mhurhangee/ep-ind-claims huggingface dataset:
A system comprising: a plurality of processing nodes, wherein each processing node of the plurality of processing nodes comprises one or more processors and a cache subsystem; one or more memory devices; and one or more region-based cache directories, wherein each region-based cache directory is configured to track shared regions of memory which have cache lines cached by at least two different processing nodes; characterised in that each processing node of the plurality of processing nodes is configured to maintain an entry with a reference count field to track a number of accesses by the processing node to separate cache lines of a given region responsive to receiving an indication from a corresponding region-based cache directory that the given region is private, wherein a private region is accessed by only a single processing node. a plurality of processing nodes, wherein each processing node of the plurality of processing nodes comprises one or more processors and a cache subsystem; one or more memory devices; and one or more region-based cache directories, wherein each region-based cache directory is configured to track shared regions of memory which have cache lines cached by at least two different processing nodes; characterised in that each processing node of the plurality of processing nodes is configured to maintain an entry with a reference count field to track a number of accesses by the processing node to separate cache lines of a given region responsive to receiving an indication from a corresponding region-based cache directory that the given region is private, wherein a private region is accessed by only a single processing node.
A processing system for an establishment for a merchant, comprising: a wireless communication interface arranged to wirelessly communicate with one or more wireless client devices in the vicinity of the establishment, the wireless communication interface receiving a remote order corresponding to an item selected by at least one of the wireless client devices, the item to be provided by the merchant; a local server computer (210, 306), located in proximity to the establishment, in communication with the wireless communication interface that receives the remote order from the wireless communication interface and generates instructions for processing the remote order, wherein the local server computer (210, 306) generates a processing command that includes processing requirements for a next to be processed selected item; a processing queue (228, 1110) in communication with the local server computer (210, 306) that receives the processing instructions from the local server computer (210, 306) in preparation for processing of the remote order; a local processing center coupled to the processing queue (228, 1110) that responds to the processing command by processing the selected item according to the processing requirements; and a pick up station coupled to the local processing center for staging a fully processed selected item for pick up. a wireless communication interface arranged to wirelessly communicate with one or more wireless client devices in the vicinity of the establishment, the wireless communication interface receiving a remote order corresponding to an item selected by at least one of the wireless client devices, the item to be provided by the merchant; a local server computer (210, 306), located in proximity to the establishment, in communication with the wireless communication interface that receives the remote order from the wireless communication interface and generates instructions for processing the remote order, wherein the local server computer (210, 306) generates a processing command that includes processing requirements for a next to be processed selected item; a processing queue (228, 1110) in communication with the local server computer (210, 306) that receives the processing instructions from the local server computer (210, 306) in preparation for processing of the remote order; a local processing center coupled to the processing queue (228, 1110) that responds to the processing command by processing the selected item according to the processing requirements; and a pick up station coupled to the local processing center for staging a fully processed selected item for pick up.
A manufacturing apparatus for depositing a material on a carrier body, said manufacturing apparatus comprising: a base plate; a housing having a flange for coupling with said base plate to define a reaction chamber; an inlet defined by said housing for introducing a deposition composition, which comprises the material or a precursor thereof into said reaction chamber; and at least one gasket disposed between said base plate and said housing for sealing between said housing and said base plate for preventing the deposition composition from escaping said reaction chamber; wherein said gasket comprises a flexible graphite material for preventing said gasket from contaminating the material within said reaction chamber. a base plate; a housing having a flange for coupling with said base plate to define a reaction chamber; an inlet defined by said housing for introducing a deposition composition, which comprises the material or a precursor thereof into said reaction chamber; and at least one gasket disposed between said base plate and said housing for sealing between said housing and said base plate for preventing the deposition composition from escaping said reaction chamber; wherein said gasket comprises a flexible graphite material for preventing said gasket from contaminating the material within said reaction chamber.
