mhurhangee/ep-ind-claims huggingface dataset:
High-pressure fuel pump, in particular plug-in pump, for a fuel injection system for injecting fuel into the combustion chamber of an internal combustion engine, comprising a pump piston which can perform stroke movements and whose first end (1.1) is guided in a hollow cylinder and whose second end (1.2) is supported indirectly via a cup-shaped component on a camshaft or eccentric shaft, furthermore comprising a seal which is preferably in the form of a corrugated bellows and which, forming a ring-shaped chamber, is fastened at one side to the pump piston and at the other side to the hollow cylinder, characterized in that, to seal off the ring-shaped chamber, a guide gap formed between the pump piston and the hollow cylinder is in the form of a ring-shaped gap seal and the guide gap opens into a ring-shaped groove formed in the hollow cylinder, which ring-shaped groove is, for the return of a leakage quantity, connected to a leakage line.
A processor-implemented gaze estimation method, comprising: obtaining an image including an eye region of a user; extracting, from the obtained image, a test feature using a neural network model; obtaining a calibration feature which was extracted using the neural network model and which was used for calibration of the neural network model; and estimating a gaze of the user using the test feature and the calibration feature, wherein the estimating a gaze of the user comprises estimating a position of a gaze point in a gaze area of the user from the test feature and the calibration feature using the neural network model, characterized in that the estimating a gaze of the user further comprises: calculating a feature difference between the test feature and the calibration feature; using a classifier to output a result of classifying the feature difference; calculating, based on the result output by the classifier, a probability that the gaze point is included in each of a plurality of subareas into which the gaze area is divided; and determining, to be the position of the gaze point, a center position of a subarea having a greatest probability among probabilities calculated for the subareas. obtaining an image including an eye region of a user; extracting, from the obtained image, a test feature using a neural network model; obtaining a calibration feature which was extracted using the neural network model and which was used for calibration of the neural network model; and estimating a gaze of the user using the test feature and the calibration feature, wherein the estimating a gaze of the user comprises estimating a position of a gaze point in a gaze area of the user from the test feature and the calibration feature using the neural network model, characterized in that the estimating a gaze of the user further comprises: calculating a feature difference between the test feature and the calibration feature; using a classifier to output a result of classifying the feature difference; calculating, based on the result output by the classifier, a probability that the gaze point is included in each of a plurality of subareas into which the gaze area is divided; and determining, to be the position of the gaze point, a center position of a subarea having a greatest probability among probabilities calculated for the subareas. calculating a feature difference between the test feature and the calibration feature; using a classifier to output a result of classifying the feature difference; calculating, based on the result output by the classifier, a probability that the gaze point is included in each of a plurality of subareas into which the gaze area is divided; and determining, to be the position of the gaze point, a center position of a subarea having a greatest probability among probabilities calculated for the subareas.
A missile comprising: a fuselage; and a flight termination system comprising: deployable roll-producing lift surfaces that deploy during flight from the fuselage, forward of a center of gravity of the missile; wherein the lift surfaces are configured, when deployed, to provide a roll moment to the missile, which causes a rolling attitude that approaches or reaches a rolling rate equal to a natural frequency of the missile. a fuselage; and a flight termination system comprising: deployable roll-producing lift surfaces that deploy during flight from the fuselage, forward of a center of gravity of the missile; wherein the lift surfaces are configured, when deployed, to provide a roll moment to the missile, which causes a rolling attitude that approaches or reaches a rolling rate equal to a natural frequency of the missile. deployable roll-producing lift surfaces that deploy during flight from the fuselage, forward of a center of gravity of the missile; wherein the lift surfaces are configured, when deployed, to provide a roll moment to the missile, which causes a rolling attitude that approaches or reaches a rolling rate equal to a natural frequency of the missile.
