mhurhangee/ep-ind-claims huggingface dataset:
A GNSS receiver comprising a processor configured to implement an integrity monitoring method comprising: accessing an original geometry matrix G and an original weighting matrix W stored in a memory of the GNSS receiver, for a plurality of satellites arranged in one or more constellations; computing an original covariance matrix A corresponding to the original geometry matrix G and the original weighting matrix W; generating a first modified geometry matrix G î corresponding to a modified satellite geometry with a first satellite removed; precomputing a first vector v i based on the original covariance matrix A and a first set of geometry matrix values g i corresponding to the first satellite in the original geometry matrix G, wherein the first vector v i is precomputed as a dot product of the original covariance matrix A and the vector g i T corresponding to the i -th row values of the original geometry matrix G; precomputing a first weighting factor x' i based on the first vector v i, the first set of geometry matrix values g i, and a first weighting value w ii corresponding to the first satellite in the original weighting matrix W, using the following equations: x i = 1 − g i T w ii A g i = 1 − g i T w ii v i, and x ′ i = w ii / x i; and computing a plurality of elements a' rs of a modified covariance matrix A î based on the original covariance matrix A, the first vector v i, and the first weighting factor x' i, using the following equation: a ′ rs = a rs + x ′ i ⋅ v r v s. accessing an original geometry matrix G and an original weighting matrix W stored in a memory of the GNSS receiver, for a plurality of satellites arranged in one or more constellations; computing an original covariance matrix A corresponding to the original geometry matrix G and the original weighting matrix W; generating a first modified geometry matrix G î corresponding to a modified satellite geometry with a first satellite removed; precomputing a first vector v i based on the original covariance matrix A and a first set of geometry matrix values g i corresponding to the first satellite in the original geometry matrix G, wherein the first vector v i is precomputed as a dot product of the original covariance matrix A and the vector g i T corresponding to the i -th row values of the original geometry matrix G; precomputing a first weighting factor x' i based on the first vector v i, the first set of geometry matrix values g i, and a first weighting value w ii corresponding to the first satellite in the original weighting matrix W, using the following equations: x i = 1 − g i T w ii A g i = 1 − g i T w ii v i, and x ′ i = w ii / x i; and computing a plurality of elements a' rs of a modified covariance matrix A î based on the original covariance matrix A, the first vector v i, and the first weighting factor x' i, using the following equation: a ′ rs = a rs + x ′ i ⋅ v r v s.
A measurement device for measuring the pressure of a tire of a wheel mounted on an axle of a vehicle, the measurement device comprising a stationary portion for securing to the axle and a movable portion for being driven in rotation by the wheel, characterized in that the stationary portion comprises a first printed circuit having at least one first track formed thereon defining a first winding, the movable portion comprising a second printed circuit having at least one second track formed thereon defining a second winding, the second printed circuit being arranged to be connected to a pressure sensor, the first winding and the second winding being coupled together electromagnetically to form a wireless communication channel, the measurement device being arranged in such a manner that the pressure sensor is electrically powered by the stationary portion via the wireless communication channel, and in such a manner that uplink data comprising pressure measurement data is transmitted to the stationary portion by the movable portion via the wireless communication channel.
An electric power supply device comprising: a switch interposed between an electric power system and a predetermined load (5, 8) to which electric power needs to be supplied in an uninterrupted manner in a power failure; a power storage system having a secondary battery, a first charging and discharging unit interposed between the secondary battery and the electric power system, and a second charging and discharging unit interposed between the secondary battery and the predetermined load; and a control unit configured to control the switch, the first charging and discharging unit, and the second charging and discharging unit, wherein the control unit is configured to, when system abnormality occurs, cause the switch to open to disconnect between the electric power system and the predetermined load, and cause the second charging and discharging unit to supply electric power to the predetermined load; characterized in that the control unit is configured to, when system abnormality occurs, cause the first charging and discharging unit to cause reverse power flow from the secondary battery for a prescribed time,. a switch interposed between an electric power system and a predetermined load (5, 8) to which electric power needs to be supplied in an uninterrupted manner in a power failure; a power storage system having a secondary battery, a first charging and discharging unit interposed between the secondary battery and the electric power system, and a second charging and discharging unit interposed between the secondary battery and the predetermined load; and a control unit configured to control the switch, the first charging and discharging unit, and the second charging and discharging unit, wherein the control unit is configured to, when system abnormality occurs, cause the switch to open to disconnect between the electric power system and the predetermined load, and cause the second charging and discharging unit to supply electric power to the predetermined load; characterized in that the control unit is configured to, when system abnormality occurs, cause the first charging and discharging unit to cause reverse power flow from the secondary battery for a prescribed time,.
