mhurhangee/patent-ind-claim-en huggingface dataset:
A part made of composite material, in particular for an aircraft turbine engine , comprising: - a body made of fibres woven in three-dimensions and immersed in a resin, in particular an organic or polymer resin, - at least one crack sensor capable of detecting a crack in the part , and - at least one link element connected to the crack sensor and configured to transmit a signal (S), in particular to a member outside of the part , when a crack in the part is detected, characterised in that : - the crack sensor comprises at least one conductive wire woven with the fibres of the body and extending into an area (Z1) of the body in which the presence of the crack is to be monitored, and - the link element is connected to ends of the conductive wire and is configured to measure the resistance of the conductive wire and to wirelessly transmit the signal (S), when the measured resistance of the conductive wire is above a predetermined threshold. - a body made of fibres woven in three-dimensions and immersed in a resin, in particular an organic or polymer resin, - at least one crack sensor capable of detecting a crack in the part , and - at least one link element connected to the crack sensor and configured to transmit a signal (S), in particular to a member outside of the part , when a crack in the part is detected, - the crack sensor comprises at least one conductive wire woven with the fibres of the body and extending into an area (Z1) of the body in which the presence of the crack is to be monitored, and - the link element is connected to ends of the conductive wire and is configured to measure the resistance of the conductive wire and to wirelessly transmit the signal (S), when the measured resistance of the conductive wire is above a predetermined threshold.
A thermal management system , comprising: a drive shaft ; one or more air management baffles surrounding at least a portion of the drive shaft ; insulation positioned about at least a portion of the drive shaft when in use, adjacent to an engine compartment of an aircraft, wherein the insulation surrounds at least a portion of the one or more air management baffles ; and one or more fans or impellers (138a-c) in fluid communication with at least a portion of the drive shaft , wherein the one or more fans or impellers (138a-c) are located around the drive shaft , connected to the drive shaft , and powered independently of the drive shaft ; wherein the one or more air management baffles are configured to direct air to the one or more fans or impellers (138a-c); and wherein the one or more air management baffles are configured to direct air flow between the impeller and the at least a portion of the drive shaft wherein the directed air flow removes heat from the drive shaft that originates, when in use, in the engine compartment of the aircraft . a drive shaft ; one or more air management baffles surrounding at least a portion of the drive shaft ; insulation positioned about at least a portion of the drive shaft when in use, adjacent to an engine compartment of an aircraft, wherein the insulation surrounds at least a portion of the one or more air management baffles ; and one or more fans or impellers (138a-c) in fluid communication with at least a portion of the drive shaft , wherein the one or more fans or impellers (138a-c) are located around the drive shaft , connected to the drive shaft , and powered independently of the drive shaft ; wherein the one or more air management baffles are configured to direct air to the one or more fans or impellers (138a-c); and wherein the one or more air management baffles are configured to direct air flow between the impeller and the at least a portion of the drive shaft wherein the directed air flow removes heat from the drive shaft that originates, when in use, in the engine compartment of the aircraft .
A compound represented by Formula (I) below or a salt thereof; where A is a linking group represented as -X-NHCO- where X is a C 1 to C 6 alkylene group, each of R 1 , R 2 , R 4 , R 5 , R 7 , R 8 , R 10 , and R 11 is a hydrogen atom, each of R 3 , R 6 , and R 9 is a substituent of Formulae (iii) below; R 12 is selected from a group of substituents represented by Formula (i) or (ii) above, R 13 is a sulfo group, Ra, Rb, and Rc in Formula (i) and (ii) above are substituents independently selected from C 1 to C 6 alkyl groups, and Rd in Formula (iii) above is a hydrogen atom or a C 1 to C 6 alkyl group, and Rx in Formula (iii) above is a substituent represented by General Formula (i) or (ii) above. where A is a linking group represented as -X-NHCO- where X is a C 1 to C 6 alkylene group, each of R 1 , R 2 , R 4 , R 5 , R 7 , R 8 , R 10 , and R 11 is a hydrogen atom, each of R 3 , R 6 , and R 9 is a substituent of Formulae (iii) below; R 12 is selected from a group of substituents represented by Formula (i) or (ii) above, R 13 is a sulfo group, Ra, Rb, and Rc in Formula (i) and (ii) above are substituents independently selected from C 1 to C 6 alkyl groups, and Rd in Formula (iii) above is a hydrogen atom or a C 1 to C 6 alkyl group, and Rx in Formula (iii) above is a substituent represented by General Formula (i) or (ii) above.
