mhurhangee/ep-ind-claims huggingface dataset:
A method for wireless communications at a first user equipment (215-a), comprising: receiving, from a base station, a configuration message comprising an indication of one or more resources for performing cross-link interference measurements of additional UEs (215-b), wherein the configuration message comprises one or more cell parameters associated with one or more of the additional UEs (215-b), wherein the one or more cell parameters comprise one or more cell identity indicators, the one or more cell identity indicators comprising a flag in the configuration message, wherein a first value of the flag indicates a first relationship between a first serving cell (205-a) associated with the first UE (215-a) and a second serving cell (205-b) associated with a second UE (215-b) of the one or more of the additional UEs (215-b), and a second value of the flag indicates a second relationship between the first serving cell (205-a) and the second serving cell (205-b); determining, based at least in part on the one or more cell parameters, a relationship between the first serving cell (205-a) associated with the first UE (215-a) and the second serving cell (205-b) associated with the second UE (215-b) of the one or more of the additional Ues (215-b); and performing a cross-link interference measurement for the second UE (215-b) during at least a portion of the one or more resources, based at least in part on the determined relationship. receiving, from a base station, a configuration message comprising an indication of one or more resources for performing cross-link interference measurements of additional UEs (215-b), wherein the configuration message comprises one or more cell parameters associated with one or more of the additional UEs (215-b), wherein the one or more cell parameters comprise one or more cell identity indicators, the one or more cell identity indicators comprising a flag in the configuration message, wherein a first value of the flag indicates a first relationship between a first serving cell (205-a) associated with the first UE (215-a) and a second serving cell (205-b) associated with a second UE (215-b) of the one or more of the additional UEs (215-b), and a second value of the flag indicates a second relationship between the first serving cell (205-a) and the second serving cell (205-b); determining, based at least in part on the one or more cell parameters, a relationship between the first serving cell (205-a) associated with the first UE (215-a) and the second serving cell (205-b) associated with the second UE (215-b) of the one or more of the additional Ues (215-b); and performing a cross-link interference measurement for the second UE (215-b) during at least a portion of the one or more resources, based at least in part on the determined relationship.
A method of monitoring regional lung functions of a person, the method including: a) projecting a pattern of radiation onto a portion of the person for monitoring; b) recording at a first instant in time first image data representing at least a portion of said projected pattern of radiation on the portion of the person, said first image data being representative of a three dimensional configuration of said portion of the person at said first instant in time; c) recording at a second instant in time second image data representing at least a portion of said projected pattern of radiation on the portion of the person, said second image data being representative of a three dimensional configuration of said portion of the person at said second instant in time; and d) processing said first and second image data to generate differential data representative of a change in volume of said portion of the person between the first and second instants in time. a) projecting a pattern of radiation onto a portion of the person for monitoring; b) recording at a first instant in time first image data representing at least a portion of said projected pattern of radiation on the portion of the person, said first image data being representative of a three dimensional configuration of said portion of the person at said first instant in time; c) recording at a second instant in time second image data representing at least a portion of said projected pattern of radiation on the portion of the person, said second image data being representative of a three dimensional configuration of said portion of the person at said second instant in time; and d) processing said first and second image data to generate differential data representative of a change in volume of said portion of the person between the first and second instants in time.
A balloon coating method for forming a coating layer on an outer surface of a balloon (30, 190) of a balloon catheter (10, 130), the method comprising: a coating step of moving a coating section for applying a coating liquid containing a drug relative to the balloon (30, 190) in an axial direction, while rotating the balloon (30, 190) about an axis of the balloon (30, 190), thereby to apply the coating liquid to an outer surface of the balloon (30, 190); characterised in that the method further comprises a detection step of detecting the distance between the coating section and a dried part where the coating liquid applied to the outer surface of the balloon (30, 190) has been dried from the coating section; and a control step of controlling moving velocity (Sx) of the coating section relative to the balloon (30, 190) in such a manner that the distance between the coating section and the dried part is maintained at a preliminarily set designated distance. a coating step of moving a coating section for applying a coating liquid containing a drug relative to the balloon (30, 190) in an axial direction, while rotating the balloon (30, 190) about an axis of the balloon (30, 190), thereby to apply the coating liquid to an outer surface of the balloon (30, 190); characterised in that the method further comprises a detection step of detecting the distance between the coating section and a dried part where the coating liquid applied to the outer surface of the balloon (30, 190) has been dried from the coating section; and a control step of controlling moving velocity (Sx) of the coating section relative to the balloon (30, 190) in such a manner that the distance between the coating section and the dried part is maintained at a preliminarily set designated distance.
