mhurhangee/ep-ind-claims huggingface dataset:
Fastening device for fastening an object to a wall, having a fastening element, a bearing element for bearing against the wall and a holding element at least for holding at least part of the object as well as a through opening running at least through the holding element and the bearing element to allow passage of the fastening element, characterised in that the bearing element and the holding element are connected to one another by way of a connecting element, the holding element, the connecting element and the bearing element together form a single-piece fastening unit and the connecting element is an eccentric.
Cover made of cast iron with at least one upper traffic surface subjected to wear, the traffic surface subjected to wear having an anti-slip property produced by fine structuring in the cast iron, the structuring having a groove height of 2 to 8 mm, and the traffic surface having a wear layer at least in parts and the wear layer being partially formed by chilling of the cast iron.
Portable device for externally starting up a computer installation, comprising: - a connection interface to the computer installation, - a data medium comprising data and executable codes (22a, 24a) of a host operating system that can be activated by a start-up program of the computer installation and configured to automatically detect hardware and/or software elements (12, 14, 16) of the computer installation and to activate corresponding computer drivers, characterized in that the data medium further comprises: - data and executable codes (22b, 24b) of a driving software interface that is configured to present the computer drivers that are activated by the host operating system in the form of at least one predetermined generic computer driver, and - data and executable codes (22c, 24c) of a guest operating system that can be activated by the driving software interface and configured to manage the hardware and/or software elements of the computer installation using the predetermined generic computer driver. - a connection interface to the computer installation, - a data medium comprising data and executable codes (22a, 24a) of a host operating system that can be activated by a start-up program of the computer installation and configured to automatically detect hardware and/or software elements (12, 14, 16) of the computer installation and to activate corresponding computer drivers, - data and executable codes (22b, 24b) of a driving software interface that is configured to present the computer drivers that are activated by the host operating system in the form of at least one predetermined generic computer driver, and - data and executable codes (22c, 24c) of a guest operating system that can be activated by the driving software interface and configured to manage the hardware and/or software elements of the computer installation using the predetermined generic computer driver.
A method of measuring the geometric characteristics of a crepe structure on a paper sheet, the method comprising the steps of: generating light intensity values representing characteristics of positions on a paper sheet by repeatedly emitting at least two emission beams against each of the positions on the paper sheet and reflecting the two beams off of the positions and into a sensor constructed and arranged to absorb and measure the intensity of the reflected emission beams, correcting the measured intensity of the light intensity values by using an n order polynomial fit by taking the point-by-point difference between the region of interest intensity values and the polynomial fit so that the mean of the corrected values approaches zero, performing a row-by-row pixel smoothing operation of the corrected light intensity values using a filter algorithm, identifying positive to negative transitions within the smoothed light intensity values, and correlating the identified transitions with previously identified values known to correspond to particular geometric dimensions to determine geometric features of the crepe structure. generating light intensity values representing characteristics of positions on a paper sheet by repeatedly emitting at least two emission beams against each of the positions on the paper sheet and reflecting the two beams off of the positions and into a sensor constructed and arranged to absorb and measure the intensity of the reflected emission beams, correcting the measured intensity of the light intensity values by using an n order polynomial fit by taking the point-by-point difference between the region of interest intensity values and the polynomial fit so that the mean of the corrected values approaches zero, performing a row-by-row pixel smoothing operation of the corrected light intensity values using a filter algorithm, identifying positive to negative transitions within the smoothed light intensity values, and correlating the identified transitions with previously identified values known to correspond to particular geometric dimensions to determine geometric features of the crepe structure.
