mhurhangee/ep-ind-claims huggingface dataset:
A laser beam amplification device comprising: a laser medium unit; an excitation light source configured to cause excitation light to enter the laser medium unit; and a cooling medium flow path configured to be arranged around the laser medium unit, wherein the laser beam amplification device amplifies and outputs a laser beam input to the laser medium unit; wherein the laser medium unit comprises: a plate-like first laser medium, a plate-like second laser medium, and a sealing material arranged between the first and the second laser media; wherein the first and the second laser media are aligned along a thickness direction of the first and the second laser media; and wherein a space between the first and the second laser media is a sealed space and is under a reduced pressure environment or is filled with gas and the cooling medium flow path is configured to cool the laser medium unit from outside. a laser medium unit; an excitation light source configured to cause excitation light to enter the laser medium unit; and a cooling medium flow path configured to be arranged around the laser medium unit, wherein the laser beam amplification device amplifies and outputs a laser beam input to the laser medium unit; wherein the laser medium unit comprises: a plate-like first laser medium, a plate-like second laser medium, and a sealing material arranged between the first and the second laser media; wherein the first and the second laser media are aligned along a thickness direction of the first and the second laser media; and wherein a space between the first and the second laser media is a sealed space and is under a reduced pressure environment or is filled with gas and the cooling medium flow path is configured to cool the laser medium unit from outside. a plate-like first laser medium, a plate-like second laser medium, and a sealing material arranged between the first and the second laser media; wherein the first and the second laser media are aligned along a thickness direction of the first and the second laser media; and wherein a space between the first and the second laser media is a sealed space and is under a reduced pressure environment or is filled with gas and the cooling medium flow path is configured to cool the laser medium unit from outside.
A releasable clip, suitable for securing two panels of a knock-down structure to one another, the releasable clip including: two legs (21, 23) extending away from one another, the legs (21, 23) being connected at one end (21.1, 23.1), with each leg (21, 23) having an opposite free end (21.2, 23.2) that terminates in a panel engagement formation (22, 24); wherein at least one of the panel engagement formations (22, 24) is an adjustable engagement formation that is adjustable between a locked position, in which the engagement formation is adapted to engage a securing aperture provided in a panel, and a release position, in which the engagement formation is adapted to be released from the securing aperture; and wherein the adjustable engagement formation includes a stationary section (24.1) which is stationary relative to the leg with which it is associated, and a displaceable section, which is displaceable relative to the leg with which it is associated; characterised in that the displaceable section of the adjustable engagement formation includes a primary body (34.1) configured and dimensioned to fit inside the securing aperture in the panel to be secured, and a lateral extension (34.4) extending sideways from the body (34.1), the lateral extension (34.4) being configured and dimensioned suitable for, in use, engaging a retaining recess (12.2) of the securing aperture in the panel. two legs (21, 23) extending away from one another, the legs (21, 23) being connected at one end (21.1, 23.1), with each leg (21, 23) having an opposite free end (21.2, 23.2) that terminates in a panel engagement formation (22, 24); wherein at least one of the panel engagement formations (22, 24) is an adjustable engagement formation that is adjustable between a locked position, in which the engagement formation is adapted to engage a securing aperture provided in a panel, and a release position, in which the engagement formation is adapted to be released from the securing aperture; and wherein the adjustable engagement formation includes a stationary section (24.1) which is stationary relative to the leg with which it is associated, and a displaceable section, which is displaceable relative to the leg with which it is associated; characterised in that the displaceable section of the adjustable engagement formation includes a primary body (34.1) configured and dimensioned to fit inside the securing aperture in the panel to be secured, and a lateral extension (34.4) extending sideways from the body (34.1), the lateral extension (34.4) being configured and dimensioned suitable for, in use, engaging a retaining recess (12.2) of the securing aperture in the panel.
