mhurhangee/ep-ind-claims huggingface dataset:
A film resistor having a piezoresistive layer, wherein the piezoresistive layer has a M 1+n AX n phase, wherein M has at least one transition metal, A has a main-group element, X has carbon and/or nitrogen, and wherein n = 1, 2 or 3.
An insulating material comprising: a base fabric having a moisture vapor transfer rate (MVTR) of at least 2000 g/m 2 /24h measured in accordance with JIS 1099 A1; a plurality of heat-reflecting elements coupled to a first side of the base fabric, wherein the first side of the base fabric is an innermost surface of the base fabric, each heat-reflecting element having a heat-reflecting surface positioned to reflect heat towards a wearer of the insulating material; and a plurality of spacer elements, wherein at least some of the plurality of spacer elements at least partially overlay the heat-reflecting surfaces of at least some of the plurality of heat-reflecting elements, the at least some of the plurality of spacer elements attached to and extending from the first side of the base fabric and from the heat-reflecting surfaces to be directed toward and exposed to contact by the wearer of the insulating material, each spacer element sized and shaped to reduce contact of the heat-reflecting elements with an underlying surface or with the wearer, wherein the spacer elements comprise foam pods or pods comprising, woven, nonwoven or knitted materials or vertically oriented fiber elements, or wherein each VOF element comprises a plurality of fibers oriented perpendicular to a surface of the base fabric, and wherein at least some of the plurality of VOF elements at least partially overlay at least some of the plurality of heat-reflecting elements. a base fabric having a moisture vapor transfer rate (MVTR) of at least 2000 g/m 2 /24h measured in accordance with JIS 1099 A1; a plurality of heat-reflecting elements coupled to a first side of the base fabric, wherein the first side of the base fabric is an innermost surface of the base fabric, each heat-reflecting element having a heat-reflecting surface positioned to reflect heat towards a wearer of the insulating material; and a plurality of spacer elements, wherein at least some of the plurality of spacer elements at least partially overlay the heat-reflecting surfaces of at least some of the plurality of heat-reflecting elements, the at least some of the plurality of spacer elements attached to and extending from the first side of the base fabric and from the heat-reflecting surfaces to be directed toward and exposed to contact by the wearer of the insulating material, each spacer element sized and shaped to reduce contact of the heat-reflecting elements with an underlying surface or with the wearer, wherein the spacer elements comprise foam pods or pods comprising, woven, nonwoven or knitted materials or vertically oriented fiber elements, or wherein each VOF element comprises a plurality of fibers oriented perpendicular to a surface of the base fabric, and wherein at least some of the plurality of VOF elements at least partially overlay at least some of the plurality of heat-reflecting elements.
An indoor environment regulating system, wherein the system is provided with an indoor surface structural member (200, 300) constructed of a material comprising a far-infrared emitting substance that emits and absorbs far-infrared rays and has a far-infrared emissivity of 0.6 or greater, the indoor surface structural member (200, 300) being a member forming a surface exposed in a space where the environment is to be regulated, and a cooling and/or heating source (110, 302) having a cooling and/or heating surface (200, 301) constructed of a material comprising the same far-infrared emitting substance as the far-infrared emitting substance of the indoor surface structural member (200, 300), whereby the far-infrared emitting substance of the cooling and/or heating surface (200, 301) resonates with the far-infrared emitting substance of the indoor surface structural member (200, 300) via far-infrared rays, and wherein the cooling and/or heating surface (200, 301) is exposed to an indoor space, wherein when the cooling surface of the cooling source is cooled, the far-infrared emitting substance of the cooling surface absorbs, via resonance, the far-infrared rays emitted by the far-infrared emitting substance of the indoor surface structural member (200, 300), and/or when the heating surface of the heating source is heated, the far-infrared rays emitted by the far-infrared emitting substance of the heating surface are absorbed, via a resonance phenomenon of molecular vibration between identical molecules via electromagnetic waves by the far-infrared emitting substance of the indoor surface structural member, characterized in that the cooling and/or heating surface (200, 301) of the cooling and/or heating source (110, 302) is constructed with a covering layer that contains the far-infrared emitting substance at 1 wt% or greater, wherein the covering layer is formed on the surfaces of heat exchange fins made of a metal material, wherein the cooling and/or heating source (110, 302) is a device that cools and/or heats the cooling and/or heating surface (200, 301) by circulating a medium through an internally formed fluid channel.
