mhurhangee/ep-ind-claims huggingface dataset:
Portable electronic device, comprising a housing, a chemical sensor arranged inside the housing, which chemical sensor is adapted to measure a property of different analytes and to detect at least one property of at least two different analytes, an opening in the housing for exposing the chemical sensor to a fluid to be analyzed, and at least one additional sensor out of the following list of sensors: - a humidity sensor, - a pressure sensor, - an airflow sensor, wherein the chemical sensor and the at least one additional sensor face the same common opening. - a humidity sensor, - a pressure sensor, - an airflow sensor,
A force measurement device comprising: a closed contour load sensing element axisymmetric along a loading axis (y-axis) and an axis (x-axis) normal to the loading axis; a first rigid cantilever arm (1,11) mounted on the contour in one of the four quadrants of the contour, and a second rigid cantilever arm (2,12) mounted in the opposite quadrant of the contour, where free ends of both the first and second rigid cantilever arms being inward of the contour such that the arms are perpendicular to an arc at the fixed end on the contour; wherein deformation ( δ / 2) caused by applied load causes quasi-linear movement of the free ends of the cantilever arms to enable mechanical amplification of the deformation along the axis of loading. a closed contour load sensing element axisymmetric along a loading axis (y-axis) and an axis (x-axis) normal to the loading axis; a first rigid cantilever arm (1,11) mounted on the contour in one of the four quadrants of the contour, and a second rigid cantilever arm (2,12) mounted in the opposite quadrant of the contour, where free ends of both the first and second rigid cantilever arms being inward of the contour such that the arms are perpendicular to an arc at the fixed end on the contour; wherein deformation ( δ / 2) caused by applied load causes quasi-linear movement of the free ends of the cantilever arms to enable mechanical amplification of the deformation along the axis of loading.
An information processing device for object recognition comprising: a setting unit configured to set an object region, for image information obtained by capturing an imaging range of an imaging unit, the object region corresponding to an object existing in the imaging range; a luminance information acquiring unit configured to acquire luminance information indicating brightness of subjects in the imaging range, wherein the setting unit sets the object region based on the luminance information, characterized by a correcting unit configured to set a luminance detection region which is a region from a lower end position of the object region to an upper position at a predetermined vertical distance in pixels from the lower end position of the object, to calculate average luminance in the luminance detection region containing the object for each of pixel row in order from the lowest to the highest pixel row of the luminance detection region, and to correct the lower end position of the object region so as to shift the lower end position up to a position of a pixel row in which the row average luminance is smaller than a predetermined value to include a shadow formed under the object but exclude the road marking underneath the lowermost portion of the object. a setting unit configured to set an object region, for image information obtained by capturing an imaging range of an imaging unit, the object region corresponding to an object existing in the imaging range; a luminance information acquiring unit configured to acquire luminance information indicating brightness of subjects in the imaging range, wherein the setting unit sets the object region based on the luminance information, characterized by a correcting unit configured to set a luminance detection region which is a region from a lower end position of the object region to an upper position at a predetermined vertical distance in pixels from the lower end position of the object, to calculate average luminance in the luminance detection region containing the object for each of pixel row in order from the lowest to the highest pixel row of the luminance detection region, and to correct the lower end position of the object region so as to shift the lower end position up to a position of a pixel row in which the row average luminance is smaller than a predetermined value to include a shadow formed under the object but exclude the road marking underneath the lowermost portion of the object.
A computer-implemented method for performing a validation of a test result from an analyzing instrument, comprising the steps of: receiving information related to a collection source of a body fluid sample collected from a body cavity; determining, based on the received information, whether the body fluid sample corresponds to a first group including at least one specific type of body fluid, or a second group including at least a plurality of types of body fluids other than the specific type of body fluid; obtaining a test result of the body fluid sample from the analyzing instrument; and validating the obtained test result based on a first validation rule when the body fluid sample corresponds to the first group, and validating the obtained test result based on a second validation rule different from the first validation rule when the body fluid sample corresponds to the second group. receiving information related to a collection source of a body fluid sample collected from a body cavity; determining, based on the received information, whether the body fluid sample corresponds to a first group including at least one specific type of body fluid, or a second group including at least a plurality of types of body fluids other than the specific type of body fluid; obtaining a test result of the body fluid sample from the analyzing instrument; and validating the obtained test result based on a first validation rule when the body fluid sample corresponds to the first group, and validating the obtained test result based on a second validation rule different from the first validation rule when the body fluid sample corresponds to the second group.
