mhurhangee/ep-ind-claims huggingface dataset:
A method of decoding video data, the method comprising: selecting a source affine block, the source affine block being an affine-coded block that spatially neighbors a current block; extrapolating motion vectors of control points of the source affine block to determine motion vector predictors for control points of the current block based on the extrapolated motion vectors; inserting, into an affine motion vector predictor set candidate list, an affine MVP set that includes the motion vector predictors for the control points of the current block; determining, based on an index signaled in a bitstream, a selected affine MVP set in the affine MVP set candidate list; obtaining, from the bitstream, motion vector differences (MVDs) that indicate differences between motion vectors of the control points of the current block and motion vector predictors in the selected affine MVP set; determining, based on the motion vector predictors included in the selected affine MVP set and the MVDs, motion vectors of the control points of the current block; generating, based on the motion vectors of the control points of the current block, a predictive block; and reconstructing the current block based on residual data and the predictive block. selecting a source affine block, the source affine block being an affine-coded block that spatially neighbors a current block; extrapolating motion vectors of control points of the source affine block to determine motion vector predictors for control points of the current block based on the extrapolated motion vectors; inserting, into an affine motion vector predictor set candidate list, an affine MVP set that includes the motion vector predictors for the control points of the current block; determining, based on an index signaled in a bitstream, a selected affine MVP set in the affine MVP set candidate list; obtaining, from the bitstream, motion vector differences (MVDs) that indicate differences between motion vectors of the control points of the current block and motion vector predictors in the selected affine MVP set; determining, based on the motion vector predictors included in the selected affine MVP set and the MVDs, motion vectors of the control points of the current block; generating, based on the motion vectors of the control points of the current block, a predictive block; and reconstructing the current block based on residual data and the predictive block.
An antenna comprising: a substrate; a radiator attached to the substrate and configured to radiate an electromagnetic signal, wherein the radiator extends in two directions (x/u direction, y/v direction), which are perpendicular to a vertical direction (z/w direction) of the radiator; a metal plate antenna square-shaped and disposed to be spaced apart from the radiator in the vertical direction of the radiator; four fixing rods (451 to 454) supporting the metal plate antenna; and four sub patch antennas (461 to 464) attached respectively to the four fixing rods (451 to 454) and disposed on the substrate, wherein a partial region of the metal plate antenna overlaps a partial region of the radiator in the two directions (x/u direction, y/v direction) perpendicular to the vertical direction (z/w direction), and the four fixing rods (451 to 454) are disposed respectively to correspond to four corners of the metal plate antenna. a substrate; a radiator attached to the substrate and configured to radiate an electromagnetic signal, wherein the radiator extends in two directions (x/u direction, y/v direction), which are perpendicular to a vertical direction (z/w direction) of the radiator; a metal plate antenna square-shaped and disposed to be spaced apart from the radiator in the vertical direction of the radiator; four fixing rods (451 to 454) supporting the metal plate antenna; and four sub patch antennas (461 to 464) attached respectively to the four fixing rods (451 to 454) and disposed on the substrate, wherein a partial region of the metal plate antenna overlaps a partial region of the radiator in the two directions (x/u direction, y/v direction) perpendicular to the vertical direction (z/w direction), and the four fixing rods (451 to 454) are disposed respectively to correspond to four corners of the metal plate antenna.
A method of determining intrusion of an avionics component or avionics system in an aircraft having multiple avionics components and avionics systems communicating over an aircraft communications network monitored by an intrusion system, the method comprising: monitoring, by the intrusion system, data communication over the aircraft communications network for one or more of the avionics components or avionics systems; comparing, by the intrusion system, the monitored communications for at least one of the avionics components or avionics systems to a corresponding operational profile that includes acceptable interactions between multiple avionics components or avionics systems; determining an intrusion for the at least one of the avionics components or avionics systems when the comparison indicates that the at least one of the avionics components or avionics systems satisfies an intrusion profile, the intrusion profile comprising an uncharacteristic operational profile indicative of malicious or unintended use of the at least one of the avionics components or avionics systems for which the data communications are monitored; and providing an alert of the determined intrusion. monitoring, by the intrusion system, data communication over the aircraft communications network for one or more of the avionics components or avionics systems; comparing, by the intrusion system, the monitored communications for at least one of the avionics components or avionics systems to a corresponding operational profile that includes acceptable interactions between multiple avionics components or avionics systems; determining an intrusion for the at least one of the avionics components or avionics systems when the comparison indicates that the at least one of the avionics components or avionics systems satisfies an intrusion profile, the intrusion profile comprising an uncharacteristic operational profile indicative of malicious or unintended use of the at least one of the avionics components or avionics systems for which the data communications are monitored; and providing an alert of the determined intrusion.
