mhurhangee/patent-ind-claim-en huggingface dataset:
An apparatus for applying micro-glass beads for forming the road marking on the road surface , comprising a transportation means with mounted thereon a container with a base provided with a free edge , with a scraper , an inlet and an outlet , a belt with holes , two drums , a feeding device , a blowing means , the belt is configured closed, is stretched on the drums that are mounted to rotate them around the axis thereof and disposed at a distance from each other so that the axes thereof are parallel, with the formation of the lower portion of the belt between the drums and with the provision of capability to move the belt from drum to drum , wherein the holes are configured through and disposed on the belt in a certain order, the inlet and the outlet are disposed in the container opposite to each other, the outlet is disposed directly against the base , the lower portion of the belt is passed successively through the inlet , the base and through the outlet , the feeding device is attached to supply the micro-glass beads onto the lower portion of the belt in the container , the scraper is mounted in the container to obstruct the passage of the micro-glass beads present on the lower portion of the belt to the free edge of the base , disposed near the outlet , the blowing means is disposed at the free edge to blow the micro-glass beads present in the holes in the lower portion of the belt in the direction of the road surface .
A system for use with landing gear having an aircraft attachment , the system comprising: a shock strut having a cylinder and a piston configured to be at least partially received by the cylinder; a brace configured to be coupled to the shock strut in order to lock the landing gear in a deployed position, and to fold towards the shock strut during retraction of the landing gear; a collar coupled to the brace and the piston and configured to rotate relative to the cylinder in response to folding of the brace, the system characterized by further comprising an upper cam fastened to the piston; a lower cam fastened to the cylinder; wherein the collar is configured to rotate relative to the cylinder in response to folding of the brace such that rotation of the collar rotates the piston and the upper cam relative to the lower cam, the rotation of the upper cam relative to the lower cam forcing the piston towards the aircraft attachment within the cylinder; and wherein the upper bearing and lower bearing are each located such that the upper cam and the lower cam are located between the upper bearing and the lower bearing. a shock strut having a cylinder and a piston configured to be at least partially received by the cylinder; a brace configured to be coupled to the shock strut in order to lock the landing gear in a deployed position, and to fold towards the shock strut during retraction of the landing gear; a collar coupled to the brace and the piston and configured to rotate relative to the cylinder in response to folding of the brace, the system characterized by further comprising an upper cam fastened to the piston; a lower cam fastened to the cylinder; wherein the collar is configured to rotate relative to the cylinder in response to folding of the brace such that rotation of the collar rotates the piston and the upper cam relative to the lower cam, the rotation of the upper cam relative to the lower cam forcing the piston towards the aircraft attachment within the cylinder; and wherein the upper bearing and lower bearing are each located such that the upper cam and the lower cam are located between the upper bearing and the lower bearing.
A system for generating an output signal comprising a high frequency component from an input audio signal comprising a low frequency component using a transposition order T , comprising: an analysis window unit configured to apply an analysis window of a length of L A samples, thereby extracting a frame of the input signal; an analysis transformation unit of order M and having a frequency resolution Δ f configured to transform the L A samples into M complex coefficients; a nonlinear processing unit , configured to alter the phase of the complex coefficients by using the transposition order T ; a synthesis transformation unit of order M and having a frequency resolution Q Δ f , configured to transform the altered coefficients into M time domain samples; wherein Q is a frequency resolution factor smaller than or equal to the transposition order T ; and a synthesis window unit configured to apply a synthesis window of a length of L s samples to the M time domain samples, thereby generating a frame of the output signal; wherein the transformation order M is M = F · L S , and wherein F ≥ Q + 1 2 . an analysis window unit configured to apply an analysis window of a length of L A samples, thereby extracting a frame of the input signal; an analysis transformation unit of order M and having a frequency resolution Δ f configured to transform the L A samples into M complex coefficients; a nonlinear processing unit , configured to alter the phase of the complex coefficients by using the transposition order T ; a synthesis transformation unit of order M and having a frequency resolution Q Δ f , configured to transform the altered coefficients into M time domain samples; wherein Q is a frequency resolution factor smaller than or equal to the transposition order T ; and a synthesis window unit configured to apply a synthesis window of a length of L s samples to the M time domain samples, thereby generating a frame of the output signal;
Phase-change material comprising germanium Ge, tellurium Te and antimony Sb, characterised in that it comprises at least 37% germanium Ge and in that the ratio between the quantity of antimony Sb and the quantity of tellurium Te is comprised between 2.3 and 2.5.
