mhurhangee/ep-ind-claims huggingface dataset:
A system comprising: a buffer configured to store an output from all the sensors of a sensor array, wherein the buffer is separate from the sensor array; means for processing the stored output to create an image for display corresponding to an output from a plurality of sensors within a first area of the sensor array, wherein the plurality of sensors within the first area of the sensor array are a subset of the sensors of the sensor array; a memory for receiving and storing the image; and means for changing the image displayed by translating the first area, wherein the buffer is configured to enable the system to capture the output from the sensors of the sensor array at a rate greater than the processing rate of the means for processing to create an image for display. a buffer configured to store an output from all the sensors of a sensor array, wherein the buffer is separate from the sensor array; means for processing the stored output to create an image for display corresponding to an output from a plurality of sensors within a first area of the sensor array, wherein the plurality of sensors within the first area of the sensor array are a subset of the sensors of the sensor array; a memory for receiving and storing the image; and means for changing the image displayed by translating the first area, wherein the buffer is configured to enable the system to capture the output from the sensors of the sensor array at a rate greater than the processing rate of the means for processing to create an image for display.
A collecting box for a heat exchanger having flat tubes, with a bottom part having a bottom and two side walls (3b, 3c) and in particular one or two front walls, wherein the bottom has slit-shaped openings extending between the side walls (3b, 3c) for receiving ends of the flat tubes and wherein the openings have-analogous to the cross-section of the ends of the flat tubes - narrow sides and longitudinal sides, wherein the narrow sides are arranged in the region of the wall thickness (s) of the side walls (3b, 3c), wherein the side walls (3b, 3c) partially have pockets with a depth (t) in the region of the narrow sides of the openings, wherein t<s and the pockets are formed as shapes of the side walls (3b, 3c) and the shapes have an inner contour which is adapted to the outer contour of the ends of the flat tubes in the region of their narrow sides, wherein the openings are formed in the form of rim holes with narrow sides and longitudinal sides, wherein the rim holes have opposite, inwardly-directed noses in their middle region which, when used, engage with a beading of a flat tube with a middle beading running in the longitudinal direction.
An air traffic control, ATC, system comprising: a processing device; a memory; and an interface for communicating with aircraft; said system programmed with a plurality of geographical points that define, with respect to a runway, a downwind approach path, a final approach path, and a plurality of constant radius paths connecting the downwind approach path to the final approach path; said system further programmed to define an approach path for an approaching aircraft by selecting one of the constant radius paths for the aircraft to fly; if the aircraft is flying in required navigation performance, RNP, mode, said system further programmed to assign a speed for the aircraft to maintain at various points along the defined approach path, the defined approach path and assigned speed calculated to maintain a separation between other aircraft flying defined approach paths, at assigned speeds, that include one of the constant radius paths; and if the aircraft is not flying in RNP mode, said system further programmed to monitor the speed and direction of the aircraft on the defined approach path to maintain its separation and sequencing relative to other aircraft approaching the runway. a processing device; a memory; and an interface for communicating with aircraft; said system programmed with a plurality of geographical points that define, with respect to a runway, a downwind approach path, a final approach path, and a plurality of constant radius paths connecting the downwind approach path to the final approach path; said system further programmed to define an approach path for an approaching aircraft by selecting one of the constant radius paths for the aircraft to fly; if the aircraft is flying in required navigation performance, RNP, mode, said system further programmed to assign a speed for the aircraft to maintain at various points along the defined approach path, the defined approach path and assigned speed calculated to maintain a separation between other aircraft flying defined approach paths, at assigned speeds, that include one of the constant radius paths; and if the aircraft is not flying in RNP mode, said system further programmed to monitor the speed and direction of the aircraft on the defined approach path to maintain its separation and sequencing relative to other aircraft approaching the runway.
A method for drying writings and/or images made by digital inkjet printing on a glass sheet in a plant comprising a work surface which supports said glass sheet, an inkjet printhead and drying means supplied by an electric power source and mechanically associated with means for moving said drying means along at least one displacement direction parallel to the underlying glass sheet, said method comprising a plurality of translations (T, Ts, Ts', Ts") of said drying means along said at least one displacement direction and according to mutually opposite directions (Ya; Yr) starting from the initial/final edge to end up on the final/initial edge of said glass sheet, and vice versa, characterized in that the intensity value of the electric current supplying said drying means during any one of said translations (T, Ts, Ts', Ts") is greater than the intensity value of the electric current supplying said drying means during the previous translation.
