mhurhangee/patent-ind-claim-en huggingface dataset:
A measuring system including: a first sensor that is configured to emit light to a first portion of a subject, compress the first portion, and measure reflected light or transmitted light from the first portion; a second sensor that is configured to emit light to a second portion of the subject, compress the second portion, and measure reflected light or transmitted light from the second portion a first measurement value calculator that is configured to, based on a change of an amount of received light that is measured by the first sensor , calculate a first measurement value indicating an index related to a first blood refill time; a second measurement value calculator that is configured to, based on a change of an amount of received light that is measured by a second sensor , calculate a second measurement value indicating an index related to a second blood refill time; and a pressure controller that is configured to control the first sensor and the second sensor so that a time difference between a start of compression release by the first sensor and a start of compression release by the second sensor is within a predetermined time period; and an evaluator that is configured to evaluate a cardiovascular system of the subject based on a comparison process using the first measurement value and the second measurement value. a first sensor that is configured to emit light to a first portion of a subject, compress the first portion, and measure reflected light or transmitted light from the first portion; a second sensor that is configured to emit light to a second portion of the subject, compress the second portion, and measure reflected light or transmitted light from the second portion a first measurement value calculator that is configured to, based on a change of an amount of received light that is measured by the first sensor , calculate a first measurement value indicating an index related to a first blood refill time; a second measurement value calculator that is configured to, based on a change of an amount of received light that is measured by a second sensor , calculate a second measurement value indicating an index related to a second blood refill time; and a pressure controller that is configured to control the first sensor and the second sensor so that a time difference between a start of compression release by the first sensor and a start of compression release by the second sensor is within a predetermined time period; and an evaluator that is configured to evaluate a cardiovascular system of the subject based on a comparison process using the first measurement value and the second measurement value.
A method for monitoring hydrogen-induced cracking in at least one test specimen, comprising: saturating a test solution with a gas comprising H 2 S; delivering the saturated test solution into a test cell , wherein the test cell comprises at least one specimen port and at least one test specimen , the at least one specimen port being configured to receive the at least one test specimen ; exposing the at least one test specimen to the saturated test solution, wherein only one surface of each specimen is exposed to the saturated test solution; and characterized in that it comprises the steps of: scanning the at least one test specimen with at least one ultrasonic transducer at two or more time points, wherein each of the at least one ultrasonic transducers is operatively connected to one of the at least one specimen ports opposite the surface of each specimen exposed to the saturated test solution, and wherein each of the at least one ultrasonic transducer is configured to rotate completely around a symmetry axis of the test specimen to complete each scan. saturating a test solution with a gas comprising H 2 S; delivering the saturated test solution into a test cell , wherein the test cell comprises at least one specimen port and at least one test specimen , the at least one specimen port being configured to receive the at least one test specimen ; exposing the at least one test specimen to the saturated test solution, wherein only one surface of each specimen is exposed to the saturated test solution; and characterized in that it comprises the steps of: scanning the at least one test specimen with at least one ultrasonic transducer at two or more time points, wherein each of the at least one ultrasonic transducers is operatively connected to one of the at least one specimen ports opposite the surface of each specimen exposed to the saturated test solution, and wherein each of the at least one ultrasonic transducer is configured to rotate completely around a symmetry axis of the test specimen to complete each scan.
A method for updating network access application, NAA, authentication information, wherein the method comprises: receiving, by a terminal , a first message from a remote server , wherein the first message comprises NAA authentication parameter update information and a first identifier; updating, by the terminal , authentication information of a profile corresponding to the first identifier based on the NAA authentication parameter update information; and detaching, by the terminal , from a network, and re-attaching to the network based on updated authentication information of the profile, wherein the terminal comprises an embedded universal integrated circuit card, eUICC , the first message further comprises profile content and firmware update request information, and the profile content and the firmware update request information are used to instruct the eUICC to update eUICC firmware and content of the profile corresponding to the first identifier. receiving, by a terminal , a first message from a remote server , wherein the first message comprises NAA authentication parameter update information and a first identifier; updating, by the terminal , authentication information of a profile corresponding to the first identifier based on the NAA authentication parameter update information; and detaching, by the terminal , from a network, and re-attaching to the network based on updated authentication information of the profile, wherein the terminal comprises an embedded universal integrated circuit card, eUICC , the first message further comprises profile content and firmware update request information, and the profile content and the firmware update request information are used to instruct the eUICC to update eUICC firmware and content of the profile corresponding to the first identifier.
