mhurhangee/patent-ind-claim-en huggingface dataset:
A management method, comprising: receiving, by a network functions virtualization orchestrator, NFVO, unit from an operations support system or business support system, OSS/BSS, a management request of a network service, NS, wherein the management request carries affinity information, and the affinity information is used to configure affinity and/or anti-affinity between a virtualized network function, VNF, instance of the NS and an existing VNF instance; and managing, by the NFVO unit, the NS according to the affinity information. receiving, by a network functions virtualization orchestrator, NFVO, unit from an operations support system or business support system, OSS/BSS, a management request of a network service, NS, wherein the management request carries affinity information, and the affinity information is used to configure affinity and/or anti-affinity between a virtualized network function, VNF, instance of the NS and an existing VNF instance; and managing, by the NFVO unit, the NS according to the affinity information.
Aerosol-generating system comprising: - a capsule comprising a shell comprising a base and at least one side wall extending from the base , the capsule further comprising a lid sealed on the at least one side wall for forming a sealed capsule , the shell containing an aerosol-forming substrate and the shell comprising susceptor material for heating the aerosol-forming substrate within the shell ; - a power source connected to a load network, the load network comprising an inductor for being inductively coupled to the susceptor material of the shell , further comprising a thermal insulation layer at least partially surrounding the susceptor material of the shell . - a capsule comprising a shell comprising a base and at least one side wall extending from the base , the capsule further comprising a lid sealed on the at least one side wall for forming a sealed capsule , the shell containing an aerosol-forming substrate and the shell comprising susceptor material for heating the aerosol-forming substrate within the shell ; - a power source connected to a load network, the load network comprising an inductor for being inductively coupled to the susceptor material of the shell , further comprising a thermal insulation layer at least partially surrounding the susceptor material of the shell .
A synchronization device for a manual transmission of a motor vehicle, comprising a sliding sleeve and at least one clutch body , wherein the sliding sleeve comprises an internal toothing having a multitude of sliding sleeve teeth and sliding sleeve tooth gaps located therebetween, wherein the clutch body comprises an external toothing having a multitude of clutch teeth and clutch tooth gaps located therebetween, wherein the sliding sleeve and the clutch body are adjustable relative to each other in the axial sliding direction (X), and wherein, in a synchronized position of the synchronization device , the sliding sleeve teeth are positioned at least partially in the clutch tooth gaps and the clutch teeth are positioned at least partially in the sliding sleeve tooth gaps , wherein two neighboring sliding sleeve teeth each include a contact portion both of which are associated with a special clutch tooth that has two stop portions provided on opposite sides of the special clutch tooth , and/or in that two neighboring clutch teeth each include a stop portion both of which are associated with a special sliding sleeve tooth that has two contact portions provided on opposite sides of the special sliding sleeve tooth , and wherein, in the synchronized position, the two stop portions rest against the two stop portions , whereby a mechanical shift stop is formed in the axial sliding direction (X), which prevents a further movement in the axial sliding direction (X) beyond the synchronized position, characterized in that compared to the other clutch teeth , the special clutch tooth is shortened as viewed in the axial sliding direction (X), and/or compared to the other sliding sleeve teeth , the special sliding sleeve tooth is shortened as viewed in the axial sliding direction (X). wherein two neighboring sliding sleeve teeth each include a contact portion both of which are associated with a special clutch tooth that has two stop portions provided on opposite sides of the special clutch tooth , and/or in that two neighboring clutch teeth each include a stop portion both of which are associated with a special sliding sleeve tooth that has two contact portions provided on opposite sides of the special sliding sleeve tooth , and wherein, in the synchronized position, the two stop portions rest against the two stop portions , whereby a mechanical shift stop is formed in the axial sliding direction (X), which prevents a further movement in the axial sliding direction (X) beyond the synchronized position, characterized in that compared to the other clutch teeth , the special clutch tooth is shortened as viewed in the axial sliding direction (X), and/or compared to the other sliding sleeve teeth , the special sliding sleeve tooth is shortened as viewed in the axial sliding direction (X).
