mhurhangee/patent-ind-claim-en huggingface dataset:
A method for preparing a cosmetic cleansing agent, comprising the following steps: a) providing an aqueous dispersion which contains at least one inorganic pigment and/or at least one opacifier and/or pearlescing agent, b) providing a preparation which contains at least one acrylate homopolymer or acrylate copolymer, c) mixing the aqueous dispersion from method step a) with the preparation from method step b), d) providing an O/W emulsion, e) mixing the O/W emulsion from method step d) with the mixture from method step c), f) providing a cosmetically acceptable carrier which contains at least one surfactant, g) mixing the cosmetically acceptable carrier from method step f) with the mixture from method step e). a) providing an aqueous dispersion which contains at least one inorganic pigment and/or at least one opacifier and/or pearlescing agent, b) providing a preparation which contains at least one acrylate homopolymer or acrylate copolymer, c) mixing the aqueous dispersion from method step a) with the preparation from method step b), d) providing an O/W emulsion, e) mixing the O/W emulsion from method step d) with the mixture from method step c), f) providing a cosmetically acceptable carrier which contains at least one surfactant, g) mixing the cosmetically acceptable carrier from method step f) with the mixture from method step e).
A decoration member comprising: a pattern layer comprising two or more unit patterns; and an inorganic layer formed on the pattern layer, wherein the inorganic layer comprises a region in which a thickness t(x) of the inorganic layer formed on each of the two or more unit patterns increases in a direction x in which the unit patterns are arranged, wherein the unit pattern is a unit prism pattern, wherein the prism pattern has a ridge line in a first direction and is continuously arranged in a second direction perpendicular to the first direction, wherein the inorganic layer comprises a unit inorganic layer provided on each of unit prism pattern, and wherein an average thickness of the unit inorganic layer provided on any one unit prism pattern is different from the average thickness of the unit inorganic layer provided on another unit prism pattern arranged adjacent to the unit prism pattern. a pattern layer comprising two or more unit patterns; and an inorganic layer formed on the pattern layer, wherein the inorganic layer comprises a region in which a thickness t(x) of the inorganic layer formed on each of the two or more unit patterns increases in a direction x in which the unit patterns are arranged, wherein the unit pattern is a unit prism pattern, wherein the prism pattern has a ridge line in a first direction and is continuously arranged in a second direction perpendicular to the first direction, wherein the inorganic layer comprises a unit inorganic layer provided on each of unit prism pattern, and wherein an average thickness of the unit inorganic layer provided on any one unit prism pattern is different from the average thickness of the unit inorganic layer provided on another unit prism pattern arranged adjacent to the unit prism pattern.
Instrument for counting the duration for differentiated phases, comprising a plurality of means for recording a time duration, each actuatable, for activation and deactivation thereof, by a first control means , said instrument comprising a general control means for controlling, from an inactive position where all said recording means are deactivated, the activation of only one of them, selected by selection means which said instrument comprises, and for again controlling, at a final moment, the deactivation of all said recording means, said instrument further comprising switching means which are designed, during a command for activation of one of said recording means, to trigger the deactivation of all other recording means and to save the totality of the recorded times, counted on each of said recording means, said first control means being designed to be controlled by a user or/and by measuring means or/and by a signal in order to trigger the activation of one of said recording means, each of said recording means is designed, during a reactivation, to resume the counting of the duration from the total duration recorded by said recording means.
A method, at a user equipment , of carrying out dual connectivity with a secondary access node , the method comprising: determining that no user plane bearers are mapped to the secondary access node ; characterized in that the method further comprises: based on the determining, limiting a listening time of a physical downlink control channel from the secondary access node to a procedure for updating timing information, wherein the timing information comprises a timing advance between the secondary access node and the user equipment . determining that no user plane bearers are mapped to the secondary access node ; characterized in that the method further comprises: based on the determining, limiting a listening time of a physical downlink control channel from the secondary access node to a procedure for updating timing information, wherein the timing information comprises a timing advance between the secondary access node and the user equipment .
