mhurhangee/ep-ind-claims huggingface dataset:
An apparatus for detecting a faulty antenna among a plurality of antennas contained in a communication device, comprising: a measurer adapted to measure signal strengths of signals obtained from the plurality of antennas each; a calculator adapted to calculate differences between each two of the measured signal strengths; a first comparator adapted to compare each of the calculated differences with a first predetermined threshold value; and a first decider adapted to decide, among the plurality of antennas, an antenna to be faulty on the basis of a respective result of the comparison; wherein the first decider comprises: a counter adapted to count a number of differences related to each of the measured signal strengths which are greater than the first predetermined threshold value; a second comparator adapted to compare the number of differences with a second predetermined threshold value; and a second decider adapted to decide, among the plurality of antennas, an antenna related to the number of differences which is greate than the second predetermined threshold value to be faulty. a measurer adapted to measure signal strengths of signals obtained from the plurality of antennas each; a calculator adapted to calculate differences between each two of the measured signal strengths; a first comparator adapted to compare each of the calculated differences with a first predetermined threshold value; and a first decider adapted to decide, among the plurality of antennas, an antenna to be faulty on the basis of a respective result of the comparison; wherein the first decider comprises: a counter adapted to count a number of differences related to each of the measured signal strengths which are greater than the first predetermined threshold value; a second comparator adapted to compare the number of differences with a second predetermined threshold value; and a second decider adapted to decide, among the plurality of antennas, an antenna related to the number of differences which is greate than the second predetermined threshold value to be faulty. a counter adapted to count a number of differences related to each of the measured signal strengths which are greater than the first predetermined threshold value; a second comparator adapted to compare the number of differences with a second predetermined threshold value; and a second decider adapted to decide, among the plurality of antennas, an antenna related to the number of differences which is greate than the second predetermined threshold value to be faulty.
A compound having the following structure, or a pharmaceutically acceptable salt thereof: wherein Y 1 is C or N; Z is NO 2 or CN; each R 1 is independently H, halogen, OH, CN, (C 1 -C 6)alkyl, (C 2 -C 6)alkenyl, (C 2 -C 6) alkynyl, (C 1 -C 6) alkoxy, (C 3 -C 7)cycloalkyl, (C 1 -C 6)alkylthio, NR a R b or haloalkyl; each occurrence of R a and R b is independently hydrogen or (C 1 -C 6)alkyl, or R a and R b, form a saturated or unsaturated heterocyclic ring containing from three to seven ring atoms, which ring may optionally contain another heteroatom selected from the group consisting of nitrogen, oxygen and sulfur and may be optionally substituted by from one to three groups which may be the same or different selected from the group consisting of (C 1 -C 4)alkyl, phenyl and benzyl; each R 2 and R 3 is independently H, halogen, OH, or CN; m is 1-4; and n is 1-5; provided the compound is not: 2-(4-chlorophenyl)-3-(2-nitro-1-phenylethyl)-1 H -indole or 3-(2-nitro-1-phenylethyl)-2-phenyl-1 H -indole or 2-(4-chlorophenyl)-3-(1-(2,4-dichlorophenyl)-2-nitroethyl)-1 H -indole or 2-(4-chlorophenyl)-3-(1-(4-chlorophenyl)-2-nitroethyl)-1 H -indole or 3-(1-(2,4-dichlorophenyl)-2-nitroethyl)-2-phenyl-1 H -indole or 3-(1-(4-fluorophenyl)-2-nitroethyl)-2-phenyl-1 H -indole or 3-[1-(4-chlorophenyl)-2-nitroethyl]-2-phenyl-1H-indole. wherein Y 1 is C or N; Z is NO 2 or CN; each R 1 is independently H, halogen, OH, CN, (C 1 -C 6)alkyl, (C 2 -C 6)alkenyl, (C 2 -C 6) alkynyl, (C 1 -C 6) alkoxy, (C 3 -C 7)cycloalkyl, (C 1 -C 6)alkylthio, NR a R b or haloalkyl; each occurrence of R a and R b is independently