mhurhangee/patent-ind-claim-en huggingface dataset:
A user terminal that receives downlink control information from a radio base station by an enhanced downlink control channel which is frequency-division-multiplexed with a downlink shared data channel, the user terminal comprising: a receiving section configured to receive allocation information of a plurality of frequency resource sets each including a plurality of physical resource block (PRB) pairs placed for the enhanced downlink control channel; and an acquisition section configured to blind decode search space candidates for a given frequency resource set based on the allocation information to acquire the downlink control information, wherein a number of search space candidates per frequency resource set is configured such that a total number of search space candidates for the plurality of frequency resource sets as a whole is not larger than sixteen, characterised in that wherein the plurality of frequency resource sets are two frequency resource sets, and wherein the downlink control information is mapped in a distributed manner to PRB pairs that constitute one of the two frequency resource sets, and the downlink control information is mapped in a localized manner to PRB pairs that constitute an other frequency resource set. a receiving section configured to receive allocation information of a plurality of frequency resource sets each including a plurality of physical resource block (PRB) pairs placed for the enhanced downlink control channel; and an acquisition section configured to blind decode search space candidates for a given frequency resource set based on the allocation information to acquire the downlink control information, wherein a number of search space candidates per frequency resource set is configured such that a total number of search space candidates for the plurality of frequency resource sets as a whole is not larger than sixteen, characterised in that wherein the plurality of frequency resource sets are two frequency resource sets, and wherein the downlink control information is mapped in a distributed manner to PRB pairs that constitute one of the two frequency resource sets, and the downlink control information is mapped in a localized manner to PRB pairs that constitute an other frequency resource set.
A carbamate compound of the following Formula 1, or a pharmaceutically acceptable salt, solvate or hydrate thereof for use in the prevention or treatment of diseases associated with an increase in late sodium current in the heart selected from the group consisting of long QT3 syndrome, arrhythmia, angina pectoris, atrial fibrillation, ventricular tachycardia, ventricular fibrillation, heart failure and hypertrophic cardiomyopathy: wherein, R 1 and R 2 are each independently selected from the group consisting of hydrogen, halogen, C 1 -C 8 alkyl, halo-C 1 -C 8 alkyl, C 1 -C 8 thioalkoxy and C 1 -C 8 alkoxy; and one of A 1 and A 2 is CH, and the other is N. R 1 and R 2 are each independently selected from the group consisting of hydrogen, halogen, C 1 -C 8 alkyl, halo-C 1 -C 8 alkyl, C 1 -C 8 thioalkoxy and C 1 -C 8 alkoxy; and one of A 1 and A 2 is CH, and the other is N.
A method of manufacturing an elevator safety spring characterised in that it comprises: determining a plurality of dimensional parameters (P1-P7, D1-D7) of the elevator safety spring ; selecting a plurality of dimensions within the dimensional parameters (P1-P7, D1-D7); and manufacturing the elevator safety spring based on the selected parameters, the elevator safety spring having an I-beam cross-section. determining a plurality of dimensional parameters (P1-P7, D1-D7) of the elevator safety spring ; selecting a plurality of dimensions within the dimensional parameters (P1-P7, D1-D7); and manufacturing the elevator safety spring based on the selected parameters, the elevator safety spring having an I-beam cross-section.