A hub motor arrangement , comprising: a housing defining an interior space and an axis of rotation; a first lateral support member positioned at least partially within the interior space of the housing ; a second lateral support member positioned at least partially within the interior space of the housing and spaced from the first lateral support member along the axis of rotation; a plurality of connecting shafts extending between the first lateral support member and the second lateral support member ; a plurality of planet gears , each planet gear being a double spur gear supported on a respective one of the plurality of connecting shafts ; a motor ; a sun gear driven by the motor and that drives a first gear portion of each of the plurality of planet gears ; a ring gear driven by a second gear portion of each of the plurality of planet gears , wherein the ring gear drives the housing for rotation about the axis of rotation; and a first bearing and a second bearing which support the housing for rotation, characterized in that the second bearing is axially aligned with an intermediate portion of the motor such that a first portion of the motor is located outboard of the second bearing and outside of the housing , and a second portion of the motor is located inboard of the second bearing and within the housing . a housing defining an interior space and an axis of rotation; a first lateral support member positioned at least partially within the interior space of the housing ; a second lateral support member positioned at least partially within the interior space of the housing and spaced from the first lateral support member along the axis of rotation; a plurality of connecting shafts extending between the first lateral support member and the second lateral support member ; a plurality of planet gears , each planet gear being a double spur gear supported on a respective one of the plurality of connecting shafts ; a motor ; a sun gear driven by the motor and that drives a first gear portion of each of the plurality of planet gears ; a ring gear driven by a second gear portion of each of the plurality of planet gears , wherein the ring gear drives the housing for rotation about the axis of rotation; and a first bearing and a second bearing which support the housing for rotation, characterized in that the second bearing is axially aligned with an intermediate portion of the motor such that a first portion of the motor is located outboard of the second bearing and outside of the housing , and a second portion of the motor is located inboard of the second bearing and within the housing .
A freeze-dried formulation obtained by freeze-drying an aqueous formulation comprising (i) at least one poxvirus-based material, (ii) between 5g/L and 80g/L of at least one polymer selected in the group of polyvinylpyrrolidone, copovidone and mixtures thereof, (iii) between 20g/L and 80g/L of at least one disaccharide, (iv) between 5g/L and 100g/L of arginine and between 1g/L and 10g/L of glutamate, (v) at least 0.1g/L of at least one pharmaceutical acceptable phosphate salt and between 1g/L and 5g/L of at least one pharmaceutical acceptable monovalent salt and, optionally (vi) a pharmaceutical acceptable buffer.
A control system for a crane in which an actuator is controlled based on a target speed signal relating to a moving direction and a speed of a load (W), the control system comprising: a feedback control section that computes a target course signal for the load (W) from the target speed signal by integration, corrects the target course signal based on a difference of a current position of the load (W) from the target course signal for the load (W), and computes a target position of the load (W) from the corrected target course signal; and a feedforward control section that adjusts a weight coefficient of a transfer function representing a characteristic of the crane based on the corrected target course signal and corrects the corrected target course signal using the transfer function with the weight coefficient adjusted, wherein each time the target course signal is corrected by the feedback control section , the weight coefficient of the transfer function is adjusted by the feedforward control section . a feedback control section that computes a target course signal for the load (W) from the target speed signal by integration, corrects the target course signal based on a difference of a current position of the load (W) from the target course signal for the load (W), and computes a target position of the load (W) from the corrected target course signal; and a feedforward control section that adjusts a weight coefficient of a transfer function representing a characteristic of the crane based on the corrected target course signal and corrects the corrected target course signal using the transfer function with the weight coefficient adjusted, wherein each time the target course signal is corrected by the feedback control section , the weight coefficient of the transfer function is adjusted by the feedforward control section .
