mhurhangee/ep-ind-claims huggingface dataset:
A method for runway traction estimation and reporting using an aircraft, comprising: receiving, by a runway traction estimation and reporting processor, a first sensor input indicating a first triggering event; starting, by the runway traction estimation and reporting processor and in response to the receiving of the first sensor input, a polling timer; receiving, by the runway traction estimation and reporting processor, a second sensor input in response to the polling timer indicating that a first period has elapsed, wherein the second sensor input comprises a wheel speed identification and a brake pressure identification; resetting the polling time; repeating the receiving step and resetting step until a third sensor input indicating an ending event is received, wherein the first period is varied between repetitions and is based on a current aircraft velocity, such that the second sensor input is received more frequently when the aircraft velocity is higher; and sending, by the runway traction estimation and reporting processor, a message to an output device (8,10,12) in response to the second sensor input wherein the message comprises a runway traction estimate. receiving, by a runway traction estimation and reporting processor, a first sensor input indicating a first triggering event; starting, by the runway traction estimation and reporting processor and in response to the receiving of the first sensor input, a polling timer; receiving, by the runway traction estimation and reporting processor, a second sensor input in response to the polling timer indicating that a first period has elapsed, wherein the second sensor input comprises a wheel speed identification and a brake pressure identification; resetting the polling time; repeating the receiving step and resetting step until a third sensor input indicating an ending event is received, wherein the first period is varied between repetitions and is based on a current aircraft velocity, such that the second sensor input is received more frequently when the aircraft velocity is higher; and sending, by the runway traction estimation and reporting processor, a message to an output device (8,10,12) in response to the second sensor input wherein the message comprises a runway traction estimate.
A device for monitoring a cardiovascular property of a subject, wherein the device comprises an input configured to obtain measurement data from a primary pressure wave sensor (4a-4c) which is arranged to detect pressure waves in an extracorporeal fluid circuit which is connected in fluid communication with the cardiovascular system of the subject, wherein the device further comprises a signal processor configured to: generate a time-dependent monitoring signal based on the measurement data, such that the monitoring signal comprises a sequence of heart pulses, wherein each heart pulse represents a pressure wave originating from a heart beat in the subject; determine beat classification data for each heart pulse in the monitoring signal; and calculate, based at least partly on the beat classification data, a parameter value indicative of the cardiovascular property, characterized in that the beat classification data distinguishes between heart pulses originating from normal heart beats and heart pulses originating from ectopic heart beats, and that the signal processor is configured to determine the beat classification data by: extracting at least part of a temporal profile of each heart pulse, and matching said at least part of the temporal profile against a set of templates, wherein the set of templates represents one or more temporal profiles of the normal heart beats and the ectopic heart beats. generate a time-dependent monitoring signal based on the measurement data, such that the monitoring signal comprises a sequence of heart pulses, wherein each heart pulse represents a pressure wave originating from a heart beat in the subject; determine beat classification data for each heart pulse in the monitoring signal; and calculate, based at least partly on the beat classification data, a parameter value indicative of the cardiovascular property, characterized in that the beat classification data distinguishes between heart pulses originating from normal heart beats and heart pulses originating from ectopic heart beats, and that the signal processor is configured to determine the beat classification data by: extracting at least part of a temporal profile of each heart pulse, and matching said at least part of the temporal profile against a set of templates, wherein the set of templates represents one or more temporal profiles of the normal heart beats and the ectopic heart beats.
A method of controlling a polymerization reaction in a polymerization reactor system, the method comprising: (i) contacting a dual catalyst system with an olefin monomer and an optional olefin comonomer in the polymerization reactor system under polymerization conditions to produce an olefin polymer, wherein the dual catalyst system comprises a first metallocene catalyst component, a second metallocene catalyst component, an activator, and a co-catalyst; and (ii) introducing an amount of an alcohol compound into the polymerization reactor system to reduce a melt index parameter of the olefin polymer; increase a molecular weight parameter of the olefin polymer selected from Mw, Mz, or both; or reduce a melt index parameter of the olefin polymer and increase a molecular weight parameter of the olefin polymer selected from Mw, Mz, or both. (i) contacting a dual catalyst system with an olefin monomer and an optional olefin comonomer in the polymerization reactor system under polymerization conditions to produce an olefin polymer, wherein the dual catalyst system comprises a first metallocene catalyst component, a second metallocene catalyst component, an activator, and a co-catalyst; and (ii) introducing an amount of an alcohol compound into the polymerization reactor system to reduce a melt index parameter of the olefin polymer; increase a molecular weight parameter of the olefin polymer selected from Mw, Mz, or both; or reduce a melt index parameter of the olefin polymer and increase a molecular weight parameter of the olefin polymer selected from Mw, Mz, or both.