A lift mechanism comprising: a first leg assembly, the first leg assembly including: a first member; and a second member moveable relative to the first member along a first longitudinal axis; a second leg assembly, the second leg assembly including: a third member; and a fourth member moveable relative to the third member along a second longitudinal axis; a first pulley rotationally attached near the top of the second member; a second pulley rotationally attached near the top of the second member; a third pulley rotationally attached near the bottom of the second member; and a synchronization assembly connecting the first and second leg assemblies, the synchronization assembly configured to balance movement between the first and second leg assemblies, the synchronization assembly including a first tension member and a second tension member; a wheel assembly connected to the first tension member and the second tension member, the first tension member connected to at least one of the first leg assembly and the second leg assembly and the second tension member connected at least one of the first leg assembly and the second leg assembly;a third tension member connected to the wheel assembly; and a fourth tension member connected to the wheel assembly; wherein the first tension member extends around the first pulley and the third pulley and is attached to the first member. a first leg assembly, the first leg assembly including: a first member; and a second member moveable relative to the first member along a first longitudinal axis; a first member; and a second member moveable relative to the first member along a first longitudinal axis; a second leg assembly, the second leg assembly including: a third member; and a fourth member moveable relative to the third member along a second longitudinal axis; a third member; and a fourth member moveable relative to the third member along a second longitudinal axis; a first pulley rotationally attached near the top of the second member; a second pulley rotationally attached near the top of the second member; a third pulley rotationally attached near the bottom of the second member; and a synchronization assembly connecting the first and second leg assemblies, the synchronization assembly configured to balance movement between the first and second leg assemblies, the synchronization assembly including a first tension member and a second tension member; a wheel assembly connected to the first tension member and the second tension member, the first tension member connected to at least one of the first leg assembly and the second leg assembly and the second tension member connected at least one of the first leg assembly and the second leg assembly;a third tension member connected to the wheel assembly; and a fourth tension member connected to the wheel assembly; wherein the first tension member extends around the first pulley and the third pulley and is attached to the first member.
A stented valve comprising: a stent structure (10, 20, 30, 40) comprising a generally tubular body portion having a first end (12, 22) and a second end (14, 24), and a valve structure attached within the generally tubular body portion, wherein the first end (12, 22) of the stent structure (10, 20, 30, 40) is an inflow end and the second end (14, 24) of the stent structure (10, 20, 30, 40) is an outflow end, wherein the stent structure (10, 20, 30, 40) comprises a number of strut or wire portions, wherein the arrangement of wires provides twelve crowns at the inflow end of the stent structure, wherein the stent structure (10, 20, 30, 40) further provides twelve or less crowns at the outflow end of the stent structure (10, 20, 30, 40), and wherein the stent structure comprises a plurality of longitudinally extending wires, wherein the plurality of wires includes multiple commissure wires and at least one structural wire positioned between each two adjacent commissure wires, and wherein a wire structure extends between one end of the longitudinal wires and the first end (12, 22) and an additional wire structure extends between the other end of the longitudinal wires and the second end (14, 24), characterized in that the stent structure (10, 20, 30, 40) is provided with a lower density wire portion formed by the longitudinally extending wires, wherein the lower density wire portion is provided in the area of the stent structure (10, 20, 30, 40) positioned where the coronary arteries are located when the stent structure (10, 20, 30, 40) is implanted. a stent structure (10, 20, 30, 40) comprising a generally tubular body portion having a first end (12, 22) and a second end (14, 24), and a valve structure attached within the generally tubular body portion, wherein the first end (12, 22) of the stent structure (10, 20, 30, 40) is an inflow end and the second end (14, 24) of the stent structure (10, 20, 30, 40) is an outflow end, wherein the stent structure (10, 20, 30, 40) comprises a number of strut or wire portions, wherein the arrangement of wires provides twelve crowns at the inflow end of the stent structure, wherein the stent structure (10, 20, 30, 40) further provides twelve or less crowns at the outflow end of the stent structure (10, 20, 30, 40), and wherein the stent structure comprises a plurality of longitudinally extending wires, wherein the plurality of wires includes multiple commissure wires and at least one structural wire positioned between each two adjacent commissure wires, and wherein a wire structure extends between one end of the longitudinal wires and the first end (12, 22) and an additional wire structure extends between the other end of the longitudinal wires and the second end (14, 24), characterized in that the stent structure (10, 20, 30, 40) is provided with a lower density wire portion formed by the longitudinally extending wires, wherein the lower density wire portion is provided in the area of the stent structure (10, 20, 30, 40) positioned where the coronary arteries are located when the stent structure (10, 20, 30, 40) is implanted.
A composition comprising a peptide vaccine for use in a method of inducing an immune response to a tumor characterized as having an IHC of 0 or 1+ for FRa protein expression in a human subject, wherein the peptide vaccine comprises about 1.0 mg of a peptide comprising the amino acid sequence of SEQ ID NO: 1 and an adjuvant and is administered to the subject every 3 to 4 weeks for a period of at least about six months.
