby to modify a centre of gravity of the projectile.
A computer-implemented method of determining utilisation of resources in a system having autonomous capability. The method comprises receiving (304) a plurality of input data from a respective plurality of components of the system, and receiving (302) rule set data comprising a plurality of rules. Each of the plurality of rules is configured to determine an integrity value for the input data. The method further comprises processing (306) the plurality of input data and the rule set data to generate an integrity value for each of the plurality of input data, and using (308) the integrity values to determine utilisation of resources of the system.
G06F 21/55 - Détection d’intrusion locale ou mise en œuvre de contre-mesures
B60W 40/10 - Calcul ou estimation des paramètres de fonctionnement pour les systèmes d'aide à la conduite de véhicules routiers qui ne sont pas liés à la commande d'un sous-ensemble particulier liés au mouvement du véhicule
G08G 3/00 - Systèmes de commande du trafic pour les véhicules marins
B60W 50/04 - COMMANDE CONJUGUÉE DE PLUSIEURS SOUS-ENSEMBLES D'UN VÉHICULE, DE FONCTION OU DE TYPE DIFFÉRENTS; SYSTÈMES DE COMMANDE SPÉCIALEMENT ADAPTÉS AUX VÉHICULES HYBRIDES; SYSTÈMES D'AIDE À LA CONDUITE DE VÉHICULES ROUTIERS, NON LIÉS À LA COMMANDE D'UN SOUS-ENSEMBLE PARTICULIER - Détails des systèmes d'aide à la conduite des véhicules routiers qui ne sont pas liés à la commande d'un sous-ensemble particulier pour surveiller le fonctionnement du système d'aide à la conduite
B60W 60/00 - Systèmes d’aide à la conduite spécialement adaptés aux véhicules routiers autonomes
49.
TRIPLE MODULAR REDUNDANCY (TMR) RADIATION HARDENED MEMORY SYSTEM
BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC. (USA)
Inventeur(s)
Moser, David D.
Ferguson, Richard J.
Stanley, Daniel L.
Abrégé
Techniques are provided for a radiation hardened memory system. A memory system implementing the techniques according to an embodiment includes a redundancy comparator configured to detect differences between data stored redundantly in a first memory, a second memory, and a third memory. The redundancy comparator is further configured to identify a memory error based on the detected differences. The memory system also includes an error collection buffer configured to store a memory address associated with the memory error, and a memory scrubber circuit configured to overwrite, at the memory address associated with the memory error, erroneous data with corrected data. The corrected data is based on a majority vote among the three memories. The memory system further includes a priority arbitrator configured to arbitrate between the memory scrubber overwriting and functional memory accesses associated with software execution performed by a processor configured to utilize the memory system.
G06F 11/10 - Détection ou correction d'erreur par introduction de redondance dans la représentation des données, p.ex. en utilisant des codes de contrôle en ajoutant des chiffres binaires ou des symboles particuliers aux données exprimées suivant un code, p.ex. contrôle de parité, exclusion des 9 ou des 11
G06F 11/18 - Détection ou correction d'erreur dans une donnée par redondance dans le matériel en utilisant un masquage passif du défaut des circuits redondants, p.ex. par logique combinatoire des circuits redondants, par circuits à décision majoritaire
G11C 8/00 - Dispositions pour sélectionner une adresse dans une mémoire numérique
H03K 19/003 - Modifications pour accroître la fiabilité
H03M 13/00 - Codage, décodage ou conversion de code pour détecter ou corriger des erreurs; Hypothèses de base sur la théorie du codage; Limites de codage; Méthodes d'évaluation de la probabilité d'erreur; Modèles de canaux; Simulation ou test des codes
BAE Systems Information and Electronic Systems Integration Inc. (USA)
Inventeur(s)
Sherman, Matthew J.
Sinha, Mritunjay
Yang, Lawrence
Abrégé
The system and method generates a pulse or a signal that is transmitted between a central processing unit or processor and an Ethernet integrated circuit card to program a trigger generator in the IC. The pulse is effectively a 1PPS signal that is provided to the IC, which may be in the form a field programmable gate array to enable timing synchronization. The trigger in the IC may also generates an interrupt to the processor so a driver in the CPU is instructed to set the next trigger. For the trigger to be accurately controlled, the control routine is implemented in the driver existing in kernel space rather than user space. A routine or protocol periodically polls the interrupt to determine when the trigger must be reset.
Techniques are provided for x-ray onset detection for an intraoral dental sensor. A methodology implementing the techniques according to an embodiment includes calculating a plurality of superpixel values for each of a plurality of rows of detector pixels of a sensor. Each of the superpixel values is based on a sum of pixel values of a set of pixels associated with the superpixel value, the set of pixels selected from the detection row of a current frame of the sensor. The method also includes calculating a difference between each of the superpixel values and a corresponding stored superpixel value generated from a previous sensor frame and determining if the differences exceed a superpixel threshold value. The method further includes incrementing a hit counter in response to the determination and generating a detection signal if the hit counter exceeds a hit count threshold, otherwise proceeding to process the next detection row.
H04N 5/369 - Transformation d'informations lumineuses ou analogues en informations électriques utilisant des capteurs d'images à l'état solide [capteurs SSIS] circuits associés à cette dernière
H04N 5/378 - Circuits de lecture, p.ex. circuits d’échantillonnage double corrélé [CDS], amplificateurs de sortie ou convertisseurs A/N
H04N 5/351 - Réglage du capteur SSIS en fonction de la scène, p.ex. luminosité ou mouvement dans la scène
A61B 6/14 - Applications ou adaptations à l'art dentaire
Techniques are provided for x-ray onset detection for an intraoral dental sensor. A methodology implementing the techniques according to an embodiment includes calculating a plurality of superpixel values for each of a plurality of rows of detector pixels of a sensor. Each of the superpixel values is based on a sum of pixel values of a set of pixels associated with the superpixel value, the set of pixels selected from the detection row of a current frame of the sensor. The method also includes calculating a difference between each of the superpixel values and a corresponding stored superpixel value generated from a previous sensor frame and determining if the differences exceed a superpixel threshold value. The method further includes incrementing a hit counter in response to the determination and generating a detection signal if the hit counter exceeds a hit count threshold, otherwise proceeding to process the next detection row.