Cryogenic refrigeration device comprising an enclosure delimiting a vacuum-sealed volume closed by a cover, the device comprising at least one cryogenic cooler mounted through the cover and having a first end located outside the enclosure and a second end located inside the enclosure, the cryogenic cooler being configured to supply cold at its second end, the device comprising at least two thermally conductive plates (5, 6, 10) distributed in a distribution direction in the enclosure and forming thermal stages, at least some of the plates (5, 6, 10) being cooled by the cryogenic cooler to respective determined temperatures which decrease in the distribution direction, the device comprising a shield (19, 20) and a set of heat exchangers, at least one of the plates (5, 6, 10) being connected to said thermal shield (19, 20) forming a volume which encloses at least one following plate, the cryogenic cooler being of the type which uses a cold source of liquefied cycle fluid such as helium or nitrogen, characterized in that in the device the cooling power of the cryogenic cooler is stored and/or produced at its first end, in that at least some of the plates (5, 6, 10) are cooled by the cycle fluid via a set of heat exchangers in heat exchange with said plates (5, 6) and with a flow of the cycle fluid which transfers cooling power from the first end to the second end of the cryogenic cooler.
A socket comprising an annular socket part and a lamella basket at least partly disposed in the interior of the annular socket part, the lamella basket comprising a plurality of lamellae and an annular carrier strip located at the rear part of the lamella basket, each of the lamellae having a first end and a second end, with the first end being firmly attached to or integrally moulded with the annular carrier strip and with the second end being implemented as a free end, with the lamellae extending from the annular carrier strip towards the front end of the socket, wherein at least one of the lamellae comprises a bulge that stands out in a radially inward direction, wherein the inner surface of the annular socket part comprises a bulge that stands out in a radially inward direction, wherein the bulge of the annular socket part is configured for supporting the lamellae when the lamellae are resiliently deformed in a radially outward direction, characterised in that the inner surface of the annular socket part and the rear surface of the resiliently deformed lamellae are of complementary shape, wherein the longitudinal position of the lamellae's bulge corresponds to the longitudinal position of the annular socket part's bulge, with the annular socket part's bulge being configured for supporting the lamellae's bulge when the lamellae are resiliently deformed in a radially outward direction.
A sleeve assembly for a combustion system, said sleeve assembly comprising: a first duct comprising a first circumferential surface, wherein the first duct is a transition duct; a second duct comprising a second circumferential surface, wherein the second duct is a liner and wherein said first circumferential surface radially overlaps said second circumferential surface such that said first duct and said second duct collectively define a continuous combustion chamber therein, the continuous combustion chamber configured to receive high temperature gases flowing therethrough; and a wear insert removably coupled to said first circumferential surface and extending radially therefrom to engage said second circumferential surface; wherein said second duct further comprises a body and a seal extending axially from said body, wherein said seal comprises said second circumferential surface, wherein said first duct defines a groove radially recessed from said first circumferential surface, wherein said wear insert is seated within the groove; and wherein said first duct further comprises a first radial surface for engaging a first radial edge of said wear insert and a second radial surface, wherein the groove is defined axially between said first radial surface and said second radial surface, wherein said second radial surface is axially spaced from said first radial surface to engage a second radial edge of said wear insert to inhibit axial movement of said wear insert within the groove. a first duct comprising a first circumferential surface, wherein the first duct is a transition duct; a second duct comprising a second circumferential surface, wherein the second duct is a liner and wherein said first circumferential surface radially overlaps said second circumferential surface such that said first duct and said second duct collectively define a continuous combustion chamber therein, the continuous combustion chamber configured to receive high temperature gases flowing therethrough; and a wear insert removably coupled to said first circumferential surface and extending radially therefrom to engage said second circumferential surface; wherein said second duct further comprises a body and a seal extending axially from said body, wherein said seal comprises said second circumferential surface, wherein said first duct defines a groove radially recessed from said first circumferential surface, wherein said wear insert is seated within the groove; and wherein said first duct further comprises a first radial surface for engaging a first radial edge of said wear insert and a second radial surface, wherein the groove is defined axially between said first radial surface and said second radial surface, wherein said second radial surface is axially spaced from said first radial surface to engage a second radial edge of said wear insert to inhibit axial movement of said wear insert within the groove.