hydrogen or (C 1 -C 6)alkyl, or R a and R b, form a saturated or unsaturated heterocyclic ring containing from three to seven ring atoms, which ring may optionally contain another heteroatom selected from the group consisting of nitrogen, oxygen and sulfur and may be optionally substituted by from one to three groups which may be the same or different selected from the group consisting of (C 1 -C 4)alkyl, phenyl and benzyl; each R 2 and R 3 is independently H, halogen, OH, or CN; m is 1-4; and n is 1-5; provided the compound is not: 2-(4-chlorophenyl)-3-(2-nitro-1-phenylethyl)-1 H -indole or 3-(2-nitro-1-phenylethyl)-2-phenyl-1 H -indole or 2-(4-chlorophenyl)-3-(1-(2,4-dichlorophenyl)-2-nitroethyl)-1 H -indole or 2-(4-chlorophenyl)-3-(1-(4-chlorophenyl)-2-nitroethyl)-1 H -indole or 3-(1-(2,4-dichlorophenyl)-2-nitroethyl)-2-phenyl-1 H -indole or 3-(1-(4-fluorophenyl)-2-nitroethyl)-2-phenyl-1 H -indole or 3-[1-(4-chlorophenyl)-2-nitroethyl]-2-phenyl-1H-indole. 2-(4-chlorophenyl)-3-(2-nitro-1-phenylethyl)-1 H -indole or 3-(2-nitro-1-phenylethyl)-2-phenyl-1 H -indole or 2-(4-chlorophenyl)-3-(1-(2,4-dichlorophenyl)-2-nitroethyl)-1 H -indole or 2-(4-chlorophenyl)-3-(1-(4-chlorophenyl)-2-nitroethyl)-1 H -indole or 3-(1-(2,4-dichlorophenyl)-2-nitroethyl)-2-phenyl-1 H -indole or 3-(1-(4-fluorophenyl)-2-nitroethyl)-2-phenyl-1 H -indole or 3-[1-(4-chlorophenyl)-2-nitroethyl]-2-phenyl-1H-indole.
A two-stroke cycle, compression-ignition, opposed-piston engine including at least one cylinder with longitudinally-separated exhaust and intake ports, a pair of pistons (60, 62) disposed in opposition to one another in a bore of the cylinder and a fuel injection system for injecting fuel into the bore between the end surfaces of the pistons, characterized in that: the fuel injection system includes at least two fuel injectors (68, 70) mounted to the cylinder for injecting fuel into the bore; and the engine includes an engine control unit capable of varying the reactivity of fuel by causing injection of predetermined charges of low reactivity fuel and high reactivity fuel in response to engine conditions. the fuel injection system includes at least two fuel injectors (68, 70) mounted to the cylinder for injecting fuel into the bore; and the engine includes an engine control unit capable of varying the reactivity of fuel by causing injection of predetermined charges of low reactivity fuel and high reactivity fuel in response to engine conditions.
Retention system for a load carrying container, comprising a retention portion arrangeable at or near a rear end of a load carrying container, which retention portion is pivotable between a first, raised position and a second, lowered position; and a drive element for moving the pivotable retention portion between the first and second positions, characterized in that the retention portion constitutes an end portion of a lining of the load carrying container, wherein the end portion of the lining constituted by the retention portion is not attached to a base of the load carrying container, contrary to the remaining portion of the lining, and wherein the retention portion is made of an elastic material. a retention portion arrangeable at or near a rear end of a load carrying container, which retention portion is pivotable between a first, raised position and a second, lowered position; and a drive element for moving the pivotable retention portion between the first and second positions, characterized in that the retention portion constitutes an end portion of a lining of the load carrying container, wherein the end portion of the lining constituted by the retention portion is not attached to a base of the load carrying container, contrary to the remaining portion of the lining, and wherein the retention portion is made of an elastic material.
A pressure sensitive adhesive composition comprising a polyurethane polymer that comprises the reaction product of a polyisocyanate component and a polyol component; wherein the polyol component has a total solubility parameter ranging from 10 to 14 (cal/cm 3) 1/2, and wherein the pressure sensitive adhesive has a G' less than 1 MPa at 25°C and a frequency of 1 hertz.