An apparatus comprises: a display device including an optically transparent display screen for displaying images to a user; a sensor configured to track a viewing direction and/or a viewing position of the user; a detector configured to determine a location of a target viewable by the user through the display screen; and a controller configured to control the display device to display an image on the display screen at screen coordinates corresponding with the viewable target, using the tracked viewing direction and/or the tracked viewing position of the user and the determined location of the target.
G09G 3/00 - Dispositions ou circuits de commande présentant un intérêt uniquement pour l'affichage utilisant des moyens de visualisation autres que les tubes à rayons cathodiques
G06T 7/70 - Détermination de la position ou de l'orientation des objets ou des caméras
G06F 3/01 - Dispositions d'entrée ou dispositions d'entrée et de sortie combinées pour l'interaction entre l'utilisateur et le calculateur
A laser weapon countermeasure device is described. The laser weapon countermeasure device comprises a sealed capsule having a filler disposed therein. The filler comprises either: a reflective particulate metal; or a precursor for a reflective metal or reflective metal alloy. The capsule is configured to burst in air such that the filler disperses into an aerosol. A countermeasure launcher and a vehicle comprising a countermeasure launcher are also described.
F42B 12/70 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché pour la signalisation pour la libération de corps solides individuels pour la libération de paillettes antiradar ou de matériaux à émission infrarouge
A method of providing a pre-impregnated tape (15), comprising reinforcement fibres (11), for manufacture of fibre-reinforced composite parts, the method comprising: non-uniformly impregnating (14) an additive composition in and/or on a tape (13), comprising reinforcement fibres, to provide the pre-impregnated tape, wherein the additive composition comprises a resin and an additive.
B29C 70/88 - Façonnage de matières composites, c. à d. de matières plastiques comprenant des renforcements, des matières de remplissage ou des parties préformées, p.ex. des inserts caractérisées principalement par des propriétés spécifiques, p.ex. électriquement conductrices ou renforcées localement
B29B 15/12 - Revêtement ou imprégnation d'agents de renforcement de longueur indéfinie
B29C 70/02 - Façonnage de matières composites, c. à d. de matières plastiques comprenant des renforcements, des matières de remplissage ou des parties préformées, p.ex. des inserts comprenant des combinaisons de renforcements et de matières de remplissage dans une matrice, formant une ou plusieurs couches, avec ou sans couches non renforcées ou non remplies
C08J 5/24 - Imprégnation de matériaux avec des prépolymères pouvant être polymérisés en place, p.ex. fabrication des "prepregs"
B29C 70/38 - Empilage automatisé, p.ex. utilisant des robots, par application de filaments selon des modèles prédéterminés
56.
FUNCTIONALIZED TAPE FOR THE MANUFACTURE OF FIBRE-REINFORCED COMPOSITE PARTS
A method of providing a functionalized veil or tape for manufacture of fibre-reinforced composite parts, the method comprising: depositing functional particles (12) in and/or on a veil or tape (11), by flowing F a fluid (13), through the veil or tape (11), to provide the functionalized veil or tape, wherein the veil or tape comprises reinforcement fibres and the fluid includes functional particles.
B29C 70/02 - Façonnage de matières composites, c. à d. de matières plastiques comprenant des renforcements, des matières de remplissage ou des parties préformées, p.ex. des inserts comprenant des combinaisons de renforcements et de matières de remplissage dans une matrice, formant une ou plusieurs couches, avec ou sans couches non renforcées ou non remplies
B29B 15/12 - Revêtement ou imprégnation d'agents de renforcement de longueur indéfinie
B29C 70/88 - Façonnage de matières composites, c. à d. de matières plastiques comprenant des renforcements, des matières de remplissage ou des parties préformées, p.ex. des inserts caractérisées principalement par des propriétés spécifiques, p.ex. électriquement conductrices ou renforcées localement
57.
IMPROVEMENTS IN AND RELATING TO VIBRATION CONTROL SYSTEMS
According to the present invention there is provided an active vibration control system comprising: a driving mechanism and a control mechanism comprising an electromagnetic actuator, the driving mechanism being operable to apply a force on a base structure to which the active vibration control system is attachable such that vibrations of the base structure are actively controllable by the application of said force, wherein the driving mechanism and control mechanism are relatively moveable such that the active vibration control system has at least two modes of vibration, and wherein movement of the driving mechanism causes movement of at least a part of the control mechanism.
F16F 7/10 - Amortisseurs de vibrations; Amortisseurs de chocs utilisant un effet d'inertie
F16F 6/00 - Ressorts magnétiques; Ressorts magnétiques à fluide
H02K 33/18 - Moteurs avec un aimant, un induit ou un système de bobines à mouvement alternatif, oscillant ou vibrant avec des systèmes de bobines se déplaçant, du fait de mises sous tension intermittentes ou inversées, par interaction avec un système de champ magnétique fixe, p.ex. des aimants permanents
58.
IMPROVEMENTS IN AND RELATING TO VIBRATION CONTROL SYSTEMS
According to the present invention there is provided an active vibration control system comprising: an electromagnetic actuator; a magnetic element; and a solenoid, the electromagnetic actuator being operable to apply a force on a base structure to which the active vibration control system is attachable such that vibrations of the base structure are actively controllable by the application of said force, wherein the electromagnetic actuator is operable to cause movement of the magnetic element through the solenoid and the solenoid is operable to apply a force on the magnetic element.
There is provided an arming apparatus for a store, the apparatus comprising: a first attachment system and a second attachment system; a linking connector coupled with the first attachment system and the second attachment system; and an arming clip; wherein each of the first attachment system and the second attachment system comprises: a first frangible connector coupled with the arming unit and the linking connector; and a second frangible connector comprising a first end coupled with the linking connector and a second end comprising a clip, the second end being configured to pass through a lug of said store and then couple to the second frangible connector.