A method of managing a route (506;704) for an aircraft, the method comprising: displaying the route (506;704)for the aircraft on a map (504;702) on a touchscreen display device ; displaying a number of aeronautical objects comprising waypoints (510,512,514,516,518; 708,714,802,804,806) on the map on the touchscreen display device ; the touchscreen detecting a movement of a number of fingers of a user with respect to the waypoints (510,512,514,516,518; 708,714,802,804,806)on the map (504;702); the touchscreen detecting a direct-to gesture when a single finger of the user is placed at a first selected waypoint and slides from the first selected waypoint to a second selected waypoint ; in response to detecting the direct-to gesture movement of the finger , changing the route displayed by the touchscreen to a new route between the first selected waypoint and the second selected waypoint ; and/or the touchscreen detecting a reroute gesture for changing the route of the aircraft to avoid an obstacle when a pair of fingers of the user are placed at a third selected waypoint and slide from a third selected waypoint around the obstacle to a fourth selected waypoint ; and in response to detecting the reroute gesture movement of the pair of fingers, changing the route displayed by the touchscreen to a new route between the third selected waypoint and the fourth selected waypoint , the new route avoiding the obstacle. displaying the route (506;704)for the aircraft on a map (504;702) on a touchscreen display device ; displaying a number of aeronautical objects comprising waypoints (510,512,514,516,518; 708,714,802,804,806) on the map on the touchscreen display device ; the touchscreen detecting a movement of a number of fingers of a user with respect to the waypoints (510,512,514,516,518; 708,714,802,804,806)on the map (504;702); the touchscreen detecting a direct-to gesture when a single finger of the user is placed at a first selected waypoint and slides from the first selected waypoint to a second selected waypoint ; in response to detecting the direct-to gesture movement of the finger , changing the route displayed by the touchscreen to a new route between the first selected waypoint and the second selected waypoint ; and/or the touchscreen detecting a reroute gesture for changing the route of the aircraft to avoid an obstacle when a pair of fingers of the user are placed at a third selected waypoint and slide from a third selected waypoint around the obstacle to a fourth selected waypoint ; and in response to detecting the reroute gesture movement of the pair of fingers, changing the route displayed by the touchscreen to a new route between the third selected waypoint and the fourth selected waypoint , the new route avoiding the obstacle.
A method of separating a component of an absorbent article comprising: advancing a substrate in a machine direction (MD); providing an ultra-short pulse laser source ; emitting a laser beam with the ultra-short pulse laser source ; directing the laser beam at a portion of the substrate ; cutting a portion of the substrate using the laser beam to form a cut edge , wherein the laser beam is pulsed at a frequency from 100 kHz to 100 MHz, wherein the laser beam has a pulse duration from 5 femtoseconds to 10 picoseconds, and wherein the laser beam has a level of peak energy from 20 μJ to 875 μJ; and forming a heat modified zone along the cut edge , wherein the heat modified zone comprises a maximum width that is less than 200 microns, wherein the maximum width is measured from the cut edge in a direction perpendicular to the cut edge toward to a central region of the substrate . advancing a substrate in a machine direction (MD); providing an ultra-short pulse laser source ; emitting a laser beam with the ultra-short pulse laser source ; directing the laser beam at a portion of the substrate ; cutting a portion of the substrate using the laser beam to form a cut edge , wherein the laser beam is pulsed at a frequency from 100 kHz to 100 MHz, wherein the laser beam has a pulse duration from 5 femtoseconds to 10 picoseconds, and wherein the laser beam has a level of peak energy from 20 μJ to 875 μJ; and forming a heat modified zone along the cut edge , wherein the heat modified zone comprises a maximum width that is less than 200 microns, wherein the maximum width is measured from the cut edge in a direction perpendicular to the cut edge toward to a central region of the substrate .
A gut microbe or culture for use in the prevention or treatment of obesity by lowering fatty acid concentration in the gut fluid contents of a mammalian gastrointestinal tract, wherein said gut microbe or culture is selected from the group consisting of Lactobacillus plantarum JBD302 (KCTC 12918BP), Lactobacillus paracasei JBD305 (KCTC 12921BP) and Lactobacillus fermentum JBD309 (KCTC 12925BP).
A polylactic acid solid composition comprising: a polylactic acid having a weight average molecular weight of not more than 40,000, which is measured in terms of polystyrene standard by GPC; and a basic compound of an alkali metal or an alkaline earth metal, which is a residue of a molecular weight reduction accelerator, wherein the basic compound is contained in an amount in a range of 0.5 to 20 mass%; and wherein the polylactic acid solid composition has a granular form with an average particle diameter (D 50 ) of not more than 10 pm, which is measured by a laser diffraction scattering method.