A manufacturing method of a hot-rolled silicon steel, which comprises a heating procedure, a rough rolling procedure and a finishing rolling procedure on a silicon steel slab, where said heating procedure is conducted in a heating furnace comprising, a preheating section, a heating section and a soaking section, wherein, the preheating section satisfies the following formula, V Tp > 220 min t × 100 ° C T C + 200 ° C × 25 ° C / min wherein, V Tp: Increasing rate of temperature of the preheating section, °C/min, t: Total heating time of the slab in the heating furnace, and t=180∼240 min, T C: Initial temperature of the slab when entering into the furnace, °C; the soaking section satisfies the following formula or, − 10 ° C ≤ TS ≤ 30 ° C 2-1, when the silicon content of the silicon steel is 1.5 wt% or above, 10 ° C ≤ TS ≤ 80 ° C 2-2, when the silicon content of the silicon steel is less then 1.5 wt%, wherein, Ts: Temperature rise of the soaking section, i.e., the difference between the temperature of the slab when entirely taken out of the furnace and its temperature at the end of the heating section, °C; and the temperature rise of the heating section satisfies the following formula: temperature rise of the heating section = temperature of the slab when entirely taken out of the furnace − temperature rise of the soaking section − temperature at the end of the preheating section wherein said preheating section refers to a section from an entering point at which the slab enters into the furnace to a point that is 1/6∼1/3 of the furnace length away from said entering point, said soaking section refers to a section from an exit point at which the slab is taken out of the furnace to a point that is 1/6∼1/3 of the furnace length away from said exit point, and said heating section refers to a section that is between the preheating section and the soaking section. V Tp: Increasing rate of temperature of the preheating section, °C/min, t: Total heating time of the slab in the heating furnace, and t=180∼240 min, T C: Initial temperature of the slab when entering into the furnace, °C;
A memory device (100, 600) for a print cartridge including data to reconstruct a color table for a printing device (206, 614), the data comprising: a compressed bitstream stored in the memory device (100, 600), wherein the compressed bitstream comprises: a plurality of quantized coefficients from a lossy compression of a plurality of difference nodes of a difference color table, the quantized coefficients being quantized using a selected step size (Δ), the quantized coefficients of the difference color table being useable with a reference table on the printing device (206, 614) to provide a reconstructed color table to be applied to a color management system, wherein color tables providing transformations between various color spaces are used in color management; wherein the value of each node in the difference color table reconstructed from the quantized coefficients is to be added to the value of a corresponding node of a reference table (210, 620) stored on the printing device (206, 614); and corrective information (104, 604) for a set of nodes to be modified corresponding to nodes of the reference table with residual values, wherein the corrective information (104, 604) includes residual values and node location information for the locations of the set of nodes to be modified with the residual values; wherein the quantized coefficients and the corrective information included in the bitstream are compressed; and the memory device (100, 600) includes the step size (Δ) as further information, wherein the compressed bit stream which is compressed with a lossless compression comprises a data stream of quantized coefficients derived from a discrete cosine transform at the selected step size (Δ), wherein the data stream of quantized coefficients of the difference color table is a one-dimensional data stream of quantized coefficients. a plurality of quantized coefficients from a lossy compression of a plurality of difference nodes of a difference color table, the quantized coefficients being quantized using a selected step size (Δ), the quantized coefficients of the difference color table being useable with a reference table on the printing device (206, 614) to provide a reconstructed color table to be applied to a color management system, wherein color tables providing transformations between various color spaces are used in color management; wherein the value of each node in the difference color table reconstructed from the quantized coefficients is to be added to the value of a corresponding node of a reference table (210, 620) stored on the printing device (206, 614); and corrective information (104, 604) for a set of nodes to be modified corresponding to nodes of the reference table with residual values, wherein the corrective information (104, 604) includes residual values and node location information for the locations of the set of nodes to be modified with the residual values; wherein the quantized coefficients and the corrective information included in the bitstream are compressed; and the memory device (100, 600) includes the step size (Δ) as further information,