BAE Systems Information and Electronic Systems Integration Inc. (USA)
Inventeur(s)
Steenson, Jr., James H.
Cullen, Joseph P.
Abrégé
Techniques to dynamically adjust the corner frequency of a high-pass filter in response to a time-domain amplitude value of an output signal, thereby preserving accuracy while promptly recovering the signal's baseline value. A system can be configured to filter frequency-domain values of an input signal based on a filtering characteristic. The filtering characteristic can be set dynamically in response to a time-domain value of an amplitude of an output signal. The filtering characteristic can comprise a corner frequency, and the system can include a high-pass filter configured to filter out frequency components at frequencies lower than the corner frequency. The system is configured to dynamically change the corner frequency from a first value to a second value, in response to the time-domain value of the amplitude crossing a threshold value. The system may dynamically change the corner frequency within a time interval after the crossing.
According to the present invention there is provided an active vibration control system comprising: an electromagnetic actuator and a control element, the electromagnetic actuator being operable to apply a force on a base structure to which the active vibration control system is attachable such that vibrations of the base structure are actively controllable by the application of said force, wherein the electromagnetic actuator and control element are relatively moveable such that the active vibration control system has at least two modes of vibration, and wherein movement of the electromagnetic actuator causes movement of at least a part of the control element.
F16F 7/10 - Amortisseurs de vibrations; Amortisseurs de chocs utilisant un effet d'inertie
F16F 6/00 - Ressorts magnétiques; Ressorts magnétiques à fluide
H02K 33/18 - Moteurs avec un aimant, un induit ou un système de bobines à mouvement alternatif, oscillant ou vibrant avec des systèmes de bobines se déplaçant, du fait de mises sous tension intermittentes ou inversées, par interaction avec un système de champ magnétique fixe, p.ex. des aimants permanents
There is provided an arming apparatus for a store, the apparatus comprising: a first attachment system and a second attachment system; a linking connector coupled with the first attachment system and the second attachment system; and an arming clip; wherein each of the first attachment system and the second attachment system comprises: a first frangible connector coupled with the arming unit and the linking connector; and a second frangible connector coupled with the linking connector and the store. The linking connector is coupled to the first attachment system via a first coupling arrangement and is coupled to the second attachment system via a second coupling arrangement, wherein the first coupling arrangement and the second coupling arrangement are different. Each of the first coupling arrangement and the second coupling arrangement are manually secure.
F42C 15/40 - Dispositifs d'armement des fusées; Dispositifs de sécurité pour empêcher l'explosion prématurée des fusées ou des charges dans lesquels l'action de sécurité ou d'armement s'effectue électriquement
F42C 15/44 - Dispositions pour désarmer des fusées ou pour les rendre inoffensives après l'armement, p.ex. après le lancement
B64D 1/06 - Mécanismes de largage des bombes; Trappes de la soute à bombes
A coating for an optical surface for reducing secondary reflections from narrow wavelength band image sources, the coating comprising multiple notch filters located at different predetermined wavelength regions
BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC. (USA)
Inventeur(s)
Steenson, James, H., Jr.
Cullen, Joseph, P.
Abrégé
Techniques to dynamically adjust the corner frequency of a high-pass filter in response to a time-domain amplitude value of an output signal, thereby preserving accuracy while promptly recovering the signal's baseline value. A system can be configured to filter frequency-domain values of an input signal based on a filtering characteristic. The filtering characteristic can be set dynamically in response to a time-domain value of an amplitude of an output signal. The filtering characteristic can comprise a corner frequency, and the system can include a high-pass filter configured to filter out frequency components at frequencies lower than the corner frequency. The system is configured to dynamically change the corner frequency from a first value to a second value, in response to the time-domain value of the amplitude crossing a threshold value. The system may dynamically change the corner frequency within a time interval after the crossing.
BAE SYSTEMS Information and Electronic Systems Integration Inc. (USA)
Inventeur(s)
Kemp, Mathieu P.
Romano, Christopher M.
Abrégé
Techniques and architectures are disclosed for a system capable of creating large changes in buoyancy that can be incorporated into underwater vehicles, embodiments of the system utilizing edge-welded, metal bellows disposed within a pressure vessel to balance a pressure differential across the bellows while using the bellows to displace fluid and thereby alter the buoyancy of a vehicle on which the system is disposed.
A method of using a robotic arm to position a part of an object at a first target position with respect to an object build frame comprising obtaining, by the robotic arm, the part; determining a move operation to apply to the part that moves the part to a second target position spatially separated from the object build frame; moving, by the robotic arm, the part according to the move operation; obtaining an actual position of the part; determining a correction operation to apply to the part that moves the part from the actual position to the second target position; moving, by the robotic arm, the part according to the correction operation; determining a relative move operation to apply to the part that moves the part from the second target position to the first target position; and moving, by the robotic arm, the part according to the relative move operation.
A control unit for a maritime vessel configurable to monitor integrity of an operation and/or data used by a system of the maritime vessel. The control unit comprises: a first computing element configured to process a first input signal to generate a first output; and a second computing element configured to process a second input signal to generate a second output. The first computing element is configured to compare the first output with the second output, and if the first output and the second output do not match within a predetermined tolerance then the first computing element is configured to initiate and/or perform a preventive action. The second computing element is configured to compare the second output with the first output, and if the first output and the second output do not match within the predetermined tolerance then the second computing element is configured to initiate and/or perform the preventive action.