A system for transmitting, the system comprising: a physical adequacy block followed by an analog front-end configured to process data in a plurality of frequency bands, wherein data in each band is processed separately, and wherein each frequency band has an associated symbol time, and each associated symbol time is a whole multiple of one half of a smallest symbol time of all of the frequency bands, and wherein the system uses a fast Fourier transform, FFT, block to make the shift between frequency and time; a signal combiner block configured to combine the data in the plurality of frequency bands into a single signal for simultaneous transmission on a transmission medium, and wherein the said fast Fourier transform, FFT, block is reused for all the frequency bands and is configured to (i) process a symbol of a first frequency band in the plurality of frequency bands, the said first frequency band being the band with the lowest frequency and, subsequently, one after another, process two or more symbols of the other frequency bands of the plurality of frequency bands according to the ratios between the associated symbol times of the each other frequency band of the plurality of frequency bands and the first band, and (ii) distribute data in a corresponding fashion, a physical adequacy block followed by an analog front-end configured to process data in a plurality of frequency bands, wherein data in each band is processed separately, and wherein each frequency band has an associated symbol time, and each associated symbol time is a whole multiple of one half of a smallest symbol time of all of the frequency bands, and wherein the system uses a fast Fourier transform, FFT, block to make the shift between frequency and time; a signal combiner block configured to combine the data in the plurality of frequency bands into a single signal for simultaneous transmission on a transmission medium, and wherein the said fast Fourier transform, FFT, block is reused for all the frequency bands and is configured to (i) process a symbol of a first frequency band in the plurality of frequency bands, the said first frequency band being the band with the lowest frequency and, subsequently, one after another, process two or more symbols of the other frequency bands of the plurality of frequency bands according to the ratios between the associated symbol times of the each other frequency band of the plurality of frequency bands and the first band, and (ii) distribute data in a corresponding fashion,
A method for monitoring the state of a tower of a wind turbine, wherein the method comprises: collecting data of a state monitoring system, wherein the state monitoring system is provided for a structure of the wind turbine which is mechanically coupled to the tower; processing the collected data of the state monitoring system which is provided for the structure of the wind turbine which is mechanically coupled to the tower; and determining a state of the tower from the processed data of the state monitoring system which is provided for the structure of the wind turbine which is mechanically coupled to the tower, characterized in that the structure is at least a rotor blade, a rotor, or a hub of the wind turbine. collecting data of a state monitoring system, wherein the state monitoring system is provided for a structure of the wind turbine which is mechanically coupled to the tower; processing the collected data of the state monitoring system which is provided for the structure of the wind turbine which is mechanically coupled to the tower; and determining a state of the tower from the processed data of the state monitoring system which is provided for the structure of the wind turbine which is mechanically coupled to the tower, characterized in that the structure is at least a rotor blade, a rotor, or a hub of the wind turbine.
A full-length antibody capable of specifically binding to an affinity complex, wherein the antibody has a variable region of a chicken immunoglobulin, wherein the affinity complex comprises a small substance and a protein, wherein the small substance is 25OH vitamin D3 and/or 25OH vitamin D2, wherein the protein is an antibody to the 250H vitamin D3 and/or 25OH vitamin D2.
A process for preparing a reverse osmosis membrane, comprising: providing a polyamine, a polyfunctional acid halide, and a flux increasing additive having the formula Z + B -, where Z + has the formula R 1 R 2 R 3 R 4 N +, where R 1, R 2, R 3, and R 4, independently, are H, a C 1 -C 6 hydrocarbyl group, a benzyl group, or a phenyl group and B - is a beta-diketonate; combining the polyamine, polyfunctional acid halide, and flux increasing additive on the surface of a porous support membrane; and interfacially polymerizing the polyamine and the polyfunctional acid halide, and flux increasing additive on the surface of the porous support membrane to form a reverse osmosis membrane comprising (i) the porous support membrane and (ii) a discrimination layer comprising a polyamide, wherein the reverse osmosis membrane is characterized by a flux that is greater than the flux of the same membrane prepared in the absence of the flux increasing additive. providing a polyamine, a polyfunctional acid halide, and a flux increasing additive having the formula Z + B -, where Z + has the formula R 1 R 2 R 3 R 4 N +, where R 1, R 2, R 3, and R 4, independently, are H, a C 1 -C 6 hydrocarbyl group, a benzyl group, or a phenyl group and B - is a beta-diketonate; combining the polyamine, polyfunctional acid halide, and flux increasing additive on the surface of a porous support membrane; and interfacially polymerizing the polyamine and the polyfunctional acid halide, and flux increasing additive on the surface of the porous support membrane to form a reverse osmosis membrane comprising (i) the porous support membrane and (ii) a discrimination layer comprising a polyamide,
Cantilever for a piezoelectric energy harvesting system, wherein the cantilever (2,20,30) comprises two layers (21,22,31,32) formed of polyvinylidene fluoride, and wherein a core layer (23,33) formed of a shim material is sandwiched between the two layers (21,22,31,32) formed of polyvinylidene fluoride, characterized in that the two layers (21,22,31,32) formed of polyvinylidene fluoride respectively have a predominantly β-type crystal structure, wherein the two layers formed of polyvinylidene fluoride (21,22,31,32) respectively have a length between 60mm and 80mm and a width between 10mm and 20mm.