An integrated analyte measurement system, comprising: a housing, a disposable configured to be position in the housing; a plurality of penetrating members positioned in the disposable, an electromechanical driver configured to be coupled to the penetrating member, the driver coupled to a processor and having position and velocity sensing capabilities to advance a penetrating member into a target tissue to create a wound from which body fluid will flow; a plurality of analyte sensors positioned in the disposable, the disposable housing used and unused penetrating members and analyte sensors, each sensor being a screen-printed three-electrode system, the sensors being printed on a support and having an aperture, each sensor includes reference and counter electrode and a working electrode, and the sensor and support being orientated perpendicularly relative to a longitudinal axis of an associated penetrating member; and a fluid channel coupled to each sensor and including a sponge like porous membrane coated on the channel walls to aid drawing blood into the sensor. a housing, a disposable configured to be position in the housing; a plurality of penetrating members positioned in the disposable, an electromechanical driver configured to be coupled to the penetrating member, the driver coupled to a processor and having position and velocity sensing capabilities to advance a penetrating member into a target tissue to create a wound from which body fluid will flow; a plurality of analyte sensors positioned in the disposable, the disposable housing used and unused penetrating members and analyte sensors, each sensor being a screen-printed three-electrode system, the sensors being printed on a support and having an aperture, each sensor includes reference and counter electrode and a working electrode, and the sensor and support being orientated perpendicularly relative to a longitudinal axis of an associated penetrating member; and a fluid channel coupled to each sensor and including a sponge like porous membrane coated on the channel walls to aid drawing blood into the sensor.
A method for aiding landing of a rotary wing aircraft (142, 160, 198) in conditions of reduced visibility of a landing area, wherein a pilot of the rotary wing aircraft is provided with a head or helmet-mounted display device arranged to display symbology to the pilot overlaid on a scene being viewed by the pilot, the method including the steps: (i) determining the line of sight (140, 204) of the pilot; (ii) indicating a desired landing point (144, 162, 192) for the rotary wing aircraft dependent on the determined line of sight of the pilot; (iii) determining the location, including the height above a ground surface (148, 196), of the rotary wing aircraft; (iv) determining the location of the desired landing point indicated at step (ii) with respect to the determined location of the rotary wing aircraft; (v) generating conformal ground-referenced landing symbology comprising one or more symbols (220-224, 242-248, 254-264, 282-290, 302, 304, 320-326) providing a three-dimensional representation of a landing area at the determined location of the desired landing point; (vi) displaying the conformal ground-referenced landing symbology to the pilot on the display device; and (vii) updating the size or the shape of the one or more symbols of the displayed conformal ground-referenced landing symbology according to a change in the determined location of the rotary wing aircraft relative to the determined location of the desired landing point. (i) determining the line of sight (140, 204) of the pilot; (ii) indicating a desired landing point (144, 162, 192) for the rotary wing aircraft dependent on the determined line of sight of the pilot; (iii) determining the location, including the height above a ground surface (148, 196), of the rotary wing aircraft; (iv) determining the location of the desired landing point indicated at step (ii) with respect to the determined location of the rotary wing aircraft; (v) generating conformal ground-referenced landing symbology comprising one or more symbols (220-224, 242-248, 254-264, 282-290, 302, 304, 320-326) providing a three-dimensional representation of a landing area at the determined location of the desired landing point; (vi) displaying the conformal ground-referenced landing symbology to the pilot on the display device; and (vii) updating the size or the shape of the one or more symbols of the displayed conformal ground-referenced landing symbology according to a change in the determined location of the rotary wing aircraft relative to the determined location of the desired landing point.
A motor comprising: a motor body including a drive shaft; a motor housing in which the motor body is housed; and a damping member (3; 6; 8) disposed on an outer surface of the motor housing, wherein the damping member (3; 6; 8) includes a damping layer (31; 61; 81) and a constraining layer (32; 62; 82), the damping layer (31; 61; 81) being made of an organic polymeric material, and the constraining layer (32; 62; 82) being disposed on the damping layer (31; 61; 81), wherein the damping layer (31; 61; 81) is bonded to the outer surface of the motor housing, characterized in that the constraining layer (32; 62; 82) is made of at least one of a resin mixed with an inorganic compound and an elastomer mixed with an inorganic compound. a motor body including a drive shaft; a motor housing in which the motor body is housed; and a damping member (3; 6; 8) disposed on an outer surface of the motor housing, wherein the damping member (3; 6; 8) includes a damping layer (31; 61; 81) and a constraining layer (32; 62; 82), the damping layer (31; 61; 81) being made of an organic polymeric material, and the constraining layer (32; 62; 82) being disposed on the damping layer (31; 61; 81), wherein the damping layer (31; 61; 81) is bonded to the outer surface of the motor housing, characterized in that the constraining layer (32; 62; 82) is made of at least one of a resin mixed with an inorganic compound and an elastomer mixed with an inorganic compound.
