mhurhangee/patent-ind-claim-en huggingface dataset:
A wireless transmit/receive unit, WTRU , configured to use a power saving state, the WTRU comprising: a transmitter; a receiver; and a processor , wherein: the transmitter is configured to send a request message, wherein the request message includes a plurality of parameters associated with a plurality of power saving states supported by the WTRU; the receiver is configured to receive, from a mobility management entity, MME, an accept message comprising at least one selected parameter associated with at least one selected power saving state, wherein the at least one selected power saving state is from the plurality of power saving states supported by the WTRU, wherein the accept message further comprises at least one value associated with the at least one selected power saving state; the processor is configured to activate the at least one selected power saving state; and the processor is further configured to, upon a determination that a time equal to the at least one value has elapsed, deactivate the at least one selected power saving state. a transmitter; a receiver; and a processor , wherein: the transmitter is configured to send a request message, wherein the request message includes a plurality of parameters associated with a plurality of power saving states supported by the WTRU; the receiver is configured to receive, from a mobility management entity, MME, an accept message comprising at least one selected parameter associated with at least one selected power saving state, wherein the at least one selected power saving state is from the plurality of power saving states supported by the WTRU, wherein the accept message further comprises at least one value associated with the at least one selected power saving state; the processor is configured to activate the at least one selected power saving state; and the processor is further configured to, upon a determination that a time equal to the at least one value has elapsed, deactivate the at least one selected power saving state. the transmitter is configured to send a request message, wherein the request message includes a plurality of parameters associated with a plurality of power saving states supported by the WTRU; the receiver is configured to receive, from a mobility management entity, MME, an accept message comprising at least one selected parameter associated with at least one selected power saving state, wherein the at least one selected power saving state is from the plurality of power saving states supported by the WTRU, wherein the accept message further comprises at least one value associated with the at least one selected power saving state; the processor is configured to activate the at least one selected power saving state; and the processor is further configured to, upon a determination that a time equal to the at least one value has elapsed, deactivate the at least one selected power saving state.
An ion inlet assembly for connecting to a mass spectrometer housing comprising: a gas cone assembly having a gas cone orifice to allow ions to pass therethrough, wherein said gas cone assembly is connectable to a gas supply such that gas is arranged to flow, in use, towards said gas cone orifice; and a sampling limiting body in the form of a nickel disk having a sampling orifice , wherein said disk and said sampling orifice are made or formed by an electroforming process, wherein said sampling limiting body is mounted beneath the gas cone assembly to the mass spectrometer housing, and wherein said sampling limiting body is arranged to sit upon the mass spectrometer housing and to be removably held in position by the gas cone assembly. a gas cone assembly having a gas cone orifice to allow ions to pass therethrough, wherein said gas cone assembly is connectable to a gas supply such that gas is arranged to flow, in use, towards said gas cone orifice; and a sampling limiting body in the form of a nickel disk having a sampling orifice , wherein said disk and said sampling orifice are made or formed by an electroforming process, wherein said sampling limiting body is mounted beneath the gas cone assembly to the mass spectrometer housing, and wherein said sampling limiting body is arranged to sit upon the mass spectrometer housing and to be removably held in position by the gas cone assembly.
A method for manufacturing a backrest and/or a seat made of a textile covering or the like, such as a canvas for example, said backrest and/or said seat being mounted on a tubular frame of a chair or the like, said method including at least the following steps of: i) folding lateral edges of the textile covering and sewing said folded edges to form lateral sheaths by means of a lateral sewing line, ii) affixing at least three visual markers, called notches , to at least one of the ends of said sheaths , a first so-called central notch at the lateral edge of said sheaths and two peripheral notches on either side of the respective central notch , iii) folding the free ends of said sheaths by pressing each central notch between the two respective peripheral notches , said peripheral notches extending facing each other, iv) sewing the free ends of the sheaths at the folding area of the three notches by means of a transverse sewing line, v) turning the textile covering over, bringing out the corners of the textile covering. i) folding lateral edges of the textile covering and sewing said folded edges to form lateral sheaths by means of a lateral sewing line, ii) affixing at least three visual markers, called notches , to at least one of the ends of said sheaths , a first so-called central notch at the lateral edge of said sheaths and two peripheral notches on either side of the respective central notch , iii) folding the free ends of said sheaths by pressing each central notch between the two respective peripheral notches , said peripheral notches extending facing each other, iv) sewing the free ends of the sheaths at the folding area of the three notches by means of a transverse sewing line, v) turning the textile covering over, bringing out the corners of the textile covering.