An expandable device for use within a hollow-body organ, said device having a first compressed configuration with a compressed diameter and a second expanded configuration with an expanded diameter for conformation against a tissue wall and defining a lumen for fluid flow therethrough, wherein the expandable device comprises at least one biodegradable polymer filament arranged to form a repeating diamond-shaped pattern, wherein the at least one biodegradable polymer filament comprises poly(lactide-co-glycolide), and characterized in that at least a portion of the expandable device is coated with a drug, impregnated with the drug, at least partially coated with a drug eluting layer including the drug, or includes one or more drug depots holding the drug, such that the expandable device is configured to release the drug at a daily dosage of about 500 μg or less per day.
A cover member for lighting devices, the cover member comprising: - an elongated light-propagation body having a light-radiation receiving surface and a light-radiation emitting surface (S) opposed to the light-radiation receiving surface , the cover member positionable with the light-radiation receiving surface facing an elongated light-radiation emission module , wherein the light-propagation body provides light-propagation paths for light radiation from the light-radiation receiving surface to the light-radiation emitting surface (S), wherein: - the light-propagation body comprises light-diffusive material, and - a light-obstructive barrier is provided at the light-radiation receiving surface leaving uncovered at least one lateral portion of the light-radiation receiving surface , wherein said light-propagation paths include tortuous light-propagation paths through said at least one lateral portion circumventing the light-obstructive barrier , characterized in that the cover member includes lateral confinement surfaces of the light-propagation body , the lateral confinement surfaces comprising material with light-reflection capability, wherein said light-propagation paths comprise reflections at said lateral confinement surfaces . - an elongated light-propagation body having a light-radiation receiving surface and a light-radiation emitting surface (S) opposed to the light-radiation receiving surface , the cover member positionable with the light-radiation receiving surface facing an elongated light-radiation emission module , wherein the light-propagation body provides light-propagation paths for light radiation from the light-radiation receiving surface to the light-radiation emitting surface (S), wherein: - the light-propagation body comprises light-diffusive material, and - a light-obstructive barrier is provided at the light-radiation receiving surface leaving uncovered at least one lateral portion of the light-radiation receiving surface , wherein said light-propagation paths include tortuous light-propagation paths through said at least one lateral portion circumventing the light-obstructive barrier ,
A combustion system for a gas turbine engine comprising: a combustor dome including a fuel manifold with an inlet and nozzle components of a plurality of nozzles circumferentially spaced around the combustor dome wherein the fuel manifold and nozzle components are integrated with the combustor dome for fluid communication from the inlet to the nozzle components , wherein the fuel manifold forms an outer combustor dome ring , wherein the nozzle components extend from the outer combustor dome ring radially inward to an inner combustor dome ring ; and an outer cowl extending from the outer combustor dome ring and an inner cowl extending from the inner combustor dome ring , wherein the inner and outer cowls cooperate to form an annular diverging inlet for feeding compressor discharge air to the nozzles; characterized in that the inner and outer cowls are mounted to the inner and outer combustor dome rings , respectively, with clips on the upstream and downstream sides of the combustor dome . a combustor dome including a fuel manifold with an inlet and nozzle components of a plurality of nozzles circumferentially spaced around the combustor dome wherein the fuel manifold and nozzle components are integrated with the combustor dome for fluid communication from the inlet to the nozzle components , wherein the fuel manifold forms an outer combustor dome ring , wherein the nozzle components extend from the outer combustor dome ring radially inward to an inner combustor dome ring ; and an outer cowl extending from the outer combustor dome ring and an inner cowl extending from the inner combustor dome ring , wherein the inner and outer cowls cooperate to form an annular diverging inlet for feeding compressor discharge air to the nozzles; characterized in that the inner and outer cowls are mounted to the inner and outer combustor dome rings , respectively, with clips on the upstream and downstream sides of the combustor dome .