A management method for a plurality of production lines (2A to 2E) producing products, wherein configuration data of working machines (5A1 to 5E2) configuring the production lines (2A to 2E), work data regarding work to produce the products, and distribution data for distributing the work data to the working machines (5A1 to 5E2) based on the configuration data are provided, and the distribution data is registered and managed for each production line (2A to 2E), wherein the production lines (2A to 2E) are mounting lines (2A to 2E) which manufacture a substrate with a component mounted thereon, the working machines (5A1 to 5E2) are component mounting machines (5A1 to 5E2), the work data is configured by the mounting position of the component expressed by a coordinate system of the substrate, the mounting angle of the component, and the type of the component wherein plural sets of distribution data are registered and managed, by distributing one set of work data to the working machines (5A1 to 5E2) for each production line (2A to 2E).
A method, comprising: receiving torque data of a powder recoater having a shaft, said powder recoater operatively connected to an additive manufacturing system, wherein the torque data includes torque data of the recoater when the recoater traverses a build area, wherein receiving torque data includes receiving force data from a plurality of load cells, each load cell operatively associated with the shaft and one of a plurality of collars rotatably disposed around the shaft, each collar rigidly connected to a blade segment of a recoater blade assembly; and determining a quality of one or more of an additive manufacturing process and/or product based on the torque data. receiving torque data of a powder recoater having a shaft, said powder recoater operatively connected to an additive manufacturing system, wherein the torque data includes torque data of the recoater when the recoater traverses a build area, wherein receiving torque data includes receiving force data from a plurality of load cells, each load cell operatively associated with the shaft and one of a plurality of collars rotatably disposed around the shaft, each collar rigidly connected to a blade segment of a recoater blade assembly; and determining a quality of one or more of an additive manufacturing process and/or product based on the torque data.
A device (100; 400) comprising at least one processor configured to: while the device is in a locked mode, cause display of an object (202; 204) in a relatively dimmed or less highlighted manner, representing an application that is present or available in the device, on a proximity screen; and respond to reception of user proximity input, at the object, the proximity input being near but not in contact with the proximity screen, by temporarily highlighting the object and temporarily activating the application such that a function of the application can be viewed, without unlocking the device and without opening the application. while the device is in a locked mode, cause display of an object (202; 204) in a relatively dimmed or less highlighted manner, representing an application that is present or available in the device, on a proximity screen; and respond to reception of user proximity input, at the object, the proximity input being near but not in contact with the proximity screen, by temporarily highlighting the object and temporarily activating the application such that a function of the application can be viewed, without unlocking the device and without opening the application.
An oral dosage form, containing (a) deferasirox, (b) binder, (c) disintegrant, and (d) optionally wicking agent wherein introducing the dosage form into water leads to a suspension wherein the suspended particles have an average particle size of 45 μm to 120 μm, especially 50 μm to 110 μm, wherein the average particle size is determined 5 minutes after the dosage form is introduced into water by means of laser diffractometry, and wherein the dosage form contains more than 35% to 60% by weight disintegrant (c), based on the total weight of the dosage form. (a) deferasirox, (b) binder, (c) disintegrant, and (d) optionally wicking agent wherein introducing the dosage form into water leads to a suspension wherein the suspended particles have an average particle size of 45 μm to 120 μm, especially 50 μm to 110 μm, wherein the average particle size is determined 5 minutes after the dosage form is introduced into water by means of laser diffractometry, and wherein the dosage form contains more than 35% to 60% by weight disintegrant (c), based on the total weight of the dosage form.
An indicator for an inflator, the inflator comprising a firing lever, said firing lever comprising: an upstanding arm and a lower leg portion, characterized in that said indicator comprising a long side wall and a short side wall joined together by a bottom wall to form a generally U-shaped configuration, said long side wall being configured and dimensioned to cover and conceal said upstanding arm of the firing lever of the inflator and said bottom wall being configured and dimensioned to cover and conceal the lower leg portion of the firing lever. an upstanding arm and a lower leg portion, characterized in that said indicator comprising a long side wall and a short side wall joined together by a bottom wall to form a generally U-shaped configuration, said long side wall being configured and dimensioned to cover and conceal said upstanding arm of the firing lever of the inflator and said bottom wall being configured and dimensioned to cover and conceal the lower leg portion of the firing lever.