Movable radiation protection system comprising: a frame which is open on one side and which comprises a lower part and an upper part, said upper part being vertically adjustable relative to the lower part, wherein the lower part of the frame comprises a chassis, at least two flexible radiation protection drapes for protecting against radiation, preferably X-ray radiation, wherein a first of the at least two radiation protection drapes is attached to the lower part of the frame and extends preferably to the lower edge of the frame, wherein a second of the at least two radiation protection drapes is attached to the upper part of the frame and is formed such that the at least two radiation protection drapes overlap in each height position in which the upper part is adjusted relative to the lower part, wherein the upper part comprises an arcuate connecting element, wherein the arcuate connecting element of the upper part has the shape of a semicircle or a half rectangle with rounded edges, characterized in that the second radiation protection drape is attached to the upper part by means of the connecting element as cover, so that both the front side and the rear side of the movable radiation protection system are covered up to a specific point above the chassis. a frame which is open on one side and which comprises a lower part and an upper part, said upper part being vertically adjustable relative to the lower part, wherein the lower part of the frame comprises a chassis, at least two flexible radiation protection drapes for protecting against radiation, preferably X-ray radiation, wherein a first of the at least two radiation protection drapes is attached to the lower part of the frame and extends preferably to the lower edge of the frame, wherein a second of the at least two radiation protection drapes is attached to the upper part of the frame and is formed such that the at least two radiation protection drapes overlap in each height position in which the upper part is adjusted relative to the lower part, wherein the upper part comprises an arcuate connecting element, wherein the arcuate connecting element of the upper part has the shape of a semicircle or a half rectangle with rounded edges, characterized in that the second radiation protection drape is attached to the upper part by means of the connecting element as cover, so that both the front side and the rear side of the movable radiation protection system are covered up to a specific point above the chassis.
Fuel cell comprising a stack comprising an assembly of overlaid electrochemical generators, along a stack axis, and end plates (5, 6) axially clasping said assembly, the fuel cell further comprising at least one holding winding surrounding said stack and bearing on said end plates (5, 6), characterized in that said holding winding comprises at least one sheet of at least on taut wire wound around the stack in the form of a plurality of turns, the ends of the taut wire being fixed on at least one of the end plates; and in that said holding winding comprises rounded portions (24, 25, 26, 27) bearing on spaced-apart bearing rounded portions (18, 19 and 20, 21) of said end plates (5, 6) and free portions (14, 15, 28, 29) joining these bearing portions.
A sunroof device including: a guided portion that is attached to a roof panel and extends along a sliding direction of the roof panel; a lifting arm that serves to lift, and support the weight of, the roof panel; and a guide member that is attached to the lifting arm and guides the sliding of the roof panel via a guide groove into which the guided portion is fit, characterised in that the guide member is configured to include a first member that is molded of a resin material and has the guide groove, and a second member as a reinforcing member that covers the first member so as to make it immovable in two directions orthogonal to the sliding direction, and wherein the first member is inserted into or removed from the second member in the sliding direction by elastically deforming an upper section of the first member toward the guide groove and is mounted to the second member so as to be immovable in the sliding direction by a snap-fit coupling means that exploits a restoring force of the elastically deformed upper section to cause the first member to engage with the second member. a guided portion that is attached to a roof panel and extends along a sliding direction of the roof panel; a lifting arm that serves to lift, and support the weight of, the roof panel; and a guide member that is attached to the lifting arm and guides the sliding of the roof panel via a guide groove into which the guided portion is fit,
A self-adjusting clutch having a disc spring (10, 22), which is arranged between an adjusting device and clutch linings, wherein the adjusting device is preloaded via at least one energy store, in particular a compression spring, characterised in that the disc spring (10, 22) comprises at least one recess (12, 24) for partially receiving a circumference of the energy store of the adjusting device of the coupling.