Method for operating a high-pressure discharge lamp, wherein the high-pressure discharge lamp is operated by an inverter with a rectangular-waveform lamp current having a positive phase with positive current flow and a negative phase with negative current flow, and the inverter is regulated by a control unit, comprising the following steps: - measuring a value representing the lamp power or the rectangular-waveform lamp current for the positive current flow, - measuring a value representing the lamp power or the rectangular-waveform lamp current for the negative current flow, - calculating a manipulated variable predefinition from a respective reference variable of a lamp power or the rectangular-waveform lamp current and the measured value for the phase with positive current flow, - calculating a manipulated variable predefinition from a respective reference variable of a lamp power or the rectangular-waveform lamp current and the measured value for the phase with negative current flow, - outputting the two manipulated variable predefinitions to the inverter, characterized in that - between the following manipulated variable predefinitions of both phases there is a time period having a length of between 1 ms and a few seconds. - measuring a value representing the lamp power or the rectangular-waveform lamp current for the positive current flow, - measuring a value representing the lamp power or the rectangular-waveform lamp current for the negative current flow, - calculating a manipulated variable predefinition from a respective reference variable of a lamp power or the rectangular-waveform lamp current and the measured value for the phase with positive current flow, - calculating a manipulated variable predefinition from a respective reference variable of a lamp power or the rectangular-waveform lamp current and the measured value for the phase with negative current flow, - outputting the two manipulated variable predefinitions to the inverter, characterized in that - between the following manipulated variable predefinitions of both phases there is a time period having a length of between 1 ms and a few seconds.
An aircraft fitted with: • pieces of equipment, each having at least one main motor or actuator and at least one emergency motor or actuator; • a main power network delivering three-phase AC power and to which the main motors or actuators are connected; and • an emergency power network, distinct from the main power network, to which the emergency motors or actuators are connected, and including a power bus (11; 28) adapted to convey three-phase AC power generated by at least one DC/AC converter (12; 27) powered by a DC voltage source of the aircraft, the converter being fitted with modulator means for modulating the voltage and/or the frequency of the three-phase power as generated in this way so as to meter the power sent simultaneously to all of the emergency motors or actuators by the emergency power network. • pieces of equipment, each having at least one main motor or actuator and at least one emergency motor or actuator; • a main power network delivering three-phase AC power and to which the main motors or actuators are connected; and • an emergency power network, distinct from the main power network, to which the emergency motors or actuators are connected, and including a power bus (11; 28) adapted to convey three-phase AC power generated by at least one DC/AC converter (12; 27) powered by a DC voltage source of the aircraft, the converter being fitted with modulator means for modulating the voltage and/or the frequency of the three-phase power as generated in this way so as to meter the power sent simultaneously to all of the emergency motors or actuators by the emergency power network.
A sport ball comprising: a casing that includes a plurality of panel elements, wherein each of the panel elements includes a central panel area with flange areas that form an edge portion of the panel and extend around the central panel area, and incisions that disconnect the flange areas from each other and permit the flange areas to flex or otherwise move independently from each other, and wherein the panel elements are joined to each other by welding flange areas together to form welds, portions of the panel elements that include the welds projecting toward an interior of the ball; a bladder located within the casing; and an intermediate layer located between the casing and the bladder. a casing that includes a plurality of panel elements, wherein each of the panel elements includes a central panel area with flange areas that form an edge portion of the panel and extend around the central panel area, and incisions that disconnect the flange areas from each other and permit the flange areas to flex or otherwise move independently from each other, and wherein the panel elements are joined to each other by welding flange areas together to form welds, portions of the panel elements that include the welds projecting toward an interior of the ball; a bladder located within the casing; and an intermediate layer located between the casing and the bladder.
