mhurhangee/patent-ind-claim-en huggingface dataset:
A radio frequency, RF, device comprising a first duplexer , a second duplexer , and a processor , the processor being configured to include a channel switch, the first duplexer being configured for transceiving a first band signal in a first band and being connected to a first transmit port (TX1) and a first receive port (RX1) of the processor, the second duplexer being configured for transceiving a second band signal in a second band and being connected to a second transmit port (TX2) and a second receive port (RX2) of the processor , the processor being configured to select a corresponding one of the duplexers to transceive a signal by the channel switch according to a frequency band of the signal; characterised in that the first band and the second band are configured such that: the first band and the second band belong to a Band 28, the Band 28 comprising an uplink band having a starting frequency point of 703MHz and an ending frequency point of 748MHz and a downlink band having a starting frequency point of 758MHz and an ending frequency point of 803MHz; an overlapping band, consisting of an overlap between Band 28 and a DVT band, belongs to the first band, the overlapping band spanning from 703MHz to 710MHz; frequency test points having the values of 725.5MHz and 723MHz belong to the second band; the first band comprises a first uplink band and a first downlink band, wherein a starting frequency point of the first uplink band is equal to the starting frequency point of the uplink band of the Band 28 and an end frequency point of the first uplink band is less than the frequency test points; and the second band comprises a second uplink band and a second downlink band, wherein a starting frequency point of the second uplink band is greater than the end frequency point of the first uplink band a frequency point unit of 0.1 MHz, and an end frequency point of the second uplink band is equal to the end frequency point of the uplink band of the Band 28. the first band and the second band belong to a Band 28, the Band 28 comprising an uplink band having a starting frequency point of 703MHz and an ending frequency point of 748MHz and a downlink band having a starting frequency point of 758MHz and an ending frequency point of 803MHz; an overlapping band, consisting of an overlap between Band 28 and a DVT band, belongs to the first band, the overlapping band spanning from 703MHz to 710MHz; frequency test points having the values of 725.5MHz and 723MHz belong to the second band; the first band comprises a first uplink band and a first downlink band, wherein a starting frequency point of the first uplink band is equal to the starting frequency point of the uplink band of the Band 28 and an end frequency point of the first uplink band is less than the frequency test points; and the second band comprises a second uplink band and a second downlink band, wherein a starting frequency point of the second uplink band is greater than the end frequency point of the first uplink band a frequency point unit of 0.1 MHz, and an end frequency point of the second uplink band is equal to the end frequency point of the uplink band of the Band 28.
Vehicle comprising a passenger compartment limited by walls interposed between the passenger compartment and an outside environment, wherein at least one of said walls is provided with: - an inside thermal barrier having a porous matrix and containing at least one PCM material - phase-change material - capable of adopting liquid and solid states respectively, having a temperature of change of state between liquid and solid comprised between 15°C and 40°C and preferably between 17°C and 35°C, and - at least one thermally insulating element , characterised in that : - from the inside where the passenger compartment is situated, towards the outside , the vehicle comprises the inside thermal barrier and then said at least one thermally insulating element , and - the vehicle furthermore comprises means for conditioning air in the passenger compartment, suitable for heating, cooling and propelling air, in order to place in the latter air derived at least in part from said air conditioning means in thermal exchange with said at least one PCM material and the porous matrix of the inside thermal barrier has open pores that vary according to the liquid or solid state of the PCM material, thus varying the thermal conductivity. - an inside thermal barrier having a porous matrix and containing at least one PCM material - phase-change material - capable of adopting liquid and solid states respectively, having a temperature of change of state between liquid and solid comprised between 15°C and 40°C and preferably between 17°C and 35°C, and - at least one thermally insulating element , - from the inside where the passenger compartment is situated, towards the outside , the vehicle comprises the inside thermal barrier and then said at least one thermally insulating element , and - the vehicle furthermore comprises means for conditioning air in the passenger compartment, suitable for heating, cooling and propelling air, in order to place in the latter air derived at least in part from said air conditioning means in thermal exchange with said at least one PCM material and the porous matrix of the inside thermal barrier has open pores that vary according to the liquid or solid state of the PCM material, thus varying the thermal conductivity.
A method for managing enhanced physical downlink control channel, EPDCCH, resources used in a wireless communications network for transmitting scheduling assignments, the method comprising: - establishing a measure on load in the wireless communications network , and - controlling whether to assign one or more user terminals to use EPDCCH resources based on the established measure on load. - establishing a measure on load in the wireless communications network , and - controlling whether to assign one or more user terminals to use EPDCCH resources based on the established measure on load.