A tablet formulation comprising; - enalapril maleate - lercanidipine hydrochloride - at least one buffering agent wherein further comprising at least two fillers and wherein said tablet formulation further comprises colloidal silicon dioxide as a glidant; wherein the total amount of enalapril maleate in the tablet is between 3.0% and 15.0% by weight, the total amount of lercanidipine hydrochloride in the tablet is between 1.0% and 8.0% by weight. - enalapril maleate - lercanidipine hydrochloride - at least one buffering agent
A method of dissolving and/or inhibiting the deposition of scale on a surface of a system, wherein the scale comprises calcium carbonate, said method comprising the step of bringing the surface of the system into contact with a composition comprising: A) from 3 to 15 parts by weight, based on 100 parts by weight of the composition, of a chelating component comprising methylglycine-N-N-diacetic acid (MGDA) and/or an alkali salt thereof, wherein MGDA is present in the chelating component in an amount of 35 to 95 parts by weight, based on 100 parts by weight of the chelating component; B) from 3 to 15 parts by weight, based on 100 parts by weight of the composition, of an aqueous acidic component comprising methanesulfonic acid in amounts of from 35 to 95 parts by weight, based on 100 parts by weight of the acidic component; C) at least 60 parts by weight of water, based on 100 parts by weight of the composition; D) optionally, a surfactant component; E) optionally, a corrosion inhibitor, wherein the composition has a pH of from 5 to 7, and wherein the method further comprises a step of applying heat to the composition and/or the system. A) from 3 to 15 parts by weight, based on 100 parts by weight of the composition, of a chelating component comprising methylglycine-N-N-diacetic acid (MGDA) and/or an alkali salt thereof, wherein MGDA is present in the chelating component in an amount of 35 to 95 parts by weight, based on 100 parts by weight of the chelating component; B) from 3 to 15 parts by weight, based on 100 parts by weight of the composition, of an aqueous acidic component comprising methanesulfonic acid in amounts of from 35 to 95 parts by weight, based on 100 parts by weight of the acidic component; C) at least 60 parts by weight of water, based on 100 parts by weight of the composition; D) optionally, a surfactant component; E) optionally, a corrosion inhibitor,
A corrugated board comprising a corrugated medium, a liner and an adhesive arranged to attach the fluted corrugated medium to the liner wherein the adhesive comprises starch and microfibrillated cellulose characterized in that the microfibrillated cellulose has a Schopper-Riegler (SR) value above 97.
A processor comprising: a first source vector register to store a first plurality of source bit groups, wherein a size for the bit groups is to be specified in an immediate of an instruction; a second source vector to store a second plurality of source bit groups; vector bit reversal and crossing logic to determine a bit group size from the immediate and to responsively reverse positions of contiguous bit groups within the first source vector register to generate a set of reversed bit groups, wherein the vector bit reversal and crossing logic is to additionally interleave the set of reversed bit groups with the second plurality of bit groups; and a destination vector register to store the reversed bit groups interleaved with the first plurality of bit groups wherein the vector bit reversal and crossing logic is to determine, from the immediate, whether to interleave the set of reversed bit groups with the second plurality of bit groups and to determine, from the immediate, an order of selecting from the set of reversed bit groups or the second plurality of bit groups to interleave. a first source vector register to store a first plurality of source bit groups, wherein a size for the bit groups is to be specified in an immediate of an instruction; a second source vector to store a second plurality of source bit groups; vector bit reversal and crossing logic to determine a bit group size from the immediate and to responsively reverse positions of contiguous bit groups within the first source vector register to generate a set of reversed bit groups, wherein the vector bit reversal and crossing logic is to additionally interleave the set of reversed bit groups with the second plurality of bit groups; and a destination vector register to store the reversed bit groups interleaved with the first plurality of bit groups wherein the vector bit reversal and crossing logic is to determine, from the immediate, whether to interleave the set of reversed bit groups with the second plurality of bit groups and to determine, from the immediate, an order of selecting from the set of reversed bit groups or the second plurality of bit groups to interleave.
Method for producing at least one silicon-based negative electrode, wherein the method comprises the following method steps: a) providing at least one silicon-based negative electrode precursor, an electrolyte and at least one lithium-based counterelectrode, b) applying at least three successive, constant voltages of respectively 1.2 V-1.8 V, 400 mV-800 mV and 200 mV-390 mV between the at least one silicon-based negative electrode precursor and the at least one lithium-based counterelectrode for in each case a time period of at least 35 minutes, and c) obtaining the silicon-based negative electrode. a) providing at least one silicon-based negative electrode precursor, an electrolyte and at least one lithium-based counterelectrode, b) applying at least three successive, constant voltages of respectively 1.2 V-1.8 V, 400 mV-800 mV and 200 mV-390 mV between the at least one silicon-based negative electrode precursor and the at least one lithium-based counterelectrode for in each case a time period of at least 35 minutes, and c) obtaining the silicon-based negative electrode.
Tray for containing a number of eggs in an incubation chamber, the tray comprising a number of egg accommodation spaces in which spaces an egg is able to be hatched, and a number of passages for a chicken through which passages a chicken hatched from said egg may pass through the tray and enter a chicken accommodation space located below the tray, characterised in that the passages are configured such that a chicken may pass the passages and an egg is not passable through the passages, and wherein the number of passages optimize the transition of chickens from the tray to a chicken accommodation space located below the tray.