A secondary battery comprising a positive electrode plate and a negative electrode plate, wherein the negative electrode plate comprises a negative electrode current collector and a negative electrode active material layer provided on at least one surface of the negative electrode current collector, an insulation layer and a reaction layer are sequentially provided on the surface of the negative electrode active material layer on the side opposite to the negative electrode current collector side, and the reaction layer comprises at least one of graphite, silicon, silicon oxide, silicon suboxide, tin oxide, copper oxide, and zinc oxide, and when the capacity of the positive electrode active material layer per unit area in the positive electrode plate is denoted as A1 (mAh/cm 2), and the capacity of the negative electrode active material layer per unit area in the negative electrode plate is denoted as B1 (mAh/cm 2), B1/A1 < 1, optionally 0.3 ≤ B1/A1 < 1. wherein the negative electrode plate comprises a negative electrode current collector and a negative electrode active material layer provided on at least one surface of the negative electrode current collector, an insulation layer and a reaction layer are sequentially provided on the surface of the negative electrode active material layer on the side opposite to the negative electrode current collector side, and the reaction layer comprises at least one of graphite, silicon, silicon oxide, silicon suboxide, tin oxide, copper oxide, and zinc oxide, and when the capacity of the positive electrode active material layer per unit area in the positive electrode plate is denoted as A1 (mAh/cm 2), and the capacity of the negative electrode active material layer per unit area in the negative electrode plate is denoted as B1 (mAh/cm 2), B1/A1 < 1, optionally 0.3 ≤ B1/A1 < 1.
A gas turbine engine for an aircraft comprising a compressor (13, 14, 15), a compressor case surrounding the compressor (13, 14, 15) and a compressor tip injector system, the compressor tip injector system comprising a cabin blower system comprising a cabin blower compressor configured to compress air for use in a cabin of the aircraft and for use by the compressor tip injector system, the compressor case comprising one or more injectors (110, 112) of the compressor tip injector system configured to inject air from the cabin blower compressor towards blade tip ends of blades of the compressor (13, 14, 15) as the blades rotate, the cabin blower system further comprising a transmission and the cabin blower compressor is drivable via the transmission, the transmission comprising a toroidal continuously variable transmission giving selectively variable control over the rate at which the cabin blower compressor is driven, the toroidal continuously variable transmission comprising at least one traction drive (52, 54) through which drive power is transmitted, the traction drive (52, 54) comprising first and second toroids (56, 58), the first and second toroids (56, 58) each having one of a pair of opposed toroidal surfaces and there being a set of rotatable variators disposed between the opposed toroidal surfaces, the first and second toroids (56, 58) are separated and are drivingly engaged via a wheel of each variator, each wheel running on both of the opposed toroidal surfaces.
A pouch-type secondary battery comprising: an electrode assembly in which electrodes and separators are stacked; a pouch-type battery case comprising a cup part configured to accommodate the electrode assembly therein, wherein the battery case comprises: a first case and a second case, of which at least one comprises the cup part; a folding part integrally connecting the first case to the second case; and a bat ear protruding outward from a portion of each of opposing ends of the folding part, wherein the bat ear has a length of 1.5 mm or less, characterised in that the battery case is manufactured by molding a pouch film, and the pouch film comprises: a sealant layer made of a first polymer and formed at an innermost layer; a surface protection layer made of a second polymer and formed at an outermost layer; and a moisture barrier layer stacked between the surface protection layer and the sealant layer, and the sealant layer has a thickness of between about 60 μm and 100 μm. an electrode assembly in which electrodes and separators are stacked; a pouch-type battery case comprising a cup part configured to accommodate the electrode assembly therein, wherein the battery case comprises: a first case and a second case, of which at least one comprises the cup part; a folding part integrally connecting the first case to the second case; and a bat ear protruding outward from a portion of each of opposing ends of the folding part, wherein the bat ear has a length of 1.5 mm or less, characterised in that the battery case is manufactured by molding a pouch film, and the pouch film comprises: a sealant layer made of a first polymer and formed at an innermost layer; a surface protection layer made of a second polymer and formed at an outermost layer; and a moisture barrier layer stacked between the surface protection layer and the sealant layer, and the sealant layer has a thickness of between about 60 μm and 100 μm. a first case and a second case, of which at least one comprises the cup part; a folding part integrally connecting the first case to the second case; and a bat ear protruding outward from a portion of each of opposing ends of the folding part, wherein the bat ear has a length of 1.5 mm or less, characterised in that the battery case is manufactured by molding a pouch film, and the pouch film comprises: a sealant layer made of a first polymer and formed at an innermost layer; a surface protection layer made of a second polymer and formed at an outermost layer; and a moisture barrier layer stacked between the surface protection layer and the sealant layer, and the sealant layer has a thickness of between about 60 μm and 100 μm. a sealant layer made of a first polymer and formed at an innermost layer; a surface protection layer made of a second polymer and formed at an outermost layer; and a moisture barrier layer stacked between the surface protection layer and the sealant layer, and the sealant layer has a thickness of between about 60 μm and 100 μm.
