mhurhangee/patent-ind-claim-en huggingface dataset:
Hot runner device, which comprises at least one needle valve nozzle and a shut-off needle which is movable with a moving means in the needle valve nozzle , as well as an overload protection device for the shut-off needle , characterized in that the overload protection device is realized as follows: the shut-off needle is connected to the moving means in at least one first direction of movement directly or indirectly by at least one frictional connection which is releasable when exceeding a limit force.
A brake pad for a disk brake assembly , comprising a lining made of friction material and a plate supporting the lining , wherein: - the lining comprises: o a friction face and a fastening face , o a rear edge , located on the side where the disk is capable of coming out of an interface with the pad when the disk rotates in a direction of advance of the vehicle, and a front edge , o an inner edge and an outer edge , and o a collection groove open on the friction face and arranged close to the rear edge , - the plate includes a hole in fluid communication with the collection groove , the hole being able to be connected to a vacuum source via communication means , the lining including a rear region comprising the rear edge and the collection groove , the rear region including a chamfered portion such that an area of a friction surface of the rear region increases when a thickness of the rear region decreases, the collection groove being arranged at a distance from a free surface of the chamfered portion characterised in that the collection groove comprises a cross-section which extends obliquely towards the free surface of the chamfered portion and in that the collection groove leads into the inner edge or outer edge . - the lining comprises: o a friction face and a fastening face , o a rear edge , located on the side where the disk is capable of coming out of an interface with the pad when the disk rotates in a direction of advance of the vehicle, and a front edge , o an inner edge and an outer edge , and o a collection groove open on the friction face and arranged close to the rear edge , o a friction face and a fastening face , o a rear edge , located on the side where the disk is capable of coming out of an interface with the pad when the disk rotates in a direction of advance of the vehicle, and a front edge , o an inner edge and an outer edge , and o a collection groove open on the friction face and arranged close to the rear edge , - the plate includes a hole in fluid communication with the collection groove , the hole being able to be connected to a vacuum source via communication means ,
A gas turbine engine comprising: one of a turbine section and a compressor section comprised of a plurality of stages; at least one of the stages in the plurality of stages defining an outer diameter comprised of a plurality of circumferentially arranged blade outer air seals , each blade outer air seal being spaced from each adjacent blade outer air seal in the plurality of circumferentially arranged blade outer air seals via a mateface gap an airstream is received at each blade outer air seal , and is flowed circumferentially through the blade outer air seal to provide cooling air to the blade outer air seal , wherein the mateface gap is oblique to a radius of the gas turbine engine , such that the cooling air entering the mateface gap from the blade outer air seals is directed to an inner diameter surface of at least one of the blade outer air seals in the plurality of blade outer air seals ; and characterised in that at least one of the mateface gaps includes a cross sectional outlet area that is smaller than a cross sectional area of the mateface gap where the cooling air enters the gap thereby creating a nozzle fluid exit. one of a turbine section and a compressor section comprised of a plurality of stages; at least one of the stages in the plurality of stages defining an outer diameter comprised of a plurality of circumferentially arranged blade outer air seals , each blade outer air seal being spaced from each adjacent blade outer air seal in the plurality of circumferentially arranged blade outer air seals via a mateface gap an airstream is received at each blade outer air seal , and is flowed circumferentially through the blade outer air seal to provide cooling air to the blade outer air seal , wherein the mateface gap is oblique to a radius of the gas turbine engine , such that the cooling air entering the mateface gap from the blade outer air seals is directed to an inner diameter surface of at least one of the blade outer air seals in the plurality of blade outer air seals ; and characterised in that at least one of the mateface gaps includes a cross sectional outlet area that is smaller than a cross sectional area of the mateface gap where the cooling air enters the gap thereby creating a nozzle fluid exit.
