mhurhangee/patent-ind-claim-en huggingface dataset:
Device for controlling the opening/closing of a door wing (A) of a piece of furniture (M) having a body comprising at least a sidewall (S) and a back (R), and defining an inner cavity, said device comprising: - a casing adapted to be mounted on said piece of furniture body; - an inextensible cable , associable at a first end with said door wing (A) and extending with respect to said casing between a retracted position, wherein said door wing (A) is in a closed position, and an extracted position, wherein said door wing (A) is in an opened position, tilted downwards with respect to the body of said piece of furniture (M); and - displacing means connected to said cable and movable with respect to said casing , said displacing means comprising elastic means , characterized in that said casing is arrangeable outside said back (R), first guiding means of said device being provided for guiding said cable along said sidewall (S), wherein said first guiding means comprise a grooved straight conduit adapted to be associated with the inner surface of said sidewall (S) and extending horizontally along the depth of said inner cavity defined by the piece of furniture (M), second guiding means of said device being provided for perpendicularly deviating said cable with respect to said first guiding means . - a casing adapted to be mounted on said piece of furniture body; - an inextensible cable , associable at a first end with said door wing (A) and extending with respect to said casing between a retracted position, wherein said door wing (A) is in a closed position, and an extracted position, wherein said door wing (A) is in an opened position, tilted downwards with respect to the body of said piece of furniture (M); and - displacing means connected to said cable and movable with respect to said casing , said displacing means comprising elastic means ,
An assay comprising: (i) assaying a biological sample obtained from a subject suspected of having an immune-mediated disease characterised by elevated IgG levels to determine the allele at position 131 of the FcγR2a protein;and (ii) selecting the subject for a therapy if the subject expresses the His131 allele of FcγR2a, wherein the therapy comprises an antibody that blocks the neonatal Fc receptor (FcRn). (i) assaying a biological sample obtained from a subject suspected of having an immune-mediated disease characterised by elevated IgG levels to determine the allele at position 131 of the FcγR2a protein;and (ii) selecting the subject for a therapy if the subject expresses the His131 allele of FcγR2a, wherein the therapy comprises an antibody that blocks the neonatal Fc receptor (FcRn).
A method for medical image segmentation, comprising: receiving a medical image set for a current patient comprising a structure of interest; processing the medical image set to produce a sparse landmark signature for the medical image set, wherein the sparse landmark signature reduces the individual slices of a medical image set to only a collection of points; counting the number of points in the sparse landmark signature; forming a base set including a plurality of reference image sets; deforming the base set to the sparse landmark signature of the medical image set to create a statistical model containing segmentation of the structures of interest in the medical image set; deforming a portion of the plurality of reference image sets of the base set to generate mappings from the base set to the medical image set; and characterized by searching a knowledge-base for representative matches of a plurality of reference image sets to the medical image set based on their similarities to the medical image set and corresponding sparse landmark signature set to form a base set; and determining, using a structure-specific segmentation tool using the statistical model, a weighted-average segmentation for each structure of interest in the medical image set. receiving a medical image set for a current patient comprising a structure of interest; processing the medical image set to produce a sparse landmark signature for the medical image set, wherein the sparse landmark signature reduces the individual slices of a medical image set to only a collection of points; counting the number of points in the sparse landmark signature; forming a base set including a plurality of reference image sets; deforming the base set to the sparse landmark signature of the medical image set to create a statistical model containing segmentation of the structures of interest in the medical image set; deforming a portion of the plurality of reference image sets of the base set to generate mappings from the base set to the medical image set; and characterized by searching a knowledge-base for representative matches of a plurality of reference image sets to the medical image set based on their similarities to the medical image set and corresponding sparse landmark signature set to form a base set; and determining, using a structure-specific segmentation tool using the statistical model, a weighted-average segmentation for each structure of interest in the medical image set.
An antenna module , comprising: a feed point ; a ground plane ; a main radiator , comprising a first portion , a second portion , and a third portion , wherein the first portion and the second portion extend from the feed point and meet at an intersection , the third portion at least comprises a first section and a second section , the first section of the third portion is connected to the intersection , and the second section is connected to the ground plane ; and a parasitic radiator , connected to the second section and extending towards the first section of the third portion and having a coupling gap (I) away from the first section , wherein a feed signal is configured to branch at the feed point and go through the first portion and the second portion and then merge at the intersection , and then sequentially go along the third portion and the ground plane to excite at a first frequency band and a second frequency band, and go along a part of the first section of the third portion , the coupling gap (I), the parasitic radiator , the second section of the third portion , and the ground plane to excite at a third frequency band. a feed point ; a ground plane ; a main radiator , comprising a first portion , a second portion , and a third portion , wherein the first portion and the second portion extend from the feed point and meet at an intersection , the third portion at least comprises a first section and a second section , the first section of the third portion is connected to the intersection , and the second section is connected to the ground plane ; and a parasitic radiator , connected to the second section and extending towards the first section of the third portion and having a coupling gap (I) away from the first section , wherein a feed signal is configured to branch at the feed point and go through the first portion and the second portion and then merge at the intersection , and then sequentially go along the third portion and the ground plane to excite at a first frequency band and a second frequency band, and go along a part of the first section of the third portion , the coupling gap (I), the parasitic radiator , the second section of the third portion , and the ground plane to excite at a third frequency band.