Casing of a turbine engine , notably for a compressor (4; 6) of an axial turbine engine, the casing comprising: - a wall , and - at least one fastening flange associated with the wall , the fastening flange comprising a fastening surface that can be applied against a corresponding mounting surface of the turbine engine , or against another fastening surface, characterized in that the fastening flange comprises at least one electrical connector with one end lying flush with the fastening surface of said fastening flange and in that the wall is a first wall , the casing further comprising a second wall with a fastening flange and electrical connector identical or similar to those associated with the first wall , the fastening flanges (30A; 30B) being fastened together so as to provide an electrical contact between the connectors . - a wall , and - at least one fastening flange associated with the wall , the fastening flange comprising a fastening surface that can be applied against a corresponding mounting surface of the turbine engine , or against another fastening surface,
Method for determining a first integrity sum (T) comprising the following steps: - determining a first masked item of data (C') by application of an "exclusive OR" operation between a first item of data (C) and a first data mask (R); - determining a second item of data (D') by application to the first masked item of data (C') of a first cryptographic function (G), the second item of data (D') being masked by a second data mask (R; S); - determining a second integrity sum (T 0 ) associated with the second item of data (D') by application to said second item of data (D') of a checksum function (Cks); and - determining the first integrity sum (T) by application of an "exclusive OR" operation between the second integrity sum (T 0 ) and a third integrity sum (T 1 ) associated with the second data mask (R; S). - determining a first masked item of data (C') by application of an "exclusive OR" operation between a first item of data (C) and a first data mask (R); - determining a second item of data (D') by application to the first masked item of data (C') of a first cryptographic function (G), the second item of data (D') being masked by a second data mask (R; S); - determining a second integrity sum (T 0 ) associated with the second item of data (D') by application to said second item of data (D') of a checksum function (Cks); and - determining the first integrity sum (T) by application of an "exclusive OR" operation between the second integrity sum (T 0 ) and a third integrity sum (T 1 ) associated with the second data mask (R; S).
A device for air-braking an artificial satellite of a planet with an atmosphere, comprising at least one air-braking wing connected to at least one propellant tank of the satellite so as to be deployable by inflation by a gas, called inflation gas, originating from such a tank , characterized in that it comprises at least one leakage monitoring device adapted to release an inflation gas leakage flow in Space during the deployment of each air-braking wing , this leakage flow being adapted to: - enable the introduction, into the air-braking wing , of a flow, called inflation flow, of an inflation gas originating from said propellant tank adapted to cause a deployment of the air-braking wing by inflation, - ensure a complete purging of said propellant tank and the air-braking wing after the deployment of the air-braking wing , such that it constitutes a device for air-braking and passivating the satellite. - enable the introduction, into the air-braking wing , of a flow, called inflation flow, of an inflation gas originating from said propellant tank adapted to cause a deployment of the air-braking wing by inflation, - ensure a complete purging of said propellant tank and the air-braking wing after the deployment of the air-braking wing , such that it constitutes a device for air-braking and passivating the satellite.