An autonomic function information acquisition device , comprising: an acceleration information measurement unit that is provided in a wearable device , and configured to measure acceleration information of motion of a subject whom the wearable device is attached to; a biological signal information measurement unit that is provided in the wearable device, and configured to measure heart rate data of the subject; an identification unit configured to identify, by executing sequential machine learning for the acceleration information and the biological signal information in a first predetermined period, a posture and an activity of the subject in a second predetermined period; an extraction unit configured to extract heart rate data corresponding to a combination of the same posture and activity identified by the identification unit; and a calculation unit configured to calculate a parameter of autonomic function evaluation from the heart rate data extracted by the extraction unit and corresponding to the combination of the same posture and activity. an acceleration information measurement unit that is provided in a wearable device , and configured to measure acceleration information of motion of a subject whom the wearable device is attached to; a biological signal information measurement unit that is provided in the wearable device, and configured to measure heart rate data of the subject; an identification unit configured to identify, by executing sequential machine learning for the acceleration information and the biological signal information in a first predetermined period, a posture and an activity of the subject in a second predetermined period; an extraction unit configured to extract heart rate data corresponding to a combination of the same posture and activity identified by the identification unit; and a calculation unit configured to calculate a parameter of autonomic function evaluation from the heart rate data extracted by the extraction unit and corresponding to the combination of the same posture and activity.
A vehicle motion control device which controls a motion of a vehicle , comprising: a target trajectory acquisition unit which acquires a target trajectory of the vehicle ; a lateral motion prediction unit which predicts a lateral motion of the vehicle based on the target trajectory; and a YAW moment control unit which controls a YAW moment generated in the vehicle by a difference of braking/driving forces of right and left wheels of the vehicle according to the lateral motion of the vehicle , wherein the YAW moment control unit controls the YAW moment generated in the vehicle in a first period predicted by the lateral motion prediction unit when the lateral motion of the vehicle is changed from a state where the vehicle takes one of right and left lateral motions to a state where the vehicle takes the other lateral motion, characterized in that the YAW moment control unit sets an absolute value of a longitudinal deceleration generated in the vehicle in a second period predicted by the lateral motion prediction unit to be smaller than an absolute value of longitudinal deceleration generated in the vehicle in the first period when the lateral motion of the vehicle is changed from a state where the vehicle takes the lateral motion to a state where the vehicle does not take the lateral motion. a target trajectory acquisition unit which acquires a target trajectory of the vehicle ; a lateral motion prediction unit which predicts a lateral motion of the vehicle based on the target trajectory; and a YAW moment control unit which controls a YAW moment generated in the vehicle by a difference of braking/driving forces of right and left wheels of the vehicle according to the lateral motion of the vehicle , wherein the YAW moment control unit controls the YAW moment generated in the vehicle in a first period predicted by the lateral motion prediction unit when the lateral motion of the vehicle is changed from a state where the vehicle takes one of right and left lateral motions to a state where the vehicle takes the other lateral motion, characterized in that the YAW moment control unit sets an absolute value of a longitudinal deceleration generated in the vehicle in a second period predicted by the lateral motion prediction unit to be smaller than an absolute value of longitudinal deceleration generated in the vehicle in the first period when the lateral motion of the vehicle is changed from a state where the vehicle takes the lateral motion to a state where the vehicle does not take the lateral motion.
A motorised manoeuvring system for a device of a motor vehicle comprising an apparatus for provisionally locking said system, the manoeuvring system comprising a drive pinion of a cable intended to be rotated around an axis (A) by a geared motor , the cable carrying a helical spline configured to cooperate with the external toothing of said drive pinion and being arranged to translate at least one actuating element of the device, the drive pinion and the cable being disposed in a casing , characterised in that the casing comprises a base , on which are mounted the drive pinion and the cable , and a closure cover which is fixed on the base , and in that the locking apparatus comprises a compression spring mounted on the base and pushing along the axis (A) the drive pinion against an inner face of the cover and means for locking the drive pinion provided on said inner face of the cover and cooperating with the drive pinion under the effect of the compression spring when the geared motor is detached from the casing .
