mhurhangee/ep-ind-claims huggingface dataset:
A method performed by a terminal (1e-05) in a wireless communication system, the method comprising: receiving (1e-15), from a base station (1e-10), BS, minimum system information, SI, which includes an ID of a dedicated preamble used for a SI request for system information other than the minimum SI and radio resource information for transmitting the preamble; triggering (1e-20) a SI request for particular system information other than the minimum SI; determining (1e-25) whether the minimum SI includes an ID of a dedicated preamble for the SI request; selecting (1e-30) a preamble corresponding to the request and requesting the particular system information through msg 1 by transmitting (1e-35) the selected preamble to the BS; receiving (1e-40) a random access response, RAR, for the purpose of acknowledgment, ACK, from the BS, which includes a first subheader which includes a backoff indicator, BI, and a field that indicates which type of random access, RA, corresponds to the BI, a second subheader including the ID of the transmitted preamble, and a MAC RAR corresponding to the second subheader including radio resource information through which the requested system information is broadcasted; ignoring the BI if it is not to be applied to a msg-1-based SI request; and receiving (1e-65), from the BS, the requested particular other SI in the radio resources of the radio resource information. receiving (1e-15), from a base station (1e-10), BS, minimum system information, SI, which includes an ID of a dedicated preamble used for a SI request for system information other than the minimum SI and radio resource information for transmitting the preamble; triggering (1e-20) a SI request for particular system information other than the minimum SI; determining (1e-25) whether the minimum SI includes an ID of a dedicated preamble for the SI request; selecting (1e-30) a preamble corresponding to the request and requesting the particular system information through msg 1 by transmitting (1e-35) the selected preamble to the BS; receiving (1e-40) a random access response, RAR, for the purpose of acknowledgment, ACK, from the BS, which includes a first subheader which includes a backoff indicator, BI, and a field that indicates which type of random access, RA, corresponds to the BI, a second subheader including the ID of the transmitted preamble, and a MAC RAR corresponding to the second subheader including radio resource information through which the requested system information is broadcasted; ignoring the BI if it is not to be applied to a msg-1-based SI request; and receiving (1e-65), from the BS, the requested particular other SI in the radio resources of the radio resource information.
Method for operating at least one wind turbine (10; 60, 62), wherein the at least one wind turbine (10; 60, 62) is shut down by a shutdown system if it casts a shadow at at least one relevant immission location (11, I2, I3; I4, I5, I6, I7, I8, I9) in the vicinity of the wind turbine (10; 60, 62), wherein the shutdown of the wind turbine (10; 60, 62) is triggered by a signal that is generated at the relevant immission location ((I1, I2, I3; I4, I5, I6, I7, I8, I9) and is transmitted via a telephone or mobile network (42, 44) to a modem in communication with the shutdown system, wherein the signal can be generated by a resident as a resident signal when required if the shadow cast at the immission location (11, I2, I3; I4, I5, I6, I7, I8, I9) is considered a nuisance by the resident, characterised in that the resident signal comprises an identifier to identify or authenticate the resident, the identifier is compared with a set of stored identifiers, and a shutdown of the wind turbine (10; 60, 62) is triggered only if the identifier is one of the stored identifiers, wherein the identifiers are stored together with the respective associated immission location (11, I2, I3; I4, I5, I6, I7, I8, I9) in a memory of the shutdown system, and a shutdown of the wind turbine (10; 60, 62) is triggered only if the identifier is one of the stored identifiers and if a calculation performed by a computer of the shutdown system shows that the wind turbine (10; 60, 62) is casting a shadow at the immission location (11, I2, I3; I4, I5, I6, I7, I8, I9) associated with the identifier.
An optical gyro for measuring a rotation rate, the optical gyro comprising: a substrate comprising a silicon layer and an insulator layer; a first silicon waveguide formed on said insulator layer, said first silicon waveguide configured to propagate first and second light beams therethrough; and a ring resonator formed in said substrate, the ring resonator having first and second counter-propagating directions, said resonator being coupled to said first silicon waveguide, characterised by: the resonator comprising at least one reflecting element (20, 22, 24, 26), wherein said at least one reflecting element is configured to circulate a portion of said first light beam in said first counter-propagating direction and to circulate a portion of said second light beam in said second counter-propagating direction, each of said first and second counter-propagating directions having a resonance frequency for light propagation within said resonator, a difference between said resonance frequencies indicating the rotation rate. a substrate comprising a silicon layer and an insulator layer; a first silicon waveguide formed on said insulator layer, said first silicon waveguide configured to propagate first and second light beams therethrough; and a ring resonator formed in said substrate, the ring resonator having first and second counter-propagating directions, said resonator being coupled to said first silicon waveguide, the resonator comprising at least one reflecting element (20, 22, 24, 26), wherein said at least one reflecting element is configured to circulate a portion of said first light beam in said first counter-propagating direction and to circulate a portion of said second light beam in said second counter-propagating direction, each of said first and second counter-propagating directions having a resonance frequency for light propagation within said resonator, a difference between said resonance frequencies indicating the rotation rate.
