mhurhangee/ep-ind-claims huggingface dataset:
A channel state information reference signal, CSI-RS, mapping method for antenna ports that include K antenna port groups each including no more than N antenna ports, the mapping method performed by an apparatus and comprising: grouping physical resource blocks, PRBs, in a wireless communication system bandwidth in the frequency domain, thereby obtaining a plurality of PRB groups each including M PRBs, where M is an integer multiple of K; in each PRB of one PRB group, determining positions at which a pilot of each antenna port is mapped to resource elements, REs, in the PRB according to an antenna port index and an index of the PRB in the PRB group or the whole system bandwidth, wherein all antenna ports within a same antenna port group are mapped to N REs in the PRB, where said antenna ports are code multiplexed, said N REs forming one of K selected and non-overlapping N-port pilot patterns in each PRB, wherein each antenna port group is mapped to more than two N-port pilot patterns in the PRB group; and wherein in a PRB group, the sum across the PRBs of the PRB group of the quantity of the N-port pilot patterns contained in the Orthogonal Frequency Division Multiplexing, OFDM, symbols where each particular antenna port group is located is the same across the antenna port groups, thereby obtaining pilot mapping in the PRB group; and reusing the pilot mapping in the PRB group to each PRB group in the system bandwidth; wherein in each PRB, there are OFDM symbols mapped with different N-port pilot patterns, and such OFDM symbols include different numbers of N-port pilot patterns. grouping physical resource blocks, PRBs, in a wireless communication system bandwidth in the frequency domain, thereby obtaining a plurality of PRB groups each including M PRBs, where M is an integer multiple of K; in each PRB of one PRB group, determining positions at which a pilot of each antenna port is mapped to resource elements, REs, in the PRB according to an antenna port index and an index of the PRB in the PRB group or the whole system bandwidth, wherein all antenna ports within a same antenna port group are mapped to N REs in the PRB, where said antenna ports are code multiplexed, said N REs forming one of K selected and non-overlapping N-port pilot patterns in each PRB, wherein each antenna port group is mapped to more than two N-port pilot patterns in the PRB group; and wherein in a PRB group, the sum across the PRBs of the PRB group of the quantity of the N-port pilot patterns contained in the Orthogonal Frequency Division Multiplexing, OFDM, symbols where each particular antenna port group is located is the same across the antenna port groups, thereby obtaining pilot mapping in the PRB group; and reusing the pilot mapping in the PRB group to each PRB group in the system bandwidth; wherein in each PRB, there are OFDM symbols mapped with different N-port pilot patterns, and such OFDM symbols include different numbers of N-port pilot patterns.
A composite build material for use in a three-dimensional printing system comprising: a carrier ink comprising a curable material; pigment particles dispersed in the carrier ink, the pigment particles comprising mica; and a colorant, the colorant differing from the pigment particles. a carrier ink comprising a curable material; pigment particles dispersed in the carrier ink, the pigment particles comprising mica; and a colorant, the colorant differing from the pigment particles.
A method for navigating two or more users to a meeting location, the method comprising: receiving, at one or more processors, a request for a first user to meet a second user at a meeting location including a first location of the first user and a second location of the second user, the first and second locations within a geographic area; retrieving, by the one or more processors from a database, a plurality of visual landmarks corresponding to physical objects within the geographic area; selecting, by the one or more processors, a shared visual landmark from the plurality of visual landmarks for directing the first user and the second user to the meeting location within the geographic area, the shared visual landmark being selected based on visibility from both the first location and the second location; and providing (810, 812), by the one or more processors, to the first user and the second user, directions to the meeting location referencing the shared visual landmark. receiving, at one or more processors, a request for a first user to meet a second user at a meeting location including a first location of the first user and a second location of the second user, the first and second locations within a geographic area; retrieving, by the one or more processors from a database, a plurality of visual landmarks corresponding to physical objects within the geographic area; selecting, by the one or more processors, a shared visual landmark from the plurality of visual landmarks for directing the first user and the second user to the meeting location within the geographic area, the shared visual landmark being selected based on visibility from both the first location and the second location; and providing (810, 812), by the one or more processors, to the first user and the second user, directions to the meeting location referencing the shared visual landmark.
