mhurhangee/patent-ind-claim-en huggingface dataset:
A buttress applier cartridge configured to retain one or more buttress assemblies , wherein the buttress applier cartridge is further configured for use with an end effector of a surgical stapler to apply the one or more buttress assemblies to a select one or more of a first jaw and a second jaw of the end effector, wherein the first jaw of the end effector comprises an anvil and the second jaw of the end effector comprises a staple cartridge, wherein the buttress applier cartridge comprises: (a) a housing assembly having a proximal end and a distal end, wherein the housing assembly defines a channel extending longitudinally and configured to receive the end effector; (b) a platform , directly or indirectly connectable with the housing assembly, wherein the platform extends longitudinally within an area defined by the channel, wherein the platform is configured to support the one or more buttress assemblies thereon; (c) an opening that extends transversely from a first side of the platform to a second side of the platform opposite the first side of the platform, wherein the opening is configured to receive a curved tip of the end effector allowing at least a portion of the curved tip to extend from the first side of the platform to the second side of the platform; and characterised in that the buttress applier cartridge further comprises (d) an alignment feature , wherein the alignment feature is connectable with the platform and extends proximally therefrom, wherein the alignment feature is configured to contact a tissue stop of the end effector when the end effector is fully positioned within the channel defined by the housing assembly. (a) a housing assembly having a proximal end and a distal end, wherein the housing assembly defines a channel extending longitudinally and configured to receive the end effector; (b) a platform , directly or indirectly connectable with the housing assembly, wherein the platform extends longitudinally within an area defined by the channel, wherein the platform is configured to support the one or more buttress assemblies thereon; (c) an opening that extends transversely from a first side of the platform to a second side of the platform opposite the first side of the platform, wherein the opening is configured to receive a curved tip of the end effector allowing at least a portion of the curved tip to extend from the first side of the platform to the second side of the platform; and characterised in that the buttress applier cartridge further comprises (d) an alignment feature , wherein the alignment feature is connectable with the platform and extends proximally therefrom, wherein the alignment feature is configured to contact a tissue stop of the end effector when the end effector is fully positioned within the channel defined by the housing assembly.
On-load tap-changer for uninterrupted diverter switch operation between different winding taps of a tapped transformer , comprising: - a on-load tap-changer plate , - a selector , - a diverter switch , where: - the selector and the diverter switch are mounted on the on-load tap-changer plate , - the diverter switch comprises a vacuum interrupter and a bridge switch , characterized in that - the diverter switch comprises a transition resistor - the selector comprises a first selector arm (5.1), a second selector arm (5.2) and a change-over selector , - the first selector arm (5.1) is mounted on the first side of the on-load tap-changer plate and the second selector arm (5.2) and the change-over selector are mounted on the second, opposite side of the on-load tap-changer plate . - a on-load tap-changer plate , - a selector , - a diverter switch , - the selector and the diverter switch are mounted on the on-load tap-changer plate , - the diverter switch comprises a vacuum interrupter and a bridge switch , characterized in that - the diverter switch comprises a transition resistor - the selector comprises a first selector arm (5.1), a second selector arm (5.2) and a change-over selector , - the first selector arm (5.1) is mounted on the first side of the on-load tap-changer plate and the second selector arm (5.2) and the change-over selector are mounted on the second, opposite side of the on-load tap-changer plate .
Method for compressing a neural network , wherein fleet members of a vehicle fleet execute the neural network locally, and in each case determine, during at least one inference phase, a selection of elements of the neural network that are intended to be pruned, wherein the fleet members transmit the selection determined in each case to a central server , wherein the central server merges the selections determined in each case and generates a merged selection , and wherein the central server prunes the neural network on the basis of the merged selection , wherein the pruned neural network is subsequently transmitted to at least one fleet member , wherein the at least one fleet member receives the pruned neural network from the central server and replaces the neural network stored locally in a storage device with the received pruned neural network . wherein fleet members of a vehicle fleet execute the neural network locally, and in each case determine, during at least one inference phase, a selection of elements of the neural network that are intended to be pruned, wherein the fleet members transmit the selection determined in each case to a central server , wherein the central server merges the selections determined in each case and generates a merged selection , and wherein the central server prunes the neural network on the basis of the merged selection , wherein the pruned neural network is subsequently transmitted to at least one fleet member , wherein the at least one fleet member receives the pruned neural network from the central server and replaces the neural network stored locally in a storage device with the received pruned neural network .