A method by a terminal in a wireless communication system, the method comprising: if the terminal is configured with multiple timing advance groups, TAGs, and if a transmission of a random access preamble on a first serving cell belonging to a first TAG in parallel with a transmission of an uplink signal on a second serving cell belonging to a second TAG is requested (711, 811), identifying (741, 841) whether a total transmission power required for the transmission of the random access preamble and the transmission of the uplink signal exceeds a maximum terminal output power; if the total transmission power exceeds the maximum terminal output power, adjusting a transmission power of the uplink signal or dropping the transmission of the uplink signal; and transmitting the random access preamble on the first serving cell. if the terminal is configured with multiple timing advance groups, TAGs, and if a transmission of a random access preamble on a first serving cell belonging to a first TAG in parallel with a transmission of an uplink signal on a second serving cell belonging to a second TAG is requested (711, 811), identifying (741, 841) whether a total transmission power required for the transmission of the random access preamble and the transmission of the uplink signal exceeds a maximum terminal output power; if the total transmission power exceeds the maximum terminal output power, adjusting a transmission power of the uplink signal or dropping the transmission of the uplink signal; and transmitting the random access preamble on the first serving cell.
A spring-loaded air rifle comprising: - a trigger; - a firing mechanism; - an interconnection piece; - a counter-ratchet; - a piston; and - a spring driving the piston, wherein said trigger drives the firing mechanism which acts on the interconnection piece, said interconnection piece exerting a force upon the counter-ratchet which releases the piston, wherein said firing mechanism is an electronic firing mechanism which comprises a flexible rod, an electromechanical actuator and a switch to operate the electromechanical actuator, said flexible rod being mechanically coupled to the trigger characterized in that the flexible rod is initially moved by the trigger using a first force until the flexible rod reaches a stop where a second force is exerted to bend the flexible rod to activate the switch, enabling the trigger to continue rotating even after the switch has been activated. - a trigger; - a firing mechanism; - an interconnection piece; - a counter-ratchet; - a piston; and - a spring driving the piston,
A shuttle trolley for a parcel-sorting logistics center, which trolley has a deck for carrying a non-standard parcel to be sorted, the deck having a central portion in the shape of a trough of V-shaped cross-section, and two side portions (7B, 7C) on either side of the central portion and that both extend in the same horizontal plane, said shuttle trolley being characterized in that the body of the deck comprises framework members forming two combs disposed back-to-back, the teeth of the combs extending parallel to one another from the central portion of the body to the edges of respective ones of the side portions (7B, 7C).
A coin cell comprising two cases (201, 208) designed to form a housing, an assembly of stacked electrodes placed inside the housing and comprising at least one positive electrode, at least one negative electrode (204, 204', 204"), and at least one separator placed in-between them, characterized in that it further comprises a insulating packing tape comprising an insulator basis and at least one packing flap integral with the insulator basis, said insulating packing tape being placed in such a way that the insulator basis is between the assembly of stacked electrodes and one of the cases to avoid electrical contact between the assembly of stacked electrodes and said case and the packing flap holds the assembly of stacked electrodes to form an electrode pack.
An imaging device comprising a photoelectric conversion unit in which a first electrode, a photoelectric conversion layer, and a second electrode (21,22,23a,23b,24) are stacked, wherein an inorganic oxide semiconductor material layer is formed between the first electrode and the photoelectric conversion layer, and the inorganic oxide semiconductor material layer contains zinc atoms and tin atoms, forming a composition expressed by Zn a Sn b O c, characterized by the following conditions: a + b + c = 1.00 b > a. a photoelectric conversion unit in which a first electrode, a photoelectric conversion layer, and a second electrode (21,22,23a,23b,24) are stacked, wherein an inorganic oxide semiconductor material layer is formed between the first electrode and the photoelectric conversion layer, and the inorganic oxide semiconductor material layer contains zinc atoms and tin atoms, forming a composition expressed by Zn a Sn b O c, characterized by the following conditions: a + b + c = 1.00 b > a.
