mhurhangee/patent-ind-claim-en huggingface dataset:
A particular matter (PM) sensor , comprising: an accumulation section that is disposed such that a passage (P) of exhaust gas containing particulate matter is blocked, the particulate matter accumulating on a first surface located upstream of the passage (P) of the accumulation section , the accumulation section including at least one through hole (H6); and at least a pair of electrodes opposed to each other across the accumulation section , wherein the pair of electrodes includes main surfaces of the respective electrodes, the accumulation section has an exposed portion (E2) not overlapping the pair of electrodes in a plan view along a normal direction to the main surfaces, and characterised in that the at least one through hole (H6) penetrates from the first surface located upstream of the passage of the exhaust gas to a second surface located downstream thereof in the exposed portion (E2) of the accumulation section . an accumulation section that is disposed such that a passage (P) of exhaust gas containing particulate matter is blocked, the particulate matter accumulating on a first surface located upstream of the passage (P) of the accumulation section , the accumulation section including at least one through hole (H6); and at least a pair of electrodes opposed to each other across the accumulation section , wherein the pair of electrodes includes main surfaces of the respective electrodes, the accumulation section has an exposed portion (E2) not overlapping the pair of electrodes in a plan view along a normal direction to the main surfaces, and characterised in that the at least one through hole (H6) penetrates from the first surface located upstream of the passage of the exhaust gas to a second surface located downstream thereof in the exposed portion (E2) of the accumulation section .
A method for fabricating a composite comprising: a) providing a phase separated system of two non-mixing solvents, the phase separated system including: (i) a first solvent and a second solvent, and (ii) an interface between the first and second solvents; b) introducing an unaltered pristine graphene or unaltered pristine graphite layered material to the interface of the phase separated system; c) forming an emulsion of the first and second solvents, at least a portion of the unaltered pristine graphene or unaltered pristine graphite layered material stabilizing the emulsion; and d) adding a monomer and polymerizing the first solvent phase of the emulsion to form a matrix material having cavities lined with portions of the unaltered pristine graphene or unaltered pristine graphite layered material. a) providing a phase separated system of two non-mixing solvents, the phase separated system including: (i) a first solvent and a second solvent, and (ii) an interface between the first and second solvents; b) introducing an unaltered pristine graphene or unaltered pristine graphite layered material to the interface of the phase separated system; c) forming an emulsion of the first and second solvents, at least a portion of the unaltered pristine graphene or unaltered pristine graphite layered material stabilizing the emulsion; and d) adding a monomer and polymerizing the first solvent phase of the emulsion to form a matrix material having cavities lined with portions of the unaltered pristine graphene or unaltered pristine graphite layered material.
Method to manage the defrosting of a refrigeration plant provided with at least one compressor and at least one evaporator, wherein said method comprises: defining a plurality of not mutually exclusive defrosting modes (d0, d1, d2, d3, d4, d5, d9), which can be selected by the end user in a non-exclusive manner, which are based on one or more functioning parameters of the refrigeration plant, said functioning parameters being detected by means of detection probes provided in the refrigeration plant such as pressure switches, thermostats, timing devices, associated with said compressor and/or said evaporator; memorizing said plurality of defrosting modes (d0, d1, d2, d3, d4, d5, d9) in an electronic device to manage the defrosting, said electronic device being configured by the end user through means able to select said plurality of defrosting modes (d0, d1, d2, d3, d4, d5, d9), in which the functioning parameters of the refrigeration plant are selected and adjustable by the end user for each of the defrosting modes (d0, d1, d2, d3, d4, d5, d9) memorized in the electronic device , such that said defrosting modes (d0, d1, d2, d3, d4, d5, d9) are activated individually according to two or more defrosting modes chosen by the end user. defining a plurality of not mutually exclusive defrosting modes (d0, d1, d2, d3, d4, d5, d9), which can be selected by the end user in a non-exclusive manner, which are based on one or more functioning parameters of the refrigeration plant, said functioning parameters being detected by means of detection probes provided in the refrigeration plant such as pressure switches, thermostats, timing devices, associated with said compressor and/or said evaporator; memorizing said plurality of defrosting modes (d0, d1, d2, d3, d4, d5, d9) in an electronic device to manage the defrosting, said electronic device being configured by the end user through means able to select said plurality of defrosting modes (d0, d1, d2, d3, d4, d5, d9), in which the functioning parameters of the refrigeration plant are selected and adjustable by the end user for each of the defrosting modes (d0, d1, d2, d3, d4, d5, d9) memorized in the electronic device , such that said defrosting modes (d0, d1, d2, d3, d4, d5, d9) are activated individually according to two or more defrosting modes chosen by the end user.