A method for leaching at least one metal in battery powder comprising at least copper and one or more of cobalt and nickel to obtain a solution comprising one or more of cobalt ions and nickel ions, the method comprising a leaching process repeating multiple times, wherein the leaching process comprises: a first leaching step of leaching at least one metal in the battery powder in an acidic leaching solution, terminating the leaching before the copper begins to be dissolved, and removing a leached residue from a resulting leached solution to obtain the solution comprising one or more of cobalt ions and nickel ions; and a second leaching step of leaching at least one metal in the leached residue of the first leaching step in an acidic leaching solution, and terminating the leaching after the copper begins to be dissolved to obtain a leached solution, wherein the leached solution obtained in the second leaching step of the leaching process is used as an acidic leaching solution in a first leaching step of a leaching process following said leaching process, and wherein a leached residue is removed from a leached solution in a second leaching step of at least one leaching process. a first leaching step of leaching at least one metal in the battery powder in an acidic leaching solution, terminating the leaching before the copper begins to be dissolved, and removing a leached residue from a resulting leached solution to obtain the solution comprising one or more of cobalt ions and nickel ions; and a second leaching step of leaching at least one metal in the leached residue of the first leaching step in an acidic leaching solution, and terminating the leaching after the copper begins to be dissolved to obtain a leached solution, wherein the leached solution obtained in the second leaching step of the leaching process is used as an acidic leaching solution in a first leaching step of a leaching process following said leaching process, and wherein a leached residue is removed from a leached solution in a second leaching step of at least one leaching process.
A method of forming friction materials, comprising: depositing a first layer of material on a work surface of a three-dimensional printing system, wherein the first layer of material comprises a resin and at least one of a carbon fiber or a carbon fiber precursor material, and wherein depositing the first layer of material comprises depositing the resin on the work surface via at least one print head of the three-dimensional printing system; carbonizing the resin of the first layer of material to form a first layer of carbon-carbon composite comprising carbon fibers and a carbonized matrix material, wherein carbonizing the resin comprises carbonizing localized sections of the resin of the first layer of material using a carbonizer of the three-dimensional printer system to convert the resin to the carbonized matrix material; depositing a second layer of material on the first layer of carbon-carbon composite, the second layer of material comprising the resin and at least one of the carbon fiber or the carbon fiber precursor material, and wherein depositing the second layer of material comprises depositing the resin on the first layer of carbon-carbon composite via the at least one print head of the three-dimensional printing system; and carbonizing localized sections of the resin of the second layer of material using the carbonizer to convert the resin of the second layer to the carbonized matrix material. depositing a first layer of material on a work surface of a three-dimensional printing system, wherein the first layer of material comprises a resin and at least one of a carbon fiber or a carbon fiber precursor material, and wherein depositing the first layer of material comprises depositing the resin on the work surface via at least one print head of the three-dimensional printing system; carbonizing the resin of the first layer of material to form a first layer of carbon-carbon composite comprising carbon fibers and a carbonized matrix material, wherein carbonizing the resin comprises carbonizing localized sections of the resin of the first layer of material using a carbonizer of the three-dimensional printer system to convert the resin to the carbonized matrix material; depositing a second layer of material on the first layer of carbon-carbon composite, the second layer of material comprising the resin and at least one of the carbon fiber or the carbon fiber precursor material, and wherein depositing the second layer of material comprises depositing the resin on the first layer of carbon-carbon composite via the at least one print head of the three-dimensional printing system; and carbonizing localized sections of the resin of the second layer of material using the carbonizer to convert the resin of the second layer to the carbonized matrix material.
An actuation system for operating an engine thrust reverser comprising a thrust-reversing element movable between a stowed position and a deployed position, the actuation system comprising: at least one hydraulic actuator coupleable to the thrust-reversing element and, when coupled, configured to convey sufficient actuating force to move the thrust-reversing element between the stowed position and the deployed position; at least one hydraulic primary lock coupleable to the thrust-reversing element and, when coupled, configured to transition between an engaged state, where movement of the thrust-reversing element is inhibited, and a released state, where movement of the thrust-reversing element is uninhibited, in response to a first activation pressure; and a directional control unit fluidly coupled to the hydraulic actuator and the hydraulic primary locks ; characterised in that the directional control unit is configured to transition from a first stage to a second stage in response to a second activation pressure that is greater than the first activation pressure, and where a transition from the first stage to the second stage by the directional control unit , when the hydraulic actuator is coupled to the thrust-reversing element , causes the hydraulic actuator to convey an actuating force to deploy the thrust-reversing element . at least one hydraulic actuator coupleable to the thrust-reversing element and, when coupled, configured to convey sufficient actuating force to move the thrust-reversing element between the stowed position and the deployed position; at least one hydraulic primary lock coupleable to the thrust-reversing element and, when coupled, configured to transition between an engaged state, where movement of the thrust-reversing element is inhibited, and a released state, where movement of the thrust-reversing element is uninhibited, in response to a first activation pressure; and a directional control unit fluidly coupled to the hydraulic actuator and the hydraulic primary locks ; characterised in that the directional control unit is configured to transition from a first stage to a second stage in response to a second activation pressure that is greater than the first activation pressure, and where a transition from the first stage to the second stage by the directional control unit , when the hydraulic actuator is coupled to the thrust-reversing element , causes the hydraulic actuator to convey an actuating force to deploy the thrust-reversing element .