An extractor for extracting harmful chemicals and particulates from air for a soldering iron station, the extractor including an intake assembly , a filter assembly including a main filter , a fan , and an exhaust assembly , wherein the extractor is arranged for: receiving harmful chemicals, particulates, and air from the soldering iron station through the intake assembly ; filtering the fumes from the air with the filter assembly , said filtering comprising filtering the fumes from the air with the main filter ; and exhausting the filtered air with the exhaust assembly , wherein the extractor includes a housing with one or more sides , wherein the main filter is removable with respect to a side of the one or more sides of the housing , and wherein the extractor is further arranged for removing the main filter from the side of the housing to replace the main by filter characterised in that the extractor is arranged for removing the main filter at least partly by rotating the main filter relative to the side of the housing to remove the main filter . receiving harmful chemicals, particulates, and air from the soldering iron station through the intake assembly ; filtering the fumes from the air with the filter assembly , said filtering comprising filtering the fumes from the air with the main filter ; and exhausting the filtered air with the exhaust assembly , wherein the extractor includes a housing with one or more sides , wherein the main filter is removable with respect to a side of the one or more sides of the housing , and wherein the extractor is further arranged for removing the main filter from the side of the housing to replace the main by filter characterised in that the extractor is arranged for removing the main filter at least partly by rotating the main filter relative to the side of the housing to remove the main filter .
A method performed by an autonomous vehicle that has a processor and video or LIDAR sensors mounted thereon, wherein the processor is configured to analyse captured data from the video or LIDAR sensors, the method comprising receiving directly at the video or LIDAR sensors of the autonomous vehicle a hailing request carried by a signaling mode that comprises a human gesture and, optionally a facial expression, the hailing request corresponding to an indication of an intention of a potential rider to use an autonomous vehicle, wherein the signaling mode comprises a common human gesture in combination with a secondary, visually distinctive stimulus in order to reduce false detections, and wherein the secondary, visually distinctive stimulus is the potential rider looking at or tracking the autonomous vehicle by her head pose while executing the common human gesture, and processing the hailing request at the processor of the autonomous vehicle to determine whether to respond to the hailing request. receiving directly at the video or LIDAR sensors of the autonomous vehicle a hailing request carried by a signaling mode that comprises a human gesture and, optionally a facial expression, the hailing request corresponding to an indication of an intention of a potential rider to use an autonomous vehicle, wherein the signaling mode comprises a common human gesture in combination with a secondary, visually distinctive stimulus in order to reduce false detections, and wherein the secondary, visually distinctive stimulus is the potential rider looking at or tracking the autonomous vehicle by her head pose while executing the common human gesture, and processing the hailing request at the processor of the autonomous vehicle to determine whether to respond to the hailing request.
A workbench-hand truck assembly comprising: a first pair of legs ; a frame ; a second pair of legs pivotally coupled to the frame and to the first pair of legs: a workbench configured to be supported by the first and second pairs of legs: a pair of brackets pivotally coupled to the first pair of legs; and a nose plate pivotally coupled to the pair of brackets for movement between a stored position, in which the nose plate extends parallel to and adjacent the workbench, and a deployed position, in which the nose plate extends away from the workbench, wherein the workbench-hand truck assembly is configurable in a hand truck position when the nose plate is in the deployed position, such that the nose plate extends perpendicular to the workbench. characterized in that the first pair of legs and the second pair of legs are movable between a first position, in which the workbench is positioned at a first height above a ground surface, and a second position, in which the workbench is positioned at a second height above the ground surface that is greater than the first height. a first pair of legs ; a frame ; a second pair of legs pivotally coupled to the frame and to the first pair of legs: a workbench configured to be supported by the first and second pairs of legs: a pair of brackets pivotally coupled to the first pair of legs; and a nose plate pivotally coupled to the pair of brackets for movement between a stored position, in which the nose plate extends parallel to and adjacent the workbench, and a deployed position, in which the nose plate extends away from the workbench, wherein the workbench-hand truck assembly is configurable in a hand truck position when the nose plate is in the deployed position, such that the nose plate extends perpendicular to the workbench. characterized in that the first pair of legs and the second pair of legs are movable between a first position, in which the workbench is positioned at a first height above a ground surface, and a second position, in which the workbench is positioned at a second height above the ground surface that is greater than the first height.
Use of esters of octahydro-4,7-methano-1H-indene-5-methanol or octahydro-4,7-methano-1H-indene-5-dimethanol and aliphatic, straight-chain C5 to C9 monocarboxylic acids comprising an odd C-number as lubricants in low temperature applications.