A nanocrystalline alloy magnetic core production method having a primary heat treatment step conducted in the absence of an applied magnetic field, comprising: increasing a temperature of an amorphous magnetic core material formed of an amorphous alloy ribbon capable of undergoing nanocrystallization, from a temperature that is lower than a crystallization onset temperature of the magnetic core material to a temperature that is higher than or equal to the crystallization onset temperature, decreasing the temperature to a temperature that is lower than the crystallization onset temperature with an actual maintenance time of 1 minute or more, wherein the actual maintenance time is defined as the period of time between when the temperature of the magnetic core reaches a temperature range of ±5°C with respect to the set temperature of the magnetic core at which the application of a magnetic field is started, and when the application of a magnetic field is started in the following secondary heat treatment step, and a secondary heat treatment step of applying a magnetic field in a direction perpendicular to a magnetic path, wherein in the secondary heat treatment step, the magnetic field is applied while the temperature is decreased at an average rate of 4°C/min or less. increasing a temperature of an amorphous magnetic core material formed of an amorphous alloy ribbon capable of undergoing nanocrystallization, from a temperature that is lower than a crystallization onset temperature of the magnetic core material to a temperature that is higher than or equal to the crystallization onset temperature, decreasing the temperature to a temperature that is lower than the crystallization onset temperature with an actual maintenance time of 1 minute or more, wherein the actual maintenance time is defined as the period of time between when the temperature of the magnetic core reaches a temperature range of ±5°C with respect to the set temperature of the magnetic core at which the application of a magnetic field is started, and when the application of a magnetic field is started in the following secondary heat treatment step, and a secondary heat treatment step of applying a magnetic field in a direction perpendicular to a magnetic path, wherein in the secondary heat treatment step, the magnetic field is applied while the temperature is decreased at an average rate of 4°C/min or less.
A face mask , comprising: an outer casing having an opening; a filter member for mounting inside the outer casing , wherein a mask cavity is defined between the filter member and the face of a user when face mask is worn by the user; and a fan module , wherein: the filter member comprises a first connector part ; the fan module comprises a second connector part , for connection to the first connector part thereby to fix the fan module to the filter member, and a third connector part ; and the outer casing comprises a fourth connector part , for connection to the third connector part thereby to fix the outer casing to fan module , with the fan module projecting through the opening. an outer casing having an opening; a filter member for mounting inside the outer casing , wherein a mask cavity is defined between the filter member and the face of a user when face mask is worn by the user; and a fan module , wherein: the filter member comprises a first connector part ; the fan module comprises a second connector part , for connection to the first connector part thereby to fix the fan module to the filter member, and a third connector part ; and the outer casing comprises a fourth connector part , for connection to the third connector part thereby to fix the outer casing to fan module , with the fan module projecting through the opening. the filter member comprises a first connector part ; the fan module comprises a second connector part , for connection to the first connector part thereby to fix the fan module to the filter member, and a third connector part ; and the outer casing comprises a fourth connector part , for connection to the third connector part thereby to fix the outer casing to fan module , with the fan module projecting through the opening.
A busbar current sensor assembly , comprising: a busbar member including a base including a first surface facing in a first direction and a second surface facing in a second direction, the first direction being opposite the second direction, a first boundary wall extending from the first surface of the base in a direction away from the second surface , the first boundary wall and the first surface cooperating to define a first cavity , and a second boundary wall extending from the second surface of the base in a direction away from the first surface , the second boundary wall and the second surface cooperating to define a second cavity ; a first current sensor disposed in the first cavity ; a second current sensor disposed in the second cavity ; a first cover ; and a second cover , wherein the first boundary wall defines a first ledge portion and the second boundary wall defines a second ledge portion , and wherein the first ledge portion receives the first cover and the second ledge portion receives the second cover so as to enclose the first cavity and the second cavity , respectively; the base , the first boundary wall , and the second boundary wall being made of an electrically conductive material. a busbar member including a base including a first surface facing in a first direction and a second surface facing in a second direction, the first direction being opposite the second direction, a first boundary wall extending from the first surface of the base in a direction away from the second surface , the first boundary wall and the first surface cooperating to define a first cavity , and a second boundary wall extending from the second surface of the base in a direction away from the first surface , the second boundary wall and the second surface cooperating to define a second cavity ; a base including a first surface facing in a first direction and a second surface facing in a second direction, the first direction being opposite the second direction, a first boundary wall extending from the first surface of the base in a direction away from the second surface , the first boundary wall and the first surface cooperating to define a first cavity , and a second boundary wall extending from the second surface of the base in a direction away from the first surface , the second boundary wall and the second surface cooperating to define a second cavity ; a first current sensor disposed in the first cavity ; a second current sensor disposed in the second cavity ; a first cover ; and a second cover , wherein the first boundary wall defines a first ledge portion and the second boundary wall defines a second ledge portion , and wherein the first ledge portion receives the first cover and the second ledge portion receives the second cover so as to enclose the first cavity and the second cavity , respectively;