A hydrocarbon composition comprising isomerised paraffins, wherein - the hydrocarbon composition has a T10 (°C) cut-off temperature from 185 to 205 °C, a T90 (°C) cut-off temperature from 270 to 295 °C and a final boiling point (°C) from 275 to 300 °C, and - the density of the hydrocarbon composition is from 768.0 to 772.0 kg/m 3 as measured using standard ASTM D4052, and - the average carbon number of the hydrocarbons in the hydrocarbon composition is from 14.3 to 15.1. - the hydrocarbon composition has a T10 (°C) cut-off temperature from 185 to 205 °C, a T90 (°C) cut-off temperature from 270 to 295 °C and a final boiling point (°C) from 275 to 300 °C, and - the density of the hydrocarbon composition is from 768.0 to 772.0 kg/m 3 as measured using standard ASTM D4052, and - the average carbon number of the hydrocarbons in the hydrocarbon composition is from 14.3 to 15.1.
A process for the preparation of Tavaborole of formula (I) comprising the steps of: a) treating (2-bromo-5-fluoro-phenyl)-methanol of formula (V) with trityl chloride in the presence of base and suitable solvent to give 1-bromo-4-fluoro-2-trityloxymethyl-benzene of formula (IV); b) reacting of compound of formula (IV) with bis(pinacolato)diboron in the presence of a transition metal catalyst and a base in suitable solvent to give 2-(4-fluoro-2-tritylmethyl-phenyl)-4,4,5,5-tetramethyl- dioxaborolane of compound of formula (III); c) optionally transesterifying the compound of formula (III) with diethanolamine in suitable solvent to provide the compound of formula (II); d) deprotecting and cyclizing the compound of formula (II) or (III) in the presence of suitable acid and solvent to give Tavaborole of formula (I); and e) optionally purifying Tavaborole of formula (I). a) treating (2-bromo-5-fluoro-phenyl)-methanol of formula (V) with trityl chloride in the presence of base and suitable solvent to give 1-bromo-4-fluoro-2-trityloxymethyl-benzene of formula (IV); b) reacting of compound of formula (IV) with bis(pinacolato)diboron in the presence of a transition metal catalyst and a base in suitable solvent to give 2-(4-fluoro-2-tritylmethyl-phenyl)-4,4,5,5-tetramethyl- dioxaborolane of compound of formula (III); c) optionally transesterifying the compound of formula (III) with diethanolamine in suitable solvent to provide the compound of formula (II); d) deprotecting and cyclizing the compound of formula (II) or (III) in the presence of suitable acid and solvent to give Tavaborole of formula (I); and e) optionally purifying Tavaborole of formula (I).
Hydropneumatic suspension system for vehicles, consisting at least of an axle suspension and a cab suspension , which can be connected to a pressure supply source for supplying them with pressurised fluid, wherein both the axle suspension and the cab suspension can be controlled together by means of an actuating device , characterised in that , by means of a priority identification including a sensor device for the respective suspension , the one suspension is supplied as a priority with pressurised fluid before the respective other suspension depending on requirements.
A rubber composition for tires, comprising: a rubber component comprising 30% by mass or more of a styrene-butadiene rubber having a SiOR group wherein R represents a hydrogen atom or a hydrocarbon group; a silica having a nitrogen adsorption specific surface area of 210 m 2 /g or more in an amount of 50 parts by mass or more per 100 parts by mass of the rubber component; and at least one surfactant selected from the group consisting of polyoxyalkylene alkenyl ether sulfate salts and polyoxyalkylene alkyl ether sulfate salts. a rubber component comprising 30% by mass or more of a styrene-butadiene rubber having a SiOR group wherein R represents a hydrogen atom or a hydrocarbon group; a silica having a nitrogen adsorption specific surface area of 210 m 2 /g or more in an amount of 50 parts by mass or more per 100 parts by mass of the rubber component; and at least one surfactant selected from the group consisting of polyoxyalkylene alkenyl ether sulfate salts and polyoxyalkylene alkyl ether sulfate salts.