An air cleaner (1-1; 1-2; 1-3; 1-4; 1-6) comprising a drone that a plurality of propellers (21, 22, 23, 24) that take in air from above and exhaust air below are disposed around a main body unit having a control unit that controls flying operations, and floats by propulsion of the plurality of propellers (21, 22, 23, 24); and a dust collector having a cylindrical dust collection electrode opened upward and downward, wherein the position where the dust collection electrode is arranged in the dust collector is set such that the central position in the height direction of the dust collection electrode is equal to or higher than the position of the rotational plane of the propellers (21, 22, 23, 24) and the lower end position of the dust collection electrode is equal to or lower than the position of an upper vicinity of the rotational plane of the propellers (21, 22, 23, 24), so that air can be taken into the dust collection electrode by rotational forces of the propellers (21, 22, 23, 24), wherein the dust collector further has an electric discharge electrode (41, 42, 43, 44) disposed in an approximately central site of the dust collection electrode for application of a high voltage between the dust collection electrode and the electric discharge electrode (41, 42, 43, 44) such that electric discharge occurs at a tip end portion of the electric discharge electrode (41, 42, 43, 44) to electrically charge and collect dust particles in the air that have flowed into the dust collection electrode, and the dust collector is assembled to the drone such that the electric discharge electrode (41, 42, 43, 44) is positioned at approximately the center above the drone. the position where the dust collection electrode is arranged in the dust collector is set such that the central position in the height direction of the dust collection electrode is equal to or higher than the position of the rotational plane of the propellers (21, 22, 23, 24) and the lower end position of the dust collection electrode is equal to or lower than the position of an upper vicinity of the rotational plane of the propellers (21, 22, 23, 24), so that air can be taken into the dust collection electrode by rotational forces of the propellers (21, 22, 23, 24), wherein the dust collector further has an electric discharge electrode (41, 42, 43, 44) disposed in an approximately central site of the dust collection electrode for application of a high voltage between the dust collection electrode and the electric discharge electrode (41, 42, 43, 44) such that electric discharge occurs at a tip end portion of the electric discharge electrode (41, 42, 43, 44) to electrically charge and collect dust particles in the air that have flowed into the dust collection electrode, and the dust collector is assembled to the drone such that the electric discharge electrode (41, 42, 43, 44) is positioned at approximately the center above the drone.
A method for compensating for spatial and slowness or angle blurring of plane-wave reflection coefficients in imaging, comprising: determining one or more source wave fields at a reference depth proximate to a reflector for one or more shot records; determining one or more receiver-side blurring functions at the reference depth, wherein a receiver-side blurring function is defined by B r x, z, x ", z R, t = W − † x z x r z r t a x r W − x r, z r, x ", z R, t where B r is a function of two depths, two lateral variables and time, W -(†) ( x,z,x r,z r,t) is the upgoing-wave propagator from the reflector to the receiver level and † denotes a time-reversed field, a ( x r) is a receiver aperture function of position x r at that level, and W - ( x r,z r,x",z R,t) is the back propagator from the receiver level to the reference depth and wherein the receiver-side blurring function is numerically estimated using a modelling engine for a given migration velocity model and acquisition geometry parameters by injecting a small source around or near the reflector, so that x" may be taken to characterize the location of the injected source; constructing an aggregate blurring function based at least partially on the one or more source wave fields and the one or more receiver-side blurring functions; and determining, using a processor, one or more plane-wave reflection coefficients based at least partially on the aggregate blurring function. determining one or more source wave fields at a reference depth proximate to a reflector for one or more shot records; determining one or more receiver-side blurring functions at the reference depth, wherein a receiver-side blurring function is defined by B r x, z, x ", z R, t = W − † x z x r z r t a x r W − x r, z r, x ", z R, t where B r is a function of two depths, two lateral variables and time, W -(†) ( x,z,x r,z r,t) is the upgoing-wave propagator from the reflector to the receiver level and † denotes a time-reversed field, a ( x r) is a receiver aperture function of position x r at that level, and W - ( x r,z r,x",z R,t) is the back propagator from the receiver level to the reference depth and wherein the receiver-side blurring function is numerically estimated using a modelling engine for a given migration velocity model and acquisition geometry parameters by injecting a small source around or near the reflector, so that x" may be taken to characterize the location of the injected source; constructing an aggregate blurring function based at least partially on the one or more source wave fields and the one or more receiver-side blurring functions; and determining, using a processor, one or more plane-wave reflection coefficients based at least partially on the aggregate blurring function.