Gas turbine assembly comprising: an outer casing; at least one vane carrier (10; 20) extending along a longitudinal axis and provided with at least one annular seat; and at least one governing ring (28; 128) housed in the annular seat; the gas turbine assembly being characterized in that the at least one governing ring (28; 128) is provided with a plurality of clearance control cavities (29; 140) distributed along a circumferential direction; wherein each clearance control cavity (29; 140) extends along an axis which is transversal with respect to the longitudinal axis; wherein each clearance control cavity (29; 140) is defined by a through hole made into the governing ring (28; 128) extending from an outer surface of the governing ring (28; 128), which faces in use the outer casing and an inner surface of the governing ring (28; 128), which faces in use the annular seat of the vane carrier or by a cylindrical blind hole extending from the outer surface of the governing ring (28; 128); wherein each clearance control cavity (29; 140) has at least one inlet connected to a source of control fluid. an outer casing; at least one vane carrier (10; 20) extending along a longitudinal axis and provided with at least one annular seat; and at least one governing ring (28; 128) housed in the annular seat; the gas turbine assembly being characterized in that the at least one governing ring (28; 128) is provided with a plurality of clearance control cavities (29; 140) distributed along a circumferential direction; wherein each clearance control cavity (29; 140) extends along an axis which is transversal with respect to the longitudinal axis; wherein each clearance control cavity (29; 140) is defined by a through hole made into the governing ring (28; 128) extending from an outer surface of the governing ring (28; 128), which faces in use the outer casing and an inner surface of the governing ring (28; 128), which faces in use the annular seat of the vane carrier or by a cylindrical blind hole extending from the outer surface of the governing ring (28; 128); wherein each clearance control cavity (29; 140) has at least one inlet connected to a source of control fluid.
A system for providing a prescribed amount of stimulation to a patient, the system comprising: an implantable stimulator device that is implantable in the patient and an external controller configured to control the implantable stimulator device, wherein the external controller is configured to: receive a prescription for stimulation from a clinician programmer, wherein the prescription quantifies a prescribed amount of stimulation that can be provided before an additional prescription is required for further stimulation, instruct the implantable stimulator device to provide stimulation, track the provided stimulation to determine an amount of provided stimulation, determine a difference between the prescribed amount of stimulation and the amount of provided stimulation, wherein the difference indicates the amount of stimulation remaining on the prescription, and when there is no stimulation remaining on the prescription, provide an indication prompting the patient to seek a further prescription from the clinician. receive a prescription for stimulation from a clinician programmer, wherein the prescription quantifies a prescribed amount of stimulation that can be provided before an additional prescription is required for further stimulation, instruct the implantable stimulator device to provide stimulation, track the provided stimulation to determine an amount of provided stimulation, determine a difference between the prescribed amount of stimulation and the amount of provided stimulation, wherein the difference indicates the amount of stimulation remaining on the prescription, and when there is no stimulation remaining on the prescription, provide an indication prompting the patient to seek a further prescription from the clinician.