A method of thinning a coating applied on a razor blade , the method comprising: providing a thinning material having a Shore OO hardness in a range of 10-100, more specifically 20-70, contacting the thinning material with an edge of the razor blade , and moving the thinning material relative to the edge of the razor blade such that a shear force is applied on the edge of the razor blade thereby removing at least a portion of the coating applied on the edge of the razor blade and wherein the coating applied on the razor blade is polyfluorocarbon. providing a thinning material having a Shore OO hardness in a range of 10-100, more specifically 20-70, contacting the thinning material with an edge of the razor blade , and moving the thinning material relative to the edge of the razor blade such that a shear force is applied on the edge of the razor blade thereby removing at least a portion of the coating applied on the edge of the razor blade and wherein the coating applied on the razor blade is polyfluorocarbon.
An assembly for a turbine engine with an axial centerline , the assembly comprising a turbine engine structure including an outer duct wall , an inner duct wall , a first flow path and a second flow path , the inner duct wall radially inward of the outer duct wall , the first flow path radially inward of the inner duct wall , and the second flow path radially outward of the inner duct wall and radially inward of the outer duct wall ; and a valve assembly including a valve element and a valve actuator , the valve element configured to regulate flow of fluid between the first flow path and the second flow path , and the valve actuator configured to move the valve element , wherein the valve actuator is positioned entirely radially outward of the outer duct wall , wherein the valve assembly further includes a rod that extends within the second flow path and mechanically couples the valve actuator to the valve element , characterised in that the rod is connected to the valve element through a first pivot joint . a turbine engine structure including an outer duct wall , an inner duct wall , a first flow path and a second flow path , the inner duct wall radially inward of the outer duct wall , the first flow path radially inward of the inner duct wall , and the second flow path radially outward of the inner duct wall and radially inward of the outer duct wall ; and a valve assembly including a valve element and a valve actuator , the valve element configured to regulate flow of fluid between the first flow path and the second flow path , and the valve actuator configured to move the valve element , wherein the valve actuator is positioned entirely radially outward of the outer duct wall , wherein the valve assembly further includes a rod that extends within the second flow path and mechanically couples the valve actuator to the valve element , characterised in that the rod is connected to the valve element through a first pivot joint .
A method for determining LED drive values (LED Drive) for backlight elements of a backlight panel of a dual modulation display in response to input image data indicative of an image to be displayed, said method including the step of: determining , for each pixel of the input image data , a data value from the color components of the pixels; the method characterized by including the steps of: determining , for each determined data value, a corresponding squared data value; determining , for each backlight element, the mean of the resulting squared data values of the pixels in a local area of the image that is illuminated by a corresponding backlight element, thereby generating a downsampled image of mean squared data values; low-pass filtering the downsampled image of mean squared data values to generate filtered mean squared data values (A); determining , for each backlight element, the mean of the resulting data values of the pixels in a local area of the image that is illuminated by a corresponding backlight element, thereby generating a downsampled image of mean data values; and low-pass filtering the downsampled image of mean data values to generate filtered mean data values; squaring the filtered mean data values to generate squared filtered mean data values (B); subtracting the squared filtered mean data values (B) from the filtered mean squared data values (A) to generate difference values (A-B); and determining the square root of each difference value (A-B) to generate a downsampled image of standard deviation values; determining , for each backlight element, an LED drive value (LED Drive) from a linear combination of the corresponding filtered mean data value and the corresponding standard deviation value. determining , for each determined data value, a corresponding squared data value; determining , for each backlight element, the mean of the resulting squared data values of the pixels in a local area of the image that is illuminated by a corresponding backlight element, thereby generating a downsampled image of mean squared data values; low-pass filtering the downsampled image of mean squared data values to generate filtered mean squared data values (A); determining , for each backlight element, the mean of the resulting data values of the pixels in a local area of the image that is illuminated by a corresponding backlight element, thereby generating a downsampled image of mean data values; and low-pass filtering the downsampled image of mean data values to generate filtered mean data values; squaring the filtered mean data values to generate squared filtered mean data values (B); subtracting the squared filtered mean data values (B) from the filtered mean squared data values (A) to generate difference values (A-B); and determining the square root of each difference value (A-B) to generate a downsampled image of standard deviation values; determining , for each backlight element, an LED drive value (LED Drive) from a linear combination of the corresponding filtered mean data value and the corresponding standard deviation value.