An image processing system for visually augmenting a real-time video stream to assist a user in fixing a problem with an inoperative electronic appliance, the image processing system , comprising: at least one processor configured to: receive the real-time video stream captured by an image sensor, the real-time video stream including images of one or more cables and an inoperative electronic appliance; process the real-time video stream using image recognition to identify a plurality of ports in the electronic appliance and the one or more cables appearing in the real-time video stream ; access a database of working solutions to identify a specific one of the one or more cables identified in the real-time video stream for association with a specific port of the plurality of ports to solve a problem with the inoperative electronic appliance; cause a movable augmented indicator to display on the real-time video stream , wherein the movable augmented indicator is configured to guide a user's connection of the specific cable to the specific port; monitor in the real-time video stream changing locations of the specific port as the image sensor moves relative to the electronic appliance; and adjust positions of the movable augmented indicator to account for the changing locations of the specific port in the real-time video stream, characterized in that the at least one processor is further configured to adjust the positions of the movable augmented indicator by altering at least one of a size and an orientation of the movable augmented indicator as a function of at least one of a distance and an angle between the specific cable and the specific port. receive the real-time video stream captured by an image sensor, the real-time video stream including images of one or more cables and an inoperative electronic appliance; process the real-time video stream using image recognition to identify a plurality of ports in the electronic appliance and the one or more cables appearing in the real-time video stream ; access a database of working solutions to identify a specific one of the one or more cables identified in the real-time video stream for association with a specific port of the plurality of ports to solve a problem with the inoperative electronic appliance; cause a movable augmented indicator to display on the real-time video stream , wherein the movable augmented indicator is configured to guide a user's connection of the specific cable to the specific port; monitor in the real-time video stream changing locations of the specific port as the image sensor moves relative to the electronic appliance; and adjust positions of the movable augmented indicator to account for the changing locations of the specific port in the real-time video stream, characterized in that the at least one processor is further configured to adjust the positions of the movable augmented indicator by altering at least one of a size and an orientation of the movable augmented indicator as a function of at least one of a distance and an angle between the specific cable and the specific port.
A method for analyzing diffraction data obtained using a crystal structure analysis sample, the crystal structure analysis sample comprising a single crystal of a porous compound, and a compound for which a structure is to be determined, the single crystal of the porous compound having a three-dimensional framework, and either or both of pores and voids that are defined by the three-dimensional framework, and are three-dimensionally arranged in an ordered manner, the three-dimensional framework having been determined by crystal structure analysis, and molecules of the compound for which the structure is to be determined being arranged in either or both of the pores and the voids in an ordered manner to such an extent that they can be observed by crystal structure analysis, the method comprising: a step of providing the crystal structure analysis sample including the single crystal of the porous compound whose space group is already known; a step of providing a diffraction data of a crystal structure of the porous compound previously analyzed; a step (I) that selects a space group that is identical to a space group of the single crystal of the porous compound, or a space group that has a symmetry lower than that of the space group of the single crystal of the porous compound; a step (II) that determines an initial structure of the crystal structure analysis sample using the space group determined by the step (I) by analyzing diffraction data of the crystal structure analysis sample using the diffraction data of a crystal structure of the porous compound previously analyzed as initial values; and a step (III) that refines the initial structure determined by the step (II) using a Fourier method, a least-square method, or a maximum likelihood method, thereby obtaining a crystal structure of the compound for which the structure is to be determined, wherein the single crystal of the porous compound is a single crystal of a polynuclear metal complex, and the compound for which the structure is to be determined is a compound having a molecular weight of 20 to 3,000. a step of providing the crystal structure analysis sample including the single crystal of the porous compound whose space group is already known; a step of providing a diffraction data of a crystal structure of the porous compound previously analyzed; a step (I) that selects a space group that is identical to a space group of the single crystal of the porous compound, or a space group that has a symmetry lower than that of the space group of the single crystal of the porous compound; a step (II) that determines an initial structure of the crystal structure analysis sample using the space group determined by the step (I) by analyzing diffraction data of the crystal structure analysis sample using the diffraction data of a crystal structure of the porous compound previously analyzed as initial values; and a step (III) that refines the initial structure determined by the step (II) using a Fourier method, a least-square method, or a maximum likelihood method, thereby obtaining a crystal structure of the compound for which the structure is to be determined,