A method for estimating a motion vector of a pixel block comprising: obtaining a plurality of candidate motion vectors of a current pixel block in a current video frame, the plurality of candidate motion vectors comprising at least a down-sampled candidate motion vector, characterized in that, the down-sampled candidate motion vector is obtained by obtaining a down-sampled frame image of the current video frame, dividing the down-sampled frame image into a plurality of candidate blocks of a same size, calculating a block matching error between each candidate block in a search region in the down-sampled frame image and the current pixel block, determining a target candidate block having a minimum matching error with respect to the current pixel block, and estimating a motion vector between the current pixel block and the target candidate block as the down-sampled candidate motion vector; calculating a confidence degree of each of other candidate motion vectors except for the down-sampled candidate motion vector in the plurality of candidate motion vectors with respect to the down-sampled candidate motion vector, wherein the confidence degree is a confidence degree for a difference value between the down-sampled candidate motion vector and each of the other candidate motion vectors; and determining the candidate motion vector in the other candidate motion vectors which has a highest confidence degree with respect to the down-sampled candidate motion vector as the motion vector of the current pixel block. obtaining a plurality of candidate motion vectors of a current pixel block in a current video frame, the plurality of candidate motion vectors comprising at least a down-sampled candidate motion vector, characterized in that, the down-sampled candidate motion vector is obtained by obtaining a down-sampled frame image of the current video frame, dividing the down-sampled frame image into a plurality of candidate blocks of a same size, calculating a block matching error between each candidate block in a search region in the down-sampled frame image and the current pixel block, determining a target candidate block having a minimum matching error with respect to the current pixel block, and estimating a motion vector between the current pixel block and the target candidate block as the down-sampled candidate motion vector; calculating a confidence degree of each of other candidate motion vectors except for the down-sampled candidate motion vector in the plurality of candidate motion vectors with respect to the down-sampled candidate motion vector, wherein the confidence degree is a confidence degree for a difference value between the down-sampled candidate motion vector and each of the other candidate motion vectors; and determining the candidate motion vector in the other candidate motion vectors which has a highest confidence degree with respect to the down-sampled candidate motion vector as the motion vector of the current pixel block.
A drain valve of an air-oil separator configured to separate oil aerosol from blow-by gas of an internal combustion engine, and discharge separated oil from a drainpipe into the engine, while supplying the gas, from which the oil aerosol is separated, to an intake, the drain valve comprising: a plug including a longitudinal axis and an outer plug wall extending upward from a lower plug wall, the outer plug wall configured to extend upward along a drainpipe exterior, the outer plug wall configured to establish at least a portion of a seal recess; a plurality of fingers (37A-37D) joined with the plug and configured to extend upward along a drainpipe interior the plurality of fingers (37A-37D) separated from one another by at least one flow path configured to allow a flow of oil therein; and a floating plate movably constrained in the drainpipe interior above the plurality of fingers (37A-37D), the floating plate operable in an open mode to allow flow of oil through the flow path, the floating plate operable in a closed mode to impair flow of oil through the flow path. a plug including a longitudinal axis and an outer plug wall extending upward from a lower plug wall, the outer plug wall configured to extend upward along a drainpipe exterior, the outer plug wall configured to establish at least a portion of a seal recess; a plurality of fingers (37A-37D) joined with the plug and configured to extend upward along a drainpipe interior the plurality of fingers (37A-37D) separated from one another by at least one flow path configured to allow a flow of oil therein; and a floating plate movably constrained in the drainpipe interior above the plurality of fingers (37A-37D), the floating plate operable in an open mode to allow flow of oil through the flow path, the floating plate operable in a closed mode to impair flow of oil through the flow path.
A braking system for a dual landing gear aircraft comprising left and right landing gears each with fore and aft inboard wheels and fore and aft outboard wheels, the braking system comprising: an outboard brake system control unit comprising at least a first processing circuit that generates brake control signals to symmetrically control braking of a first wheel pair comprising just the outboard fore wheels and a second wheel pair comprising just the outboard aft wheels in response to pilot input; an inboard brake system control unit comprising at least a second processing circuit that generates brake control signals to symmetrically control braking of a third wheel pair comprising just the inboard fore wheels and a fourth wheel pair comprising just the inboard aft wheels in response to the pilot input, the inboard brake system control unit being independent from the outboard brake system control unit; and a hydraulic system that applies braking forces to the wheels in response to the brake control signals, wherein the inboard and outboard braking system control units (20, 30) further comprise input interfaces that receive the pilot input with the pilot input comprising separate first and second inputs. an outboard brake system control unit comprising at least a first processing circuit that generates brake control signals to symmetrically control braking of a first wheel pair comprising just the outboard fore wheels and a second wheel pair comprising just the outboard aft wheels in response to pilot input; an inboard brake system control unit comprising at least a second processing circuit that generates brake control signals to symmetrically control braking of a third wheel pair comprising just the inboard fore wheels and a fourth wheel pair comprising just the inboard aft wheels in response to the pilot input, the inboard brake system control unit being independent from the outboard brake system control unit; and a hydraulic system that applies braking forces to the wheels in response to the brake control signals, wherein the inboard and outboard braking system control units (20, 30) further comprise input interfaces that receive the pilot input with the pilot input comprising separate first and second inputs.