Electrical connection enclosure, the electrical enclosure being supplied with electrical power by power supply cables and being configured to supply at least one electrical load with power, the electrical enclosure comprising: • a power supply column; and • at least one connection column, the power supply cables being connected to the electrical enclosure in the power supply column, each connection column comprising at least one monitoring-and-control unit configured to allow the electrical connection to an electrical load, each monitoring-and-control unit being electrically protected by a protection unit belonging to the connection column of this monitoring-and-control unit, each monitoring-and-control unit being configured to allow the connection and potentially the driving and/or the surveillance of an electrical load, the electrical enclosure being configured to be controlled by an industrial computer, each connection column comprising a communication module which: • centralizes operating information coming from the monitoring-and-control units of this connection column; • is configured to transmit this operating information to the industrial computer; • is configured to receive commands coming from the industrial computer; and • transmits these commands to the monitoring-and-control units of this connection column, characterized in that at least one communication module comprises a power supply block delivering at least one auxiliary voltage to each connection column. • a power supply column; and • at least one connection column, the power supply cables being connected to the electrical enclosure in the power supply column, each connection column comprising at least one monitoring-and-control unit configured to allow the electrical connection to an electrical load, each monitoring-and-control unit being electrically protected by a protection unit belonging to the connection column of this monitoring-and-control unit, each monitoring-and-control unit being configured to allow the connection and potentially the driving and/or the surveillance of an electrical load, the electrical enclosure being configured to be controlled by an industrial computer, each connection column comprising a communication module which: • centralizes operating information coming from the monitoring-and-control units of this connection column; • is configured to transmit this operating information to the industrial computer; • is configured to receive commands coming from the industrial computer; and • transmits these commands to the monitoring-and-control units of this connection column, • centralizes operating information coming from the monitoring-and-control units of this connection column; • is configured to transmit this operating information to the industrial computer; • is configured to receive commands coming from the industrial computer; and • transmits these commands to the monitoring-and-control units of this connection column, characterized in that at least one communication module comprises a power supply block delivering at least one auxiliary voltage to each connection column.
Cosmetic composition in the form of an oil-in-water nanoemulsion, characterized in that it comprises, in a cosmetically acceptable medium, one or more nonionic amphiphilic lipids, from 2% to 15% by weight relative to the total weight of the composition of one or more volatile linear alkanes, one or more cationic amphiphilic lipids and one or more oils other than the said volatile linear alkane(s), the volatile linear alkane or alkanes comprising from 7 to 15 carbon atoms, the number-average size of the globules of the nanoemulsion being between 1 and 350 nm.
A multi-functional toy for facilitating the interaction between an infant and the infant's caregiver and for causing sensory stimulation in an infant, the toy comprising: a body member (3, 4), said body member comprised of a fabric exterior containing a filler material that renders said body member (3, 4) soft and resilient, said body member (3, 4) having a front side and a back side; and a flexibly stiff tail member attached to the back side of said body member (3, 4), wherein: said tail member extends higher than said body member, said tail member has a flexible handle member disposed on one end for holding by a user, and said tail member's exterior surface comprised of soft and flexible materials to present a synthetic feather-like texture. a body member (3, 4), said body member comprised of a fabric exterior containing a filler material that renders said body member (3, 4) soft and resilient, said body member (3, 4) having a front side and a back side; and a flexibly stiff tail member attached to the back side of said body member (3, 4), wherein: said tail member extends higher than said body member, said tail member has a flexible handle member disposed on one end for holding by a user, and said tail member's exterior surface comprised of soft and flexible materials to present a synthetic feather-like texture. said tail member extends higher than said body member, said tail member has a flexible handle member disposed on one end for holding by a user, and said tail member's exterior surface comprised of soft and flexible materials to present a synthetic feather-like texture.