A method implemented by a computing device for data stream analytics for an aircraft , the method comprising: receiving a plurality of data streams (214A-C) acquired for a respective parameter of a plurality of parameters indicating an operating condition of the aircraft , wherein the aircraft is configured to operate in different flight modes, each flight mode being associated with a respective set of operating rules; selecting , from the plurality of data streams (214A-C), at least one data stream corresponding to at least one parameter of the plurality of parameters; selecting a portion of data from the at least one data stream based on which flight mode the aircraft is operating in when the portion of data is acquired; identifying a sequence of events occurring on the aircraft based on the portion of data; determining a statistical variable for the at least one parameter; comparing the portion of data to a model determined for the at least one parameter based on historical data, wherein comparing the portion of data to the model determined for the at least one parameter based on the historical data comprises comparing the determined statistical variable to a stored statistical variable associated with the historical data; determining that the sequence of events is out of order compared to an expected order; determining that a failure has occurred or is likely to occur during operation of the aircraft based on the comparing and the determining that the sequence of events is out of order; and transmitting aircraft health monitoring information indicative of occurrence or likelihood of occurrence of the failure. receiving a plurality of data streams (214A-C) acquired for a respective parameter of a plurality of parameters indicating an operating condition of the aircraft , wherein the aircraft is configured to operate in different flight modes, each flight mode being associated with a respective set of operating rules; selecting , from the plurality of data streams (214A-C), at least one data stream corresponding to at least one parameter of the plurality of parameters; selecting a portion of data from the at least one data stream based on which flight mode the aircraft is operating in when the portion of data is acquired; identifying a sequence of events occurring on the aircraft based on the portion of data; determining a statistical variable for the at least one parameter; comparing the portion of data to a model determined for the at least one parameter based on historical data, wherein comparing the portion of data to the model determined for the at least one parameter based on the historical data comprises comparing the determined statistical variable to a stored statistical variable associated with the historical data; determining that the sequence of events is out of order compared to an expected order; determining that a failure has occurred or is likely to occur during operation of the aircraft based on the comparing and the determining that the sequence of events is out of order; and transmitting aircraft health monitoring information indicative of occurrence or likelihood of occurrence of the failure.
A three-dimensional printing equipment assembly comprising a three-dimensional printing build system comprising: a cyclic, linear or oscillating conveyor system ; plural build modules (6, 6a-6L, 7a ,10, 15, 90, 175) engaged with the conveyor system and temporarily retain a powder, and_comprising respective height adjustable platforms ; at least one build station that forms respective one or more three-dimensionally printed articles on the plural build modules (6, 6a-6L, 7a ,10, 15, 90, 175), the at least one build station including 1) at least one powder layering system adapted to form incremental powder layers within build modules; and 2) at least one printing system adapted to apply a liquid according to a predetermined pattern to incremental powder layers within build modules; characterized by a control system including a proximity sensor configured to determine and specify the location of one or more of the plural build modules (6, 6a-6L, 7a ,10, 15, 90, 175) relative to the conveyor system ; wherein the conveyor system is configured to repeatedly conduct the plural build modules (6, 6a-6L, 7a ,10, 15, 90, 175) from the at least one powder layering system to the at least one printing system to form a three-dimensionally printed bed comprising one or more three-dimensionally-printed articles; and a bed transfer system adapted to transfer the three-dimensionally printed beds, one or more at a time, away from the three-dimensional printing build system. a cyclic, linear or oscillating conveyor system ; plural build modules (6, 6a-6L, 7a ,10, 15, 90, 175) engaged with the conveyor system and temporarily retain a powder, and_comprising respective height adjustable platforms ; at least one build station that forms respective one or more three-dimensionally printed articles on the plural build modules (6, 6a-6L, 7a ,10, 15, 90, 175), the at least one build station including 1) at least one powder layering system adapted to form incremental powder layers within build modules; and 2) at least one printing system adapted to apply a liquid according to a predetermined pattern to incremental powder layers within build modules; characterized by a control system including a proximity sensor configured to determine and specify the location of one or more of the plural build modules (6, 6a-6L, 7a ,10, 15, 90, 175) relative to the conveyor system ; wherein the conveyor system is configured to repeatedly conduct the plural build modules (6, 6a-6L, 7a ,10, 15, 90, 175) from the at least one powder layering system to the at least one printing system to form a three-dimensionally printed bed comprising one or more three-dimensionally-printed articles; and a bed transfer system adapted to transfer the three-dimensionally printed beds, one or more at a time, away from the three-dimensional printing build system.