A handling arrangement for handling a wind turbine rotor blade , comprising - a frame assembly realized to fit about the airfoil of the rotor blade ; - a number of add-on covers arranged to fit between the frame assembly and the airfoil surface, wherein an add-on cover is shaped to fit around a number of add-ons ; and being characterized by - an essentially non-compressible load-bearing material (M) for filling the add-on cover when the add-on cover is pressed against the rotor blade . - a frame assembly realized to fit about the airfoil of the rotor blade ; - a number of add-on covers arranged to fit between the frame assembly and the airfoil surface, wherein an add-on cover is shaped to fit around a number of add-ons ; and being characterized by - an essentially non-compressible load-bearing material (M) for filling the add-on cover when the add-on cover is pressed against the rotor blade .
Wing of an aircraft , said wing comprising: - a fixed main part ; - a movable leading edge slat at the front of the main part between a retracted position, in which it is adjoined to the front of the main part , and a deployed position, in which it is lifted towards the front of the main part , the leading edge slat has an upper surface rear edge , which, in the retracted position, is alongside an upper surface of the main part , and a lower surface rear edge , which, in the retracted position, is alongside a lower surface of the main part , the wing being such that the main part has an upper surface wall , which, in the retracted position of the leading edge slat , comes downstream and in the alignment of the upper surface rear edge , and a lower surface wall , which, in the retracted position of the leading edge slat , comes downstream and in the alignment of the lower surface rear edge , the wing having, in the retracted position of the leading edge slat , an upper surface gap between the end of the upper surface rear edge of the leading edge slat and the end of the upper surface wall of the main part that are facing each other, and a lower surface gap between the end of the lower surface rear edge of the leading edge slat and the end of the lower surface wall of the main part that are facing each other, the wing having an upper surface channel downstream of the upper surface gap and a lower surface channel downstream of the lower surface gap , and the wing comprising a suction system connected to each channel and arranged to suck the air contained in said channel . - a fixed main part ; - a movable leading edge slat at the front of the main part between a retracted position, in which it is adjoined to the front of the main part , and a deployed position, in which it is lifted towards the front of the main part ,
Use of a combination of: a ratio of Aβ1-39 (SEQ ID NO.: 1) level to Aβ1-42 (SEQ ID NO.: 3) level: Aβ1-39/Aβ1-42; a ratio of Aβ1-40 (SEQ ID NO.: 2) level to Aβ1-42 (SEQ ID NO.: 3) level: Aβ1-40/Aβ1-42; and optionally a ratio of APP669-711 (SEQ ID NO.: 4) level to Aβ1-42 (SEQ ID NO.: 3) level: APP669-711/Aβ1-42, in a living body-derived sample, as a marker for determining a cerebral Aβ accumulation state, wherein the living body-derived sample is blood. Aβ1-39/Aβ1-42; a ratio of Aβ1-40 (SEQ ID NO.: 2) level to Aβ1-42 (SEQ ID NO.: 3) level: Aβ1-40/Aβ1-42; and optionally a ratio of APP669-711 (SEQ ID NO.: 4) level to Aβ1-42 (SEQ ID NO.: 3) level: APP669-711/Aβ1-42, in a living body-derived sample, as a marker for determining a cerebral Aβ accumulation state, wherein the living body-derived sample is blood. Aβ1-40/Aβ1-42; and optionally a ratio of APP669-711 (SEQ ID NO.: 4) level to Aβ1-42 (SEQ ID NO.: 3) level: APP669-711/Aβ1-42, in a living body-derived sample, as a marker for determining a cerebral Aβ accumulation state, wherein the living body-derived sample is blood. APP669-711/Aβ1-42, in a living body-derived sample, as a marker for determining a cerebral Aβ accumulation state, wherein the living body-derived sample is blood.