A method of making a molded 3-dimensional fabric article, the process comprising the steps of: (i) providing a thermoformable fabric substrate having a top face and a bottom face; (ii) applying an uncured elastomeric coating composition comprising an elastomeric polymer onto the top and/or bottom face of the fabric substrate in accordance with a pattern to form a thermoformable blank patterned with the uncured elastomeric coating composition; (iii) thermoformably moulding the blank by applying a 3-dimensional mold for a period of time to provide a 3-dimensional molded article that is patterned with a cured elastomeric coating composition; and (iv) removing the molded article from the mold, and optionally trimming any excess fabric, to provide a molded 3-dimensional fabric article, wherein: the elastomeric coating composition further comprises an agent that retards the curing of an elastomeric coating; the 3-dimensional mold in step (iii) is applied at a temperature and pressure sufficient to form the desired 3-dimensional molded article from the thermoformable fabric substrate and cure the uncured elastomeric coating composition during the period of time that it is applied to the blank, and the molded 3-dimensional fabric article is a textile, forms the whole of a garment or forms a part of a garment. (i) providing a thermoformable fabric substrate having a top face and a bottom face; (ii) applying an uncured elastomeric coating composition comprising an elastomeric polymer onto the top and/or bottom face of the fabric substrate in accordance with a pattern to form a thermoformable blank patterned with the uncured elastomeric coating composition; (iii) thermoformably moulding the blank by applying a 3-dimensional mold for a period of time to provide a 3-dimensional molded article that is patterned with a cured elastomeric coating composition; and (iv) removing the molded article from the mold, and optionally trimming any excess fabric, to provide a molded 3-dimensional fabric article, wherein: the elastomeric coating composition further comprises an agent that retards the curing of an elastomeric coating; the 3-dimensional mold in step (iii) is applied at a temperature and pressure sufficient to form the desired 3-dimensional molded article from the thermoformable fabric substrate and cure the uncured elastomeric coating composition during the period of time that it is applied to the blank, and the molded 3-dimensional fabric article is a textile, forms the whole of a garment or forms a part of a garment. the elastomeric coating composition further comprises an agent that retards the curing of an elastomeric coating; the 3-dimensional mold in step (iii) is applied at a temperature and pressure sufficient to form the desired 3-dimensional molded article from the thermoformable fabric substrate and cure the uncured elastomeric coating composition during the period of time that it is applied to the blank, and the molded 3-dimensional fabric article is a textile, forms the whole of a garment or forms a part of a garment.
A system configured to treat a respiratory disorder, the system comprising: a sensor configured to determine an indication of a respiratory pattern of a patient; a hardware controller configured to receive the indication of the respiratory pattern of the patient and determine a phase delay procedure for applying nasal high flow therapy to treat a respiratory disorder; and a flow generator , controlled by the hardware controller, the flow generator configured to provide a nasal high flow therapy to the patient , wherein the hardware controller controls the flow generator to provide a nasal high flow therapy according to the determined phase delay procedure, wherein a phase delay of the phase delay procedure is a time delay from a detection of a decrease or increase in tidal flow of breathing of the patient to an increase or decrease in a flow of gases delivered to an interface of the patient. a sensor configured to determine an indication of a respiratory pattern of a patient; a hardware controller configured to receive the indication of the respiratory pattern of the patient and determine a phase delay procedure for applying nasal high flow therapy to treat a respiratory disorder; and a flow generator , controlled by the hardware controller, the flow generator configured to provide a nasal high flow therapy to the patient , wherein the hardware controller controls the flow generator to provide a nasal high flow therapy according to the determined phase delay procedure, wherein a phase delay of the phase delay procedure is a time delay from a detection of a decrease or increase in tidal flow of breathing of the patient to an increase or decrease in a flow of gases delivered to an interface of the patient.
An apparatus for purifying dimethyl carbonate using pervaporation, comprising: an atmospheric distillation column and a high pressure distillation column distilling a mixture containing dimethyl carbonate and methanol and separating dimethyl carbonate from the mixture; and a pervaporation membrane module disposed between the atmospheric distillation column and the high pressure distillation column and allowing for permeation of the methanol to separate the methanol from the mixture, wherein the atmospheric distillation column supplies an amount of the mixture recovered from an upper portion of the atmospheric distillation column to the pervaporation membrane module . an atmospheric distillation column and a high pressure distillation column distilling a mixture containing dimethyl carbonate and methanol and separating dimethyl carbonate from the mixture; and a pervaporation membrane module disposed between the atmospheric distillation column and the high pressure distillation column and allowing for permeation of the methanol to separate the methanol from the mixture, wherein the atmospheric distillation column supplies an amount of the mixture recovered from an upper portion of the atmospheric distillation column to the pervaporation membrane module .