Central unit (Z) for a bus system, comprising: - an input (L, N) for a voltage supply, preferably a mains voltage supply, and - a unit (PS) for providing a voltage supply to a bus connection in order to supply a connected bus, which preferably carries a voltage in the idle state, such as a DALI bus, characterized by - at least one output for looping the voltage supply voltage to at least one bus participant, - a detection unit that detects the electrical power consumption of all connected bus participants, and in that the central unit is designed, in a measuring phase, to selectively switch on only one of a plurality of connected bus participants and to detect the power consumption thereof, and in that when detecting the total consumption, the detection unit allocates the total consumption to the respective connected bus participants on the basis of the measurement in the measuring phase and a dimming command currently sent by the central unit via the bus to the relevant device. - an input (L, N) for a voltage supply, preferably a mains voltage supply, and - a unit (PS) for providing a voltage supply to a bus connection in order to supply a connected bus, which preferably carries a voltage in the idle state, such as a DALI bus, characterized by - at least one output for looping the voltage supply voltage to at least one bus participant, - a detection unit that detects the electrical power consumption of all connected bus participants, and in that the central unit is designed, in a measuring phase, to selectively switch on only one of a plurality of connected bus participants and to detect the power consumption thereof, and in that when detecting the total consumption, the detection unit allocates the total consumption to the respective connected bus participants on the basis of the measurement in the measuring phase and a dimming command currently sent by the central unit via the bus to the relevant device.
An optical communication device (120-1) comprising: a GPS receiver configured to receive and output a GPS signal from a satellite; a main controller configured to generate and output synchronization data based on the GPS signal; and an optical transceiver (1200-1) configured to generate an optical signal by superposing input payload data and the synchronization data, and to output the optical signal, wherein a first communication channel corresponding to the payload data and a second communication channel corresponding to the synchronization data are different communication channels, wherein the synchronization data includes quality information of the GPS signal including power of the GPS signal, and wherein the quality information is criteria for selecting one of a plurality of synchronization data generated by optical communication devices to generate a synchronization signal in an optical communication system. a GPS receiver configured to receive and output a GPS signal from a satellite; a main controller configured to generate and output synchronization data based on the GPS signal; and an optical transceiver (1200-1) configured to generate an optical signal by superposing input payload data and the synchronization data, and to output the optical signal, wherein a first communication channel corresponding to the payload data and a second communication channel corresponding to the synchronization data are different communication channels, wherein the synchronization data includes quality information of the GPS signal including power of the GPS signal, and wherein the quality information is criteria for selecting one of a plurality of synchronization data generated by optical communication devices to generate a synchronization signal in an optical communication system.
A system , comprising: a gas turbine system , comprising: a turbine combustor; a turbine driven by combustion products from the turbine combustor; and an exhaust gas compressor driven by the turbine, wherein the exhaust gas compressor is configured to compress and supply an exhaust gas to the turbine combustor; and an exhaust gas recirculation (EGR) system ; wherein the system further comprises an oxidant compressor configured to compress an oxidant , and to supply the compressed oxidant to the turbine combustor, characterized in that : the EGR system is configured to recirculate the exhaust gas along one or more exhaust recirculation paths from the turbine to first and second exhaust gas inlets of the gas turbine system; wherein the exhaust recirculation system comprises a scrubbing system and a moisture separator upstream of at least the second exhaust gas inlet; and wherein the first exhaust gas inlet enables the exhaust gas compressor to intake the exhaust gas for exhaust gas compression, and the second exhaust gas inlet is separate from the first exhaust gas inlet. a turbine combustor; a turbine driven by combustion products from the turbine combustor; and an exhaust gas compressor driven by the turbine, wherein the exhaust gas compressor is configured to compress and supply an exhaust gas to the turbine combustor; and an exhaust gas recirculation (EGR) system ; wherein the system further comprises an oxidant compressor configured to compress an oxidant , and to supply the compressed oxidant to the turbine combustor, characterized in that : the EGR system is configured to recirculate the exhaust gas along one or more exhaust recirculation paths from the turbine to first and second exhaust gas inlets of the gas turbine system; wherein the exhaust recirculation system comprises a scrubbing system and a moisture separator upstream of at least the second exhaust gas inlet; and wherein the first exhaust gas inlet enables the exhaust gas compressor to intake the exhaust gas for exhaust gas compression, and the second exhaust gas inlet is separate from the first exhaust gas inlet.