A method for service transmission, the method comprising: after User Equipment, UE, accesses a cell, receiving, by the UE, information sent by a network side through N bits added in a control channel, and N is a positive integer greater than 0, wherein the N bits are used for carrying the information comprising: a UE-specific Guard Period, GP, length, and one of a duration of an uplink service or a duration of a downlink service; determining, by the UE, the other of the duration of the uplink service or the duration of the downlink service according to the information; and sending, by the UE, the uplink service according to the duration of the uplink service, or receiving the downlink service according to the duration of the downlink service. after User Equipment, UE, accesses a cell, receiving, by the UE, information sent by a network side through N bits added in a control channel, and N is a positive integer greater than 0, wherein the N bits are used for carrying the information comprising: a UE-specific Guard Period, GP, length, and one of a duration of an uplink service or a duration of a downlink service; determining, by the UE, the other of the duration of the uplink service or the duration of the downlink service according to the information; and sending, by the UE, the uplink service according to the duration of the uplink service, or receiving the downlink service according to the duration of the downlink service.
A communication method, comprising: cycling operation of a first Radio Access Technology, RAT, between active periods and inactive periods of transmission, on a communication medium shared with a second RAT, in accordance with a Discontinuous Transmission, DTX, communication pattern, characterized by: selecting an identifier indicating first RAT operation; and transmitting, over the communication medium, a channel reservation message associated with the second RAT to reserve the communication medium for one of the active periods of the first RAT, the channel reservation message including the identifier. selecting an identifier indicating first RAT operation; and transmitting, over the communication medium, a channel reservation message associated with the second RAT to reserve the communication medium for one of the active periods of the first RAT, the channel reservation message including the identifier.
A sizing composition capable of crosslinking to form an organic binder of insulating products based on mineral wool characterized in that it comprises - at least one non-reducing saccharide selected from trehalose and sucrose, - at least one hydrogenated saccharide selected from erythritol, arabitol, xylitol, sorbitol, mannitol, iditol, maltitol, isomaltitol, lactitol, cellobitol, palatinitol, maltotritol and the hydrogenation products of starch hydrolysates and representing from 40 % to 80 % of the total weight of non-reducing saccharide(s) and hydrogenated saccharide(s), and - a polycarboxylic organic acid which is citric acid, and - at least 1 % and up to 20 % by weight of a catalyst selected from sodium hypophosphite, sodium phosphite and mixtures of these compounds, of the total weight of the non-reducing saccharide(s), of the hydrogenated saccharide(s) and of polycarboxylic organic acid, the non-reducing saccharide(s) and the hydrogenated saccharide(s) represent from 10 % to 90 % of the weight of the mixture consisting of the non-reducing saccharide(s), the hydrogenated saccharide(s) and the polycarboxylic organic acid. - at least one non-reducing saccharide selected from trehalose and sucrose, - at least one hydrogenated saccharide selected from erythritol, arabitol, xylitol, sorbitol, mannitol, iditol, maltitol, isomaltitol, lactitol, cellobitol, palatinitol, maltotritol and the hydrogenation products of starch hydrolysates and representing from 40 % to 80 % of the total weight of non-reducing saccharide(s) and hydrogenated saccharide(s), and - a polycarboxylic organic acid which is citric acid, and - at least 1 % and up to 20 % by weight of a catalyst selected from sodium hypophosphite, sodium phosphite and mixtures of these compounds, of the total weight of the non-reducing saccharide(s), of the hydrogenated saccharide(s) and of polycarboxylic organic acid,
A method for sterilizing a sealed container filled with a medical solution comprising a buffer, which solution evolves vapor when heated, said method comprising: providing the sealed container filled with the medical solution; applying pressure above atmospheric to the medical solution within the sealed container; and exposing the sealed container to an elevated temperature sufficient to sterilize the medical solution within the sealed container, wherein said elevated temperature would be sufficient to evolve vapor at atmospheric pressure; wherein the applied pressure is sufficient to inhibit the evolution of the vapor within the container, characterized in that the applied pressure is less than an upper limit at which, if a pressure of the medical solution exceeds the upper limit, crystallization of the buffer or other species in the medical solution can occur. providing the sealed container filled with the medical solution; applying pressure above atmospheric to the medical solution within the sealed container; and exposing the sealed container to an elevated temperature sufficient to sterilize the medical solution within the sealed container, wherein said elevated temperature would be sufficient to evolve vapor at atmospheric pressure; wherein the applied pressure is sufficient to inhibit the evolution of the vapor within the container, characterized in that the applied pressure is less than an upper limit at which, if a pressure of the medical solution exceeds the upper limit, crystallization of the buffer or other species in the medical solution can occur.