A powder conveying device for coating powder, - wherein a powder conveyor comprising a powder outlet duct (51.1) is provided, - wherein a powder outlet valve is provided for opening or for closing the powder outlet duct (51.1), - wherein a setpoint value generator for specifying a setpoint opening period (Tsoll) of the powder outlet valve is provided, characterized in that - a sensor for determining the actual opening period (Tist) of the powder outlet valve is provided, and that - an evaluation unit for determining the deviation (ΔT) between the setpoint opening period (Tsoll) and the actual opening period (Tist) is provided. - wherein a powder conveyor comprising a powder outlet duct (51.1) is provided, - wherein a powder outlet valve is provided for opening or for closing the powder outlet duct (51.1), - wherein a setpoint value generator for specifying a setpoint opening period (Tsoll) of the powder outlet valve is provided, - a sensor for determining the actual opening period (Tist) of the powder outlet valve is provided, and that - an evaluation unit for determining the deviation (ΔT) between the setpoint opening period (Tsoll) and the actual opening period (Tist) is provided.
Distributed Antenna System (DAS) for massive MIMO applications, comprising: - a plurality of Point of Interface modules (POI, POI1, POI2, UL POI) connectable to a Baseband Unit (BBU) and configured for converting a digital data flow coming from said Baseband Unit (BBU) to RF signals and/or for converting incoming RF signals to a digital data flow to be sent to said Baseband Unit (BBU); - a plurality of optical modules (OTRX1, OTRX2, OTRX3, OTRX4) operatively connected to said plurality of Point od Interface modules (POI, POI1, POI2, UL POI) and configured for performing an electro-optical conversion of the RF signals; - a plurality of Remote Units (RU1, RU2, RU3, RU4, ULRU1, ULRU2, ULRU3, ULRU4) operatively connected to said optical modules (OTRX1, OTRX2, OTRX3, OTRX4) and to a plurality of antennas (ANT1, ANT2, ANT3, ANT4); characterized in that at least one of said optical modules (OTRX1, OTRX2, OTRX3, OTRX4) comprises a plurality of uplink paths separated from each other and provided with respective uplink outputs (UL RF 1, UL RF 2). - a plurality of Point of Interface modules (POI, POI1, POI2, UL POI) connectable to a Baseband Unit (BBU) and configured for converting a digital data flow coming from said Baseband Unit (BBU) to RF signals and/or for converting incoming RF signals to a digital data flow to be sent to said Baseband Unit (BBU); - a plurality of optical modules (OTRX1, OTRX2, OTRX3, OTRX4) operatively connected to said plurality of Point od Interface modules (POI, POI1, POI2, UL POI) and configured for performing an electro-optical conversion of the RF signals; - a plurality of Remote Units (RU1, RU2, RU3, RU4, ULRU1, ULRU2, ULRU3, ULRU4) operatively connected to said optical modules (OTRX1, OTRX2, OTRX3, OTRX4) and to a plurality of antennas (ANT1, ANT2, ANT3, ANT4);
A positive electrode active material for a secondary battery, the positive electrode active material being made of secondary particles that include primary particles having a rectangular parallelepiped shape, the rectangular parallelepiped having at least one of vertices and edges formed in a round shape that is convex outward, wherein: 1% to 40% of a total surface area of the secondary particles has open porosity; and the primary particles include a lithium composite metal oxide of Formula 1 below. [Formula 1] Li a Ni 1-x-y Co x M1 y M3 z M2 w O 2 , wherein, in Formula 1, M1 is at least one selected from the group consisting of Al and Mn, M2 is any one or two or more elements selected from the group consisting of Zr, Ti, Mg, Ta, and Nb, M3 is any one or two or more elements selected from the group consisting of W, Mo, and Cr, and 1.0≤a≤1.5, 0<x≤0.5, 0<y≤0.5, 0.002≤z≤03, 0≤w≤0.02, 0≤x+y≤0.7. 1% to 40% of a total surface area of the secondary particles has open porosity; and the primary particles include a lithium composite metal oxide of Formula 1 below. [Formula 1] Li a Ni 1-x-y Co x M1 y M3 z M2 w O 2 , wherein, in Formula 1, M1 is at least one selected from the group consisting of Al and Mn, M2 is any one or two or more elements selected from the group consisting of Zr, Ti, Mg, Ta, and Nb, M3 is any one or two or more elements selected from the group consisting of W, Mo, and Cr, and 1.0≤a≤1.5, 0<x≤0.5, 0<y≤0.5, 0.002≤z≤03, 0≤w≤0.02, 0≤x+y≤0.7.