A circuit substrate comprising: first wiring (411-414) configured to transmit a first drive signal (COMB) to drive a driving element ; second wiring (431-434) configured to transmit a control signal (c1-c4) to control application of the first drive signal to the driving element; third wiring configured to transmit the first drive signal (COMA); a receiving unit configured to receive a transmission signal (d1-d4) based on a plurality of original control signals and restore the plurality of control signals based on the transmission signal; and a first input terminal that is connected to the first wiring and is configured to input the transmission signal, wherein the receiving unit is connected to the first wiring and the second wiring, characterized in that : the receiving unit, the first wiring, and the first input terminal are provided on a first layer , and the third wiring is provided on a second layer different from the first layer. first wiring (411-414) configured to transmit a first drive signal (COMB) to drive a driving element ; second wiring (431-434) configured to transmit a control signal (c1-c4) to control application of the first drive signal to the driving element; third wiring configured to transmit the first drive signal (COMA); a receiving unit configured to receive a transmission signal (d1-d4) based on a plurality of original control signals and restore the plurality of control signals based on the transmission signal; and a first input terminal that is connected to the first wiring and is configured to input the transmission signal, wherein the receiving unit is connected to the first wiring and the second wiring, characterized in that : the receiving unit, the first wiring, and the first input terminal are provided on a first layer , and the third wiring is provided on a second layer different from the first layer. the receiving unit, the first wiring, and the first input terminal are provided on a first layer , and the third wiring is provided on a second layer different from the first layer.
An external gear pump (P) that increases a pressure of fluid and discharge the fluid, the pump (P) comprising: a pair of a first gear (G1) and a second gear (G2); a pump body (B); a gear accommodation chamber that is formed within the pump body (B) and accommodates the first gear (G1) and the second gear (G2) in a meshed state: a pair of a first bushing (F11) and a second bushing (F12) that are hollow cylindrical and hold a rotational shaft (GS1) of the first gear (G1) rotatably; an inlet chamber that is formed within the pump body (B) on one side of a meshed portion of the first gear (G1) and the second gear (G2); and an outlet chamber that is formed within the pump body (B) on another side of the meshed portion, wherein a low pressure range (L) facing to the inlet chamber and a high pressure range (H) facing to the outlet chamber are segmented along an inner circumference of the gear accommodation chamber that associates with an outer circumference of the first gear (G1), wherein the pump body (B) has a first surface (P1) that faces to the first bushing (F11) and is perpendicular to the rotational shaft (GS1) of the first gear (G1), wherein the first bushing (F11) has a second surface (P2) that faces to the first surface (P1) and is perpendicular to the rotational shaft (GS1), wherein a recess for supplying lubricating oil between an inner circumferential surface of the first bushing (F11) and an outer circumferential surface of the rotational shaft (GS1) is opened on the inner circumferential surface within the low pressure range (L), wherein a bushing-side supply passage that connects a bushing-side inlet port opened on the second surface (P2) within the high pressure range (H) with the recess is formed within the first bushing (F11), characterized in that : a body-side supply passage that connects the outlet chamber with a body-side supply port opened on the first surface (P1) within the high pressure range (H) is formed within the pump body (B).
An airfoil for a fan exit stator of a gas turbine engine, the airfoil comprising: an inner diameter edge having a first chord length; an outer diameter edge having a second chord length, wherein the first chord length is larger than the second chord length; a trailing edge ; characterised by a leading edge having a positive aerodynamic sweep across substantially an entire span of the leading edge , wherein a chord of the airfoil continuously decreases from the inner diameter edge to the outer diameter edge ; and wherein a bow of the airfoil is not symmetric around a midspan of the airfoil . an inner diameter edge having a first chord length; an outer diameter edge having a second chord length, wherein the first chord length is larger than the second chord length; a trailing edge ; characterised by a leading edge having a positive aerodynamic sweep across substantially an entire span of the leading edge , wherein a chord of the airfoil continuously decreases from the inner diameter edge to the outer diameter edge ; and wherein a bow of the airfoil is not symmetric around a midspan of the airfoil .