A computer-implemented method for processing inspection data associated with cargo irradiated by a plurality N of pulses of inspection radiation, the method comprising: obtaining the inspection data, the inspection data being representative of intensity values of pixels of an inspection image of the cargo generated as a result of a plurality of detectors detecting the plurality N of pulses transmitted through the cargo, and the inspection data comprising data associated with a higher energy mode, and data associated with a lower energy mode; generating a histogram having, as a first axis, bins corresponding to pixel intensity values HM associated with the higher energy mode and, as a second axis, bins corresponding to pixel intensity values LM associated with the lower energy mode, wherein generating the histogram comprises binning, for each pixel (i,j) of the inspection image corresponding to each pulse i and each detector j of the plurality of detectors, an occurrence in the obtained inspection data such that: HM i j; LM i − 1, j + LM i + 1, j 2; selecting, on the generated histogram, for each bin of the pixel intensity values LM, a bin corresponding to a most frequent bin of the pixel intensity values HM; and generating a transformation table by mapping each bin of the pixel intensity values LM with the selected bin of the pixel intensity values HM. obtaining the inspection data, the inspection data being representative of intensity values of pixels of an inspection image of the cargo generated as a result of a plurality of detectors detecting the plurality N of pulses transmitted through the cargo, and the inspection data comprising data associated with a higher energy mode, and data associated with a lower energy mode; the inspection data being representative of intensity values of pixels of an inspection image of the cargo generated as a result of a plurality of detectors detecting the plurality N of pulses transmitted through the cargo, and the inspection data comprising data associated with a higher energy mode, and data associated with a lower energy mode; generating a histogram having, as a first axis, bins corresponding to pixel intensity values HM associated with the higher energy mode and, as a second axis, bins corresponding to pixel intensity values LM associated with the lower energy mode, wherein generating the histogram comprises binning, for each pixel (i,j) of the inspection image corresponding to each pulse i and each detector j of the plurality of detectors, an occurrence in the obtained inspection data such that: HM i j; LM i − 1, j + LM i + 1, j 2; selecting, on the generated histogram, for each bin of the pixel intensity values LM, a bin corresponding to a most frequent bin of the pixel intensity values HM; and generating a transformation table by mapping each bin of the pixel intensity values LM with the selected bin of the pixel intensity values HM.
A method of generating patient specific interlocks for a medical device, the method comprising: sensing at least one patient function of a patient with a medical device based on monitored electrical activity of the patient's heart; collecting sensed patient cardiac data from the sensing of the at least one patient function; analyzing the collected patient cardiac data; and based at least in part on the analyzed collected patient cardiac data, generating at least one patient specific interlock defining a rate limit and response by predetermined age guidelines that denies operational change requests to the medical device outside of the defined rate limit and response. sensing at least one patient function of a patient with a medical device based on monitored electrical activity of the patient's heart; collecting sensed patient cardiac data from the sensing of the at least one patient function; analyzing the collected patient cardiac data; and based at least in part on the analyzed collected patient cardiac data, generating at least one patient specific interlock defining a rate limit and response by predetermined age guidelines that denies operational change requests to the medical device outside of the defined rate limit and response.
A joint implant comprising: a) a framework comprising: i) a central longitudinal axis measured in a direction of a longest dimension of said framework and openings outward from said central longitudinal axis; ii) an anterior side comprising a cutting edge fixed to said anterior side, wherein the cutting edge is adapted to dissect through adipose, muscle and/or joint capsule tissues; iii) a surgeon facing side at an end opposite said anterior side; said surgeon facing side comprising one or more apertures; iv) a rotatable shaft, coaxial with said central axis, extending between said cutting edge and said surgeon facing side; and v) a first arm connected with said shaft; said first arm supporting a first cutter comprising one or more blades (268F, 268S), wherein on rotation of said shaft, said blades (268F, 268S) rotate in a clockwise or counterclockwise direction. a) a framework comprising: i) a central longitudinal axis measured in a direction of a longest dimension of said framework and openings outward from said central longitudinal axis; ii) an anterior side comprising a cutting edge fixed to said anterior side, wherein the cutting edge is adapted to dissect through adipose, muscle and/or joint capsule tissues; iii) a surgeon facing side at an end opposite said anterior side; said surgeon facing side comprising one or more apertures; iv) a rotatable shaft, coaxial with said central axis, extending between said cutting edge and said surgeon facing side; and v) a first arm connected with said shaft; said first arm supporting a first cutter comprising one or more blades (268F, 268S), wherein on rotation of said shaft, said blades (268F, 268S) rotate in a clockwise or counterclockwise direction. i) a central longitudinal axis measured in a direction of a longest dimension of said framework and openings outward from said central longitudinal axis; ii) an anterior side comprising a cutting edge fixed to said anterior side, wherein the cutting edge is adapted to dissect through adipose, muscle and/or joint capsule tissues; iii) a surgeon facing side at an end opposite said anterior side; said surgeon facing side comprising one or more apertures; iv) a rotatable shaft, coaxial with said central axis, extending between said cutting edge and said surgeon facing side; and v) a first arm connected with said shaft; said first arm supporting a first cutter comprising one or more blades (268F, 268S), wherein on rotation of said shaft, said blades (268F, 268S) rotate in a clockwise or counterclockwise direction.