A fuel cell system comprising: a first decompression unit that is disposed in a supply path for supplying hydrogen from a hydrogen tank to a fuel cell stack and for decompressing hydrogen to be supplied to the fuel cell stack ; an expander that is configured to decompress and expand hydrogen supplied from the hydrogen tank ; a flow rate adjusting unit that is disposed upstream from the expander in the supply path and is able to be switched to one of an open state in which hydrogen is supplied to the expander and a closed state in which a supply of hydrogen to the expander is intercepted or an amount of hydrogen supplied to the expander is less than that in the open state; characterized in that the expander is disposed upstream from the first decompression unit in the supply path , an energy recovery device is connected to the expander , and a control unit is configured to perform control of switching the flow rate adjusting unit to the closed state when a pressure difference between a first pressure upstream from the expander in the supply path and a second pressure downstream from the expander is less than a first threshold value or when a pressure ratio of the second pressure to the first pressure is equal to or greater than a second threshold value. a first decompression unit that is disposed in a supply path for supplying hydrogen from a hydrogen tank to a fuel cell stack and for decompressing hydrogen to be supplied to the fuel cell stack ; an expander that is configured to decompress and expand hydrogen supplied from the hydrogen tank ; a flow rate adjusting unit that is disposed upstream from the expander in the supply path and is able to be switched to one of an open state in which hydrogen is supplied to the expander and a closed state in which a supply of hydrogen to the expander is intercepted or an amount of hydrogen supplied to the expander is less than that in the open state; characterized in that the expander is disposed upstream from the first decompression unit in the supply path , an energy recovery device is connected to the expander , and a control unit is configured to perform control of switching the flow rate adjusting unit to the closed state when a pressure difference between a first pressure upstream from the expander in the supply path and a second pressure downstream from the expander is less than a first threshold value or when a pressure ratio of the second pressure to the first pressure is equal to or greater than a second threshold value.
An IGF-1R antibody, or an antigen-binding fragment thereof, characterized in that it comprises: i) a heavy chain with CDR-H1 of sequence SEQ ID No. 1, CDR-H2 of sequence SEQ ID No. 2 and CDR-H3 of sequence SEQ ID No. 3; and ii) a light chain with CDR-L1 of sequence SEQ ID No. 4, CDR-L2 of sequence SEQ ID No. 5 and CDR-L3 of sequence SEQ ID No. 6. i) a heavy chain with CDR-H1 of sequence SEQ ID No. 1, CDR-H2 of sequence SEQ ID No. 2 and CDR-H3 of sequence SEQ ID No. 3; and ii) a light chain with CDR-L1 of sequence SEQ ID No. 4, CDR-L2 of sequence SEQ ID No. 5 and CDR-L3 of sequence SEQ ID No. 6.