A one-piece mixer insert for a static mixer, the mixer insert comprising a first mixing element having a plurality of crossing first rods and the mixer insert comprising at least one second mixing element adjacent to the first mixing element along a longitudinal axis (L), twisted around the longitudinal axis (L) by a twist angle, in particular of 90°, relative to the first mixing element and having several crossing second rods , the first rods having first rod ends facing the second mixing element and the second rods having first rod ends facing the first mixing element and part of the first and second rod ends being distributed over the outer circumference of the mixer insert , characterized in that each of the first rod ends distributed over the outer circumference of the mixer insert is connected to one of the second rod ends distributed over the outer circumference of the mixer insert in a material-bonded manner via a connection portion , in particular a connection web.
A structure for combining a cable and a casing , the structure comprising: a screw groove provided on a front side of an inner surface of a through hole of the casing ; locking notches continuously provided on a rear side of the inner surface of the through hole ; a screw protrusion having the cable penetrating the through hole and screw-engaged with the screw groove ; and a locking protrusion provided on the cable , and having an inclined surface configured to allow the locking protrusion to move over the locking notches in a forward direction and a locking surface configured to prevent the locking protrusion from moving in a reverse direction by being engaged with the locking notches ; characterized in that a boundary between the locking notches and the screw groove has a stepped surface and a boundary between the locking protrusion and the screw protrusion of the cable has a contact surface that is in contact with the stepped surface . a screw groove provided on a front side of an inner surface of a through hole of the casing ; locking notches continuously provided on a rear side of the inner surface of the through hole ; a screw protrusion having the cable penetrating the through hole and screw-engaged with the screw groove ; and a locking protrusion provided on the cable , and having an inclined surface configured to allow the locking protrusion to move over the locking notches in a forward direction and a locking surface configured to prevent the locking protrusion from moving in a reverse direction by being engaged with the locking notches ; characterized in that a boundary between the locking notches and the screw groove has a stepped surface and a boundary between the locking protrusion and the screw protrusion of the cable has a contact surface that is in contact with the stepped surface .
A method for operating a cellular multiple-input and multiple-output, MIMO, system, the cellular MIMO system comprising a first device having an antenna array comprising a plurality of antennas , and a second device comprising at least two antennas , the method comprising: - broadcasting a same uplink pilot signal from each antenna of the at least two antennas of the second device using a single pilot signal resource, - receiving, at the antenna array of the first device , a signal resulting from transmission of the same uplink pilot signal from each antenna of the at least two antennas of the second device , - determining, at the first device , a first set of first device receiving parameters for the antenna array depending on the received same uplink pilot signal , - sending from each antenna of the at least two antennas of the second device a corresponding uplink pilot signal of a plurality of uplink pilot signals, wherein the plurality of uplink pilot signals are orthogonal to each other, - receiving the plurality of uplink pilot signals at the antenna array of the first device using the first set of first device receiving parameters, and - determining, at the first device , for each received uplink pilot signal of the plurality of uplink pilot signals a corresponding second set of first device receiving parameters for the antenna array depending on the plurality of received orthogonal uplink pilot signals . - broadcasting a same uplink pilot signal from each antenna of the at least two antennas of the second device using a single pilot signal resource, - receiving, at the antenna array of the first device , a signal resulting from transmission of the same uplink pilot signal from each antenna of the at least two antennas of the second device , - determining, at the first device , a first set of first device receiving parameters for the antenna array depending on the received same uplink pilot signal , - sending from each antenna of the at least two antennas of the second device a corresponding uplink pilot signal of a plurality of uplink pilot signals, wherein the plurality of uplink pilot signals are orthogonal to each other, - receiving the plurality of uplink pilot signals at the antenna array of the first device using the first set of first device receiving parameters, and - determining, at the first device , for each received uplink pilot signal of the plurality of uplink pilot signals a corresponding second set of first device receiving parameters for the antenna array depending on the plurality of received orthogonal uplink pilot signals .