A packet processing method, comprising: receiving, by a current network node, a first packet; determining, by the current network node, a flow identification corresponding to the first packet, wherein the first packet does not comprise the flow identification, a feature of the first packet corresponds to the flow identification, and the feature of the first packet is located in a header of the first packet; obtaining, by the current network node based on the first packet and the flow identification, a second packet, wherein the second packet comprises a field comprising the flow identification and an inband operations, administration and maintenance, IOAM, header, and in the second packet, the field comprising the flow identification is located in a hop-by-hop options header before the IOAM header when the second packet is an internet protocol version 6 IPv6 packet; and sending, by the current network node, the second packet to a next network node. receiving, by a current network node, a first packet; determining, by the current network node, a flow identification corresponding to the first packet, wherein the first packet does not comprise the flow identification, a feature of the first packet corresponds to the flow identification, and the feature of the first packet is located in a header of the first packet; obtaining, by the current network node based on the first packet and the flow identification, a second packet, wherein the second packet comprises a field comprising the flow identification and an inband operations, administration and maintenance, IOAM, header, and in the second packet, the field comprising the flow identification is located in a hop-by-hop options header before the IOAM header when the second packet is an internet protocol version 6 IPv6 packet; and sending, by the current network node, the second packet to a next network node.
Device for attaching a solar panel to a frame of the roof type, said attaching device being intended firstly to be secured to said frame by a substantially flexible connecting strip, and secondly to receive said panel, characterised in that it comprises at least one profiled member forming a first jaw and a second jaw, said profiled member being designed to be deformed in the region of said jaws (13, 14) in order to wedge said connecting strip between said jaws (13, 14).
Urine absorbent bag configured to house a penis of a user, having a planar multilayer structure folded in "C"-shape to form said absorbent bag having a longitudinal axis, wherein said absorbent bag has a top opening, configured to receive the penis of the user, that is defined by a top edge of the planar multilayer structure, wherein said absorbent bag further has a closed bottom defined by a bottom edge of the planar multilayer structure, whereby a first lateral portion of the planar multilayer structure is overlapping a central portion of the planar multilayer structure so that a first lateral edge thereof is placed below a second lateral portion of the planar multilayer structure, wherein the planar multilayer structure comprises an inner layer configured to come into contact with the penis of the user, an outer layer and an absorbent core interposed between the inner layer and the outer layer, wherein the absorbent core is configured to absorb and retain fluid, wherein an end portion of a second lateral edge of the planar multilayer structure, longitudinally extending from the bottom edge to a length not greater than 50% of the length of the second lateral edge, is permanently coupled onto the first lateral portion.
The use of compounds of general formula, in which R 1, R 2, R 3, R 4, R 5 and R 6 represent, independently of one another, hydrogen or SO 3 X, with the proviso that at least 1 of the mentioned functional groups R 1 to R 6 is not hydrogen, and X represents hydrogen, an alkali metal or ammonium, in liquid laundry detergents containing builders and no oxidative bleaching agents to improve the washing or cleaning performance against bleachable stains. in which R 1, R 2, R 3, R 4, R 5 and R 6 represent, independently of one another, hydrogen or SO 3 X, with the proviso that at least 1 of the mentioned functional groups R 1 to R 6 is not hydrogen, and X represents hydrogen, an alkali metal or ammonium, in liquid laundry detergents containing builders and no oxidative bleaching agents to improve the washing or cleaning performance against bleachable stains.
A fuel oil injector for a gas turbine engine, the injector comprising: a tubular body extending along an axis; a first fuel oil supply duct and a second fuel oil supply duct in the tubular body; characterized by a terminal member fitted into an injection end of the tubular body, the terminal member holding a plurality of flat fan nozzles in respective circumferential positions around the axis and at a common axial position; wherein the nozzles are identical to each other and are configured to deliver respective flat fuel oil jets tilted with respect to the axis, It whereby the fuel oil jets delimit respective sides of an inner fuel-free region, thus approximating a hollow cone by a frustum; and wherein the first fuel oil supply duct is coupled to a first group (22a; 22a') of the nozzles and the second fuel oil supply duct is coupled to a second group (22b; 22b') of the nozzles, the nozzles of the first group (22a; 22a') being distinct from the nozzle or nozzles of the second group (22b; 22b'). a tubular body extending along an axis; a first fuel oil supply duct and a second fuel oil supply duct in the tubular body; characterized by a terminal member fitted into an injection end of the tubular body, the terminal member holding a plurality of flat fan nozzles in respective circumferential positions around the axis and at a common axial position; wherein the nozzles are identical to each other and are configured to deliver respective flat fuel oil jets tilted with respect to the axis, It whereby the fuel oil jets delimit respective sides of an inner fuel-free region, thus approximating a hollow cone by a frustum; and wherein the first fuel oil supply duct is coupled to a first group (22a; 22a') of the nozzles and the second fuel oil supply duct is coupled to a second group (22b; 22b') of the nozzles, the nozzles of the first group (22a; 22a') being distinct from the nozzle or nozzles of the second group (22b; 22b').