H04Q 9/00 - Dispositions dans les systèmes de commande à distance ou de télémétrie pour appeler sélectivement une sous-station à partir d'une station principale, sous-station dans laquelle un appareil recherché est choisi pour appliquer un signal de commande ou
G08C 25/00 - Dispositions pour prévenir ou corriger les erreurs; Dispositions de contrôle
G05B 9/03 - Dispositions de sécurité électriques avec une boucle à canal multiple, c. à d. systèmes de commande redondants
G06F 11/16 - Détection ou correction d'erreur dans une donnée par redondance dans le matériel
H04L 67/12 - Protocoles spécialement adaptés aux environnements propriétaires ou de mise en réseau pour un usage spécial, p.ex. les réseaux médicaux, les réseaux de capteurs, les réseaux dans les véhicules ou les réseaux de mesure à distance
The invention relates to a common carrier munition ammunition device, more particularly to common carrier payload delivery shell. There is provided a common carrier munition suitable for use for a high explosive comprising a tail unit, a main body which comprises a payload cavity for receiving a payload, a fuze, and located between said main body and the fuze an ogive element, wherein the payload comprises a removable liner, wherein the removable liner comprises a high explosive, such that said removable liner and high explosive may be removed from the payload cavity.
F42B 33/02 - Remplissage des cartouches, des projectiles ou des fusées; Introduction de charges propulsives ou explosives
F42B 12/20 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant
F42B 12/22 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché du type à explosif brisant à structure de corps de fragmentation
The present disclosure relates to a mobile gun system. The mobile gun system comprises a chassis and a gun barrel mounted to the chassis such that when a projectile is fired from the gun barrel a recoil force causes recoil movement of the chassis. The mobile gun system further comprises a braking system for retarding the recoil movement of the chassis due to the recoil force from the firing of the projectile from the gun barrel. The mobile gun system further comprises a controller configured to control the braking system to retard said recoil movement of the chassis after a peak loading condition due to the firing of the projectile has passed. The present disclosure also relates to a method of operating a mobile gun system.
A method to autonomously taxi an aircraft is disclosed. The method comprises receiving, by a processing means, a route intended for the aircraft 310. Obtaining, by the processing means, a route line based on the route 320. Determining, by the processing means, at least one route feature along the route line 330. Determining, by the processing means, a deviation of a nosewheel of the aircraft from the route line based on a current position of the aircraft provided by the aircraft global navigation satellite system (GNSS) 340. Outputting, by the processing means, an adjustment of an angle of the nosewheel to correct the deviation from the route based on the deviation of the nosewheel 350. Outputting, by the processing means, an adjustment of the speed of the aircraft based on a current position on the route line and a proximity to the at least one determined route feature 360.
BAE SYSTEMS Information and Electronic Systems Integration Inc. (USA)
Inventeur(s)
Fitzgerald, Patrick D.
Kaylor, Brant M.
Abrégé
The disclosed method enables efficient registration and correction of random vertical and horizontal offsets of a plurality of images of a feature to enable combination thereof with maximum noise suppression. The method includes obtaining image cross correlations and estimating correlation peaks. If a correlation peak cannot be uniquely determined for a given correlation, all candidates are retained. An improved robust weighted regression is applied thereto to obtain estimates of the image shifts. Dimensional symmetry is exploited to remove redundancy from the weighted normal equation, and computational requirements are further reduced by analytically determining the coefficients matrix and the inhomogeneous matrix, thereby circumventing conventional computations. Solution of the resulting consistent, full rank, linear system requires only matrix inversion. For N images, the present method thereby increases computation speed and reduces storage by approximately N2.
The present invention relates to an Electronic Unit (1), EU, for a tactile cueing apparatus for a vehicle. The tactile cueing apparatus augments feel for an operator of the vehicle. The EU comprises a first channel (307A, 407A). The first channel (307A, 407A) is configured to monitor communication for determining a control mode of the first channel (307A, 407A). The control mode comprises a Reversionary Active Mode, the Reversionary Active Mode providing a control characteristic for limited augmented feel capability to the operator of the vehicle; and an Active Mode, wherein the Active Mode providing a control characteristic for fully augmented feel capability to the operator of the vehicle.
Disclosed is a RADAR system comprising a Constant False Alarm Rate, CFAR, function, wherein the CFAR function is arranged such that a detection threshold is determined at least partly on the basis of a window length which is of a variable length and the variable length is determined on the basis of a degree of variability in a first number of previous amplitude measurements of received signals.
According to the present disclosure, there is provided a structural damper for providing damping of a primary structure, the structural damper comprising: a first acoustic black hole, ABH; a second ABH; and an actuator provided in contact with the first ABH and second ABH, wherein the actuator is configured to apply an actuating force to the first ABH and the second ABH.
G10K 11/178 - Procédés ou dispositifs de protection contre le bruit ou les autres ondes acoustiques ou pour amortir ceux-ci, en général utilisant des effets d'interférence; Masquage du son par régénération électro-acoustique en opposition de phase des ondes acoustiques originales
F16F 15/02 - Suppression des vibrations dans les systèmes non rotatifs, p.ex. dans des systèmes alternatifs; Suppression des vibrations dans les systèmes rotatifs par l'utilisation d'organes ne se déplaçant pas avec le système rotatif
A drone (10) operable for flight. The drone has a fuselage (100) having a length (L) extending along an x-axis, the fuselage (100) comprising a port side fuselage section (102) spaced apart from a starboard side fuselage section (104) to define a slot (106) therebetween which extends along the length (L) of the fuselage (100). There is also provided a cannon (200) having a barrel (202). The cannon (200) is pivotably mounted in the slot (106) to the port side fuselage section (102), and/or pivotably mounted to the starboard side fuselage section (104), by a trunnion mounting assembly (110) having a trunnion axis (112) which extends at right angles to the x-axis. The barrel (202) is operable to pivot about the trunnion axis (112) to move over, and/or be positioned at, a range of angles relative to the x-axis direction.