A turbocharger system for an air-throttled internal combustion engine having an intake air conduit system for supplying intake air to the engine and an exhaust conduit system for exhausting combustion gases from the engine, the turbocharger system comprising: a turbocharger comprising a compressor disposed in the intake air conduit system and operable for compressing air received from the intake air conduit system and supplying the compressed air through the intake air conduit system to the engine, and a turbine disposed in the exhaust conduit system and operable for expanding exhaust gases received from the exhaust conduit system so as to extract power from the exhaust gases, the turbine being mechanically coupled to the compressor for rotatably driving the compressor; a variable-flow expander (VFE 150) mechanically coupled to the turbocharger (112, 116) and arranged in the intake air conduit system in parallel with the compressor, the VFE comprising a variable expansion ratio turbine that extracts power from air flowing in the intake air conduit system and uses said power to assist the rotation of the turbocharger (112, 116) the variable expansion ratio turbine being controllable to regulate the flow rate of air therethrough and thereby vary an amount of expansion of the air; and an apportioning valve arranged in the intake air conduit system upstream of the compressor and the VFE, the apportioning valve being variably positionable for variably apportioning the air flowing in the intake air conduit system between the compressor and the VFE. a turbocharger comprising a compressor disposed in the intake air conduit system and operable for compressing air received from the intake air conduit system and supplying the compressed air through the intake air conduit system to the engine, and a turbine disposed in the exhaust conduit system and operable for expanding exhaust gases received from the exhaust conduit system so as to extract power from the exhaust gases, the turbine being mechanically coupled to the compressor for rotatably driving the compressor; a variable-flow expander (VFE 150) mechanically coupled to the turbocharger (112, 116) and arranged in the intake air conduit system in parallel with the compressor, the VFE comprising a variable expansion ratio turbine that extracts power from air flowing in the intake air conduit system and uses said power to assist the rotation of the turbocharger (112, 116) the variable expansion ratio turbine being controllable to regulate the flow rate of air therethrough and thereby vary an amount of expansion of the air; and an apportioning valve arranged in the intake air conduit system upstream of the compressor and the VFE, the apportioning valve being variably positionable for variably apportioning the air flowing in the intake air conduit system between the compressor and the VFE.
Method of making a heat-insulating element comprising the steps of: - making a padding of essentially pure discontinuous silk, composed of at least 90% in weight of silk; and - enclosing said padding between a pair of containment layers to make a sandwich structure; the step of making the padding comprising the steps of: i) providing a plurality of natural silk waste; ii) macerating the waste to partially degrade the sericin and fibroin therein contained and to obtain an intermediate mass of discontinuous fibres; iii) subjecting the product of step ii) to carding steps to obtain at least a mat of fibres, or one or more veils of discontinuous silk fibres; iv) optionally overlaying and binding a plurality of fibre veils in a direction orthogonal to a surface of said one or more veils to form an interwoven three-dimensional structure; said method being characterized in that said natural silk waste of step i) are cocoons at least partially subjected to reeling, uncompleted cocoons, cocoons damaged by external elements, flown cocoons without emerged chrysalides, floss silk fibres, residual filaments on the chrysalis on completion of reeling in continuous silk production, or discontinuous silk fibres of other kinds, and in that the discontinuous fibres of the intermediate mass are fibres with a maximum length of approximately 200 millimetres. - making a padding of essentially pure discontinuous silk, composed of at least 90% in weight of silk; and - enclosing said padding between a pair of containment layers to make a sandwich structure; i) providing a plurality of natural silk waste; ii) macerating the waste to partially degrade the sericin and fibroin therein contained and to obtain an intermediate mass of discontinuous fibres; iii) subjecting the product of step ii) to carding steps to obtain at least a mat of fibres, or one or more veils of discontinuous silk fibres; iv) optionally overlaying and binding a plurality of fibre veils in a direction orthogonal to a surface of said one or more veils to form an interwoven three-dimensional structure;