A stator vane for a turbomachine comprising: a platform (52, 54, 100) defining an opening; an airfoil having a leading edge, a trailing edge, a suction side wall, and a pressure side wall, the airfoil extending radially between a base and a tip, wherein at least one of the base or the tip includes a protrusion, the protrusion extending into the opening of the platform (52, 54) such that the platform (52, 54) surrounds the protrusion of the airfoil; a braze joint disposed between and fixedly coupling the platform (52, 54, 100) and the protrusion of the airfoil; and a cooling circuit defined in the protrusion or the platform (52, 54, 100) to cool the braze joint, characterized in having: the cooling circuit comprising one or more inlet channels, a plenum, and one or more outlet channels, wherein the inlet channels, the outlet channels and the plenum are each defined in the platform (52, 54, 100), or wherein the inlet channels, the outlet channels and the plenum are each defined in the protrusion. a platform (52, 54, 100) defining an opening; an airfoil having a leading edge, a trailing edge, a suction side wall, and a pressure side wall, the airfoil extending radially between a base and a tip, wherein at least one of the base or the tip includes a protrusion, the protrusion extending into the opening of the platform (52, 54) such that the platform (52, 54) surrounds the protrusion of the airfoil; a braze joint disposed between and fixedly coupling the platform (52, 54, 100) and the protrusion of the airfoil; and a cooling circuit defined in the protrusion or the platform (52, 54, 100) to cool the braze joint, characterized in having: the cooling circuit comprising one or more inlet channels, a plenum, and one or more outlet channels, wherein the inlet channels, the outlet channels and the plenum are each defined in the platform (52, 54, 100), or wherein the inlet channels, the outlet channels and the plenum are each defined in the protrusion. the cooling circuit comprising one or more inlet channels, a plenum, and one or more outlet channels, wherein the inlet channels, the outlet channels and the plenum are each defined in the platform (52, 54, 100), or wherein the inlet channels, the outlet channels and the plenum are each defined in the protrusion.
A method of compensating for temperature error in a pneumatic pumping system of a peritoneal dialysis system, the peritoneal dialysis system including a pumping mechanism with a disposable cassette and at least one disposable chamber, wherein fluid communication is established between the peritoneal dialysis system and a peritoneal cavity of a patient, the method comprising: (i) calculating a corrected volume of air in a disposable chamber, V d = V r * Pr 2 - Pr 1 Pd 1 - Pd 2 wherein V d is the corrected volume, V r is a reference volume of the chamber, and (Pr 2 -Pr 1) is a pressure difference between a high pressure in the reference chamber and a pressure in the reference chamber after equalization, and (Pd 1 -Pd 2) is a pressure difference between a high pressure in the disposable chamber and a pressure in the delivery chamber after equalization, wherein pressures after equalization comprise pressure measurements after the delivery and reference chambers are connected; (ii) multiplying the result of (i) by a ratio of a temperature in the disposable chamber to a temperature in the reference chamber T d /T r; and (iii) multiplying the result of (ii) by a ratio of Tr cal /Td cal to determine a correction factor, wherein Tr cal is a temperature in the reference chamber during a calibration procedure and Td cal is a temperature in the disposable chamber during the calibration procedure, wherein the temperature during a calibration procedure is constant in the reference and disposable volumes; (iv) calculating a corrected volume of air delivered by the disposable chamber of the system by applying the correction factor; and (v) correcting a volume of dialysate pumped by the dialysis system using the corrected volume of air. (i) calculating a corrected volume of air in a disposable chamber, V d = V r * Pr 2 - Pr 1 Pd 1 - Pd 2 wherein V d is the corrected volume, V r is a reference volume of the chamber, and (Pr 2 -Pr 1) is a pressure difference between a high pressure in the reference chamber and a pressure in the reference chamber after equalization, and (Pd 1 -Pd 2) is a pressure difference between a high pressure in the disposable chamber and a pressure in the delivery chamber after equalization, wherein pressures after equalization comprise pressure measurements after the delivery and reference chambers are connected; (ii) multiplying the result of (i) by a ratio of a temperature in the disposable chamber to a temperature in the reference chamber T d /T r; and (iii) multiplying the result of (ii) by a ratio of Tr cal /Td cal to determine a correction factor, wherein Tr cal is a temperature in the reference chamber during a calibration procedure and Td cal is a temperature in the disposable chamber during the calibration procedure, wherein the temperature during a calibration procedure is constant in the reference and disposable volumes; (iv) calculating a corrected volume of air delivered by the disposable chamber of the system by applying the correction factor; and (v) correcting a volume of dialysate pumped by the dialysis system using the corrected volume of air.
An apparatus for vectoring the thrust of a motor that produces thrust along a longitudinal axis by expelling combustion gases through a nozzle (310,410,510,610), comprising: a plurality of linearly-positionable non-rotatable thrust deflectors (322, 324, 326, 328, 422, 424, 426, 428, 522, 524, 526, 528, 622, 624, 626, 628, 722, 724, 726, 728, 822, 824, 826, 828) disposed around a perimeter of the nozzle (310, 410, 510, 610), movable between a retracted position, a fully extended position and at least one intermediate position, wherein each thrust deflector (322, 324, 326, 328, 422, 424, 426, 428, 522, 524, 526, 528, 622, 624, 626, 628, 722, 724, 726, 728, 822, 824, 826, 828) may be independently positioned to simultaneously generate both a transverse force normal to the longitudinal axis and a torque about the longitudinal axis. a plurality of linearly-positionable non-rotatable thrust deflectors (322, 324, 326, 328, 422, 424, 426, 428, 522, 524, 526, 528, 622, 624, 626, 628, 722, 724, 726, 728, 822, 824, 826, 828) disposed around a perimeter of the nozzle (310, 410, 510, 610), movable between a retracted position, a fully extended position and at least one intermediate position, wherein each thrust deflector (322, 324, 326, 328, 422, 424, 426, 428, 522, 524, 526, 528, 622, 624, 626, 628, 722, 724, 726, 728, 822, 824, 826, 828) may be independently positioned to simultaneously generate both a transverse force normal to the longitudinal axis and a torque about the longitudinal axis.