A battery management apparatus for managing a chargeable and dischargeable battery, comprising: a battery state calculation unit which calculates a state of charge and a deterioration degree of the battery; the apparatus is characterised by a mid voltage calculation unit which calculates a mid voltage that is present between a charge-discharge voltage in a current state of charge of the battery, and a charge-discharge voltage in a minimum state of charge or a maximum state of charge of the battery; a remaining capacity calculation unit which calculates a remaining capacity or a chargeable capacity of the battery, based on the state of charge and the deterioration degree; and an available energy calculation unit which calculates available energy or chargeable energy of the battery, based on the mid voltage and the remaining capacity, or on the mid voltage and the chargeable capacity. a battery state calculation unit which calculates a state of charge and a deterioration degree of the battery; the apparatus is characterised by a mid voltage calculation unit which calculates a mid voltage that is present between a charge-discharge voltage in a current state of charge of the battery, and a charge-discharge voltage in a minimum state of charge or a maximum state of charge of the battery; a remaining capacity calculation unit which calculates a remaining capacity or a chargeable capacity of the battery, based on the state of charge and the deterioration degree; and an available energy calculation unit which calculates available energy or chargeable energy of the battery, based on the mid voltage and the remaining capacity, or on the mid voltage and the chargeable capacity.
A developer storage body comprising: a first storage member including a first opening and a first flange provided along an outer periphery of the first opening ; a second storage member including a second opening and a second flange provided along an outer periphery of the second opening so that the second flange faces the first flange ; a frame including a third flange sandwiched by the first flange and the second flange ; and a resiliently deformable partition member including a peripheral end portion fixed to the frame , wherein the frame has a harder hardness than the partition member , and the partition member and the first storage member form a first space portion therebetween, and the partition member and the second storage member form a second space portion therebetween, wherein the frame has a framework structure comprising: an outer frame , the third flange provided along an outer periphery of the outer frame , a beam extending in a widthwise direction so as to cross a space surrounded by the outer frame , a first rib connecting an upper part of the outer frame to the beam , and a second rib connecting a lower part of the outer frame to the beam ; wherein the second rib is separated from an inner surface of the second storage member . a first storage member including a first opening and a first flange provided along an outer periphery of the first opening ; a second storage member including a second opening and a second flange provided along an outer periphery of the second opening so that the second flange faces the first flange ; a frame including a third flange sandwiched by the first flange and the second flange ; and a resiliently deformable partition member including a peripheral end portion fixed to the frame , wherein the frame has a harder hardness than the partition member , and the partition member and the first storage member form a first space portion therebetween, and the partition member and the second storage member form a second space portion therebetween, wherein the frame has a framework structure comprising: an outer frame , the third flange provided along an outer periphery of the outer frame , a beam extending in a widthwise direction so as to cross a space surrounded by the outer frame , a first rib connecting an upper part of the outer frame to the beam , and a second rib connecting a lower part of the outer frame to the beam ; an outer frame , the third flange provided along an outer periphery of the outer frame , a beam extending in a widthwise direction so as to cross a space surrounded by the outer frame , a first rib connecting an upper part of the outer frame to the beam , and a second rib connecting a lower part of the outer frame to the beam ; wherein the second rib is separated from an inner surface of the second storage member .
A test method for testing a solid-propellant rocket engine comprising: - a mass of solid propellant ; - a casing extending along an axis and comprising two annular end portions opposite to each other along said axis ; - a heat protection arranged to coat an inner surface of the casing and delimiting a housing containing said mass of solid propellant ; said heat protection including a coating portion comprising: - a fixed portion , coating at least one of said annular end portions and - at least one movable portion , which has a first face that adheres to the mass of solid propellant and can be moved between a back position, where it is closer to the fixed portion , and a forward position, where it is more distant from the fixed portion ; the method comprising the steps of: - moving the movable portion to the forward position; - checking the adhesion of the mass of solid propellant to the movable portion and/or any defects after the moving step; characterized in that the movement of the movable portion to the forward position is made by exerting, on the movable portion , a thrust oriented from the fixed portion towards the mass of solid propellant . - a mass of solid propellant ; - a casing extending along an axis and comprising two annular end portions opposite to each other along said axis ; - a heat protection arranged to coat an inner surface of the casing and delimiting a housing containing said mass of solid propellant ; - a fixed portion , coating at least one of said annular end portions and - at least one movable portion , which has a first face that adheres to the mass of solid propellant and can be moved between a back position, where it is closer to the fixed portion , and a forward position, where it is more distant from the fixed portion ; - moving the movable portion to the forward position; - checking the adhesion of the mass of solid propellant to the movable portion and/or any defects after the moving step;