Process for the cold treatment of metallic workpieces, in which a workpiece is brought to a low temperature by thermal contact with a cryogenic refrigerant in a cold chamber, where the cold treatment is carried out in three sections, namely a cooling phase during which the temperature of the workpiece is reduced to a lower target temperature, a hold phase in which the workpiece is maintained essentially at the target temperature and a warming phase in which the workpiece is brought to an upper target temperature, where the cooling or warming of the workpiece is interrupted a number of times during the cooling phase and/or the warming phase and the workpiece is maintained at an intermediate temperature for a predetermined period of time, characterized in that the workpiece is warmed a number of times during the hold phase and subsequently cooled back to the lower target temperature, where the lower target temperature is in the range from -170°C to -195°C, preferably from -180°C to -185°C, and the temperature to which the workpiece is warmed during the hold phase is in each case in the range from -140°C to -160°C.
Method of actuating a variable boom loading arrangement , comprising a variable length boom that can be extended and retracted using a length actuator , wherein a first end of the variable length boom is pivotally attached to a frame, and wherein the variable length boom can be pivoted relative to the frame by means of a pivot actuator , and wherein a second end of the variable length boom is used for handling loads, wherein an input command that is given by an operator is modified if the variable boom loading arrangement reaches a predefined tipping moment, resulting in a modified output command to the actuators , so as to avoid a tipping of the variable boom loading arrangement , characterised in that the input command is used to calculate an unmodified commanded direction of the second end of the variable length boom in an external reference frame, in particular in an external Cartesian coordinate reference frame, wherein the modification scheme that is applied to the input command and that results in an modified output command to the actuators depends on the calculated unmodified commanded direction in the external reference frame. wherein a first end of the variable length boom is pivotally attached to a frame, and wherein the variable length boom can be pivoted relative to the frame by means of a pivot actuator , and wherein a second end of the variable length boom is used for handling loads, wherein an input command that is given by an operator is modified if the variable boom loading arrangement reaches a predefined tipping moment, resulting in a modified output command to the actuators , so as to avoid a tipping of the variable boom loading arrangement , characterised in that the input command is used to calculate an unmodified commanded direction of the second end of the variable length boom in an external reference frame, in particular in an external Cartesian coordinate reference frame, wherein the modification scheme that is applied to the input command and that results in an modified output command to the actuators depends on the calculated unmodified commanded direction in the external reference frame.
A method to control the synchronous rectification in a power converter having a transformer including a primary winding and a secondary winding , and a synchronous rectifier, SR, switch connected in series with the secondary winding to rectify current (ISEC) in the secondary winding, the method comprising: detecting a peak current in a secondary winding; determining a blanking threshold based on the peak current; and blanking a turning off of the SR switch for a blanking time based on the blanking threshold wherein the blanking time is scaled in proportion to the peak current and wherein determining a blanking threshold comprises: sensing a drain to source voltage, VDS, of the switch connected in series with the secondary winding; charging the gate voltage of the SR switch until the sensed drain to source voltage reaches a predetermined regulation level and changing the gate voltage of the SR switch to regulate the drain to source voltage to the predetermined level, and using the gate voltage of the SR switch to set the blanking threshold. detecting a peak current in a secondary winding; determining a blanking threshold based on the peak current; and blanking a turning off of the SR switch for a blanking time based on the blanking threshold wherein the blanking time is scaled in proportion to the peak current and wherein determining a blanking threshold comprises: sensing a drain to source voltage, VDS, of the switch connected in series with the secondary winding; charging the gate voltage of the SR switch until the sensed drain to source voltage reaches a predetermined regulation level and changing the gate voltage of the SR switch to regulate the drain to source voltage to the predetermined level, and using the gate voltage of the SR switch to set the blanking threshold. sensing a drain to source voltage, VDS, of the switch connected in series with the secondary winding; charging the gate voltage of the SR switch until the sensed drain to source voltage reaches a predetermined regulation level and changing the gate voltage of the SR switch to regulate the drain to source voltage to the predetermined level, and using the gate voltage of the SR switch to set the blanking threshold.