A method of correcting registration errors of media sheets (20; 20') that are fed to a print station in a duplex printer via a first liftable pinch and a steering mechanism , the first liftable pinch being arranged in a sheet supply path upstream of the steering mechanism , the method comprising: - at the print station alternating sheets (20; 20') supplied from the supply path with sheets supplied from a duplex loop which returns sheets from a downstream side to an upstream side of the print station ; - for each sheet fed to the print station via the supply path , a step of checking the sheet for registration errors and, if a registration error is detected, lifting the first liftable pinch and operating the steering mechanism so as to rotate the sheet; and - for a fraction of the sheets , when an image has been printed on a first side of the sheet, returning the sheet via a duplex loop and feeding it again to the print station , again with registration error correction, characterized in that the sheets that are returned via the duplex loop are fed to the print station via a second liftable pinch without passing through the first liftable pinch again, and the liftable pinches are operated independently of one another. - at the print station alternating sheets (20; 20') supplied from the supply path with sheets supplied from a duplex loop which returns sheets from a downstream side to an upstream side of the print station ; - for each sheet fed to the print station via the supply path , a step of checking the sheet for registration errors and, if a registration error is detected, lifting the first liftable pinch and operating the steering mechanism so as to rotate the sheet; and - for a fraction of the sheets , when an image has been printed on a first side of the sheet, returning the sheet via a duplex loop and feeding it again to the print station , again with registration error correction,
An extruder for producing pet food having a die with at least one opening through which a material is pressable in order to form an extrudate, wherein an apparatus for cutting off the extrudate is provided in material flow direction adjoining the die which apparatus has a knife which is mounted rotatably about an axis of rotation and which is driven by a drive, in particular an electric motor , in that a torque is transmitted from the drive to the knife , wherein a bearing element is provided which is rigidly connected to the extruder and via which the knife is rotatably connected to the extruder around the axis of rotation , whereby the drive is placed separately from the bearing element and a magnetic coupling is provided between the bearing element and the drive in order to transmit the torque from the drive to the knife via magnetic forces, characterized in that a housing is provided that is sealed to an environment , in which housing the bearing element and the knife are located, so that the extruder is suitable for a method in which the interior of the housing is subjected to a higher pressure than the environment , wherein the drive is located outside the housing and the magnetic coupling is configured to transmit the torque into the housing .
A method of displaying optimized aircraft energy level of an aircraft to a flight crew, the method comprising the steps of: processing flight plan data, in a processor , to determine an optimized aircraft energy level along a descent profile of the aircraft from cruise altitude down to aircraft destination; continuously processing aircraft data, in the processor, to continuously determine, in real-time, an actual aircraft energy level; continuously comparing , in the processor, the actual aircraft energy level of the aircraft to the optimized aircraft energy level; commanding , using the processor, a display device to render an image that indicates: (i) the optimized aircraft energy level, (ii) how the actual aircraft energy level differs from the optimized aircraft energy level, and (iii) how the actual aircraft energy level is trending relative to the optimized aircraft energy level; and characterized in that the method further comprises the step of: commanding, using the processor, the display device to render one or more visual cues that indicate actions the flight crew could take to converge the actual aircraft energy level toward the optimized aircraft energy level. processing flight plan data, in a processor , to determine an optimized aircraft energy level along a descent profile of the aircraft from cruise altitude down to aircraft destination; continuously processing aircraft data, in the processor, to continuously determine, in real-time, an actual aircraft energy level; continuously comparing , in the processor, the actual aircraft energy level of the aircraft to the optimized aircraft energy level; commanding , using the processor, a display device to render an image that indicates: (i) the optimized aircraft energy level, (ii) how the actual aircraft energy level differs from the optimized aircraft energy level, and (iii) how the actual aircraft energy level is trending relative to the optimized aircraft energy level; and (i) the optimized aircraft energy level, (ii) how the actual aircraft energy level differs from the optimized aircraft energy level, and (iii) how the actual aircraft energy level is trending relative to the optimized aircraft energy level; and characterized in that the method further comprises the step of: commanding, using the processor, the display device to render one or more visual cues that indicate actions the flight crew could take to converge the actual aircraft energy level toward the optimized aircraft energy level.