Process for producing a masterbatch comprising the following constituents: 70% to 25% by weight of polycarbonate, 30% to 70% by weight of reinforcing filler, 0% to 5% by weight of other masterbatch constituents, the sum of the constituents being 100% by weight, and wherein the masterbatch is compounded in a continuous single-shaft kneader, wherein the reinforcing filler is selected from one or more members of the group made up of titanium dioxide (TiO 2), talc (Mg 3 Si 4 O 10 2), dolomite CaMg[CO 3] 2, kaolinite Al 4 [ 8 |Si 4 O 10], and wollastonite Ca 3 [Si 3 O 9], preferably selected from one or more members of the group made up of titanium dioxide (TiO 2) and talc (Mg 3 Si 4 O 10 2), and wherein the proportion of polyester in the masterbatch is not more than 0.9% by weight. 70% to 25% by weight of polycarbonate, 30% to 70% by weight of reinforcing filler, 0% to 5% by weight of other masterbatch constituents, the sum of the constituents being 100% by weight, and wherein the masterbatch is compounded in a continuous single-shaft kneader, wherein the reinforcing filler is selected from one or more members of the group made up of titanium dioxide (TiO 2), talc (Mg 3 Si 4 O 10 2), dolomite CaMg[CO 3] 2, kaolinite Al 4 [ 8 |Si 4 O 10], and wollastonite Ca 3 [Si 3 O 9], preferably selected from one or more members of the group made up of titanium dioxide (TiO 2) and talc (Mg 3 Si 4 O 10 2), and wherein the proportion of polyester in the masterbatch is not more than 0.9% by weight.
A composition comprising a herpes simplex virus that replicates in dividing cells and exhibits attenuated replication in non-dividing cells, and that comprises one or more nucleotide sequences encoding GM-CSF, wherein the GM-CSF is expressed, and a pharmaceutically acceptable vehicle for the virus for use in a method for treating a metastasis of melanoma cells by eliciting a systemic antitumor immune response in a patient who presents with multiple metastatic melanoma cells, wherein melanoma cells of the patient are inoculated with the composition, and wherein said composition induces an immune response that is specific for the melanoma cells and that kills cells of the inoculated melanoma cells and of non-inoculated melanoma cells.
An optical component comprising: an optical fiber having a core and a clad; a light guide holding member attached to the exit end of the optical fiber and having an end face at the exit end of the optical fiber; a wavelength conversion member that contains a fluorescent substance arranged for generating light from light exiting the exit end of the optical fiber; and a reflection means provided between the end face of the light guide holding member and the wavelength conversion member, the reflection means covering the end surface of the light guide holding member, at the exit end of the optical fiber, for reflecting light reflected by or generated by the wavelength conversion member, the optical component being characterised in that the reflection means also covers the end face of the optical fiber, other than a core portion of the end face, at the exit end of the optical fiber. an optical fiber having a core and a clad; a light guide holding member attached to the exit end of the optical fiber and having an end face at the exit end of the optical fiber; a wavelength conversion member that contains a fluorescent substance arranged for generating light from light exiting the exit end of the optical fiber; and a reflection means provided between the end face of the light guide holding member and the wavelength conversion member, the reflection means covering the end surface of the light guide holding member, at the exit end of the optical fiber, for reflecting light reflected by or generated by the wavelength conversion member, the optical component being characterised in that the reflection means also covers the end face of the optical fiber, other than a core portion of the end face, at the exit end of the optical fiber.