A method for creating an image of a region of interest of a body comprising: transmitting a first ultrasonic pulse into the region of interest; sensing first received signals corresponding to ultrasonic energy from the first ultrasonic pulse reflected from within the region of interest; transmitting a second ultrasonic pulse into the region of interest; sensing second received signals corresponding to ultrasonic energy from the second ultrasonic pulse reflected from within the region of interest; and creating the image of the region of interest as a function of the first and second received signals; in which the second ultrasonic pulse is phase-shifted relative to the first ultrasonic pulse by an amount other than zero degrees and 180 degrees the method being CHARACTERISED BY: interleaving discrete representations of the first and second received signals to form a resultant operating signal; and creating the image as a function of the resultant operating signal. transmitting a first ultrasonic pulse into the region of interest; sensing first received signals corresponding to ultrasonic energy from the first ultrasonic pulse reflected from within the region of interest; transmitting a second ultrasonic pulse into the region of interest; sensing second received signals corresponding to ultrasonic energy from the second ultrasonic pulse reflected from within the region of interest; and creating the image of the region of interest as a function of the first and second received signals; in which the second ultrasonic pulse is phase-shifted relative to the first ultrasonic pulse by an amount other than zero degrees and 180 degrees the method being CHARACTERISED BY: interleaving discrete representations of the first and second received signals to form a resultant operating signal; and creating the image as a function of the resultant operating signal. interleaving discrete representations of the first and second received signals to form a resultant operating signal; and creating the image as a function of the resultant operating signal.
Method for producing a component from hardenable material, in a first step at least one layer (2, 3) of the material being printed in a 3D printing method, in a second step a plurality of similar bar-shaped reinforcement elements being inserted into the layer(s) (2, 3), and the two method steps being cyclically repeated until the component is complete, wherein the bar-shaped reinforcement elements are arranged in strands which extend through all the layers (2, 3), characterized in that, with the exception of the two lowermost and uppermost layers, each reinforcement element extends over at least three layers (2, 3), and the strands comprise at least three reinforcement elements in each layer (2, 3), the lateral spacing of which from one another within one strand is considerably smaller than the diameter of each reinforcement element.
A product performance prediction modeling method, comprising: acquiring first sample data, wherein the first sample data comprises device outlier data generated in a process of manufacturing a product by a device in case of device exception; acquiring a production line configuration simulation parameter of a production line where the device is located, and product information of the product manufactured by the production line; selecting, according to the device outlier data, the production line configuration simulation parameter and the product information, a product performance simulation model to perform simulation test on the performance of the product, so as to obtain product performance simulation data; and inputting the device outlier data, the production line configuration simulation parameter, the product information and the product performance simulation data into a machine learning model to perform machine learning training, so as to obtain a product performance prediction model to accurately predict the final product performance in time in case of device exception. acquiring first sample data, wherein the first sample data comprises device outlier data generated in a process of manufacturing a product by a device in case of device exception; acquiring a production line configuration simulation parameter of a production line where the device is located, and product information of the product manufactured by the production line; selecting, according to the device outlier data, the production line configuration simulation parameter and the product information, a product performance simulation model to perform simulation test on the performance of the product, so as to obtain product performance simulation data; and inputting the device outlier data, the production line configuration simulation parameter, the product information and the product performance simulation data into a machine learning model to perform machine learning training, so as to obtain a product performance prediction model to accurately predict the final product performance in time in case of device exception.