A liquid ejection head , comprising an ejection hole surface at which a plurality of nozzles , being through holes formed in a nozzle plate , ejecting liquid open, wherein the ejection hole surface comprises a nozzle arrangement region in which the plurality of nozzles are arranged, each nozzle comprises an inversely tapered part where a cross-sectional area increases toward the ejection hole surface at least on the ejection hole surface side, a first nozzle (8-1) of the nozzles is arranged at a center part of a predetermined direction of the nozzle arrangement region , while second nozzles (8-2) of the nozzles are arranged at the end parts at the two sides in the predetermined direction, when viewed from the ejection hole surface side, the inversely tapered part looks like a ring-shaped region on the periphery of a circular portion penetrating through the nozzle plate , with a width of the ring-shaped region being defined as the width T, the width T of the first nozzle (8-1) is larger than the widths T of the second nozzles (8-2), and in the nozzle arrangement region , the ejection hole surface comprises a shape that the center part in the predetermined direction projects with respect to the end parts on the two sides in the predetermined direction.
A gas turbine casing made of composite material comprising reinforcement densified by a matrix, said casing being in the form of a body of revolution and comprising at least one stiffener portion extending at a radius greater than the radius of upstream and downstream portions of the casing that are adjacent to said stiffener portion so as to form an annular recess in the inside surface of the casing , characterized in that the annular recess is empty or is filled in with an acoustic attenuation material or structure .
A gas turbine engine comprising: a compressor section having a low pressure compressor and a high pressure compressor , and said high pressure compressor having a downstream most location ; and a cooling air system including a tap from a location upstream of said downstream most location , said tap passing air to a boost compressor and a heat exchanger , said boost compressor passing the air to a location to be cooled, and said boost compressor being driven by a shaft which drives said lower pressure compressor , characterised in that : said heat exchanger includes a first heat exchanger positioned between said tap and said boost compressor ; and said boost compressor is located in a tail cone of said engine . a compressor section having a low pressure compressor and a high pressure compressor , and said high pressure compressor having a downstream most location ; and a cooling air system including a tap from a location upstream of said downstream most location , said tap passing air to a boost compressor and a heat exchanger , said boost compressor passing the air to a location to be cooled, and said boost compressor being driven by a shaft which drives said lower pressure compressor , said heat exchanger includes a first heat exchanger positioned between said tap and said boost compressor ; and said boost compressor is located in a tail cone of said engine .
A user equipment comprising: receiving circuitry configured to: receive, when the user equipment is in Radio Resource Control connected mode/state, and from a base station apparatus , a radio resource control signaling including an indication, the indication being used for identifying a synchronization signal block type of a synchronization signal block in which a primary synchronization signal, a secondary synchronization signal, a physical broadcast channel, and a reference signal for decoding the physical broadcast channel are transmitted, the synchronization signal block type being indicated by the indication, the synchronization signal block consisting of a constant number of OFDM symbols; and receive, from the base station apparatus , the synchronization signal block in which the primary synchronization signal, the secondary synchronization signal, the physical broadcast channel, and the reference signal for decoding the physical broadcast channel are transmitted; and processing circuitry configured to determine the synchronization signal block type based on the indication, wherein the processing circuitry is configured to: perform a time and frequency synchronization based on the primary synchronization signal and the secondary synchronization signal; and obtain System Frame Number information provided by the physical broadcast channel. receive, when the user equipment is in Radio Resource Control connected mode/state, and from a base station apparatus , a radio resource control signaling including an indication, the indication being used for identifying a synchronization signal block type of a synchronization signal block in which a primary synchronization signal, a secondary synchronization signal, a physical broadcast channel, and a reference signal for decoding the physical broadcast channel are transmitted, the synchronization signal block type being indicated by the indication, the synchronization signal block consisting of a constant number of OFDM symbols; and receive, from the base station apparatus , the synchronization signal block in which the primary synchronization signal, the secondary synchronization signal, the physical broadcast channel, and the reference signal for decoding the physical broadcast channel are transmitted; and processing circuitry configured to determine the synchronization signal block type based on the indication, wherein the processing circuitry is configured to: perform a time and frequency synchronization based on the primary synchronization signal and the secondary synchronization signal; and obtain System Frame Number information provided by the physical broadcast channel. perform a time and frequency synchronization based on the primary synchronization signal and the secondary synchronization signal; and obtain System Frame Number information provided by the physical broadcast channel.