A writing instrument, comprising: a tubular body with a first and a second end (2, 12) and with an opening arranged in the first end, and having a longitudinal axis extending through the opening in the first end and to the second end; at least one marking or erasing member extending in the tubular body along said longitudinal axis, and out through the opening in the first end; a first building block having a body part with a substantially plane surface and one or more coupling knobs extending from the substantially plane surface, and where a recess is arranged on the outside of the tubular body, characterised in that the the recess allows the first building block to be mounted in a countersunk position on one side of the tubular body so that the coupling knobs extend away from said longitudinal axis. a tubular body with a first and a second end (2, 12) and with an opening arranged in the first end, and having a longitudinal axis extending through the opening in the first end and to the second end; at least one marking or erasing member extending in the tubular body along said longitudinal axis, and out through the opening in the first end; a first building block having a body part with a substantially plane surface and one or more coupling knobs extending from the substantially plane surface, and where a recess is arranged on the outside of the tubular body, characterised in that the the recess allows the first building block to be mounted in a countersunk position on one side of the tubular body so that the coupling knobs extend away from said longitudinal axis.
A method for controlling the capacity of a compressor, comprising: receiving operational parameters; based on the operational parameters, retrieving a map of compressor efficiency based on compressor speeds and mechanical unloading; determining a desired compressor speed based on the map of compressor efficiency; commanding a variable frequency drive to operate the compressor at the desired compressor speed; comparing a compressor capacity to a compressor load when the compressor is operating at the desired compressor speed; and increasing the extent to which one or more mechanical unloaders reduce the capacity of the compressor if the compressor capacity exceeds the compressor load. receiving operational parameters; based on the operational parameters, retrieving a map of compressor efficiency based on compressor speeds and mechanical unloading; determining a desired compressor speed based on the map of compressor efficiency; commanding a variable frequency drive to operate the compressor at the desired compressor speed; comparing a compressor capacity to a compressor load when the compressor is operating at the desired compressor speed; and increasing the extent to which one or more mechanical unloaders reduce the capacity of the compressor if the compressor capacity exceeds the compressor load.
A method for pooling at least one ROI, i.e. region of interest, by using one or more masking parameters, comprising steps of: (a) a computing device, if an input image is acquired, instructing a convolutional layer of a CNN, i.e. convolutional neural network, to generate a feature map corresponding to the input image; (b) the computing device instructing an RPN, i.e. regions proposal network, of the CNN to determine the ROI corresponding to at least one object included in the input image by using the feature map; and characterised in that (c) the computing device instructing an ROI pooling layer of the CNN to apply each of pooling operations correspondingly to each of sub-regions in the ROI by referring to each of the masking parameters corresponding to each of the pooling operations, to thereby generate a masked pooled feature map, wherein, each of the masking parameters is determined as either a first value or a second value, and wherein, at the step of (c), the computing device instructs the ROI pooling layer to apply each of the pooling operations correspondingly to each of the sub-regions in the ROI by referring to information on whether each of the masking parameters is the first value or the second value, to thereby generate the masked pooled feature map. (a) a computing device, if an input image is acquired, instructing a convolutional layer of a CNN, i.e. convolutional neural network, to generate a feature map corresponding to the input image; (b) the computing device instructing an RPN, i.e. regions proposal network, of the CNN to determine the ROI corresponding to at least one object included in the input image by using the feature map; and characterised in that (c) the computing device instructing an ROI pooling layer of the CNN to apply each of pooling operations correspondingly to each of sub-regions in the ROI by referring to each of the masking parameters corresponding to each of the pooling operations, to thereby generate a masked pooled feature map, wherein, each of the masking parameters is determined as either a first value or a second value, and wherein, at the step of (c), the computing device instructs the ROI pooling layer to apply each of the pooling operations correspondingly to each of the sub-regions in the ROI by referring to information on whether each of the masking parameters is the first value or the second value, to thereby generate the masked pooled feature map.