A method for making naphthenic process oils, the method comprising: a) vacuum distilling naphthenic crude residual bottoms from a naphthenic crude atmospheric distillation unit to provide one or more naphthenic vacuum gas oils in one or more viscosity ranges; b) blending at least one such naphthenic vacuum gas oil with a high aromatic carbon content (C A ) distilled aromatic extract feedstock to provide at least one blended oil; and c) hydrotreating the at least one blended oil obtained from step b) to provide an enhanced C A content naphthenic process oil; wherein the high C A distilled aromatic extract feedstock and enhanced C A content naphthenic process oil each have greater C A content than that of a comparison oil made by similarly hydrotreating the same one or more naphthenic vacuum gas oils alone without blending step b); and wherein the high C A distilled aromatic extract feedstock is a liquid material having a viscosity-gravity constant of greater than 0.95 as determined by ASTM D2501. a) vacuum distilling naphthenic crude residual bottoms from a naphthenic crude atmospheric distillation unit to provide one or more naphthenic vacuum gas oils in one or more viscosity ranges; b) blending at least one such naphthenic vacuum gas oil with a high aromatic carbon content (C A ) distilled aromatic extract feedstock to provide at least one blended oil; and c) hydrotreating the at least one blended oil obtained from step b) to provide an enhanced C A content naphthenic process oil;
A copolymer composition comprising a phosphorus acid group containing telomeric copolymer of acrylic acid and methacrylic acid and/or salts thereof having a weight average molecular weight (Mw) of up to 20,000 as determined by aqueous gel permeation chromatography (GPC) against poly(acrylic acid) (pAA) standards, and having an average of (i) from 19 to 74 wt.% of the copolymerization residue of methacrylic acid, anhydride, or its salts, (ii) from 1 to 20 wt.% of phosphorus acid groups chosen from hypophosphite, phosphite, alkyl phosphinate, alkyl phosphonate, dialkyl phosphinate, and mixtures thereof, (iii) from 0 to 20 wt.% of the copolymerization residue of a third vinyl monomer, and (iv) from 25 to 80 wt.% of the copolymerization residue of acrylic acid, anhydride, or its salts, the wt.% of all monomers and phosphorus acid group forming reactants being based on the total weight of reactants used to make the telomeric copolymer, wherein the telomeric copolymer comprises at least one copolymerization residue of propene (-CH2-CH(CH3)-) .
An X-ray diagnosis apparatus , comprising: a detecting unit configured to use an image recognition process to detect an element from X-ray image data taken of an examined subject; a determining unit configured to determine parameters of multi-frequency processing on a basis of a detection result of the element; and an image processing unit configured to execute the multi-frequency processing on one or both of the X-ray image data and another piece of X-ray image data taken later than the X-ray image data, on a basis of the determined parameters, wherein the multi-frequency processing includes a frequency separation process configured to generate a plurality of pieces of separate frequency band data from one or both of the X-ray image data and said another piece of X-ray image data, the determined parameters of the multi-frequency processing include threshold values used in the frequency separation process; and the image processing unit is configured to separate the plurality of pieces of separate frequency band data on a basis of the threshold values. a detecting unit configured to use an image recognition process to detect an element from X-ray image data taken of an examined subject; a determining unit configured to determine parameters of multi-frequency processing on a basis of a detection result of the element; and an image processing unit configured to execute the multi-frequency processing on one or both of the X-ray image data and another piece of X-ray image data taken later than the X-ray image data, on a basis of the determined parameters, wherein the multi-frequency processing includes a frequency separation process configured to generate a plurality of pieces of separate frequency band data from one or both of the X-ray image data and said another piece of X-ray image data, the determined parameters of the multi-frequency processing include threshold values used in the frequency separation process; and the image processing unit is configured to separate the plurality of pieces of separate frequency band data on a basis of the threshold values.