A method for determining weight on wheels for an aircraft, comprising: receiving (310, 312, 314), with a processor, signals indicative of Light Detection And Ranging, LIDAR, image information for a landing gear (116, 118, 120) from a LIDAR scanner; evaluating, with the processor, the LIDAR image information against a landing gear model; determining (316, 318, 320), with the processor, information indicative that the landing gear (116, 118, 120) is locked in response to the evaluating of the LIDAR image information; and determining (322, 324, 326), with the processor, information indicative that the landing gear is compressed in response to the evaluating of the LIDAR image information against the landing gear model, characterized in that a test is run on the LIDAR scanner to determine operability of the LIDAR scanner for acquiring images of the landing gear (116, 118, 120), while the aircraft is airborne and prior to approaching a landing zone. receiving (310, 312, 314), with a processor, signals indicative of Light Detection And Ranging, LIDAR, image information for a landing gear (116, 118, 120) from a LIDAR scanner; evaluating, with the processor, the LIDAR image information against a landing gear model; determining (316, 318, 320), with the processor, information indicative that the landing gear (116, 118, 120) is locked in response to the evaluating of the LIDAR image information; and determining (322, 324, 326), with the processor, information indicative that the landing gear is compressed in response to the evaluating of the LIDAR image information against the landing gear model, characterized in that a test is run on the LIDAR scanner to determine operability of the LIDAR scanner for acquiring images of the landing gear (116, 118, 120), while the aircraft is airborne and prior to approaching a landing zone.
A method of decoding a bitstream of encoded video by reconstructing coefficients for a transform unit, wherein the transform unit is partitioned into non-overlapping coefficient groups each containing a respective set of coefficients, and each of the non-zero coefficients having a sign bit indicating whether the coefficient is positive or negative, the method comprising: for each of at least two coefficient groups in the transform unit, decoding sign bits for all but one of the non-zero coefficients in that coefficient group; summing an absolute value of the coefficients in that coefficient group; and based on whether the absolute value is even or odd, assigning a sign to the non-zero coefficient within that coefficient group for which a sign bit was not decoded. for each of at least two coefficient groups in the transform unit, decoding sign bits for all but one of the non-zero coefficients in that coefficient group; summing an absolute value of the coefficients in that coefficient group; and based on whether the absolute value is even or odd, assigning a sign to the non-zero coefficient within that coefficient group for which a sign bit was not decoded. summing an absolute value of the coefficients in that coefficient group; and based on whether the absolute value is even or odd, assigning a sign to the non-zero coefficient within that coefficient group for which a sign bit was not decoded.
A drive rotor with a rotor hub and several rotor blades (14a, 14b), wherein an air inlet that faces the inflowing air is provided in the rotor hub and followed by a spiral-shaped hub flow channel that transforms into at least two identical openings, characterized in that the hub flow channel has a decreasing curvature radius and hub flow channel cross section in the flow direction, and in that the hub flow channel transforms into rotor flow channels (22a, 22b) that extend in the rotor blades (14a, 14b) and have a radially increasing cross section, wherein several turning vanes (26a, 26b) are respectively arranged on the ends of said rotor flow channels in order to deflect the air flow in the circumferential direction to a respective air outlet (28a, 28b) on the trailing rotor blade edges.
A scintillator panel comprising: a plate-like substrate; a barrier rib provided on the substrate; and a scintillator layer comprising a phosphor filled in cells divided by the barrier rib, wherein the barrier rib is formed of a material which is mainly composed of a low-melting-point glass containing 2 to 20% by mass of an alkali metal oxide, a value obtained by dividing a top width Lt of the barrier rib or a 90%-height width L90 of the barrier rib by a half-value width Lh of the barrier rib is 0.45 to 1, and a value obtained by dividing a bottom width Lb of the barrier rib or a 10%-height width L10 of the barrier rib by the half-value width Lh is 1 to 3.