F41A 27/08 - Paliers, p.ex. tourillons; Dispositions pour le freinage ou le blocage
B64D 7/06 - Agencement à bord aéronefs des équipements militaires, p.ex. des armes, des accessoires d'armement ou des blindages de protection; Adaptations des installations d'armement aux aéronefs les armes étant des armes à feu mobiles
B64C 39/02 - Aéronefs non prévus ailleurs caractérisés par un emploi spécial
B64C 39/04 - Aéronefs non prévus ailleurs à fuselages ou poutres de queue multiples
B64U 101/15 - Véhicules aériens sans pilote spécialement adaptés à des utilisations ou à des applications spécifiques à la guerre conventionnelle ou électronique
B64U 101/30 - Véhicules aériens sans pilote spécialement adaptés à des utilisations ou à des applications spécifiques à l’imagerie, à la photographie ou à la vidéographie
B64U 101/60 - Véhicules aériens sans pilote spécialement adaptés à des utilisations ou à des applications spécifiques au transport de marchandises autres que des armes
BAE Systems Information and Electronic Systems Integration Inc. (USA)
Inventeur(s)
Adasczik, Walter K.
Lizotte, Jeffrey A.
Remeis, Peter H.
Collard, Nicholas
Abrégé
A switch assembly and a method of effecting a battery to initiate. The switch assembly includes a support that is adapted to operably engage with a battery. The switch assembly also include a slide operably engaged with the support and moveable in a first direction relative to the support between a primed position and a released position. The switch assembly also includes a cover operably engaged with the support and enclosing the slide. The switch assembly also includes a firing pin mechanism operably engaged with the support, the slide, and the cover and moveable in a second direction relative to the slide and the support. In the switch assembly, the second direction of the firing pin mechanism is different than the first direction of the slide.
F42C 15/21 - Dispositifs d'armement des fusées; Dispositifs de sécurité pour empêcher l'explosion prématurée des fusées ou des charges dans lesquels une goupille de sécurité ou un verrou est enlevé pour armer la fusée, p.ex. retiré du percuteur en utilisant la force d'un ressort
There is provided a heat exchanger comprising: a housing comprising: an inlet at a proximal end for receiving a first fluid; and an outlet, downstream of the inlet at the distal end of the housing, through which the fluid is configured to exit the housing; and a plurality of heat exchanger cores within the housing, wherein the plurality of heat exchanger cores meet at a junction and diverge from each other towards one of the inlet or the outlet of the housing; wherein the plurality of heat exchanger cores comprises a plate fin arrangement; and, wherein the plurality of heat exchanger cores comprise one or more first flow paths through which the first fluid can pass through the heat exchanger cores, in use.
F28D 9/00 - Appareils échangeurs de chaleur comportant des ensembles de canalisations fixes en forme de plaques ou de laminés pour les deux sources de potentiel calorifique, ces sources étant en contact chacune avec un côté de la paroi d'une canalisation
A rotor unit assembly (10) having a rotor unit (90). The rotor unit (90) comprises a chamber (104) and a rotor (200) located within the chamber (104). The rotor (200) has a piston (214) which extends radially outward from the main body (202) of the rotor (200); and a valve flange (240) with an aperture (242). The rotor unit further comprises a rotatable hub (300), with a cavity (314) configured to receive the piston (214). The rotor unit (90) further comprises a first low pressure port (130) provided in the path described the piston (214); a first high pressure port (120) positioned in the path described the valve flange aperture (242) around the clearance volume (210); and a second high pressure port (122) positioned in the path described by the cavity (314) around the hub axis (306).
F01C 1/12 - "Machines" ou machines motrices à piston rotatif d'un type à engrènement extérieur, c. à d. avec engrènement des organes coopérants semblable à celui d'engrenages dentés d'un autre type qu'à axe interne
F01C 21/18 - Dispositions pour l'admission ou l'échappement du fluide de travail, p.ex. caractéristiques de structure de l'admission ou de l'échappement
The invention relates to an anti-corrosion and anti-fouling composition, particularly to a protective composition for a marine body, wherein in said composition comprises a copper alloy of the form Cu(M*), wherein M* is at least one metal which is more electronegative than copper, wherein said composition comprises ceramic filler particles in the range of from 0.1 to 20 wt %.
BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC. (USA)
Inventeur(s)
Lavely, Eugene M.
Weichman, Peter B.
Abrégé
An underwater sensing system includes a cable structure, a water surface mount coupled to the cable structure, and a processor. The cable structure is configured to be deployed in a vertical orientation underwater and includes one or more sensors along a length of the cable structure. The one or more sensors are configured to detect maritime data associated with one or more marine-based parameters in an underwater maritime region around the cable structure. The water surface mount is configured to be at least partially exposed above a surface of the underwater maritime region and includes a transmitter configured to transmit the maritime data. The processor is configured to access a maritime model comprising parameters associated with the maritime region and update the maritime model based on the maritime data. The maritime model can be used as an input, or otherwise made accessible, to a navigation system of an underwater vehicle.
BAE SYSTEMS Information and Electronic Systems Integration Inc. (USA)
Inventeur(s)
Rambaran, Rishi
Abrégé
A system for front end protection of an RF receiver against interfering pulsed high power RF signals includes a dual-diode device comprising a first Transient Voltage Suppressor (TVS) diode; and a second TVS diode; wherein the first TVS diode and the second TVS diode are located between an RF input/output and an RF receiver front end.
H02H 9/04 - Circuits de protection de sécurité pour limiter l'excès de courant ou de tension sans déconnexion sensibles à un excès de tension
G01S 13/78 - Systèmes utilisant la reradiation d'ondes radio, p.ex. du type radar secondaire; Systèmes analogues dans lesquels des signaux de type pulsé sont transmis effectuant la discrimination entre différents types de cibles, p.ex. radar pour l'identification ami–ennemi
82.
Triple modular redundancy (TMR) radiation hardened memory system
BAE Systems Information and Electronic Systems Integration Inc. (USA)
Inventeur(s)
Moser, David D.
Ferguson, Richard J.
Stanley, Daniel L.