An apparatus for fixing molded blanks of eyeglass frames to a multi-axis machine tool for finishing operations such as, for example, milling and boring, comprising a base plate, to be fixed to the worktable of the machine tool, a pair of adjacent cylinders (2, 3), vertically extending from respective closing plates (4, 5) and fixed thereto, at their lower ends, with the interposition of a hydraulic or pneumatic seal (10, 11), the vertical axes (X-X, Y-Y) of the pair of adjacent cylinders being horizontally spaced apart from each other by a length that substantially corresponds to the center-to-center distance between the lens receptacles formed in eyeglass frame blank to be finished, each cylinder (2, 3) having a respective piston element (8, 9) therein, connected to a respective cylindrical core (12, 14) whose upper end portion (13, 15), distal to said base plate, has a frustoconical shape, said piston elements being movable in their respective cylinders (2, 3), under pneumatic control and to raise and lower their respective cylindrical core (12, 14) connected thereto at the upper end, distal to said base plate, of each cylinder of the pair of cylinders (2, 3), respective radial slide groups (20, 21) being provided, each slide of each group having a respective block of plastic material whose profile is adapted to be machined into such a shape as to be able to fit into and engage with the inner profile of the respective lens receptacle, to hold it in position during the processing operations, characterized in that the end of each slide of the plurality of slides (20, 21) facing toward the axes (X-X, Y-Y) of their respective cylinders (2, 3), has a guide slidingly engaged in an opposed axial guide which radially projects from the frustoconical sections (13, 15) of their respective cylindrical cores (12, 14) connected to said piston elements (8, 9).
A system comprising: a battery; a power supply; a switch; a device being configured to be alternatively powered by the battery or by the power supply; at least one sensor (110-114; 105) being configured for sensing data that impacts the operation and the lifetime of the battery; a battery monitoring module operatively coupled to the switch and configured to control the switch for switching, based at least on the sensor data and at least one predefined curve, between a first mode where the device and the battery are powered by the power supply and the switch is open and a second mode where the device is powered by the battery and the switch is closed, said predefined curve being a characteristic curve of the battery, wherein the at least one sensor (110-114; 105) comprises one or several among: - a temperature sensor arranged for sensing a temperature of the battery; - a humidity sensor arranged for sensing a humidity ratio of an environment of the battery, - a pressure sensor arranged for sensing pressure of the environment of the battery; - a vibration sensor arranged for sensing vibrations around the battery; and a shunt and an amperemeter arranged for determining a load value applied to the battery. a battery; a power supply; a switch; a device being configured to be alternatively powered by the battery or by the power supply; at least one sensor (110-114; 105) being configured for sensing data that impacts the operation and the lifetime of the battery; a battery monitoring module operatively coupled to the switch and configured to control the switch for switching, based at least on the sensor data and at least one predefined curve, between a first mode where the device and the battery are powered by the power supply and the switch is open and a second mode where the device is powered by the battery and the switch is closed, said predefined curve being a characteristic curve of the battery, wherein the at least one sensor (110-114; 105) comprises one or several among: - a temperature sensor arranged for sensing a temperature of the battery; - a humidity sensor arranged for sensing a humidity ratio of an environment of the battery, - a pressure sensor arranged for sensing pressure of the environment of the battery; - a vibration sensor arranged for sensing vibrations around the battery; and a shunt and an amperemeter arranged for determining a load value applied to the battery. - a temperature sensor arranged for sensing a temperature of the battery; - a humidity sensor arranged for sensing a humidity ratio of an environment of the battery, - a pressure sensor arranged for sensing pressure of the environment of the battery; - a vibration sensor arranged for sensing vibrations around the battery; and a shunt and an amperemeter arranged for determining a load value applied to the battery.