An aircraft (1000, 2000, 3000, 4000) comprising: a fuselage (2, 224, 424, 524); a wing (4, 6, 44, 54, 64, 74, 202, 222, 420, 422, 500, 502); a propulsion system comprising a rotor (20, 30, 40, 50, 60, 70, 206, 208, 212, 216, 402, 406, 612, 622, 632, 642) having both collective and cyclic control; an axis of thrust rotation substantially aligned with a spanwise direction of the wing (4, 6, 44, 54, 64, 74, 202, 222, 420, 422, 500, 502) wherein the propulsion system is rotatable around the axis of thrust rotation with respect to the fuselage (2, 224, 424, 524); a control system configured to utilize torque generated through cyclic control of the rotor (20, 30, 40, 50, 60, 70, 206, 208, 212, 216, 402, 406, 612, 622, 632, 642) to rotate the propulsion system around the axis of thrust rotation; characterised by a ratchet mechanism (520, 522, 650, 660, 670, 680) configured to prevent rotation of the propulsion system around the axis of thrust rotation in a first direction and permit rotation in a second direction. a fuselage (2, 224, 424, 524); a wing (4, 6, 44, 54, 64, 74, 202, 222, 420, 422, 500, 502); a propulsion system comprising a rotor (20, 30, 40, 50, 60, 70, 206, 208, 212, 216, 402, 406, 612, 622, 632, 642) having both collective and cyclic control; an axis of thrust rotation substantially aligned with a spanwise direction of the wing (4, 6, 44, 54, 64, 74, 202, 222, 420, 422, 500, 502) wherein the propulsion system is rotatable around the axis of thrust rotation with respect to the fuselage (2, 224, 424, 524); a control system configured to utilize torque generated through cyclic control of the rotor (20, 30, 40, 50, 60, 70, 206, 208, 212, 216, 402, 406, 612, 622, 632, 642) to rotate the propulsion system around the axis of thrust rotation; characterised by a ratchet mechanism (520, 522, 650, 660, 670, 680) configured to prevent rotation of the propulsion system around the axis of thrust rotation in a first direction and permit rotation in a second direction.
A system for simultaneously forming and filling a polymeric container with a product, the system comprising: a mold defining a container profile and a mold vacuum vent extending from the container profile to an upper surface of the mold; and a striker plate secured to the upper surface of the mold, wherein the striker plate defines a striker vacuum vent that aligns with the mold vacuum vent to allow some of the product to be pulled by vacuum out of the mold through the mold vacuum vent and the striker vacuum vent, characterized in that the system further comprises a knock-out vessel configured to regulate the vacuum and receive the product pulled by the vacuum out of the mold; and a vacuum valve between the striker plate and the knock-out vessel, the vacuum valve configured to sync the vacuum with consecutive container forming and filling processes. a mold defining a container profile and a mold vacuum vent extending from the container profile to an upper surface of the mold; and a striker plate secured to the upper surface of the mold, wherein the striker plate defines a striker vacuum vent that aligns with the mold vacuum vent to allow some of the product to be pulled by vacuum out of the mold through the mold vacuum vent and the striker vacuum vent, characterized in that the system further comprises a knock-out vessel configured to regulate the vacuum and receive the product pulled by the vacuum out of the mold; and a vacuum valve between the striker plate and the knock-out vessel, the vacuum valve configured to sync the vacuum with consecutive container forming and filling processes.
Electrode comprising a holder segment, a base segment having a cutout in which the holder segment is accommodated and optionally at least one intermediate segment arranged between the base segment and the holder segment, wherein at least two of the segments (12, 14, 18) differ in respect of their specific thermal conductivity, wherein the holder segment has the lowest and the base segment the highest specific thermal conductivity and wherein adjacent segments have opposing interfaces which are at least partially in mechanical contact with one another and thus form a contact area (K, K1, K2), characterized in that to reduce the contact area (K, K1, K2) at least one of the interfaces has at least one depression (20, 21, 22, 23, 24) and/or elevation and at least one insert (32, 33, 34) is arranged between two segments (12, 14, 18).
A driver for at least one LED, the driver comprising a switched-mode power supply, SMPS, configured to supply the at least one LED; a closed-loop control for regulating a controlled variable supplied to the at least one LED in accordance with a reference variable; characterized by a feed-forward control for adjusting a control variable of the closed-loop control in dependence of a frequency component of a control error of the closed-loop control and a frequency component of a DC link voltage of the SMPS. a switched-mode power supply, SMPS, configured to supply the at least one LED; a closed-loop control for regulating a controlled variable supplied to the at least one LED in accordance with a reference variable; characterized by a feed-forward control for adjusting a control variable of the closed-loop control in dependence of a frequency component of a control error of the closed-loop control and a frequency component of a DC link voltage of the SMPS.
A membrane valve with a propulsion casing and a propulsion assembly inside the propulsion casing for positioning a process fluid with a membrane, whereby the membrane valve has a pretension assembly for alignment between the propulsion assembly and the membrane, whereby - the propulsion assembly is kept in a pre-stressed state before insertion into the propulsion casing via a first spring element, distinguished by the fact that - the pretension assembly is kept in a pre-stressed state before insertion into the propulsion casing via a second spring element. - the propulsion assembly is kept in a pre-stressed state before insertion into the propulsion casing via a first spring element, distinguished by the fact that - the pretension assembly is kept in a pre-stressed state before insertion into the propulsion casing via a second spring element.