Abrégé
Techniques are provided for a radiation hardened memory system. A memory system implementing the techniques according to an embodiment includes a redundancy comparator configured to detect differences between data stored redundantly in a first memory, a second memory, and a third memory. The redundancy comparator is further configured to identify a memory error based on the detected differences. The memory system also includes an error collection buffer configured to store a memory address associated with the memory error, and a memory scrubber circuit configured to overwrite, at the memory address associated with the memory error, erroneous data with corrected data. The corrected data is based on a majority vote among the three memories. The memory system further includes a priority arbitrator configured to arbitrate between the memory scrubber overwriting and functional memory accesses associated with software execution performed by a processor configured to utilize the memory system.
G06F 11/07 - Réaction à l'apparition d'un défaut, p.ex. tolérance de certains défauts
G06F 3/06 - Entrée numérique à partir de, ou sortie numérique vers des supports d'enregistrement
G06F 11/14 - Détection ou correction d'erreur dans les données par redondance dans les opérations, p.ex. en utilisant différentes séquences d'opérations aboutissant au même résultat
83.
Grid munition pattern utilizing orthogonal interferometry reference frame and range radio frequency code determination
BAE Systems Information and Electronic Systems Integration Inc. (USA)
Inventeur(s)
Choiniere, Michael J.
Ekhaus, Ira B.
Lam, Quang M.
Abrégé
The system and method of projectile flight management using a combination of radio frequency orthogonal interferometry for the long range navigation and guidance of one or more projectiles that does not need to be accurate all the way to the ground based on the use of larger artillery. The system provides for more accurate targeting, especially in GPS-denied and GPS-limited environments.
BAE SYSTEMS Information and Electronic Systems Integration Inc. (USA)
Inventeur(s)
Madison, Gary M.
Abrégé
Techniques are provided for a transimpedance amplifier (TIA). A TIA implementing the techniques according to an embodiment includes a pre-amplifier stage configured to amplify an input signal. The pre-amplifier stage includes a first P-channel metal oxide semiconductor field effect transistor (MOSFET) (P1), a second P-channel MOSFET (P2), a first N-channel MOSFET (N1), and a second N-channel MOSFET (N2), coupled in series. The gates of P1 and N2 are driven by the input signal. The output of the pre-amplifier stage is provided at a coupling between the drain of P2 and the drain of N1. The pre-amplifier stage also includes an active resistor network configured to provide a variable resistance based on a provided current bias generated from a gain control signal. The active resistor network is coupled between the gate of P1 and the drain of P2. The variable resistance is used to control the gain of the pre-amplifier stage.
H03F 3/08 - Amplificateurs comportant comme éléments d'amplification uniquement des tubes à décharge ou uniquement des dispositifs à semi-conducteurs comportant uniquement des dispositifs à semi-conducteurs commandés par la lumière
H03F 1/08 - Modifications des amplificateurs pour réduire l'influence défavorable de l'impédance interne des éléments amplificateurs
BAE SYSTEMS Information and Electronic Systems Integration Inc. (USA)
Inventeur(s)
Peters, Christopher N.
Moser, David D.
Abrégé
Techniques are provided for a polyphase filtering in a dynamically reconfigurable two times (2×) oversampled channelizer. A polyphase filter implementing the techniques according to an embodiment includes a first plurality of dual port memory circuits and a multiplexer circuit configured to distribute input data for storage to the first plurality of dual port memory circuits. The polyphase filter also includes a second plurality of dual port memory circuits configured to store polyphase filter coefficients and a data alignment crossbar circuit configured to align the input data stored in the first plurality of dual port memory circuits with the polyphase filter coefficients stored in the second plurality of dual port memory circuits. The polyphase filter further includes a multiply circuit configured to perform multiplications of the aligned input data with the polyphase filter coefficients and an adder circuit to sum the results of the multiplications to generate a filtered output.
BAE SYSTEMS Information and Electronic Systems Integration Inc. (USA)
Inventeur(s)
Peters, Christopher N.
Moser, David D.
Abrégé
Techniques are provided for a fast Fourier transform (FFT) butterfly circuit. A circuit implementing the techniques according to an embodiment includes a first multiplexer configured to select a first channel or a delayed version of a second channel based on a frame index associated with the first or second channel; a second multiplexer configured to select the channel that was not selected by the first multiplexer; and a butterfly core circuit. The butterfly core circuit configured to receive a delayed version of the selected channel from the first multiplexer as a top butterfly branch; receive the selected channel from the second multiplexer as a bottom butterfly branch; apply FFT twiddle factors to the bottom butterfly branch to generate a scaled bottom butterfly branch; and generate sum and difference channel outputs of the top butterfly branch and the scaled bottom butterfly branch.
An optical device made according to an augmented reality optical design, the optical device comprising a plurality of optical elements for transmitting a light from a light source for display on an eye of a user, wherein the optical device comprises: a light source generating the light; a lens assembly off-axis from the light source and configured to receive the light; a combiner, receiving the light from the lens assembly via one or more further optical elements of the plurality of optical elements and directing the light to form a virtual image at an exit pupil at the position of the eye, wherein the combiner comprises a first inner optical surface form and a second outer optical surface form, wherein the first inner optical surface form and the second outer optical surface are different to minimize deviations in an outside view from the combiner.
According to an aspect of the present invention there is provided an optical device made according to an augmented reality optical design, the optical device comprising a plurality of optical elements for transmitting a light from a light source for display on an eye of a user, wherein the optical device comprises: a light source generating the light; a lens assembly off-axis from the light source and configured to receive the light; a first at least partially mirrored device; a second optical device located intermediate the lens assembly and the first at least partially mirrored device, the second optical device configured to receive the light from the lens assembly and transmit the light to the first at least partially mirrored device; and a combiner receiving the light from the first at least partially mirrored device and directing the light to form a virtual image at an exit pupil at the position of the eye.
BAE SYSTEMS Information and Electronic Systems Integration Inc. (USA)
Inventeur(s)
Peters, Christopher N.
Moser, David D.