Turbine engine with a longitudinal axis comprising: - a rotor supporting at least one variable pitch blade, said rotor being guided in rotation relative to a fixed structure of said turbine engine via a first bearing and a second bearing, the rotor comprises a ring for supporting said at least one blade; - a system for controlling the pitch of said at least one blade, said controlling system being secured to said rotor and comprising at least one first actuator set in motion by an energy, said controlling system being arranged axially upstream of said first and second bearings (6, 7); - a device for transferring said energy disposed axially between the first bearing and the second bearing, said transferring device comprising a fixed member secured to said fixed structure and a moving member secured to said rotor; characterised in that the rotor comprises a shaft having a frustoconical portion and a cylindrical portion on which said first and second bearings (6, 7) and said moving member of said transferring device are attached, the frustoconical portion of the shaft extending around the cylindrical portion. - a rotor supporting at least one variable pitch blade, said rotor being guided in rotation relative to a fixed structure of said turbine engine via a first bearing and a second bearing, the rotor comprises a ring for supporting said at least one blade; - a system for controlling the pitch of said at least one blade, said controlling system being secured to said rotor and comprising at least one first actuator set in motion by an energy, said controlling system being arranged axially upstream of said first and second bearings (6, 7); - a device for transferring said energy disposed axially between the first bearing and the second bearing, said transferring device comprising a fixed member secured to said fixed structure and a moving member secured to said rotor;
A system for inerting a fuel tank of an aircraft, comprising: a first compressor fluidly coupled to the fuel tank for removing an air and fuel vapor mixture from an ullage of the fuel tank; a fuel processor fluidly coupled to the first compressor and configured to receive the air and fuel vapor mixture and to generate hydrogen from the air and fuel vapor mixture; a fuel cell fluidly coupled to the fuel processor and configured to receive the hydrogen as anode fuel to produce electricity, the fuel cell generating an exhaust product; a combustor fluidly coupled to the fuel cell and configured to combust the exhaust product to produce combustion gas; and a first heat exchanger fluidly coupled to the combustor and configured to cool the combustion gas into inerting gas for the fuel tank. a first compressor fluidly coupled to the fuel tank for removing an air and fuel vapor mixture from an ullage of the fuel tank; a fuel processor fluidly coupled to the first compressor and configured to receive the air and fuel vapor mixture and to generate hydrogen from the air and fuel vapor mixture; a fuel cell fluidly coupled to the fuel processor and configured to receive the hydrogen as anode fuel to produce electricity, the fuel cell generating an exhaust product; a combustor fluidly coupled to the fuel cell and configured to combust the exhaust product to produce combustion gas; and a first heat exchanger fluidly coupled to the combustor and configured to cool the combustion gas into inerting gas for the fuel tank.
A method of physical vapor deposition comprising: applying a radio frequency signal to a cathode in a physical vapor deposition apparatus, wherein the cathode includes a dielectric sputtering target; electrically connecting a chuck in the physical vapor deposition apparatus to an impedance matching network, wherein the chuck supports a substrate, and wherein the impedance matching network includes at least one capacitor; selecting or adjusting a capacitance of the at least one capacitor such that a positive self bias direct current voltage is generated on the substrate, wherein the positive self bias direct current voltage is between 10V and 100V; and depositing material from the dielectric sputtering target onto the substrate. applying a radio frequency signal to a cathode in a physical vapor deposition apparatus, wherein the cathode includes a dielectric sputtering target; electrically connecting a chuck in the physical vapor deposition apparatus to an impedance matching network, wherein the chuck supports a substrate, and wherein the impedance matching network includes at least one capacitor; selecting or adjusting a capacitance of the at least one capacitor such that a positive self bias direct current voltage is generated on the substrate, wherein the positive self bias direct current voltage is between 10V and 100V; and depositing material from the dielectric sputtering target onto the substrate.
Method to produce a polymeric product, said method comprising: - fragmentation into desired sizing of a primary heterogeneous mixture comprising polymeric material, obtaining a fragmented material of the desired sizing, said primary heterogeneous mixture comprising two or more chosen from the following polymers: polyethylene, polypropylene, high-density polyethylene (HDPE), low-density polyethylene (LDPE), polyethylene terephthalate; - mechanical primary selection, waterless, of said fragmented material to remove metallic material, non-polyolefin polymers and non-polymeric foreign fraction; - subjecting said fragmented material to plastification, obtaining a densified material; - subjecting said densified material to quenching at least by means of air cooling carried out with pneumatic transport, thus obtaining a densified and cooled material which constitutes said polymeric product. - fragmentation into desired sizing of a primary heterogeneous mixture comprising polymeric material, obtaining a fragmented material of the desired sizing, said primary heterogeneous mixture comprising two or more chosen from the following polymers: polyethylene, polypropylene, high-density polyethylene (HDPE), low-density polyethylene (LDPE), polyethylene terephthalate; - mechanical primary selection, waterless, of said fragmented material to remove metallic material, non-polyolefin polymers and non-polymeric foreign fraction; - subjecting said fragmented material to plastification, obtaining a densified material; - subjecting said densified material to quenching at least by means of air cooling carried out with pneumatic transport, thus obtaining a densified and cooled material which constitutes said polymeric product.