A detector configuration , comprising: a scintillator crystal block comprising a plurality of elongated scintillator elements arranged in a matrix of rows and columns; a plurality of semiconductor photomultiplier sensor elements (24; 24a - 24p) optically coupled to said scintillator crystal block , wherein said sensor elements (24; 24a - 24p) comprise elongated strips (24; 24a - 24p) and wherein each of said sensor elements (24; 24a - 24p) has a width (w) in a direction perpendicular to a length direction, characterized in said width (w) being at least two times smaller than a width of a scintillator element to which said sensor element (24; 24a - 24p) is optically coupled such that each of said scintillator elements is optically coupled to a plurality of said sensor elements; and readout means (30a - 30e) electrically coupled to said plurality of sensor elements (24; 24a - 24p), wherein said detector configuration is adapted to differentially couple each said sensor element (24; 24a - 24p) to said readout means (30a - 30e). a scintillator crystal block comprising a plurality of elongated scintillator elements arranged in a matrix of rows and columns; a plurality of semiconductor photomultiplier sensor elements (24; 24a - 24p) optically coupled to said scintillator crystal block , wherein said sensor elements (24; 24a - 24p) comprise elongated strips (24; 24a - 24p) and wherein each of said sensor elements (24; 24a - 24p) has a width (w) in a direction perpendicular to a length direction, characterized in said width (w) being at least two times smaller than a width of a scintillator element to which said sensor element (24; 24a - 24p) is optically coupled such that each of said scintillator elements is optically coupled to a plurality of said sensor elements; and readout means (30a - 30e) electrically coupled to said plurality of sensor elements (24; 24a - 24p), wherein said detector configuration is adapted to differentially couple each said sensor element (24; 24a - 24p) to said readout means (30a - 30e).
A base station device which is mounted to a high-altitude platform system, HAPS, and forms a multi-cell including a plurality of cells on a ground to provide a wireless communication service to a user terminal in the multi-cell , the base station device comprising: a location information acquisition unit which is configured to acquire location information of a user terminal present in the multi-cell ; a flight vehicle associated information acquisition unit which is configured to acquire flight vehicle associated information including location information and attitude information of the HAPS , the attitude information including the attitude of the HAPS during flight; an interference estimation unit which is configured to estimate, based on location information of a plurality of the user terminals and the flight vehicle associated information, an interfered user terminal having a chance of experiencing an interference from a cell other than a cell in which the user terminal is present among the plurality of user terminals and an interference amount; an MCS decision unit which is configured to decide an MCS of an uplink to be assigned to the interfered user terminal based on the interference amount; and an MCS notification unit which is configured to notify the interfered user terminal of the MCS decided by the MCS decision unit . a location information acquisition unit which is configured to acquire location information of a user terminal present in the multi-cell ; a flight vehicle associated information acquisition unit which is configured to acquire flight vehicle associated information including location information and attitude information of the HAPS , the attitude information including the attitude of the HAPS during flight; an interference estimation unit which is configured to estimate, based on location information of a plurality of the user terminals and the flight vehicle associated information, an interfered user terminal having a chance of experiencing an interference from a cell other than a cell in which the user terminal is present among the plurality of user terminals and an interference amount; an MCS decision unit which is configured to decide an MCS of an uplink to be assigned to the interfered user terminal based on the interference amount; and an MCS notification unit which is configured to notify the interfered user terminal of the MCS decided by the MCS decision unit .
An apparatus for processing a semiconductor wafer surface with fluids containing ozone, comprising: an ozone generator , a solvent flask , a gas-liquid mixing device , a closed chamber for containing the wafer to be processed, and a gas-liquid delivery system and a gas-liquid discharge system; wherein the ozone generator and the solvent flask are connected with corresponding inlets of the gas-liquid mixing device, respectively, and outlets of the gas-liquid mixing device are connected with at least one inlet of the closed chamber, characterized in that : a gas-liquid separation device or another ozone generator is provided for ensuring a concentration of ozone in solution by transferring gas-liquid mixed fluids containing ozone via the gas-liquid separation device or solutions containing ozone and ozone gas after generation by the another ozone generator into the closed chamber and by increasing a partial pressure of ozone in gas phase.
Heat exchanger comprising a heating body made up of a plurality of circulation plates (2, 2a-2c) which are nested one inside the other and formed between which are spaces configured to be flowed through by a fluid, the heating body comprising at least one header (5, 5a-5d) which connects the spaces , the heat exchanger comprising a manifold via which the header (5, 5a-5d) is connected to a circuit outside the heat exchanger , characterized in that the header (5, 5a-5d) has a header cross section , the manifold has a manifold cross section different from the header cross section , the heat exchanger comprising an adapter which is interposed between the header and the manifold and joins the header cross section to the manifold cross section , the heating body comprising a first end plate having four openings : a first opening , a second opening , a third opening and a fourth opening , the heat exchanger being characterized in that the adapter is an independent part having a first end secured to the first end plate and a second end secured to the manifold , the adapter comprising at least one bearing end stop for bearing against the first end plate , the end stop being configured to limit the insertion of the adapter into the first end plate by coming into contact with the rim of one of the openings of the first end plate , for example the first opening .