A system for linking two points a long distance apart from one another of a motor vehicle, in particular between the engine at the front and a battery at the rear of the vehicle, which comprises at least two cables each extending along a respective path between the two points having at least path sections in common, characterised in that the at least two cables (20, 21) are rigid bars and have respective circular transverse sections, and the two cables are held along the path section or sections in common by a plurality of stiffening sleeves (60, 61, 62, 63, 64, 65) such as to combat the bending of the cables.
Apparatus for making a connection with a part of a body to transfer an electromagnetic signal for a predetermined purpose, the apparatus including: - a controller for controlling the nature of, or for measuring, the signal dependent on one or more parameters, the controller comprising an on-board memory and output terminals; - a garment adapted to be in contact with a part of the body, wherein the garment includes at least two electrodes, wherein the controller is adapted to deliver the signal to the output terminals to cause a current to flow between the at least two electrodes and/or the controller is adapted to process the signal detected on the at least two electrodes, wherein the electrodes are connected to the controller by a connector and wherein the controller is electrically detachable from the garment, characterized in that: at least one parameter of the one or more parameters is stored on a data storage device included in the garment, wherein the controller is adapted to load the one or more parameters from the data storage device to the on-board memory to deliver the signal to the output terminals. - a controller for controlling the nature of, or for measuring, the signal dependent on one or more parameters, the controller comprising an on-board memory and output terminals; - a garment adapted to be in contact with a part of the body, wherein the garment includes at least two electrodes, wherein the controller is adapted to deliver the signal to the output terminals to cause a current to flow between the at least two electrodes and/or the controller is adapted to process the signal detected on the at least two electrodes, wherein the electrodes are connected to the controller by a connector and wherein the controller is electrically detachable from the garment, characterized in that: at least one parameter of the one or more parameters is stored on a data storage device included in the garment, wherein the controller is adapted to load the one or more parameters from the data storage device to the on-board memory to deliver the signal to the output terminals.
An on-board train control system that interfaces with a wayside cab-signalling installation comprising: an on-board location determination subsystem (12, 14), on-board means for receiving, and de-coding cab-signalling speed codes, on-board means for converting said cab-signalling speed codes to corresponding movement authority limits, and on-board means for generating a stopping profile to enforce a movement authority limit; wherein the generation of the movement authority limit is a dynamic process that corresponds directly to the cab-signalling speed code received from the wayside devices, such that a more restrictive speed code will result in a truncation of the movement authority limit and a more permissive speed code will result in an expanded movement authority limit. an on-board location determination subsystem (12, 14), on-board means for receiving, and de-coding cab-signalling speed codes, on-board means for converting said cab-signalling speed codes to corresponding movement authority limits, and on-board means for generating a stopping profile to enforce a movement authority limit;
An active clearance control system of a gas turbine engine, the system comprising: a multiple of blade outer air seal assemblies; and a sync ring with a multiple of graduation sets, each of the graduation sets associated with one of the multiple of blade outer air seal assemblies, wherein each of the multiple of blade outer air seal assemblies includes a blade outer air seal and a follower rod that extends therefrom, wherein each of the multiple of follower rods terminates in a follower transverse to the follower rod, wherein each of the followers supports an insert, which rides upon the sync ring, characterised in that: each insert is manufactured of a material different than the follower; and/or each of the followers supports an insert through a dovetail interface; a multiple of blade outer air seal assemblies; and a sync ring with a multiple of graduation sets, each of the graduation sets associated with one of the multiple of blade outer air seal assemblies, wherein each of the multiple of blade outer air seal assemblies includes a blade outer air seal and a follower rod that extends therefrom, wherein each of the multiple of follower rods terminates in a follower transverse to the follower rod, wherein each of the followers supports an insert, which rides upon the sync ring, characterised in that: each insert is manufactured of a material different than the follower; and/or each of the followers supports an insert through a dovetail interface;
An optical reflective film comprising at least one unit obtained by laminating a high refractive index layer and a low refractive index layer on a substrate, wherein a difference in refractive index between the high refractive index layer and the low refractive index layer is 0.1 or more, the high refractive index layer and the low refractive index layer each contain at least one kind of polyvinyl alcohol, and when a polyvinyl alcohol having the highest content in the high refractive index layer is referred to as a "polyvinyl alcohol " and a polyvinyl alcohol having the highest content in the low refractive index layer is referred to as a "polyvinyl alcohol ", a degree of saponification of the polyvinyl alcohol is different from a degree of saponification of the polyvinyl alcohol and the difference in the degree of saponification between the polyvinyl alcohol and the polyvinyl alcohol is 3% by mol or more.