A method for controlling a mineral material processing plant, comprising producing operating power for actuators with a motor or motors, wherein the actuators comprise a crusher, a feeder and a conveyor; giving to the processing plant a command to switch to a standby mode, wherein the command to switch to the standby mode is given by an operating switch (111,111') or automatically after a predetermined time has elapsed from fulfilment of a standby mode triggering condition; characterized by limiting mineral material feeding to the processing plant in response to the said command to switch to the standby mode wherein the feeding of mineral material into the processing plant is limited by stopping the actuators participating in the feeding or by reducing the speed thereof sufficiently so that the actuators participating in the feeding are not able to feed material into the mineral material processing plant; reducing speed of a motor or motors of the processing plant from a processing speed (Rf) to a reduced standby speed (Rsb) in response to the said command to switch to the standby mode; and ensuring that actuators directly in contact with the processing of mineral material apart from the actuators participating in the feeding of the processing plant remain operating with a reduced speed. producing operating power for actuators with a motor or motors, wherein the actuators comprise a crusher, a feeder and a conveyor; giving to the processing plant a command to switch to a standby mode, wherein the command to switch to the standby mode is given by an operating switch (111,111') or automatically after a predetermined time has elapsed from fulfilment of a standby mode triggering condition; characterized by limiting mineral material feeding to the processing plant in response to the said command to switch to the standby mode wherein the feeding of mineral material into the processing plant is limited by stopping the actuators participating in the feeding or by reducing the speed thereof sufficiently so that the actuators participating in the feeding are not able to feed material into the mineral material processing plant; reducing speed of a motor or motors of the processing plant from a processing speed (Rf) to a reduced standby speed (Rsb) in response to the said command to switch to the standby mode; and ensuring that actuators directly in contact with the processing of mineral material apart from the actuators participating in the feeding of the processing plant remain operating with a reduced speed.
Method for controlling a material flow system, in which goods packages are transported on multidirectional conveyor modules that communicate with one another in order to autonomously negotiate with one another material flow paths from a goods package start to a goods package destination by reserving modules for the transport of a particular, identifiable goods package and releasing them after transport of the goods package, characterized in that by the modules a prior reservation token from a neighbouring module is accepted, prior reservation for the transport of the goods package in a particular direction of movement of goods packages is effected, the prior reservation token is forwarded to a neighbouring module that, on the basis of topology information, is situated closer to the destination and hence is downstream and that has not yet denied the prior reservation, and either, upon confirmation of the prior reservation by a downstream conveyor module, the prior reservation is strengthened into a reservation, wherein the modules are reserved for the transport of a goods package in a particular direction of movement of goods packages and at a particular future time or for a particular future period, or in the event of being occupied, a prior reservation denial is received, upon receiving a prior reservation denial, the token is sent to further, neighbouring modules that lead to the goods package destination on the basis of stored topology information, and/or, following reception of prior reservation denials by all or a sufficient number of neighbours, by themselves a prior reservation denial is sent to an upstream conveyor module and a prior reservation is cancelled. from a goods package start to a goods package destination reserving modules for the transport of a particular, identifiable goods package wherein the modules are reserved for the transport of a goods package in a particular direction of movement of goods packages and at a particular future time or for a particular future period, for the transport of a goods package in a particular direction of movement of goods packages and at a particular future time or for a particular future period, a prior reservation denial is received, upon receiving a prior reservation denial, the token is sent to further, neighbouring modules that lead to the goods package destination on the basis of stored topology information, and/or, following reception of prior reservation denials by all or a sufficient number of neighbours, by themselves a prior reservation denial is sent to an upstream conveyor module and a prior reservation is cancelled.