A thrust reverser for a nacelle of a gas turbine engine of an aircraft, the thrust reverser comprising: an upper reverser door and a lower reverser door defining a portion of an aft section of the nacelle; the doors having a respective trailing edge (24a, 26a) adjacent to a propulsive jet outlet of the nacelle; the doors being pivotable together between respective stowed and a deployed positions; the trailing edge of the upper door being positioned behind the trailing edge of the lower door in the deployed position, the trailing edges of the doors in the deployed position delimiting a rear opening that is generally oriented aft and downwardly relative to the engine, and the deployed doors communicating in use with efflux generated by the engine to redirect a first portion (A2, A3) of the engine efflux forwardly to create a braking force and a second portion of the engine efflux downwardly through said rear opening to create a nose-down pitching moment on the aircraft. an upper reverser door and a lower reverser door defining a portion of an aft section of the nacelle; the doors having a respective trailing edge (24a, 26a) adjacent to a propulsive jet outlet of the nacelle; the doors being pivotable together between respective stowed and a deployed positions; the trailing edge of the upper door being positioned behind the trailing edge of the lower door in the deployed position, the trailing edges of the doors in the deployed position delimiting a rear opening that is generally oriented aft and downwardly relative to the engine, and the deployed doors communicating in use with efflux generated by the engine to redirect a first portion (A2, A3) of the engine efflux forwardly to create a braking force and a second portion of the engine efflux downwardly through said rear opening to create a nose-down pitching moment on the aircraft.
A compressor vane or blade for an engine used in an environment containing abundant foreign substances, the compressor vane or blade comprising: a base body of the compressor vane or blade; a coating covering the base body, the coating consisting essentially of one or more selected from the group of molybdenum disulfide and tungsten disulfide; and an intermediate coating interposed between the coating and the base body, characterized in that: the coating and the intermediate coating are alternately layered to form a multi-layered coating of three or more sets of the alternate layers, in which the coating is exposed to the atmosphere, and the coatings (3, 5) are limited at and fully cover an airfoil face, a platform section or an inner band section, and an outer band section. a base body of the compressor vane or blade; a coating covering the base body, the coating consisting essentially of one or more selected from the group of molybdenum disulfide and tungsten disulfide; and an intermediate coating interposed between the coating and the base body, characterized in that: the coating and the intermediate coating are alternately layered to form a multi-layered coating of three or more sets of the alternate layers, in which the coating is exposed to the atmosphere, and the coatings (3, 5) are limited at and fully cover an airfoil face, a platform section or an inner band section, and an outer band section. the coating and the intermediate coating are alternately layered to form a multi-layered coating of three or more sets of the alternate layers, in which the coating is exposed to the atmosphere, and the coatings (3, 5) are limited at and fully cover an airfoil face, a platform section or an inner band section, and an outer band section.
A method for implementing data transmission of a convergence of 3rd Generation Partnership project, 3GPP, and a Wireless Local Area Network, WLAN, networks, comprising: a bottom layer WLAN entity of a User Equipment, UE, encapsulating signaling and/or data issued by a UE upper layer entity of the UE into a WLAN protocol stack, the stack comprising a WLAN Media Access Control, MAC, layer and a WLAN physical, PHY, layer, and transmitting it to a 3GPP access network device through an air interface that uses the WLAN MAC and PHY layers; and the bottom layer WLAN entity receiving signaling and/or data transmitted by the 3GPP access network device through the air interface, and decapsulating and then transmitting it to the UE upper layer entity, wherein, the UE upper layer entity is configured to establish a control plane connection and/or a user plane connection with the 3GPP access network device through the bottom layer WLAN entity characterized in that the UE upper layer entity comprises at least a 3GPP air interface protocol based Media Access Control, MAC, layer entity and one or more of the following entities: a 3GPP air interface protocol based Radio Resource Control, RRC, layer entity, a 3GPP air interface protocol based Packet Data Convergence Protocol, PDCP, layer entity, a 3GPP air interface protocol based Radio Link Control, RLC, layer entity. a bottom layer WLAN entity of a User Equipment, UE, encapsulating signaling and/or data issued by a UE upper layer entity of the UE into a WLAN protocol stack, the stack comprising a WLAN Media Access Control, MAC, layer and a WLAN physical, PHY, layer, and transmitting it to a 3GPP access network device through an air interface that uses the WLAN MAC and PHY layers; and the bottom layer WLAN entity receiving signaling and/or data transmitted by the 3GPP access network device through the air interface, and decapsulating and then transmitting it to the UE upper layer entity, wherein, the UE upper layer entity is configured to establish a control plane connection and/or a user plane connection with the 3GPP access network device through the bottom layer WLAN entity characterized in that the UE upper layer entity comprises at least a 3GPP air interface protocol based Media Access Control, MAC, layer entity and one or more of the following entities: a 3GPP air interface protocol based Radio Resource Control, RRC, layer entity, a 3GPP air interface protocol based Packet Data Convergence Protocol, PDCP, layer entity, a 3GPP air interface protocol based Radio Link Control, RLC, layer entity.
A method comprising: irradiating edible residues that have been produced as a by-product of an ethanol manufacturing process, wherein the edible residues comprise an antibiotic, and irradiating is performed under conditions selected to inactivate or destroy the antibiotic.