A method for making a biomolecule microarray on a substrate having a patterned surface with a plurality of hydrophobic and hydrophilic areas, the method comprising a) providing a substrate with a pattern on its surface; b) contacting the patterned surface with a fluorocarbon plasma wherein a hydrophobic material is selectively deposited on selected areas of the surface of the substrate while, at the same time, the rest of the surface of the substrate is etched; c) without any further modifications other than plasma exposure described in step b) above, contacting the said patterned surface exposed to plasma with a biomolecule solution, or with a plurality of biomolecule solutions, to enable adsorption of the biomolecule, wherein the biomolecule is a protein. a) providing a substrate with a pattern on its surface; b) contacting the patterned surface with a fluorocarbon plasma wherein a hydrophobic material is selectively deposited on selected areas of the surface of the substrate while, at the same time, the rest of the surface of the substrate is etched; c) without any further modifications other than plasma exposure described in step b) above, contacting the said patterned surface exposed to plasma with a biomolecule solution, or with a plurality of biomolecule solutions, to enable adsorption of the biomolecule, wherein the biomolecule is a protein.
Polymer matrix with the capability of controlled release of active substance incorporated therein, wherein the polymer matrix is formed from gel-forming polymers and a cross-linking agent, wherein the gel-forming polymers have binding sites that react with the cross-linking agent to form cross-links, wherein the matrix additionally contains dissolving agent, which, after activation, breaks once again the cross-links and brings about the self-dissolution of the polymer matrix, wherein the dissolving agent is a complex forming agent, the complex formation constant of which is higher after activation with the cross-linking agent than the complex formation constant of the binding site, wherein activation is caused by the environmental conditions at the application site, and wherein the active substance is released in the course of the self-dissolution.
An intervertebral implant configured to be implanted in an intervertebral disc space of a quadruped, the intervertebral disc space defined by a cranial vertebral body and a caudal vertebral body, the implant comprising: a plate defining a ventral plate end and a dorsal plate end spaced opposite the ventral plate end in a dorsal direction, and a plurality of fixation apertures that extend through the plate from the ventral plate end to the dorsal plate end; and a spacer that extends in the dorsal direction from the plate, wherein the spacer defines a caudal surface and a cranial surface opposite the caudal surface in a cranial direction, the caudal and cranial surfaces (44, 42) configured to grip the caudal and cranial vertebral bodies (28, 30), respectively, characterized in that the cranial surface is convex in a first plane that is oriented along the dorsal direction and the cranial direction, and the cranial surface is convex in a second plane that is oriented along the cranial direction and a lateral direction that is substantially perpendicular to each of the dorsal direction and the cranial direction, and the caudal surface is substantially straight and linear in the first plane, and the caudal surface is concave in the second plane. a plate defining a ventral plate end and a dorsal plate end spaced opposite the ventral plate end in a dorsal direction, and a plurality of fixation apertures that extend through the plate from the ventral plate end to the dorsal plate end; and a spacer that extends in the dorsal direction from the plate, wherein the spacer defines a caudal surface and a cranial surface opposite the caudal surface in a cranial direction, the caudal and cranial surfaces (44, 42) configured to grip the caudal and cranial vertebral bodies (28, 30), respectively, characterized in that the cranial surface is convex in a first plane that is oriented along the dorsal direction and the cranial direction, and the cranial surface is convex in a second plane that is oriented along the cranial direction and a lateral direction that is substantially perpendicular to each of the dorsal direction and the cranial direction, and the caudal surface is substantially straight and linear in the first plane, and the caudal surface is concave in the second plane.