A process for manufacturing a composite material part comprising a particulate reinforcement densified by a ceramic matrix, the process comprising the following steps: - formation of a blank (S4) of the part to be manufactured by shaping a mixture comprising a binder, first ceramic or carbon particles intended to form the particulate reinforcement of the part and second ceramic or carbon particles distinct from the first particles, - removal or pyrolysis of the binder (S5) present in the blank to obtain a porous preform of the part, and - infiltration of the porosity of the preform (S6) by a molten composition comprising a metal in order to obtain the part, characterized in that it further comprises, before the infiltration step, a step of hot isostatic compression of the porous preform obtained after removal or pyrolysis of the binder. - formation of a blank (S4) of the part to be manufactured by shaping a mixture comprising a binder, first ceramic or carbon particles intended to form the particulate reinforcement of the part and second ceramic or carbon particles distinct from the first particles, - removal or pyrolysis of the binder (S5) present in the blank to obtain a porous preform of the part, and - infiltration of the porosity of the preform (S6) by a molten composition comprising a metal in order to obtain the part,
A heat exchanger, for two-phase refrigerant, the heat exchanger comprising: a plurality of parallel stacked plates defining at least one flow passage there between; a manifold arranged adjacent the plurality of parallel plates, the manifold having a generally hollow interior; an opening disposed between adjacent stacked plates, the opening being configured to fluidly couple the hollow interior of the manifold and the at least one flow passage; and a distributor assembly including an insert disposed at least partially within the hollow interior of the manifold; characterised in that the insert including distribution flow paths comprising a plurality of circumferentially spaced axial flow channels and a plurality of radial connecting channels arranged in fluid communication with the axial flow channels, the radial flow channels being fluidly coupled to the at least one flow passage via the opening; wherein the distribution flow paths are sized to maintain the velocity of the two-phase refrigerant so as to limit separation a plurality of parallel stacked plates defining at least one flow passage there between; a manifold arranged adjacent the plurality of parallel plates, the manifold having a generally hollow interior; an opening disposed between adjacent stacked plates, the opening being configured to fluidly couple the hollow interior of the manifold and the at least one flow passage; and a distributor assembly including an insert disposed at least partially within the hollow interior of the manifold; characterised in that the insert including distribution flow paths comprising a plurality of circumferentially spaced axial flow channels and a plurality of radial connecting channels arranged in fluid communication with the axial flow channels, the radial flow channels being fluidly coupled to the at least one flow passage via the opening; wherein the distribution flow paths are sized to maintain the velocity of the two-phase refrigerant so as to limit separation
An apparatus for use with a memory , comprising: a memory controller having input power mode selection logic configured to select a level of input power to the memory as a function of noise tolerance level of a workload wherein the workload includes a first workload having a first level of noise tolerance and a second workload having a second level of noise tolerance, wherein the second level of noise tolerance of the second workload is lower than that of the first level of noise tolerance of the first workload, and wherein a level of the power input to the memory associated with second workload is higher than a level of the power input to the memory associated with the first workload the memory controller further having a multi-level power supply configured to provide the selected level of power to the memory, wherein the first workload is a first layer of a deep learning neural network and the second workload is a second, subsequent layer of the deep learning neural network. a memory controller having input power mode selection logic configured to select a level of input power to the memory as a function of noise tolerance level of a workload wherein the workload includes a first workload having a first level of noise tolerance and a second workload having a second level of noise tolerance, wherein the second level of noise tolerance of the second workload is lower than that of the first level of noise tolerance of the first workload, and wherein a level of the power input to the memory associated with second workload is higher than a level of the power input to the memory associated with the first workload the memory controller further having a multi-level power supply configured to provide the selected level of power to the memory, wherein the first workload is a first layer of a deep learning neural network and the second workload is a second, subsequent layer of the deep learning neural network.
A mixture comprising: - gold particles, and - graphene particles or a derivative thereof or mixtures thereof, and a linker binding said gold particles to said graphene particles or derivative thereof or mixtures thereof, wherein said linker is alpha lipoic acid, for use in the treatment and/or prevention of urogenital tract infections, wherein said derivative is graphene oxide. - gold particles, and - graphene particles or a derivative thereof or mixtures thereof, and a linker binding said gold particles to said graphene particles or derivative thereof or mixtures thereof, wherein said linker is alpha lipoic acid, for use in the treatment and/or prevention of urogenital tract infections, wherein said derivative is graphene oxide.