Abrégé
Techniques are provided for a dynamically reconfigurable two times (2×) oversampled channelizer. A channelizer implementing the techniques according to an embodiment includes a polyphase filter, a two phase reorder circuit, a fast Fourier transform (FFT) circuit, and a two phase merge circuit. The polyphase filter is configured to filter time domain input data to control spectral shaping of frequency bins of the channelizer output. The two phase reorder circuit is configured to split a 2× oversampled data stream into two parallel, critically sampled data streams. The FFT circuit is configured to transform each stream into the frequency domain. The two phase merge circuit is configured to merge the two streams of frequency domain data into a single stream of 2× oversampled frequency domain data for distribution onto frames of frequency bins. Reconfigurable parameters for the channelizer include filter coefficients, number of filter folds, and number of frequency bins.
BAE SYSTEMS Information and Electronic Systems Integration Inc. (USA)
Inventeur(s)
Peters, Christopher N.
Moser, David D.
Abrégé
Techniques are provided for a fast Fourier transform (FFT) sample reorder circuit for a dynamically reconfigurable oversampled channelizer. An FFT sample reorder circuit implementing the techniques according to an embodiment includes a plurality of dual port memory circuits. The circuit also includes a first crossbar circuit configured to route input data samples to write ports of the plurality of dual port memory circuits. The circuit further includes a second crossbar circuit configured to route reordered output data samples from read ports of the plurality of dual port memory circuits to a multi-stage FFT circuit. The circuit further includes a controller circuit configured to control the routing of the input data samples and the routing of the reordered output data samples based on a selection of a stage of the multi-stage FFT circuit.
An optical device made according to an augmented reality optical design, the optical device comprising a plurality of optical elements for transmitting a light from a light source for display on an eye of a user, wherein the optical device comprises: a light source generating the light; a lens assembly off-axis from the light source and configured to receive the light wherein the lens assembly includes a plurality of lenses and wherein the lens assembly has been truncated by removal of material from the or each lens of the plurality of lenses where an expected light beam is not predicted to pass; a combiner, receiving the light from the lens assembly via one or more further optical elements of the plurality of optical elements and directing the light to form a virtual image at an exit pupil at the position of the eye.
BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC. (USA)
Inventeur(s)
Rambaran, Rishi
Abrégé
A system for front end protection of an RF receiver against interfering pulsed high power RF signals includes a dual-diode device comprising a first Transient Voltage Suppressor (TVS) diode; and a second TVS diode; wherein the first TVS diode and the second TVS diode are located between an RF input/output and an RF receiver front end.
H01L 27/02 - Dispositifs consistant en une pluralité de composants semi-conducteurs ou d'autres composants à l'état solide formés dans ou sur un substrat commun comprenant des éléments de circuit passif intégrés avec au moins une barrière de potentiel ou une barrière de surface
H01H 9/04 - Enveloppes étanches à la poussière, aux projections, aux éclaboussures, à l'eau ou aux flammes
G01S 17/74 - Systèmes utilisant la reradiation d'ondes électromagnétiques autres que les ondes radio, p.ex. pour l'identification ami–ennemi
BAE Systems Information and Electronic Systems Integration Inc. (USA)
Inventeur(s)
Moser, David D.
Stanley, Daniel L.
Keegan, Tate J.
Grass, Sheldon L.
Schabel, Joshua C.
Peters, Christopher N.
Abrégé
A system that includes a plurality of encapsulation blocks having a plurality of digital signal processing (DSP) blocks provided with preconfigured logic functions and a plurality of pacing control networks operatively connected with the plurality of DSP blocks. The system also includes a streaming cross bar operatively connected with each encapsulation block of the plurality of encapsulation blocks. Each encapsulation block of the plurality of encapsulation blocks includes a DSP block of the plurality of DSP blocks and a pacing control network of the plurality of the pacing control networks. Each DSP block of the plurality of DSP blocks is independently and separately connected with the streaming cross bar via the plurality of pacing control networks.
BAE Systems Information and Electronic Systems Integration Inc. (USA)
Inventeur(s)
Johnson, Alexander D.
Jensen, Jonothan S.
Abrégé
A Simultaneous Transmit and Receive (STaR) system utilizing high power transmitters and high sensitivity receivers in conjunction with one or more signal polarizers to maintain far-field polarization efficiency for both transmission and reception of same (or similar) frequency content at the same time. This STaR system maintains far-field polarization efficiency to remote target(s) while simultaneously introducing a near-field polarization mismatch between the transmission and receiver subsystems for higher isolation and reduced coupling.
G01S 7/02 - DÉTERMINATION DE LA DIRECTION PAR RADIO; RADIO-NAVIGATION; DÉTERMINATION DE LA DISTANCE OU DE LA VITESSE EN UTILISANT DES ONDES RADIO; LOCALISATION OU DÉTECTION DE LA PRÉSENCE EN UTILISANT LA RÉFLEXION OU LA RERADIATION D'ONDES RADIO; DISPOSITIONS ANALOGUES UTILISANT D'AUTRES ONDES - Détails des systèmes correspondant aux groupes , , de systèmes selon le groupe
G01S 7/03 - DÉTERMINATION DE LA DIRECTION PAR RADIO; RADIO-NAVIGATION; DÉTERMINATION DE LA DISTANCE OU DE LA VITESSE EN UTILISANT DES ONDES RADIO; LOCALISATION OU DÉTECTION DE LA PRÉSENCE EN UTILISANT LA RÉFLEXION OU LA RERADIATION D'ONDES RADIO; DISPOSITIONS ANALOGUES UTILISANT D'AUTRES ONDES - Détails des systèmes correspondant aux groupes , , de systèmes selon le groupe - Détails de sous-ensembles HF spécialement adaptés à ceux-ci, p.ex. communs à l'émetteur et au récepteur
A head tracking system HTS, configured to determine a head position and a head orientation of a user to which display images are configured to align with the outside world scene and are configured to be presented, the HTS comprising: one or more optical sensors generating an optical measurement; 5 and a number of inertial sensors generating an inertial measurement; a processor configured to determine the head position and the head orientation from one or both of the one or more optical sensors and the number of inertial sensors and configured to: determine an optical tracking state from the optical measurement and an inertial tracking state from the inertial measurement; when 10 both the optical tracking state and the inertial tracking state are valid, flagging/asserting HTS operation as normal; when both the optical tracking state and the inertial tracking state are invalid, flagging/asserting HTS failure; when the optical tracking state and the inertial tracking state are valid comparing the optical measurement and the inertial measurement to determine 15 if the HTS can operate safely based on a predetermined tracking performance required by the system.