Interior aircraft LED light unit comprising: at least one printed circuit board, on which a plurality of LEDs (2a, 2b, 2c, 2d, 2e) are connected to a power source, each one of the plurality of LEDs (2a, 2b, 2c, 2d, 2e) having a predetermined distance (Da, Db, Dc, Dd, De) to the power source, and each one of the plurality of LEDs (2a, 2b, 2c, 2d, 2e) being associated with a respective thermal transfer member (5a, 5b, 5c, 5d, 5e; 7a, 7b, 7c, 7d, 7e) having a predetermined size, for transferring heat away from the respective LED (2a, 2b, 2c, 2d, 2e), wherein, for at least five of the plurality of LEDs (2a, 2b, 2c, 2d, 2e), the predetermined size of the respective thermal transfer member (5a, 5b, 5c, 5d, 5e; 7a, 7b, 7c, 7d, 7e) varies with the predetermined distance (Da, Db, Dc, Dd, De) of the LED (2a, 2b, 2c, 2d, 2e) to the power source, with the predetermined size of the thermal transfer members decreasing for an increase in the predetermined distance of the LED to the power source, and wherein an operating temperature of each of the plurality of LEDs (2a, 2b, 2c, 2d, 2e) is between 70% and 130% of an average operating temperature of the plurality of LEDs (2a, 2b, 2c, 2d, 2e). at least one printed circuit board, on which a plurality of LEDs (2a, 2b, 2c, 2d, 2e) are connected to a power source, each one of the plurality of LEDs (2a, 2b, 2c, 2d, 2e) having a predetermined distance (Da, Db, Dc, Dd, De) to the power source, and each one of the plurality of LEDs (2a, 2b, 2c, 2d, 2e) being associated with a respective thermal transfer member (5a, 5b, 5c, 5d, 5e; 7a, 7b, 7c, 7d, 7e) having a predetermined size, for transferring heat away from the respective LED (2a, 2b, 2c, 2d, 2e), wherein, for at least five of the plurality of LEDs (2a, 2b, 2c, 2d, 2e), the predetermined size of the respective thermal transfer member (5a, 5b, 5c, 5d, 5e; 7a, 7b, 7c, 7d, 7e) varies with the predetermined distance (Da, Db, Dc, Dd, De) of the LED (2a, 2b, 2c, 2d, 2e) to the power source, with the predetermined size of the thermal transfer members decreasing for an increase in the predetermined distance of the LED to the power source, and wherein an operating temperature of each of the plurality of LEDs (2a, 2b, 2c, 2d, 2e) is between 70% and 130% of an average operating temperature of the plurality of LEDs (2a, 2b, 2c, 2d, 2e).
A method of processing a linked series of metallic plates, in which each metallic plate is connected to an adjacent metallic plate along adjoining edges, the method comprising: providing the series of metallic plates as a first fan-folded stack of plates; using a first rotatable transfer spool assembly to draw the metallic plates in sequence from the first fan-folded stack; applying a surface treatment to one or more of the metallic plates; and using the first rotatable transfer spool assembly or a second rotatable transfer spool assembly to stack the metallic plates in reverse order to form a second fan-folded stack of metallic plates; wherein the first rotatable transfer spool assembly and/or the second rotatable transfer spool if present, each comprise a series of arms equally spaced around the rotatable transfer spool assembly, wherein the arms are configured to engage with the adjoining edges of the metallic plates, the spacing of the arms corresponding with the distance between consecutive adjoining edges in the series of metallic plates in the first fan-folded stack. providing the series of metallic plates as a first fan-folded stack of plates; using a first rotatable transfer spool assembly to draw the metallic plates in sequence from the first fan-folded stack; applying a surface treatment to one or more of the metallic plates; and using the first rotatable transfer spool assembly or a second rotatable transfer spool assembly to stack the metallic plates in reverse order to form a second fan-folded stack of metallic plates; wherein the first rotatable transfer spool assembly and/or the second rotatable transfer spool if present, each comprise a series of arms equally spaced around the rotatable transfer spool assembly, wherein the arms are configured to engage with the adjoining edges of the metallic plates, the spacing of the arms corresponding with the distance between consecutive adjoining edges in the series of metallic plates in the first fan-folded stack.