An ice bank cooler comprising a bath containing water or water containing an additive that suppresses the freezing point of water to produce a sub-zero ice bank as a coolant, an evaporator coil in the bath for cooling the coolant and forming a thermal reserve of frozen coolant on the evaporator coil, an agitator for agitating the coolant in the bath, a motor for driving the agitator, a first temperature sensor to monitor the temperature of the coolant in the bath and control operation of the motor driving the agitator in response to the coolant temperature in the bath, a pump (13;23) for circulating still or carbonated water, which is supplied via a water line, in a loop (9,21) between the cooler and a remote dispense tower for the dispense of drinks comprising carbonated water or still water and said loop including a cooling coil (17,35) immersed in the bath, and a motor (14;40) for driving the pump (13;23), characterised by a second temperature sensor (20;39) to monitor the temperature of the return flow of the circulating still or carbonated water and control operation of the motor (14;40) driving the pump (13;23) in response to still or carbonated water temperature.
Domestic appliance wall arrangement, in particular oven wall arrangement, having at least two wall parts (16, 18) which are attached to one another by means of a welded joint, wherein one of the wall parts has a third subregion which encompasses the other wall part, characterised in that the welded joint penetrates at least one of the wall parts and the third subregion forms, in interaction with the other wall part, a collection space for collecting welding material during the production of the welded joint.
Method of remanufacturing a laser printer toner cartridge, the toner cartridge having a primary charge roller with a cylindrical body, the toner cartridge not having a primary charge roller cleaning roller before remanufacturing, the method being characterized in that it comprises: providing a primary charge roller cleaning roller having a body portion adapted to clean the primary charge roller through rotatable contact; modifying the toner cartridge to add the primary charge roller cleaning roller; and installing the primary charge roller cleaning roller in the laser printer toner cartridge. providing a primary charge roller cleaning roller having a body portion adapted to clean the primary charge roller through rotatable contact; modifying the toner cartridge to add the primary charge roller cleaning roller; and installing the primary charge roller cleaning roller in the laser printer toner cartridge.
A clamping clip made of a clamping band the two end portions (11, 12) of which overlap one another in the closed condition of the clamping clip, comprising a tongue arranged at the overlapped inner band portion and a tongue channel provided in the overlapping outer band portion and being complementary to the shape of the tongue for receiving the tongue, characterized in that the tongue has a root part in which the tongue width measured in the axial direction of the clamp decreases from the full clamping band width to a smaller value, and an end part adjoining the root part in which the tongue width constantly has said smaller value.
A system for determining a decision using a traffic proxy measure, comprising: an input interface to: receive a vehicle data and road data; and a processor to: determine a traffic proxy measure based at least in part on the vehicle data and the road data, wherein the traffic proxy measure comprises a heavy traffic indication, a moderate traffic indication, or a low traffic indication; determine a decision based at least in part on the traffic proxy measure being less than a traffic proxy measure threshold, wherein determining the decision comprises determining whether to record event data or comprises determining whether to transmit event data; determine (504, 560) whether to update an event recorder threshold based at least in part on the traffic proxy measure, wherein the event recorder threshold comprises a threshold that is used to increase or decrease a likelihood of detection of an event and to collect data for the event, wherein in response to the traffic proxy measure including a heavy traffic indication, the vehicle event recorder threshold is modified to increase likelihood of detection of the event, and wherein in response to the traffic proxy measure including a low traffic indication, the vehicle event recorder threshold is modified to decrease likelihood of detection of the event; and in the event that it is determined to update the event recorder threshold, update the event recorder threshold. determine a traffic proxy measure based at least in part on the vehicle data and the road data, wherein the traffic proxy measure comprises a heavy traffic indication, a moderate traffic indication, or a low traffic indication; determine a decision based at least in part on the traffic proxy measure being less than a traffic proxy measure threshold, wherein determining the decision comprises determining whether to record event data or comprises determining whether to transmit event data; determine (504, 560) whether to update an event recorder threshold based at least in part on the traffic proxy measure, wherein the event recorder threshold comprises a threshold that is used to increase or decrease a likelihood of detection of an event and to collect data for the event, wherein in response to the traffic proxy measure including a heavy traffic indication, the vehicle event recorder threshold is modified to increase likelihood of detection of the event, and wherein in response to the traffic proxy measure including a low traffic indication, the vehicle event recorder threshold is modified to decrease likelihood of detection of the event; and in the event that it is determined to update the event recorder threshold, update the event recorder threshold.