A method of estimating a permeability of an earth formation, comprising: generating at least one acoustic wave in a borehole fluid acoustically coupled to the earth formation; measuring a pressure attenuation of the at least one acoustic wave over time in the borehole fluid using an acoustic sensor; and estimating the permeability using the attenuation over time and at least one theoretical attenuation over time. generating at least one acoustic wave in a borehole fluid acoustically coupled to the earth formation; measuring a pressure attenuation of the at least one acoustic wave over time in the borehole fluid using an acoustic sensor; and estimating the permeability using the attenuation over time and at least one theoretical attenuation over time.
A sequence calibration method, comprising: (a) sequencing a nucleic acid; (b) obtaining a plurality of reading sequences from sequencing the nucleic acid by a receiving unit; (c) selecting one of the plurality of reading sequences as a template sequence by the determining unit; (d) setting a comparing condition by a determining unit; (e) comparing the template sequence to each of the other sequences according to the comparison condition, to respectively generate comparison results by the determining unit; (f) generating a sequence comparison result according to all respectively generated comparison results by the determining unit; and (g) outputting a calibrated sequence according to the sequence comparison result by the deter-mining unit, wherein the comparison condition is set according to a first seed table of the template sequence and second seed tables for reading sequences which are not selected as the template sequence, wherein a seed is a segment of the sequence, wherein a seed table of a sequence is built by dividing a sequence into a plurality of seed sets from the different start sites of the sequence, respectively, by per seed K-mers, representing a specific length of the seeds, wherein K is a positive integer of greater than 2, and a content and position of each seed are recorded, wherein the first seed table of the template sequence comprises a plurality of first seeds with a specific length constituting a plurality of first seed sets with different seeding start sites and the second seed table of the reading sequence which is not selected as the template sequence comprises a plurality of second seeds with a specific length constituting a plurality of second seed sets with different seeding start sites, and wherein the specific length of the first seeds of the first seed table and the specific length of the second seeds of the second seed table are of the same specific length. (a) sequencing a nucleic acid; (b) obtaining a plurality of reading sequences from sequencing the nucleic acid by a receiving unit; (c) selecting one of the plurality of reading sequences as a template sequence by the determining unit; (d) setting a comparing condition by a determining unit; (e) comparing the template sequence to each of the other sequences according to the comparison condition, to respectively generate comparison results by the determining unit; (f) generating a sequence comparison result according to all respectively generated comparison results by the determining unit; and (g) outputting a calibrated sequence according to the sequence comparison result by the deter-mining unit,
An aircraft engine sound attenuation apparatus comprising: a perforated face member; a backing member; a plurality of connecting members coupling the perforated face member to the backing member to form a plurality of channels spanning from the perforated face member to the backing member; and a bulk absorber disposed in each of the plurality of channels; wherein the plurality of channels are configured to be connected to an interior portion of an aircraft engine nacelle component so that the plurality of channels are oriented in a direction substantially normal to a direction of fluid flow pressure drop passing through the aircraft engine and each channel has a width, in the direction substantially normal to the direction of fluid flow pressure drop passing through the aircraft engine, that substantially prevents sound propagation inside the channel substantially parallel to a surface of the channel in the direction substantially normal to the direction of fluid flow pressure drop passing through the aircraft engine. a perforated face member; a backing member; a plurality of connecting members coupling the perforated face member to the backing member to form a plurality of channels spanning from the perforated face member to the backing member; and a bulk absorber disposed in each of the plurality of channels; wherein the plurality of channels are configured to be connected to an interior portion of an aircraft engine nacelle component so that the plurality of channels are oriented in a direction substantially normal to a direction of fluid flow pressure drop passing through the aircraft engine and each channel has a width, in the direction substantially normal to the direction of fluid flow pressure drop passing through the aircraft engine, that substantially prevents sound propagation inside the channel substantially parallel to a surface of the channel in the direction substantially normal to the direction of fluid flow pressure drop passing through the aircraft engine.