Tyre tread comprising a tread surface intended to come into contact with a roadway, this tread having a total thickness E and comprising: - at least one main groove opening along its entire length when new onto the tread surface of the tread, this groove having a total depth P at most equal to the total thickness E of the tread, and, in the vicinity of this main groove, - at least one discontinuous secondary groove extending in the thickness of the tread down to a depth equal or close to the depth P of the main groove, this discontinuous secondary groove having a plurality of parts hidden beneath the tread surface when new and a plurality of open parts open onto the tread surface when new, these open parts being disjointed with respect to one another on the tread surface when new, - the main groove and the discontinuous secondary groove each respectively having a mean surface defined as a virtual surface that divides this groove, in the main direction of this groove, into two equal or substantially equal parts, - the main groove and the discontinuous secondary groove having roughly identical main directions, this tread being characterized in that all the open parts of the discontinuous secondary groove are at a mean distance L1 from the main groove, this distance L1 being measured at the open parts between the mean surface of the main groove and the mean surface of the discontinuous secondary groove, this distance L1 is less than the mean distance L2 measured between the mean surface of the main groove and the mean surface of the discontinuous groove in the regions of the discontinuous secondary groove that do not have open parts. - at least one main groove opening along its entire length when new onto the tread surface of the tread, this groove having a total depth P at most equal to the total thickness E of the tread, and, in the vicinity of this main groove, - at least one discontinuous secondary groove extending in the thickness of the tread down to a depth equal or close to the depth P of the main groove, this discontinuous secondary groove having a plurality of parts hidden beneath the tread surface when new and a plurality of open parts open onto the tread surface when new, these open parts being disjointed with respect to one another on the tread surface when new, - the main groove and the discontinuous secondary groove each respectively having a mean surface defined as a virtual surface that divides this groove, in the main direction of this groove, into two equal or substantially equal parts, - the main groove and the discontinuous secondary groove having roughly identical main directions,
Method for operating an automated guided vehicle, comprising the following method steps: - by means of a measuring device of an automated guided vehicle determining whether the current movement of the automated guided vehicle would cause the latter to potentially collide with at least one obstacle, - determining the points on the automated guided vehicle that will potentially collide with the obstacle, - determining the respective movement-dependent distance (d) between the obstacle and the point of the automated guided vehicle and - calculating a maximum velocity for the current movement of the automated guided vehicle on the basis of the determined distance (d), so that as a result of the possible braking of the automated guided vehicle the latter reliably comes to a stop in front of the obstacle. - by means of a measuring device of an automated guided vehicle determining whether the current movement of the automated guided vehicle would cause the latter to potentially collide with at least one obstacle, - determining the points on the automated guided vehicle that will potentially collide with the obstacle, - determining the respective movement-dependent distance (d) between the obstacle and the point of the automated guided vehicle and - calculating a maximum velocity for the current movement of the automated guided vehicle on the basis of the determined distance (d), so that as a result of the possible braking of the automated guided vehicle the latter reliably comes to a stop in front of the obstacle.
A process for obtaining reaction products comprising olefins comprising: converting a solid carbonaceous material with a first reaction scheme to a gaseous component comprising condensable gases and non-condensable gases and a solid component comprising char and ash, wherein a temperature of the first reaction scheme is in the range of 350 to 600 deg C, and a residence time of the first reaction scheme is less than 5 sec, and at least 0.0001 sec; and converting at least a portion of the condensable gases and at least a portion of the non-condensable gases that contain 2 or more carbon atoms with a second reaction scheme to reaction products comprising olefins, wherein a temperature of second reaction scheme is in the range of 600 to 1000 deg C and a residence time of the second reaction scheme is less than 5 sec and at least 0.000001 sec; wherein the portion of the condensable gases and the portion of the non-condensable gases that contain 2 or more carbon atoms are directly fed from the first reaction scheme to the second reaction scheme without being cooled; the first reaction scheme is pyrolysis performed in the absence of a catalyst; the second reaction scheme is similar to the reaction occurring only in the radiant section of a steam cracker, and is performed in the absence of a catalyst, and in the presence of steam and in the absence of molecular oxygen; and wherein hydrogen is not added during the process. converting a solid carbonaceous material with a first reaction scheme to a gaseous component comprising condensable gases and non-condensable gases and a solid component comprising char and ash, wherein a temperature of the first reaction scheme is in the range of 350 to 600 deg C, and a residence time of the first reaction scheme is less than 5 sec, and at least 0.0001 sec; and converting at least a portion of the condensable gases and at least a portion of the non-condensable gases that contain 2 or more carbon atoms with a second reaction scheme to reaction products comprising olefins, wherein a temperature of second reaction scheme is in the range of 600 to 1000 deg C and a residence time of the second reaction scheme is less than 5 sec and at least 0.000001 sec; wherein the portion of the condensable gases and the portion of the non-condensable gases that contain 2 or more carbon atoms are directly fed from the first reaction scheme to the second reaction scheme without being cooled; the first reaction scheme is pyrolysis performed in the absence of a catalyst; the second reaction scheme is similar to the reaction occurring only in the radiant section of a steam cracker, and is performed in the absence of a catalyst, and in the presence of steam and in the absence of molecular oxygen; and wherein hydrogen is not added during the process.