Method for automated particle-size measurement of particles, characterized in that it comprises at least the following steps: - acquiring a three-dimensional cloud of points of the surface of the particle to be examined by passing said particle in front of an optical device (2, 2a), - utilizing the cloud of points in order to characterize the overall shape of the particle (4, 6) by the set of projection coefficients C E on a projection base, which projection base is determined by the steps of: o acquiring a three-dimensional cloud of points of the surface of at least one reference particle by passing this particle (4, 6) in front of an optical device (2, 2a), o reducing the characterization of the surface of the reference particle (4, 6) to an N-dimensional vector R on the basis of the cloud of points which were obtained in the preceding step, and o determining the projection base which makes it possible to characterize the overall shape of the reference particle by the set of projection coefficients C R on said base. - acquiring a three-dimensional cloud of points of the surface of the particle to be examined by passing said particle in front of an optical device (2, 2a), - utilizing the cloud of points in order to characterize the overall shape of the particle (4, 6) by the set of projection coefficients C E on a projection base, which projection base is determined by the steps of: o acquiring a three-dimensional cloud of points of the surface of at least one reference particle by passing this particle (4, 6) in front of an optical device (2, 2a), o reducing the characterization of the surface of the reference particle (4, 6) to an N-dimensional vector R on the basis of the cloud of points which were obtained in the preceding step, and o determining the projection base which makes it possible to characterize the overall shape of the reference particle by the set of projection coefficients C R on said base. o acquiring a three-dimensional cloud of points of the surface of at least one reference particle by passing this particle (4, 6) in front of an optical device (2, 2a), o reducing the characterization of the surface of the reference particle (4, 6) to an N-dimensional vector R on the basis of the cloud of points which were obtained in the preceding step, and o determining the projection base which makes it possible to characterize the overall shape of the reference particle by the set of projection coefficients C R on said base.
A method for operating an aircraft (300; 600), the method comprising: flying the aircraft (300; 600) at a supersonic speed while the aircraft (300; 600) is in a first configuration; changing the configuration of the aircraft (300; 600) from the first configuration to a second configuration, including changing the streamwise lift distribution of the aircraft (300; 600) from a first streamwise lift distribution to a second streamwise lift distribution; and flying the aircraft (300; 600) at the supersonic speed while the aircraft (300; 600) is in the second configuration, wherein the aircraft (300; 600) produces a first sonic boom having a first noise level when the aircraft (300; 600) is flying at the supersonic speed in the first configuration, and wherein the aircraft (300; 600) produces a second sonic boom having a second noise level that is less than the first noise level when the aircraft (300; 600) is flying at the supersonic speed in the second configuration; wherein changing the configuration of the aircraft (300; 600) from the first configuration to the second configuration includes moving a wing leading edge surface (324; 424; 624) of the aircraft (300; 600) from a first position to a second position, and moving a wing trailing edge surface (328; 428; 628) of the aircraft (300; 600) from a third position to a fourth position, in which the lift generated by the wing is distributed toward a trailing edge position thereof; and in that the second streamwise lift distribution increases more gradually over a length of the aircraft (300; 600) than the first streamwise lift distribution. flying the aircraft (300; 600) at a supersonic speed while the aircraft (300; 600) is in a first configuration; changing the configuration of the aircraft (300; 600) from the first configuration to a second configuration, including changing the streamwise lift distribution of the aircraft (300; 600) from a first streamwise lift distribution to a second streamwise lift distribution; and flying the aircraft (300; 600) at the supersonic speed while the aircraft (300; 600) is in the second configuration, wherein the aircraft (300; 600) produces a first sonic boom having a first noise level when the aircraft (300; 600) is flying at the supersonic speed in the first configuration, and wherein the aircraft (300; 600) produces a second sonic boom having a second noise level that is less than the first noise level when the aircraft (300; 600) is flying at the supersonic speed in the second configuration; wherein changing the configuration of the aircraft (300; 600) from the first configuration to the second configuration includes moving a wing leading edge surface (324; 424; 624) of the aircraft (300; 600) from a first position to a second position, and moving a wing trailing edge surface (328; 428; 628) of the aircraft (300; 600) from a third position to a fourth position, in which the lift generated by the wing is distributed toward a trailing edge position thereof; and in that the second streamwise lift distribution increases more gradually over a length of the aircraft (300; 600) than the first streamwise lift distribution.