G06F 3/01 - Dispositions d'entrée ou dispositions d'entrée et de sortie combinées pour l'interaction entre l'utilisateur et le calculateur
G06F 3/0346 - Dispositifs de pointage déplacés ou positionnés par l'utilisateur; Leurs accessoires avec détection de l’orientation ou du mouvement libre du dispositif dans un espace en trois dimensions [3D], p.ex. souris 3D, dispositifs de pointage à six degrés de liberté [6-DOF] utilisant des capteurs gyroscopiques, accéléromètres ou d’inclinaiso
A head tracking system HTS (100, 200) and associated method and head worn assembly, configured to determine a head position and/or a head orientation of a user, the HTS comprising: one or more optical sensors (112) producing optical measurements; and one or more inertial sensors (104) producing inertial measurements; a processor configured, when the optical sensors fail to provide optical measurements to determine the head location and the head orientation of a user, to operate in a coasting mode using the inertial measurements from the one or more inertial sensors to determine the head location and the head orientation of a user, the processor configured to further: determine a figure of merit FOM (346) for coasting errors based on a combination of one or more of errors in an estimated inertial sensor bias, a random drift and noise of the inertial sensor and the inertial sensor gain and alignment errors; compare (348) the FOM with a threshold to determine whether the inertial measurements provide a valid or invalid head location and/or head orientation; and determine a subsequent operation from a plurality of possible subsequent operations of the HTS based on whether the head location and/or head orientation is valid or invalid.
A method of performing analogue to digital conversion of an analogue input signal. The method comprises: obtaining a laser signal; modulating, using an electro-optic phase modulator, the laser signal on the basis of the analogue input signal; determining, on the basis of the modulated laser signal, a voltage of the analogue input signal; and generating a digital signal indicative of the determined voltage. An apparatus for performing analogue to digital conversion of an analogue input signal. The apparatus comprises an electro-optic phase modulator and a processor. The electro-optic phase modulator is configured to receive a laser signal and modulate the laser signal on the basis of the analogue input signal. The processor is configured to determine, on the basis of the modulated laser signal, a voltage of the analogue input signal and generate a digital signal indicative of the determined voltage.
BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC. (USA)
Inventeur(s)
Moser, David D.
Stanley, Daniel L.
Keegan, Tate J.
Grass, Sheldon L.
Schabel, Joshua C.
Peters, Christopher N.
Abrégé
A system that includes a plurality of encapsulation blocks having a plurality of digital signal processing (DSP) blocks provided with preconfigured logic functions and a plurality of pacing control networks operatively connected with the plurality of DSP blocks. The system also includes a streaming cross bar operatively connected with each encapsulation block of the plurality of encapsulation blocks. Each encapsulation block of the plurality of encapsulation blocks includes a DSP block of the plurality of DSP blocks and a pacing control network of the plurality of the pacing control networks. Each DSP block of the plurality of DSP blocks is independently and separately connected with the streaming cross bar via the plurality of pacing control networks.
G06F 13/372 - Gestion de demandes d'interconnexion ou de transfert pour l'accès au bus ou au système à bus communs avec commande d'accès décentralisée utilisant une priorité dépendant du temps, p.ex. des compteurs de temps individuellement chargés ou des tranches de temps
G06F 13/24 - Gestion de demandes d'interconnexion ou de transfert pour l'accès au bus d'entrée/sortie utilisant l'interruption
G06F 15/173 - Communication entre processeurs utilisant un réseau d'interconnexion, p.ex. matriciel, de réarrangement, pyramidal, en étoile ou ramifié
G06F 21/74 - Protection de composants spécifiques internes ou périphériques, où la protection d'un composant mène à la protection de tout le calculateur pour assurer la sécurité du calcul ou du traitement de l’information opérant en mode dual ou compartimenté, c. à d. avec au moins un mode sécurisé
BAE Systems Information and Electronic Systems Integration Inc. (USA)
Inventeur(s)
Moser, David D.
Peters, Christopher N.
Stanley, Daniel L.
Aslam, Umair
Williams, Elizabeth J.
Sunga, Angelica
Abrégé
An encapsulation block for a digital signal processing (DSP) block. The encapsulation block includes DSP block having an input terminal, an output terminal, and an input clock. The encapsulation block also includes pacing control network operatively connected with the input terminal, the output terminal, and the input clock of the DSP block. The input terminal of the DSP block is configured to receive a samples-in data stream inputted at a predefined clock period defined by the input clock. The output terminal of the DSP block is configured to receive a samples-out data stream outputted at a predefined paced parameter. The pacing control network is configured to control data flow at the samples-in data stream and the samples-out data stream independently of the DSP block.
BAE SYSTEMS Information and Electronic Systems Integration Inc. (USA)
Inventeur(s)
Thompson, David E.
Pelletier, Gerard J.
Snell, Katherine J.
Abrégé
The system and method for mounting a high power laser having a coefficient of thermal expansion that is thermally matched for the gain medium and the mount. In some cases, the gain medium is clamped by the mount along longitudinal edges and has a pair of free ends not in thermal contact with the mount. A thermal interface may be present along at least a portion of the longitudinal edges.
H01S 3/02 - Lasers, c. à d. dispositifs utilisant l'émission stimulée de rayonnement électromagnétique dans la gamme de l’infrarouge, du visible ou de l’ultraviolet - Détails de structure