Supersonic air inlet of an aircraft propulsion assembly, said aircraft propulsion assembly extending longitudinally along an axis oriented from upstream to downstream and comprising a turbine engine configured to enable propulsion of the aircraft at supersonic speeds from the acceleration of a subsonic air flow circulating from upstream to downstream in the turbine engine, said supersonic air inlet comprising: • a pipe with a longitudinal axis comprising an inner wall configured to guide the air flow into the turbine engine and an outer wall connected upstream by an air inlet lip and together delimiting an annular cavity, • a speed reducer fixedly mounted inside the pipe along the longitudinal axis and comprising a conical external wall with an upstream tapered edge so as to generate a shock wave reducing the supersonic speed of the air flow entering the pipe to a subsonic speed, and • at least one support arm connecting the speed reducer to the pipe, said support arm comprising an upstream external wall and a downstream external wall together delimiting a cavity extending from the inner wall of the pipe to the speed reducer along an axis directed inwards, • a supersonic air inlet characterized in that it comprises at least one de-icing device comprising: • an internal wall mounted in the cavity of the support arm opposite the upstream external wall so as to delimit together a calibrated de-icing space, • at least one member for supplying the de-icing space with a de-icing air flow (F D), and • at least one member for discharging the de-icing air flow (F D) from the de-icing space. • a pipe with a longitudinal axis comprising an inner wall configured to guide the air flow into the turbine engine and an outer wall connected upstream by an air inlet lip and together delimiting an annular cavity, • a speed reducer fixedly mounted inside the pipe along the longitudinal axis and comprising a conical external wall with an upstream tapered edge so as to generate a shock wave reducing the supersonic speed of the air flow entering the pipe to a subsonic speed, and • at least one support arm connecting the speed reducer to the pipe, said support arm comprising an upstream external wall and a downstream external wall together delimiting a cavity extending from the inner wall of the pipe to the speed reducer along an axis directed inwards, • a supersonic air inlet characterized in that it comprises at least one de-icing device comprising: • an internal wall mounted in the cavity of the support arm opposite the upstream external wall so as to delimit together a calibrated de-icing space, • at least one member for supplying the de-icing space with a de-icing air flow (F D), and • at least one member for discharging the de-icing air flow (F D) from the de-icing space. • an internal wall mounted in the cavity of the support arm opposite the upstream external wall so as to delimit together a calibrated de-icing space, • at least one member for supplying the de-icing space with a de-icing air flow (F D), and • at least one member for discharging the de-icing air flow (F D) from the de-icing space.
A data transmission method, applied to a terminal which establishes a communication connection with a correspondent node through a first link provided by a cellular network and a second link provided by a Wireless Local Area Network, WLAN, respectively, and the method comprising: acquiring relevant information of the WLAN which is accessed by the terminal, the relevant information of the WLAN being used to indicate a data distribution capability of the WLAN (201, 301); acquiring a current amount of data in an uplink buffer that is configured to store the uplink data; determining the amount of the data to be transmitted to the correspondent node by means of the second link in accordance with the relevant information of the WLAN and the current amount of data; sending a Buffer Status Report, BSR, to a base station in the cellular network, wherein the BSR comprises a difference value between the current amount of data and the amount of the data to be transmitted by means of the second link; and transmitting, according to the amount of the data to be transmitted by means of the second link, the uplink data to the correspondent node by means of the second link. acquiring relevant information of the WLAN which is accessed by the terminal, the relevant information of the WLAN being used to indicate a data distribution capability of the WLAN (201, 301); acquiring a current amount of data in an uplink buffer that is configured to store the uplink data; determining the amount of the data to be transmitted to the correspondent node by means of the second link in accordance with the relevant information of the WLAN and the current amount of data; sending a Buffer Status Report, BSR, to a base station in the cellular network, wherein the BSR comprises a difference value between the current amount of data and the amount of the data to be transmitted by means of the second link; and
A patient monitor adapted to receive an intravenous line pole comprising: a channel, positioned on a rear surface of the monitor and configured to receive an intravenous line pole; and characterized by a handle for carrying said monitor which, upon closing, creates a friction fit between an elastomer layer positioned on the handle and the intravenous line pole, wherein the friction fit, in combination with the intravenous line pole positioned within the channel, is capable of maintaining the monitor elevated off the ground. a channel, positioned on a rear surface of the monitor and configured to receive an intravenous line pole; and characterized by a handle for carrying said monitor which, upon closing, creates a friction fit between an elastomer layer positioned on the handle and the intravenous line pole, wherein the friction fit, in combination with the intravenous line pole positioned within the channel, is capable of maintaining the monitor elevated off the ground.