An out-of-synchronization determining method, comprising: receiving , by a control network element, interference metrics sent by N base stations, wherein the interference metrics comprise first interference and noise, second interference and noise, and third interference and noise, and the first interference and noise, the second interference and noise, and the third interference and noise are interference received in different uplink sub frame symbols; determining , based on the interference metrics, by the control network element, M first to-be-inspected base stations in the N base stations and/or neighboring stations of the N base stations; determining , by the control network element, P second to-be-inspected base stations, wherein the P second to-be-inspected base stations meet a detection condition that are selected from the M first to-be-inspected base stations, wherein the detection condition is that a characteristic sequence broadcast by the first to-be-inspected base station at a specified position in a radio frame is not received by any neighboring station at the specified position; and determining , by the control network element, an out-of-synchronization base station in the P second to-be-inspected base stations; wherein N and M are positive integers, P is an integer, and P is less than or equal to M. receiving , by a control network element, interference metrics sent by N base stations, wherein the interference metrics comprise first interference and noise, second interference and noise, and third interference and noise, and the first interference and noise, the second interference and noise, and the third interference and noise are interference received in different uplink sub frame symbols; determining , based on the interference metrics, by the control network element, M first to-be-inspected base stations in the N base stations and/or neighboring stations of the N base stations; determining , by the control network element, P second to-be-inspected base stations, wherein the P second to-be-inspected base stations meet a detection condition that are selected from the M first to-be-inspected base stations, wherein the detection condition is that a characteristic sequence broadcast by the first to-be-inspected base station at a specified position in a radio frame is not received by any neighboring station at the specified position; and determining , by the control network element, an out-of-synchronization base station in the P second to-be-inspected base stations; wherein N and M are positive integers, P is an integer, and P is less than or equal to M.
A positive electrode active material for a nonaqueous electrolyte secondary battery, the positive electrode active material comprising lithium composite oxide A containing W and Ni and W-free lithium composite oxide B containing Ni, wherein, regarding the lithium composite oxide A, the proportion of Ni relative to the total moles of metal elements except for lithium is 30 to 60 mol%, 50% particle size D50 in a cumulative particle size distribution on a volume basis is 2 to 6 μm, 10% particle size D10 in a cumulative particle size distribution on a volume basis is 1.0 μm or more, and 90% particle size D90 in a cumulative particle size distribution on a volume basis is 6.8 μm or less, wherein the cumulative particle size distribution on a volume basis is measured by using a laser diffraction/scattering particle size distribution analyzer under a wet condition, regarding the lithium composite oxide B, the proportion of Ni relative to the total moles of metal elements except for lithium is 50 to 95 mol%, 50% particle size D50 in a cumulative particle size distribution on a volume basis is 10 to 22 μm, 10% particle size D10 in a cumulative particle size distribution on a volume basis is 7.0 μm or more, and 90% particle size D90 in a cumulative particle size distribution on a volume basis is 22.5 μm or less, and a mass ratio of the lithium composite oxide B to the lithium composite oxide A is 1:1 to 5.7:1. wherein, regarding the lithium composite oxide A, the proportion of Ni relative to the total moles of metal elements except for lithium is 30 to 60 mol%, 50% particle size D50 in a cumulative particle size distribution on a volume basis is 2 to 6 μm, 10% particle size D10 in a cumulative particle size distribution on a volume basis is 1.0 μm or more, and 90% particle size D90 in a cumulative particle size distribution on a volume basis is 6.8 μm or less, wherein the cumulative particle size distribution on a volume basis is measured by using a laser diffraction/scattering particle size distribution analyzer under a wet condition, regarding the lithium composite oxide B, the proportion of Ni relative to the total moles of metal elements except for lithium is 50 to 95 mol%, 50% particle size D50 in a cumulative particle size distribution on a volume basis is 10 to 22 μm, 10% particle size D10 in a cumulative particle size distribution on a volume basis is 7.0 μm or more, and 90% particle size D90 in a cumulative particle size distribution on a volume basis is 22.5 μm or less, and a mass ratio of the lithium composite oxide B to the lithium composite oxide A is 1:1 to 5.7:1.