A helicopter flight support for a helicopter comprising: a first outer support having a first end configured to be pivotally coupled to a bottom of the helicopter near the front of the helicopter; a second outer support having a second end configured to be pivotally coupled to the bottom of the helicopter opposite the first outer support; a rotatable shaft having a threaded portion configured to be coupled to the helicopter between the first outer support and the second outer support; a motor for rotating the threaded shaft; a deployment support having a threaded opening configured to mate with the threaded portion of the rotatable shaft; a first inner support having a third end pivotally coupled to a fourth end of the first outer support at a first pivot joint; a second inner support having a fifth end pivotally coupled to a sixth end of the second outer support at a second pivot joint, wherein a seventh end of the first inner support is pivotally coupled to the deployment support, and wherein an eighth end of the second inner support is pivotally coupled to the deployment support; and a first layer of fabric and a second layer of fabric having a wing shape coupled to the first outer support, the second outer support, the first inner support, and the second inner support; wherein rotation of the rotatable shaft in a first direction by the motor causes movement of the deployment support along the threaded section towards, in use, a rear of the helicopter to cause deployment of the helicopter flight support. a first outer support having a first end configured to be pivotally coupled to a bottom of the helicopter near the front of the helicopter; a second outer support having a second end configured to be pivotally coupled to the bottom of the helicopter opposite the first outer support; a rotatable shaft having a threaded portion configured to be coupled to the helicopter between the first outer support and the second outer support; a motor for rotating the threaded shaft; a deployment support having a threaded opening configured to mate with the threaded portion of the rotatable shaft; a first inner support having a third end pivotally coupled to a fourth end of the first outer support at a first pivot joint; a second inner support having a fifth end pivotally coupled to a sixth end of the second outer support at a second pivot joint, wherein a seventh end of the first inner support is pivotally coupled to the deployment support, and wherein an eighth end of the second inner support is pivotally coupled to the deployment support; and a first layer of fabric and a second layer of fabric having a wing shape coupled to the first outer support, the second outer support, the first inner support, and the second inner support; wherein rotation of the rotatable shaft in a first direction by the motor causes movement of the deployment support along the threaded section towards, in use, a rear of the helicopter to cause deployment of the helicopter flight support.
A hairpin welding method in which the wire ends of at least two copper wires , the wire ends being arranged flush next to one another, are welded to one another by a laser beam , the method being characterized by : generating a laser beam with a beam cross section which impinges the wire ends at an end side and which has a round core region and a ring region surrounding, in particular directly surrounding, the core region , wherein - the ratio of the outer diameter (d R ) of the ring region to the diameter (d K ) of the core region is between 5:1 and 2:1, preferably approximately 4:1, - the spot diameter (s K ) of the core region at the wire ends is between 50 μm and 200 μm, in particular approximately 85 μm, - the spot diameter (s R ) of the ring region at the wire ends is between 250 μm and 700 μm, in particular approximately 340 μm, and - the ratio of the laser power in the core region to the laser power in the ring region is between 25:75 and 70:30, particularly preferably approximately 30:70. - the ratio of the outer diameter (d R ) of the ring region to the diameter (d K ) of the core region is between 5:1 and 2:1, preferably approximately 4:1, - the spot diameter (s K ) of the core region at the wire ends is between 50 μm and 200 μm, in particular approximately 85 μm, - the spot diameter (s R ) of the ring region at the wire ends is between 250 μm and 700 μm, in particular approximately 340 μm, and - the ratio of the laser power in the core region to the laser power in the ring region is between 25:75 and 70:30, particularly preferably approximately 30:70.
An Light-Emitting Diode (LED) chip module comprising: a first electrode plate , wherein a first set of LED chips is set on the upper surface of the first electrode plate; a second electrode plate , wherein a second set of LED chips is set on the upper surface of the second electrode plate, and the second set of LED chips is electrically connected to the first set of LED chips; a plastic shell , wherein the plastic shell is fixedly connected to the first electrode plate and the second electrode plate by injection molding to make the first electrode plate and the second electrode plate keep a predetermined space between each other and make a lower surface of the first electrode plate and a lower surface of the second electrode plate be respectively connected to two different polarity terminals of the power supply to drive the first set of LED chips and the second set of LED chips to emit light; and fluorescent, wherein the fluorescent covers the first set of LED chips and the second set of LED chips; characterized in that : an extending direction is a direction vertical to a facing direction in which the first electrode plate and the second electrode plate face each other, a length of the first electrode plate and the second electrode plate in an extending direction is larger than 90% with respect to the total length of the plastic shell in the extending direction. a first electrode plate , wherein a first set of LED chips is set on the upper surface of the first electrode plate; a second electrode plate , wherein a second set of LED chips is set on the upper surface of the second electrode plate, and the second set of LED chips is electrically connected to the first set of LED chips; a plastic shell , wherein the plastic shell is fixedly connected to the first electrode plate and the second electrode plate by injection molding to make the first electrode plate and the second electrode plate keep a predetermined space between each other and make a lower surface of the first electrode plate and a lower surface of the second electrode plate be respectively connected to two different polarity terminals of the power supply to drive the first set of LED chips and the second set of LED chips to emit light; and fluorescent, wherein the fluorescent covers the first set of LED chips and the second set of LED chips; characterized in that : an extending direction is a direction vertical to a facing direction in which the first electrode plate and the second electrode plate face each other, a length of the first electrode plate and the second electrode plate in an extending direction is larger than 90% with respect to the total length of the plastic shell in the extending direction.