Method for producing a fan housing for a radial fan with an air-guiding cavity which comprises a receiving space for at least one fan wheel which is rotatable about an axis of rotation and an air outlet duct which is connected to the receiving space , wherein the fan housing has at least two housing parts which are made at least in sections of sound-absorbing material, wherein the air-guiding cavity is formed by air-conducting geometries in the at least two housing parts and the air-conducting geometries each have a spiral-shaped defining wall, wherein in each of the at least two housing parts , a part of the receiving space is formed at least partially of sound-absorbing material, wherein at least two air outlet ducts are formed in the fan housing , wherein at least one part of one of the air outlet ducts is formed in each housing part and wherein the defining wall represents a part of the surrounding wall in the receiving space and a side wall of an air outlet duct , characterised in that the air-conducting geometries of the at least two housing parts are created in a single section , that the at least two housing parts are formed by separating the section along at least one plane which is perpendicular to the axis of rotation of the fan wheel and that the at least two housing parts are rotated about the axis of rotation relative to one another and are fastened to one another. wherein the air-guiding cavity is formed by air-conducting geometries in the at least two housing parts and the air-conducting geometries each have a spiral-shaped defining wall, wherein in each of the at least two housing parts , a part of the receiving space is formed at least partially of sound-absorbing material, wherein at least two air outlet ducts are formed in the fan housing , wherein at least one part of one of the air outlet ducts is formed in each housing part and wherein the defining wall represents a part of the surrounding wall in the receiving space and a side wall of an air outlet duct , characterised in that the air-conducting geometries of the at least two housing parts are created in a single section , that the at least two housing parts are formed by separating the section along at least one plane which is perpendicular to the axis of rotation of the fan wheel and that the at least two housing parts are rotated about the axis of rotation relative to one another and are fastened to one another.
A method of, in a machine tool installed on a target user side, calculating a thermal displacement amount between a workpiece (W) and a tool (T) corresponding to a temperature at a measurement point previously set on the machine tool , based on a parameter defining a relation between the temperature at the measurement point and the thermal displacement amount, and correcting a positioning position for the workpiece (W) and the tool (T) in accordance with the calculated thermal displacement amount, characterized in that the method comprises: on a manufacturer side, obtaining, through a telecommunication network , operational status information of the machine tool installed on the target user side, reproducing an operational status identical to the obtained operational status on the target user side with a machine tool of a same type as the machine tool installed on the target user side based on the obtained operational status information without stopping the machine tool installed on the target user side, measuring during reproduction a temperature at a measurement point identical to the measurement point set on the machine tool installed on the target user side and a thermal displacement amount between a workpiece (W) and a tool (T), and calculating the parameter by backpropagation-based supervised machine learning using a neural network based on the measured temperature and thermal displacement amount; and transmitting the calculated parameter to the target user side through the telecommunication network and updating the parameter in the machine tool installed on the target user side with the transmitted parameter. on a manufacturer side, obtaining, through a telecommunication network , operational status information of the machine tool installed on the target user side, reproducing an operational status identical to the obtained operational status on the target user side with a machine tool of a same type as the machine tool installed on the target user side based on the obtained operational status information without stopping the machine tool installed on the target user side, measuring during reproduction a temperature at a measurement point identical to the measurement point set on the machine tool installed on the target user side and a thermal displacement amount between a workpiece (W) and a tool (T), and calculating the parameter by backpropagation-based supervised machine learning using a neural network based on the measured temperature and thermal displacement amount; and transmitting the calculated parameter to the target user side through the telecommunication network and updating the parameter in the machine tool installed on the target user side with the transmitted parameter.