An isolated modified polynucleotide encoding a modified full-length protease, wherein the portion of said modified polynucleotide that encodes the pro region of said full-length protease comprises a mutation encoding a substitution at least at one amino acid position chosen from positions equivalent to amino acid positions 28-108 and 109 of SEQ ID NO: 5, 13 or 244, said substitution at least at one amino acid position being selected from the group consisting of: A28Q, A28T, E29T, E29Y, E29V, E29Q, E29K, E29M, E29P, E29N, E29S, E29G, E29A, E30Q, E30K, E30M, E30A, E30G, E30R, E30S, E30H, E30N, E30T, A31 R, A31G, A31S, A31 K, A31 P, E33R, E33Q, E33G, E33H, E33N, E33S, E33D, E33I, E33K, E33M, K34R, N40V, N40K, N40E, N40Q, N40H, N40Y, N40T, N40A, N40L, N40W, N40F, N40R, E41A, E41 S, E41 N, E41T, E41H, E41 R, Q42M, Q42R, Q42P, Q42W, E43S, E43R, E43D, E43H, E43A, A44D, A44Q, A44E, A44S, V45L, V45A, V45C, S46H, S46R, S46T, S46A, S46Q, S46Y, S46W, E47D, E47R, E47K, E47Q, E47H, F48W, V49G, E50H, Q51M, Q51R, V52L, V52W, E53A, E53K, E53R, E53H, A54L, A54S, D56G, D56S, D56K, D56R, E57N, E57H, E57S, E57G, E57Q, E57C, E57M, E57D, E57R, E57K, E57W, E57F, V58R, V58Y, V58H, V58M, V58K, V58C, V58L, V58A, V58F, A59R, A59Y, A59V, A59I, A59F, A59W, A59M, A59L, A59H, I60L, L61M, L61T, L61A, L61I, L61V, L61G, L61P, L61D, S62V, S62W, S62M, S62P, S62N, S62H, S62Q, S62D, S62G, S62I, S62A, S62L, S62C, S62R, S62T, E63A, E63G, E63D, E63R, E63T, E63Q, E63C, E63K, E63H, E63I, E63S, E64T, E64R, E64S, E64A, E65M, E65R, E65Q, E65A, E65V, E65Y, E66S, E66A, E66T, E66P, E66R, E66Y, E66K, E66G, E66V, E66M, E66Q, V67I, E68K, E68Q, I69V, E70T, E70R, E70N, E70S, E70V, L71V, L71I, E74Q, E74R, E74V, E74K, E74A, E74I, F75Y, E76K, E76S, E76T, E76H, E76N, E76D, T77N, T77H, I78T, S82L, S82Q, S82V, V83N, V83Y, E84L, E84K, E84V, E84M, E84S, E84A, E84G, E84T, E84R, E84F, E84Q, L85F, S86R, S86D, S86K, S86N, S86A, E88P, E88D, D89K, D89H, D91 E, D91 P, D91A, D91T, D91N, D91K, D91W, D91R, D91 F, A92R, A92K, A92T, A92M, A92V, A92Q, A92I, A92L, A92S, E94A, E94M, E94T, E94R, E94S, E94L, L95E, L95R, L95K, L95S, L95C, L95A, L95T, L95D, L95G, L95V, L95H, D96Y, D96H, D96C, D96S, D96L, D96E, D96I, D96W, D96V, A98R, A98K, A98D, A98L, S100A, E103T, E103P, E104P, A106F, A106K, A106V, A106L, A106M, E107Q, E107P, T109Y, T109E, T109G, T109N, T109S, T109M, T109R, T109Q and T109W, and wherein the mature region of said modified full-length protease has at least 98% amino acid sequence identity with the amino acid sequence of SEQ ID NO: 8, 16 or 247.
Muzzle brake for a firearm comprising a body that is joined to said firearm, and where said body has a central channel, which allows the projectile to exit once it has been fired; wherein the body incorporates two recesses (1a, 1b) on its surface, and in each recess (1a, 1b) a plurality of first holes which are inclined at approximately 45° is located; and where on each of said recesses (1a, 1b) a second body is respectively located, wherein each second body comprises, in turn, a plurality of second holes coinciding in number with the first holes in the recesses (1a, 1b); said second holes being inclined in the opposite direction to the inclination of the first holes in the recesses (1a, 1b) in such a way that there is a reverse of gases coming from the firing of the projectile from the firearm; and where the body incorporates a series of internal springs that are housed in third holes in the body and cross the body longitudinally through said third holes through which there also extend guide rods and tubular bodies that join said body with a series of baffles or hammer module responsible for redirecting the rest of the gases that have not been redirected through the first and second holes (1c, 2a) and for violently pulling the solid body that holds said baffles, in the same direction as the gas outflow.