Elevator system with a first elevator car, at least a second elevator car, a drive-machine unit, and a plurality of suspension means, which pass over a traction sheave of the drive-machine unit, wherein the first elevator car and the second elevator car can, by means of the suspension means, be caused by the drive-machine unit to travel one above the other in a travel space which is provided for the joint travel of the first elevator car and the second elevator car, wherein the suspension means are divided into a first suspension-means set and at least a second suspension-means set, wherein at least one displacement mechanism, which is locationally fixed relative to the travel space, is provided, which, between the traction sheave and the second elevator car, interacts with the second suspension-means set, and wherein the displacement mechanism interacts with the second suspension-means set in such manner that a distance between the first elevator car and the second elevator car is variable, characterized in that the distance is adjustable independent of the traction sheave, in particular also with stationary traction sheave.
An aircraft fuel ice capturing filter device housing comprising: (a) an aircraft fuel inlet; (b) an aircraft fuel outlet; (c) a main housing body receiving a flow of aircraft fuel from the aircraft fuel inlet, the main housing body comprising a cylindrical element having a central cavity, an inner surface, an outer surface, and a vertical axis (A-A); and, (d) a cylindrical hollow insert contacting the inner surface of the main housing body; wherein the aircraft fuel inlet is arranged generally perpendicular to the vertical axis (A-A) of the cylindrical element and is configured to provide tangential aircraft fuel flow around the cylindrical element; and, wherein the cylindrical hollow insert in the main housing body is configured to receive an aircraft fuel filter comprising a porous aircraft fuel filter element; characterized in that the cylindrical hollow insert having a plurality of spaced-apart ice-capturing filters, each of the plurality of spaced-apart ice-capturing filters having a front end, a rear end, a top wall, a first side, a second side, a bottom opening, and a plurality of apertures passing through the top wall, wherein the top wall at the front end of each of the plurality of spaced-apart ice-capturing filters is raised a distance from the inner surface of the cylindrical element, forming an opening arranged normal to aircraft fuel flow. (a) an aircraft fuel inlet; (b) an aircraft fuel outlet; (c) a main housing body receiving a flow of aircraft fuel from the aircraft fuel inlet, the main housing body comprising a cylindrical element having a central cavity, an inner surface, an outer surface, and a vertical axis (A-A); and, (d) a cylindrical hollow insert contacting the inner surface of the main housing body; wherein the aircraft fuel inlet is arranged generally perpendicular to the vertical axis (A-A) of the cylindrical element and is configured to provide tangential aircraft fuel flow around the cylindrical element; and, wherein the cylindrical hollow insert in the main housing body is configured to receive an aircraft fuel filter comprising a porous aircraft fuel filter element; wherein the aircraft fuel inlet is arranged generally perpendicular to the vertical axis (A-A) of the cylindrical element and is configured to provide tangential aircraft fuel flow around the cylindrical element; and, wherein the cylindrical hollow insert in the main housing body is configured to receive an aircraft fuel filter comprising a porous aircraft fuel filter element;
Magnetic microparticles coated with glycosaminoglycan for use in the repair of damaged glycosaminoglycan layer in the bladder due to interstitial cystitis.
A laser optical fiber storage device (10,100) for temporarily storing a free end section of an elongated flexible laser optical fiber, comprising: a storage housing (14,114) having an open end (16, 116); the storage housing (14, 114) comprising an elongated flexible tube (28,128) secured at one end to the open end and disposed in a coiled configuration within the storage housing whereby the free end section of the elongated flexible laser optical fiber is insertable through the open end of the storage housing (14,114) so as to safely contain laser light discharged from the flexible laser optical fiber within the storage housing; and a restrictor (32,117a,117b) within the storage housing to reduce the Inner diameter of the elongated flexible tube configured to catch the free end section of the elongated flexible laser optical fiber. a storage housing (14,114) having an open end (16, 116); the storage housing (14, 114) comprising an elongated flexible tube (28,128) secured at one end to the open end and disposed in a coiled configuration within the storage housing whereby the free end section of the elongated flexible laser optical fiber is insertable through the open end of the storage housing (14,114) so as to safely contain laser light discharged from the flexible laser optical fiber within the storage housing; and a restrictor (32,117a,117b) within the storage housing to reduce the Inner diameter of the elongated flexible tube configured to catch the free end section of the elongated flexible laser optical fiber.