A cryostat housing for a superconducting wired circuit, said cryostat housing including: • a partition wall delimiting a first space and a second space internal to the cryostat housing ; • a first opening and a second opening of the cryostat housing are located at one side and the other of the partition, opening out into the first internal space and into the second internal space , respectively, and each configured to fasten, in a leak-tight manner, an end of a cryogenic jacket (20a, 20b; 20) surrounding at least one superconducting wire (21a, 21b; 21) and to let through at least one superconducting wire (21a, 21b;21) into the first internal space and into the second internal space , respectively; • a third opening of the cryostat housing , communicating with the first internal space and forming an outlet for a cooling fluid flowing in a cryogenic jacket (20a; 20) fastened to the first opening ; • a fourth opening of the cryostat housing , communicating with the second internal space and forming an inlet for a pressurized cooling fluid flowing in a cryogenic jacket (20b; 20) fastened to the second opening ; the cryostat housing being characterized in that said separating partition incorporates a cavity forming at least one partition feedthrough for the passage of at least one superconducting wire (21a, 21b; 21), and an opening for access to said cavity enabling said cavity to be filled with an electrically insulating material injected in polymerizable liquid form in order to make said at least one partition feedthrough leak-tight with regard to cooling fluids after the polymerization of the electrically insulating material. • a partition wall delimiting a first space and a second space internal to the cryostat housing ; • a first opening and a second opening of the cryostat housing are located at one side and the other of the partition, opening out into the first internal space and into the second internal space , respectively, and each configured to fasten, in a leak-tight manner, an end of a cryogenic jacket (20a, 20b; 20) surrounding at least one superconducting wire (21a, 21b; 21) and to let through at least one superconducting wire (21a, 21b;21) into the first internal space and into the second internal space , respectively; • a third opening of the cryostat housing , communicating with the first internal space and forming an outlet for a cooling fluid flowing in a cryogenic jacket (20a; 20) fastened to the first opening ; • a fourth opening of the cryostat housing , communicating with the second internal space and forming an inlet for a pressurized cooling fluid flowing in a cryogenic jacket (20b; 20) fastened to the second opening ;
Monitoring system for monitoring and setting at least one air parameter in a room, the monitoring system comprising a fume extraction device , a sensor , at least one monitoring unit , which is provided separately from the sensor and is connected to the sensor via a wireless communications link of a communications network, and at least one mobile terminal device of the communications network, characterised in that the fume extraction device comprises at least the one sensor for acquiring the at least one air parameter and at least one wireless communications interface for communication with the at least one mobile terminal device of the communications network so that at least sensor data from the at least one sensor can be transmitted from the fume extraction device to the part of the monitoring unit which is provided in the mobile terminal device in the form of an application, said part serving for outputting and further processing monitoring results, for activating warning mechanisms and/or for actuating home automation devices.
An intravascular blood pump, comprising a rotatable shaft carrying an impeller and a housing having an opening , wherein the shaft extends through the opening with the impeller positioned outside said housing, the shaft and the housing having surfaces forming a circumferential gap within said opening , wherein the gap has a length and has a gap width of 2 μm or less over at least a part of said length and wherein at least one of the surfaces forming the gap is made of a material having a thermal conductivity of at least 100 W/mK.
A method for agronomic and agricultural monitoring, the method comprising: monitoring, by a central processing unit (CPU) at a base station , an unmanned aerial vehicle (UAV) , as the UAV flies along a flight path above an area and as the UAV performs: capturing, by a CPU of the UAV , a plurality of initial normalized difference vegetation index (NDVI) images of the area as the UAV flies along the flight path; receiving an identification, by the CPU of the UAV , of one or more target areas having low nitrogen levels shown in the NDVI images, for capturing one or more additional different images at higher resolution; in response to receiving the identification: causing the UAV to return to said one or more target areas; causing, by the CPU of the UAV , the UAV to capture the one or more additional different images at higher resolution of the one or more target areas; and transmitting, via the CPU of the UAV , the plurality of initial NDVI images and the one or more additional different images to an image recipient. monitoring, by a central processing unit (CPU) at a base station , an unmanned aerial vehicle (UAV) , as the UAV flies along a flight path above an area and as the UAV performs: capturing, by a CPU of the UAV , a plurality of initial normalized difference vegetation index (NDVI) images of the area as the UAV flies along the flight path; receiving an identification, by the CPU of the UAV , of one or more target areas having low nitrogen levels shown in the NDVI images, for capturing one or more additional different images at higher resolution; in response to receiving the identification: causing the UAV to return to said one or more target areas; capturing, by a CPU of the UAV , a plurality of initial normalized difference vegetation index (NDVI) images of the area as the UAV flies along the flight path; receiving an identification, by the CPU of the UAV , of one or more target areas having low nitrogen levels shown in the NDVI images, for capturing one or more additional different images at higher resolution; in response to receiving the identification: causing the UAV to return to said one or more target areas; causing, by the CPU of the UAV , the UAV to capture the one or more additional different images at higher resolution of the one or more target areas; and transmitting, via the CPU of the UAV , the plurality of initial NDVI images and the one or more additional different images to an image recipient.