A power electronics system , comprising: an environmentally sealed electronics compartment for housing power electronics equipment; a fan configured to circulate air within the environmentally sealed electronics compartment; a plenum within the sealed electronics compartment for circulating the air across an upper portion of the compartment and down one interior side wall of the compartment to the fan; a first liquid cooling loop configured to cool the air flowing through the plenum; a second liquid cooling loop configured to directly cool the power electronics equipment, the second cooling loop being separate from the first cooling loop; and a controller for independently controlling airflow rates and coolant flow rates of the first liquid cooling loop and the second liquid cooling loop. an environmentally sealed electronics compartment for housing power electronics equipment; a fan configured to circulate air within the environmentally sealed electronics compartment; a plenum within the sealed electronics compartment for circulating the air across an upper portion of the compartment and down one interior side wall of the compartment to the fan; a first liquid cooling loop configured to cool the air flowing through the plenum; a second liquid cooling loop configured to directly cool the power electronics equipment, the second cooling loop being separate from the first cooling loop; and a controller for independently controlling airflow rates and coolant flow rates of the first liquid cooling loop and the second liquid cooling loop.
Unit for a nebulizer , the unit comprising: a container containing a fluid and comprising a rigid housing which is made of metal; and an indicator device configured to count and visually indicate a number of uses of the nebulizer performed or still possible with the container , wherein the indicator device is fixedly arranged at a base of the container and wherein the indicator device comprises an indicator housing which is made of plastic, wherein the housing of the container comprises a protrusion, and wherein the indicator housing comprises a collar or a gripping section , and wherein the collar or gripping section of the indicator housing grips over the protrusion of the housing of the container , wherein the collar or gripping section has been bent over the protrusion in an ultrasonic forming process, so that the indicator housing is inseparably connected with the housing of the container opposite to an outlet or head of the container , and the indicator housing and the container housing cannot be moved against each other. a container containing a fluid and comprising a rigid housing which is made of metal; and an indicator device configured to count and visually indicate a number of uses of the nebulizer performed or still possible with the container , wherein the indicator device is fixedly arranged at a base of the container and wherein the indicator device comprises an indicator housing which is made of plastic, wherein the housing of the container comprises a protrusion, and wherein the indicator housing comprises a collar or a gripping section , and wherein the collar or gripping section of the indicator housing grips over the protrusion of the housing of the container , wherein the collar or gripping section has been bent over the protrusion in an ultrasonic forming process, so that the indicator housing is inseparably connected with the housing of the container opposite to an outlet or head of the container , and the indicator housing and the container housing cannot be moved against each other.
A palladium plate coated material comprising: a base material; an underlying alloy layer formed on the base material; and a palladium plated layer formed on the underlying alloy layer, wherein the underlying alloy layer is formed of a Ni-Pd-P alloy, characterized in that a ratio of each element in the Ni-Pd-P alloy is that Ni is 15 to 65 at. %, Pd is 20 to 60 at. %, and P is 15 to 40 at. %, the base material is one selected from steel, stainless steel, Al, Al alloy, Ti, Ti alloy, Cu, Cu alloy, Ni, and Ni alloy, a thickness of the underlying alloy layer is 5 to 100 nm, and a modifying layer is optionally comprised between the base material and the underlying alloy layer to enhance the interfacial adhesion property between the base material and the underlying alloy layer, the modifying layer being a Ni-based layer. a base material; an underlying alloy layer formed on the base material; and a palladium plated layer formed on the underlying alloy layer, wherein the underlying alloy layer is formed of a Ni-Pd-P alloy, characterized in that a ratio of each element in the Ni-Pd-P alloy is that Ni is 15 to 65 at. %, Pd is 20 to 60 at. %, and P is 15 to 40 at. %, the base material is one selected from steel, stainless steel, Al, Al alloy, Ti, Ti alloy, Cu, Cu alloy, Ni, and Ni alloy, a thickness of the underlying alloy layer is 5 to 100 nm, and a modifying layer is optionally comprised between the base material and the underlying alloy layer to enhance the interfacial adhesion property between the base material and the underlying alloy layer, the modifying layer being a Ni-based layer.