A method, comprising: receiving a basis variable set , wherein basis variables are sensor measurements or determined from sensor measurements, and wherein the basis variable set includes an engine speed , a commanded fueling value , and an in-cylinder oxygen concentration value ; determining a reference value set having a plurality of reference values based on the basis variable set and a fuel controller specification set , wherein the fuel controller specification set defines acceptable types and range of inputs for a fuel controller , such that the reference value set is a set of target values for meeting a performance requirement of an engine system and includes a start-of-injection command ; and providing the reference value set to a fuel control commander . receiving a basis variable set , wherein basis variables are sensor measurements or determined from sensor measurements, and wherein the basis variable set includes an engine speed , a commanded fueling value , and an in-cylinder oxygen concentration value ; determining a reference value set having a plurality of reference values based on the basis variable set and a fuel controller specification set , wherein the fuel controller specification set defines acceptable types and range of inputs for a fuel controller , such that the reference value set is a set of target values for meeting a performance requirement of an engine system and includes a start-of-injection command ; and providing the reference value set to a fuel control commander .
A method for monitoring a pitch control system for a rotor blade of a wind turbine , the method comprising: - receiving a blade pitch signal representative of a pitch position of the rotor blade , - determine a pitch deviation, based on the blade pitch signal and a blade pitch reference , characterized in that - when the determined pitch deviation exceeds a first pitch deviation threshold, increasing a pitch deviation variable as a running counter value by an amount that depends on - the determined pitch deviation, - the first pitch deviation threshold, and - a duration of a time period during which the determined pitch deviation has been exceeding the first pitch deviation threshold, - provide an error signal when the increased pitch deviation variable exceeds a pitch deviation variable threshold. - receiving a blade pitch signal representative of a pitch position of the rotor blade , - determine a pitch deviation, based on the blade pitch signal and a blade pitch reference , characterized in that - when the determined pitch deviation exceeds a first pitch deviation threshold, increasing a pitch deviation variable as a running counter value by an amount that depends on - the determined pitch deviation, - the first pitch deviation threshold, and - a duration of a time period during which the determined pitch deviation has been exceeding the first pitch deviation threshold, - the determined pitch deviation, - the first pitch deviation threshold, and - a duration of a time period during which the determined pitch deviation has been exceeding the first pitch deviation threshold, - provide an error signal when the increased pitch deviation variable exceeds a pitch deviation variable threshold.
The bilayer tablet comprising; a) a first layer containing a PDE 5 inhibitor or mixtures of PDE 5 inhibitors or their pharmaceutically acceptable salts thereof and a pharmaceutically acceptable carrier or carriers and b) a second layer containing dapoxetine or its pharmaceutically acceptable salt thereof and a pharmaceutically acceptable carrier or carriers wherein the first layer is an immediate release formulation and the second layer is a modified release formulation to provide dapoxetine in a release profile to have efficient dapoxetine blood level concentration for a longer period of time than without modification.
Method for controlling a wind turbine which has an aerodynamic rotor having a variable radius (R), wherein the aerodynamic rotor has at least one rotor blade , whose length (L) can be adjusted, having the steps of: - detecting a speed (n) and/or a torque (M) of the aerodynamic rotor , - detecting an air density in the environment of the wind turbine , - controlling the length (L) of the at least one rotor blade in accordance with the speed (n) and/or the torque (M) of the aerodynamic rotor , the detected air density in the environment of the wind turbine and a predetermined maximum permissible sound pressure level, and - reducing the length (L) of the at least one rotor blade when the speed (n) is above a second threshold value, characterised in that the second threshold value of the speed (n) is set to be inversely proportional to the air density. - detecting a speed (n) and/or a torque (M) of the aerodynamic rotor , - detecting an air density in the environment of the wind turbine , - controlling the length (L) of the at least one rotor blade in accordance with the speed (n) and/or the torque (M) of the aerodynamic rotor , the detected air density in the environment of the wind turbine and a predetermined maximum permissible sound pressure level, and - reducing the length (L) of the at least one rotor blade when the speed (n) is above a second threshold value, characterised in that the second threshold value of the speed (n) is set to be inversely proportional to the air density.