An optical coherence tomographic apparatus adapted to obtain a tomographic image of a fundus of an eye to be examined based on light obtained by combining return light from the eye irradiated with measurement light through a first lens and reference light corresponding to the measurement light, the apparatus comprising: scanning means (122-1, 122-2) provided on an optical path of the measurement light configured to scan the measurement light on the fundus; a second lens disposed between said scanning means (122-1, 122-2) and the first lens on the optical path of the measurement light; first optical path branching means disposed between the first lens and said second lens configured to make the optical path of the measurement light branch off to a fundus observation optical path for observation of the fundus; observation scanning means (117-1, 117-2) configured to scan observation light emitted from an observation light source on the fundus; and a third lens disposed between said observation scanning means (117-1, 117-2) and the first optical path branching means on the fundus observation optical path, characterized in that said first lens, said second lens, and said scanning means (122-1, 122-2) are disposed so as to make light parallel on the optical path of the measurement light between said first lens and said second lens, and to make an incident angle of the measurement light scanned by said scanning means (122-1, 122-2) on said first optical path branching means constant, and said first lens, said third lens, and said observation scanning means (117-1, 117-2) are disposed so as to make light parallel on the optical path of the observation light between said first lens and said third lens. scanning means (122-1, 122-2) provided on an optical path of the measurement light configured to scan the measurement light on the fundus; a second lens disposed between said scanning means (122-1, 122-2) and the first lens on the optical path of the measurement light; first optical path branching means disposed between the first lens and said second lens configured to make the optical path of the measurement light branch off to a fundus observation optical path for observation of the fundus; observation scanning means (117-1, 117-2) configured to scan observation light emitted from an observation light source on the fundus; and a third lens disposed between said observation scanning means (117-1, 117-2) and the first optical path branching means on the fundus observation optical path, characterized in that said first lens, said second lens, and said scanning means (122-1, 122-2) are disposed so as to make light parallel on the optical path of the measurement light between said first lens and said second lens, and to make an incident angle of the measurement light scanned by said scanning means (122-1, 122-2) on said first optical path branching means constant, and said first lens, said third lens, and said observation scanning means (117-1, 117-2) are disposed so as to make light parallel on the optical path of the observation light between said first lens and said third lens.
A polyolefin composition comprising: (a) From 10 weight percent to 50 weight percent of a thermoplastic olefin polymer having a density in the range of 0.85 g/cm 3 to 0.92 g/cm 3 and a flexural modulus of less than 700 MPa as measured by ISO 178:2010, which thermoplastic olefin polymer comprises a polypropylene and an olefin copolymer,, wherein the olefin copolymer is selected from the group consisting of: (i) a copolymer of ethylene with propylene or a CH 2 =CHR olefin where R is a 2-8 carbon alkyl radical, and optionally minor quantities of a diene, or (ii) a copolymer of ethylene, propylene, and a CH 2 =CHR olefin where R is a 2-8 carbon alkyl radical, and optionally minor quantities of a diene, the copolymers containing ethylene in a quantity from 16 weight percent to 85 weight percent and having solubility in xylene at room temperature greater than 70 weight percent; and (b) 50 weight percent to 90 weight percent of a polyethylene selected from the group consisting of (i) a high density polyethylene having a density of greater than or equal to 0.941 g/cm 3 and (ii) a medium density polyethylene having a density in the range of 0.926 g/cm 3 to 0.940 g/cm 3. (a) From 10 weight percent to 50 weight percent of a thermoplastic olefin polymer having a density in the range of 0.85 g/cm 3 to 0.92 g/cm 3 and a flexural modulus of less than 700 MPa as measured by ISO 178:2010, which thermoplastic olefin polymer comprises a polypropylene and an olefin copolymer,, wherein the olefin copolymer is selected from the group consisting of: (i) a copolymer of ethylene with propylene or a CH 2 =CHR olefin where R is a 2-8 carbon alkyl radical, and optionally minor quantities of a diene, or (ii) a copolymer of ethylene, propylene, and a CH 2 =CHR olefin where R is a 2-8 carbon alkyl radical, and optionally minor quantities of a diene, the copolymers containing ethylene in a quantity from 16 weight percent to 85 weight percent and having solubility in xylene at room temperature greater than 70 weight percent; and (i) a copolymer of ethylene with propylene or a CH 2 =CHR olefin where R is a 2-8 carbon alkyl radical, and optionally minor quantities of a diene, or (ii) a copolymer of ethylene, propylene, and a CH 2 =CHR olefin where R is a 2-8 carbon alkyl radical, and optionally minor quantities of a diene, the copolymers containing ethylene in a quantity from 16 weight percent to 85 weight percent and having solubility in xylene at room temperature greater than 70 weight percent; and (b) 50 weight percent to 90 weight percent of a polyethylene selected from the group consisting of (i) a high density polyethylene having a density of greater than or equal to 0.941 g/cm 3 and (ii) a medium density polyethylene having a density in the range of 0.926 g/cm 3 to 0.940 g/cm 3. (i) a high density polyethylene having a density of greater than or equal to 0.941 g/cm 3 and (ii) a medium density polyethylene having a density in the range of 0.926 g/cm 3 to 0.940 g/cm 3.