A wind turbine rotor blade comprising a flatback trailing edge , wherein the flatback trailing edge has at least one insert which has a flat outside and a curved inside , characterized in that a preform or an outer laminate is placed at the inside of the insert during production, wherein a core material and an inner laminate is placed on the preform or the outer laminate. a flatback trailing edge , wherein the flatback trailing edge has at least one insert which has a flat outside and a curved inside , characterized in that a preform or an outer laminate is placed at the inside of the insert during production, wherein a core material and an inner laminate is placed on the preform or the outer laminate.
A Flying Sensor comprising an unmanned aerial vehicle (UAV) and at least one profiler being mounted on the UAV , wherein the at least one profiler comprises • a base , • a scanning unit configured for providing Light Detection And Ranging (LiDAR) data, the scanning unit mounted on the base and comprising □ a shaft carrying a deflector , the shaft being mounted in the scanning unit and rotatable about a rotation axis (A), □ a first transmitter configured for transmitting a first transmission beam (T, T") via the deflector towards a setting, □ a first receiver configured for receiving a first reception beam (R, R") reflected from the setting via the deflector, and • an electric port configured for connecting the profiler to the UAV , said electric port comprising a data interface and a power interface, and wherein the UAV comprises • a visual sensor for providing visual data, the visual sensor comprising one or more cameras , • a pose sensor for providing pose data, the pose sensor comprising □ an Inertial Measuring Unit (IMU) and □ a Global Navigation Satellite System (GNSS) sensor or a Pseudo GNSS sensor, • a computer configured to generate a 3D point cloud (P) of the setting based on the LiDar data and a Simultaneous Localisation and Mapping (SLAM) algorithm using the visual data and the pose data. • a base , • a scanning unit configured for providing Light Detection And Ranging (LiDAR) data, the scanning unit mounted on the base and comprising □ a shaft carrying a deflector , the shaft being mounted in the scanning unit and rotatable about a rotation axis (A), □ a first transmitter configured for transmitting a first transmission beam (T, T") via the deflector towards a setting, □ a first receiver configured for receiving a first reception beam (R, R") reflected from the setting via the deflector, and □ a shaft carrying a deflector , the shaft being mounted in the scanning unit and rotatable about a rotation axis (A), □ a first transmitter configured for transmitting a first transmission beam (T, T") via the deflector towards a setting, □ a first receiver configured for receiving a first reception beam (R, R") reflected from the setting via the deflector, and • an electric port configured for connecting the profiler to the UAV , said electric port comprising a data interface and a power interface, and wherein the UAV comprises • a visual sensor for providing visual data, the visual sensor comprising one or more cameras , • a pose sensor for providing pose data, the pose sensor comprising □ an Inertial Measuring Unit (IMU) and □ a Global Navigation Satellite System (GNSS) sensor or a Pseudo GNSS sensor, □ an Inertial Measuring Unit (IMU) and □ a Global Navigation Satellite System (GNSS) sensor or a Pseudo GNSS sensor, • a computer configured to generate a 3D point cloud (P) of the setting based on the LiDar data and a Simultaneous Localisation and Mapping (SLAM) algorithm using the visual data and the pose data.
An aircraft including a wing unit comprising two wings each having a lateral wing box , each lateral wing box being extended toward the interior by a center wing box half having an interior end , and the two wings being attached to one another using attachment bolts linking the two interior ends of the two center wing box halves , characterized in that it includes at least a first and second fuselage frame , each of which has a lower part in frame wall form, the two frame walls being connected by an intermediate wall falling within a vertical midplane (P) of the aircraft, the intermediate wall being arranged between the two center wing box halves and crossed by the attachment bolts .
A process for preparing Larotrectinib sulfate containing less than 0.10% by weight S-Larotrectinib, comprising: (a) the unblocking reaction of Larotrectinib hydrochloride in dichloromethane, in the presence of bases selected from an alkaline or alkaline earth hydroxide; (b) the treatment of Larotrectinib obtained in step a) with sulfuric acid in methyl ethyl ketone, and water; (c) the filtration of Larotrectinib sulfate. (a) the unblocking reaction of Larotrectinib hydrochloride in dichloromethane, in the presence of bases selected from an alkaline or alkaline earth hydroxide; (b) the treatment of Larotrectinib obtained in step a) with sulfuric acid in methyl ethyl ketone, and water; (c) the filtration of Larotrectinib sulfate.
Chemical preservative comprising: - a) - phenoxyethanol, - b) - 2-butyl-1,2-benzisothiazolin-3-one and - c) - N,N-bis(3-aminopropyl) dodecylamine, in which the weight ratio compound b) on compound a) (b/a) is greater than or equal to 10 -3 and less than or equal to 10 -1 , and the weight ratio compound c) on compound a) (c/a) is greater than or equal to 5 x 10 -4 and less than or equal to 6 x 10 -2 . - a) - phenoxyethanol, - b) - 2-butyl-1,2-benzisothiazolin-3-one and - c) - N,N-bis(3-aminopropyl) dodecylamine,