An apparatus comprising; a sensor arrangement comprising a plurality of sensor cells wherein a sensor cell comprises a transistor and a sensor coupled to the transistor; first selection circuitry configured to select a subset of sensor cells to which a gate input signal is provided, wherein the gate input signal is provided to the gate of the transistors within the sensor cells; second selection circuitry configured to activate a subset of sensor cells from which an output signal is received; sensing signal circuitry configured to provide an input signal as a sensing signal to the sensor cells, wherein the sensor arrangement is connected in series between the sensing signal circuitry and the second selection circuitry such that the output signal provides an indication of the impedance of the sensors.
An anti-resonant hollow-core optical fiber comprising a first tubular cladding element which defines an internal cladding surface, a plurality of second tubular elements which are attached to the internal cladding surface and together define a core with an effective radius, and a plurality of third tubular elements, each nested within a respective one of the second tubular elements to provide nested tubular arrangements (11a-f); characterized in that: the second tubular elements are arranged in spaced relation and adjacent ones of the second tubular elements have a spacing (d) therebetween; a ratio (d/t) of the spacing (d) of the adjacent second tubular elements and a wall thickness (t) of the second tubular elements is greater than 0.5 and less than 12; and a ratio (z/R) of a radial spacing (z) between radially-inner walls of the second and third tubular elements (5, 7) to the core radius is between 0.35 and 0.95. the second tubular elements are arranged in spaced relation and adjacent ones of the second tubular elements have a spacing (d) therebetween; a ratio (d/t) of the spacing (d) of the adjacent second tubular elements and a wall thickness (t) of the second tubular elements is greater than 0.5 and less than 12; and a ratio (z/R) of a radial spacing (z) between radially-inner walls of the second and third tubular elements (5, 7) to the core radius is between 0.35 and 0.95.
A light engine for a projection system, characterized by: a color splitting-converging prism having a plurality of color sub-assemblies and respective color light valves; at least one additional light valve (10, 10') in series with at least one of said color sub-assemblies and respective color light valves; and a module for converting source pixel data to color bit planes and generating a further bit plane from said color bit planes, said color bit planes driving said respective color light valves and said further bit plane driving said additional light valve (10, 10'), wherein the timing of switching the additional light valve (10, 10') and respective color light valves is related so as to prevent unpredictable color and intensity variations and image artifacts, wherein said additional light valve (10, 10') and said respective colored light valves (10, 10') are digital micromirror devices wherein said module includes an OR gate for combining said color bit planes and outputting a white bit plane such that said additional light valve (10, 10') is on whenever any of said respective color light valves is on and said additional light valve (10, 10') is off whenever all of said respective color light valves are off. a color splitting-converging prism having a plurality of color sub-assemblies and respective color light valves; at least one additional light valve (10, 10') in series with at least one of said color sub-assemblies and respective color light valves; and a module for converting source pixel data to color bit planes and generating a further bit plane from said color bit planes, said color bit planes driving said respective color light valves and said further bit plane driving said additional light valve (10, 10'), wherein the timing of switching the additional light valve (10, 10') and respective color light valves is related so as to prevent unpredictable color and intensity variations and image artifacts,
Stapling device, which extends in a longitudinal direction from a front region to a rear region, having a lower part that has a set-down surface on its underside, having an anvil leg that carries an anvil plate in the front region, which anvil leg is mounted in the front region so as to pivot in restricted manner relative to the lower part about a first pivot axle, having a staple magazine that is mounted on a bearing block in the rear region, so as to pivot about a second pivot axle, relative to the anvil leg, in restricted manner, having a driver leg that is mounted so as to pivot about the second pivot axle in restricted manner, relative to the anvil leg and relative to the staple magazine, which driver leg has a driver for guiding staples through a gap at the front end of the staple magazine and for pressing the staples down against the anvil plate, and having at least one lever (56, 56') that extends in the longitudinal direction, which lever is mounted on the lower part in the rear region, by means of a first bearing, and on the anvil leg by means of a second bearing between the front region and the rear region, wherein one of the bearings (58, 60) is a third pivot axle and the other bearing is a floating bearing, and wherein the at least one lever (56, 56') is coupled with the driver leg, at its front end that faces the front region, in such a manner that a movement of the front end toward the anvil leg results in a movement of the driver toward the anvil plate.