A hazard detection system, comprising: a housing; a fire detector disposed within the housing and adapted to generate a detection signal in response to a detection of a fire condition; a pressure tube having an internal pressure, wherein at least a portion of the pressure tube is configured to leak in response to exposure to heat, wherein the leak changes the internal pressure and generates a pneumatic signal; and a pressure control valve coupled to the fire detector and to the pressure tube and disposed within the housing, wherein the pressure control valve is configured to: maintain an internal pressure inside the pressure tube; and change the internal pressure of the pressure tube and generate the pneumatic signal in response to the detection signal to activate a fire control system. a housing; a fire detector disposed within the housing and adapted to generate a detection signal in response to a detection of a fire condition; a pressure tube having an internal pressure, wherein at least a portion of the pressure tube is configured to leak in response to exposure to heat, wherein the leak changes the internal pressure and generates a pneumatic signal; and a pressure control valve coupled to the fire detector and to the pressure tube and disposed within the housing, wherein the pressure control valve is configured to: maintain an internal pressure inside the pressure tube; and change the internal pressure of the pressure tube and generate the pneumatic signal in response to the detection signal to activate a fire control system.
A method for testing a fuel tank for an aircraft at a phase of manufacturing, the method comprising: sending electrical power to an optical data concentrator for the fuel tank for the aircraft, the optical data concentrator being located outside the fuel tank,from a power supply such that the optical data concentrator sends optical signals to optical sensors installed inside the fuel tank through optical fibers connecting the optical data concentrator to the optical sensors inside the fuel tank, wherein the electrical power is sent during the phase of manufacturing of the aircraft, converting, by photovoltaic converters located within each of the optical sensors, the optical signals sent by the optical data concentrator into electrical power in order to power the respective optical sensors; receiving, by a computer system in communication with the optical data concentrator, test data from the optical data concentrator, wherein the test data is based on optical response signals received from the optical sensors; determining, by the computer system, states for the optical sensors using the test data; and displaying, by the computer system a graphical indication of the states determined for the optical sensors in the fuel tank in a graphical user interface on a display system wherein the powered optical sensor is configured to automatically start producing raw sensor data, convert the raw sensor data back into an optical signal, and transmit the converted optical signal back to the optical fuel quantity data concentrator. sending electrical power to an optical data concentrator for the fuel tank for the aircraft, the optical data concentrator being located outside the fuel tank,from a power supply such that the optical data concentrator sends optical signals to optical sensors installed inside the fuel tank through optical fibers connecting the optical data concentrator to the optical sensors inside the fuel tank, wherein the electrical power is sent during the phase of manufacturing of the aircraft, converting, by photovoltaic converters located within each of the optical sensors, the optical signals sent by the optical data concentrator into electrical power in order to power the respective optical sensors; receiving, by a computer system in communication with the optical data concentrator, test data from the optical data concentrator, wherein the test data is based on optical response signals received from the optical sensors; determining, by the computer system, states for the optical sensors using the test data; and displaying, by the computer system a graphical indication of the states determined for the optical sensors in the fuel tank in a graphical user interface on a display system wherein the powered optical sensor is configured to automatically start producing raw sensor data, convert the raw sensor data back into an optical signal, and transmit the converted optical signal back to the optical fuel quantity data concentrator.