A vane airfoil comprising: an airfoil section including an outer wall that defines an internal cavity, the airfoil section including a third zone, the third zone being defined in a third radial extent of the vane airfoil; and an insert (212; 312; 412) situated in the internal cavity, the insert including a first zone defined in a radial extent of the insert, the first zone including a first plurality of cooling holes, and a second zone defined in a radial extent of the insert, the second zone including a second plurality of cooling holes, wherein the first plurality of cooling holes provide a first cooling density and the second plurality of cooling holes provide a second cooling density, and wherein the first cooling density is different from the second cooling density and the first plurality of cooling holes and the second plurality of cooling holes are configured to jet air towards the outer wall of the airfoil section, the insert (212; 312; 412) including a third zone defined in a radial extent that is aligned with the third zone of the airfoil section, wherein the third zone of the insert includes a third plurality of cooling holes that provide a third cooling density, the third cooling density being different from at least one of the first and second cooling densities, characterised by: the first cooling density being higher than the second cooling density and the third cooling density; the first zone being between the second and third zones along the radial extent. an airfoil section including an outer wall that defines an internal cavity, the airfoil section including a third zone, the third zone being defined in a third radial extent of the vane airfoil; and an insert (212; 312; 412) situated in the internal cavity, the insert including a first zone defined in a radial extent of the insert, the first zone including a first plurality of cooling holes, and a second zone defined in a radial extent of the insert, the second zone including a second plurality of cooling holes, wherein the first plurality of cooling holes provide a first cooling density and the second plurality of cooling holes provide a second cooling density, and wherein the first cooling density is different from the second cooling density and the first plurality of cooling holes and the second plurality of cooling holes are configured to jet air towards the outer wall of the airfoil section, the insert (212; 312; 412) including a third zone defined in a radial extent that is aligned with the third zone of the airfoil section, wherein the third zone of the insert includes a third plurality of cooling holes that provide a third cooling density, the third cooling density being different from at least one of the first and second cooling densities, characterised by: the first cooling density being higher than the second cooling density and the third cooling density; the first zone being between the second and third zones along the radial extent. the first cooling density being higher than the second cooling density and the third cooling density; the first zone being between the second and third zones along the radial extent.
A method of identifying a subject as suitable for treatment with an alternative glucocerebrosidase enzyme, the method comprising: determining if a neutralizing antibody to a glucocerebrosidase enzyme is present in a sample from a subject that is currently taking or has previously received the glucocerebrosidase enzyme to obtain a measured value of the antibody; comparing the measured value to a standard, wherein if the measured value is greater than the standard, the subject is identified as having tested positive for the production of the antibodies; and selecting a subject for the alternative glucocerebrosidase enzyme on the basis that the subject has tested positive for the production of the antibodies. determining if a neutralizing antibody to a glucocerebrosidase enzyme is present in a sample from a subject that is currently taking or has previously received the glucocerebrosidase enzyme to obtain a measured value of the antibody; comparing the measured value to a standard, wherein if the measured value is greater than the standard, the subject is identified as having tested positive for the production of the antibodies; and selecting a subject for the alternative glucocerebrosidase enzyme on the basis that the subject has tested positive for the production of the antibodies.
A method for monitoring a heap of material, the method comprising: defining, in a video stream of a scene captured by a thermal camera, a region of interest covering the heap of material; determining, from a video frame of the video stream, a reference spatial property of the heap of material by, from pixel data within the region of interest, measuring a spatial property of the heap of material, wherein the spatial property is a measure of a spatial frequency of thermal image data constituting the thermal video stream, and setting the measured spatial property as the reference spatial property; setting a spatial property threshold in relation to the reference spatial property; adjusting the region of interest such that regions in the video stream exhibiting a sample spatial property above the spatial property threshold are included by the region of interest and such that regions in the video stream exhibiting a sample spatial property below the spatial property threshold are excluded by adjusting the region of interest, wherein the adjusting is performed on pixel data of thermal image data of image frames being subsequent to the image frame used for setting the reference spatial property; monitoring, over time and within the region of interest, a temperature measure in the video stream; upon the temperature measure exceeds a predetermined threshold generating an alarm event. defining, in a video stream of a scene captured by a thermal camera, a region of interest covering the heap of material; determining, from a video frame of the video stream, a reference spatial property of the heap of material by, from pixel data within the region of interest, measuring a spatial property of the heap of material, wherein the spatial property is a measure of a spatial frequency of thermal image data constituting the thermal video stream, and setting the measured spatial property as the reference spatial property; setting a spatial property threshold in relation to the reference spatial property; adjusting the region of interest such that regions in the video stream exhibiting a sample spatial property above the spatial property threshold are included by the region of interest and such that regions in the video stream exhibiting a sample spatial property below the spatial property threshold are excluded by adjusting the region of interest, wherein the adjusting is performed on pixel data of thermal image data of image frames being subsequent to the image frame used for setting the reference spatial property; monitoring, over time and within the region of interest, a temperature measure in the video stream; upon the temperature measure exceeds a predetermined threshold generating an alarm event.