A vehicle radar system comprising a transmitter section , a receiver section and a control unit , where the transmitter section comprises a plurality of transmitter antenna devices and where the receiver section comprises a plurality of receiver antenna devices , where furthermore the vehicle radar system is arranged to generate SFCW, Stepped Frequency Continuous Wave, ramps , each SFCW ramp comprising a sequence of SFCW constant frequency steps separated by a frequency step span (Δf s ), where each SFCW frequency step in an SFCW ramp has a time duration equal to an OFDM, Orthogonal Frequency Division Multiplexing, symbol time duration (T o ) of the vehicle radar system , characterized in that the radar system is arranged to generate OFDM symbols having the OFDM symbol time duration (T o ) and an OFDM symbol bandwidth (B), where each OFDM symbol comprises a plurality of modulated subcarriers separated by a frequency span (Δf c ) , and to mix each OFDM symbol with a corresponding SFCW frequency step in an SFCW ramp such that a resulting stepped OFDM ramp waveform is obtained, where the subcarriers of each OFDM symbol are each allocated exclusively to, and transmitted by, a corresponding transmitting antenna device , where the receiver section is arranged to mix down a received signal of every receiver antenna device with the SFCW ramp , where the receiver section is arranged to sample the mixed down received signal of each receiver antenna device at a sampling rate equal to the bandwidth (B) of the OFDM symbol .
A coated abrasive article comprising: a plurality of formed ceramic abrasive particles each having a surface feature; the plurality of formed ceramic abrasive particles attached to a flexible backing by a make coat comprising a resinous adhesive forming an abrasive layer; the surface feature having a z-direction rotational orientation, wherein the z- direction rotational orientation refers to the particle's angular rotation about a z- axis passing through the particle and through the backing at a 90 degree angle to the backing ; wherein a specified z-direction rotational orientation occurs more frequently in the abrasive layer than would occur by a random z-direction rotational orientation of the surface feature; wherein the coated abrasive article comprises a sheet or a belt ; characterised in that: the surface feature comprises a substantially planar surface ; and a pattern created by the plurality of formed ceramic abrasive particles comprises a plurality of parallel lines or a plurality of orthogonal lines. a plurality of formed ceramic abrasive particles each having a surface feature; the plurality of formed ceramic abrasive particles attached to a flexible backing by a make coat comprising a resinous adhesive forming an abrasive layer; the surface feature having a z-direction rotational orientation, wherein the z- direction rotational orientation refers to the particle's angular rotation about a z- axis passing through the particle and through the backing at a 90 degree angle to the backing ; wherein a specified z-direction rotational orientation occurs more frequently in the abrasive layer than would occur by a random z-direction rotational orientation of the surface feature; wherein the coated abrasive article comprises a sheet or a belt ; characterised in that: the surface feature comprises a substantially planar surface ; and a pattern created by the plurality of formed ceramic abrasive particles comprises a plurality of parallel lines or a plurality of orthogonal lines. the surface feature comprises a substantially planar surface ; and a pattern created by the plurality of formed ceramic abrasive particles comprises a plurality of parallel lines or a plurality of orthogonal lines.
A method for producing a cyclic ether represented by the following formula , where a 2-hydroxy cyclic ether, represented by the following formula , is reacted with hydrogen in the presence of a catalyst, wherein the catalyst includes an element from groups 8 to 10 of the periodic table, the pH of the reaction mixture is not more than 7, and the reaction is carried out while at least one acid selected from the group consisting of carboxylic acid, phosphoric acid, sulfuric acid, hydrochloric acid, nitric acid, a heteropoly acid, sodium hydrogensulfate, toluenesulfonic acid and a peracid, or a salt thereof, or activated earth, exists in the reaction mixture: wherein n is an integer in the range of 1 to 7, and R 1 to R 5 each independently represent a hydrogen atom, an aliphatic hydrocarbon group having 1 to 4 carbon atoms or an aromatic hydrocarbon group having 6 to 12 carbon atoms, and when R 4 and R 5 exist plurally, they may differ from each other; wherein the symbols have the above-defined meanings.