An intraoperative dynamic trialing system for a knee joint, comprising: a tibial trial (300, 500, 600, 700, 800, 900a, 1000a, 1100, 1200) including: a first condylar portion; a second condylar portion; and a bridge connecting anterior ends of the first and second condylar portions; a femoral implant; and a tibial implant; characterized in that proximal surfaces of the first and second condylar portions each include a groove (310, 320, 714, 715, 814, 815, 914, 915, 1040a, 1050a, 1114, 1115, 1224) corresponding to an articular dish of the tibial implant and the grooves (310, 320) are shaped to articulate with a preliminary resected surface of a distal femur, and wherein the tibial implant is configured to articulate with the femoral implant configured to be implanted onto a final resected surface of the distal femur, a portion of the preliminary and final resected surfaces being offset between 2mm and 3mm. a tibial trial (300, 500, 600, 700, 800, 900a, 1000a, 1100, 1200) including: a first condylar portion; a second condylar portion; and a bridge connecting anterior ends of the first and second condylar portions; a first condylar portion; a second condylar portion; and a bridge connecting anterior ends of the first and second condylar portions; a femoral implant; and a tibial implant; characterized in that proximal surfaces of the first and second condylar portions each include a groove (310, 320, 714, 715, 814, 815, 914, 915, 1040a, 1050a, 1114, 1115, 1224) corresponding to an articular dish of the tibial implant and the grooves (310, 320) are shaped to articulate with a preliminary resected surface of a distal femur, and wherein the tibial implant is configured to articulate with the femoral implant configured to be implanted onto a final resected surface of the distal femur, a portion of the preliminary and final resected surfaces being offset between 2mm and 3mm.
A hardness tester that loads a predetermined test force and forms an indentation in a surface of a sample using an indenter, and measures the hardness of the sample by measuring dimensions of the indentation, the hardness tester comprising a processor and a memory that stores an instruction, the processor being configured to execute the instructions stored in the memory so as to serve as: an image acquirer that acquires (S1, S3) an image of the surface of the sample before and after the indentation is formed, characterized in that the processor is further configured to execute the instructions stored in the memory so as to serve as: a plurality of indentation region extractors that use mutually distinct methods, each indentation region extractor of the plurality of indentation region extractors configured to extract (S4, S6, S8) an indentation region based on the images acquired by the image acquirer; a determiner that determines (S5, S7, S9) whether the indentation region extracted by the plurality of indentation region extractors matches a predefined reference indentation condition; and a hardness calculator that calculates the hardness of the sample based on an indentation region that is determined by the determiner to match the predefined reference indentation condition, wherein: the plurality of indentation region extractors are arranged in a predefined execution hierarchy configured to execute the indentation region extraction process, and the determiner determines whether the reference indentation condition is matched each time an indentation region is extracted by one of the plurality of indentation region extractors in accordance with the execution hierarchy. a plurality of indentation region extractors that use mutually distinct methods, each indentation region extractor of the plurality of indentation region extractors configured to extract (S4, S6, S8) an indentation region based on the images acquired by the image acquirer; a determiner that determines (S5, S7, S9) whether the indentation region extracted by the plurality of indentation region extractors matches a predefined reference indentation condition; and a hardness calculator that calculates the hardness of the sample based on an indentation region that is determined by the determiner to match the predefined reference indentation condition, wherein: the plurality of indentation region extractors are arranged in a predefined execution hierarchy configured to execute the indentation region extraction process, and the determiner determines whether the reference indentation condition is matched each time an indentation region is extracted by one of the plurality of indentation region extractors in accordance with the execution hierarchy. the plurality of indentation region extractors are arranged in a predefined execution hierarchy configured to execute the indentation region extraction process, and the determiner determines whether the reference indentation condition is matched each time an indentation region is extracted by one of the plurality of indentation region extractors in accordance with the execution hierarchy.