A working machine for use in agriculture or construction with an attachment, wherein the attachment comprises a load signal control for its working hydraulics which is connected to a hydraulic system of the working machine for use in agriculture or construction by means of at least a pressure connection (P) and a tank connection (T), with at least one consumer controlled by means of a directional control valve , by means of which a primary load pressure (p LS_primary ) can be produced in a primary load signal line (17"), wherein the primary load pressure (p LS_primary ) is supplied to a control unit (26, 26', 26") which controls a volume flow in a pressure line leading to the at least one consumer , and wherein, in the control unit (16, 26', 26"), an appropriate rise in the pressure of the primary load pressure (p LS_primary ) is executed to a pressure level of a secondary load pressure (p LS_secondary ), characterized in that the control unit (26, 26', 26") is disposed within the working hydraulics of the attachment and has a pressure regulation valve which is connected on the input side to the pressure line and the primary load signal line (17") as well as on the output side to a secondary load signal line , wherein a control piston of the pressure regulation valve is pressurised on one side with the primary load pressure (p LS_primary ) as well as on the other side with the secondary load pressure (p LS_secondary ).
An ear-worn electronic device configured to be worn by a wearer, comprising: a housing configured to be supported at, by, in or on the wearer's ear; a processor disposed in the housing; a speaker or a receiver operably coupled to the processor; a radio frequency transceiver disposed in the housing and operably coupled to the processor; and an antenna (106; 220a, 220b; 300; 500; 600; 700; 800) disposed on or in the housing and operably coupled to the transceiver, the antenna comprising: a radiating element (304; 404; 504; 604; 704); a ground plane (302; 402; 502; 602; 702; 820); and a substrate (107; 221a, 221b; 306; 406; 506; 606; 706; 830) disposed between the radiating element and the ground plane, the substrate comprising a dielectric gel or a dielectric liquid. a housing configured to be supported at, by, in or on the wearer's ear; a processor disposed in the housing; a speaker or a receiver operably coupled to the processor; a radio frequency transceiver disposed in the housing and operably coupled to the processor; and an antenna (106; 220a, 220b; 300; 500; 600; 700; 800) disposed on or in the housing and operably coupled to the transceiver, the antenna comprising: a radiating element (304; 404; 504; 604; 704); a ground plane (302; 402; 502; 602; 702; 820); and a substrate (107; 221a, 221b; 306; 406; 506; 606; 706; 830) disposed between the radiating element and the ground plane, the substrate comprising a dielectric gel or a dielectric liquid. a radiating element (304; 404; 504; 604; 704); a ground plane (302; 402; 502; 602; 702; 820); and a substrate (107; 221a, 221b; 306; 406; 506; 606; 706; 830) disposed between the radiating element and the ground plane, the substrate comprising a dielectric gel or a dielectric liquid.
Lighting or signaling device for a motor vehicle comprising: - a light guide sheet having an upper face and a lower face , a rear edge with at least one lobe, and an exit edge , - at least one light source of the light-emitting diode type capable of injecting a light beam through one face of the guide sheet, which, by refraction and/or reflection on the faces and on the rear edge, gives an essentially parallel beam emerging through the exit edge , - means (F) for fixing (F) the guide web in a support (D), wherein : - the means (F) for fixing the web comprise means (S) for clamping (S) the faces of the web between an upper element (6, B) against which the upper face of the web bears, and a lower part forming the support (D) against which the lower face bears, - and positioning means (P) are provided between the lower part (7,7', 7") and the web , - and the light source is mounted so as to project from a printed circuit board (B) in order to be placed in line with a light-receiving area , the web comprising, in the vicinity of this receiving area, pins projecting so as to be applied against the printed circuit board (B) when tightened. - a light guide sheet having an upper face and a lower face , a rear edge with at least one lobe, and an exit edge , - at least one light source of the light-emitting diode type capable of injecting a light beam through one face of the guide sheet, which, by refraction and/or reflection on the faces and on the rear edge, gives an essentially parallel beam emerging through the exit edge , - means (F) for fixing (F) the guide web in a support (D), - the means (F) for fixing the web comprise means (S) for clamping (S) the faces of the web between an upper element (6, B) against which the upper face of the web bears, and a lower part forming the support (D) against which the lower face bears, - and positioning means (P) are provided between the lower part (7,7', 7") and the web , - and the light source is mounted so as to project from a printed circuit board (B) in order to be placed in line with a light-receiving area , the web comprising, in the vicinity of this receiving area, pins projecting so as to be applied against the printed circuit board (B) when tightened.
Motor vehicle internal combustion engine exhaust-gas after-treatment device comprising an enclosure defining a tubular chamber inside which there is arranged a deflector element : - at least one support means substantially in the form of a ring extending parallel to the wall of the enclosure with a predetermined clearance (J1) and supporting the deflector element substantially at the centre of the tubular chamber by at least two arms of which one end is fastened to the support means and the other end is fastened to the deflector element, characterized in that : - two retaining elements are positioned on either side of said support means axially, between said support means and the enclosure , each retaining element having a substantially annular open general shape undulating radially so as to be in contact alternately with an inner surface of the enclosure and an opposite bearing surface of said support means , said radial undulations being configured to block said support means radially with respect to said enclosure. - at least one support means substantially in the form of a ring extending parallel to the wall of the enclosure with a predetermined clearance (J1) and supporting the deflector element substantially at the centre of the tubular chamber by at least two arms of which one end is fastened to the support means and the other end is fastened to the deflector element, - two retaining elements are positioned on either side of said support means axially, between said support means and the enclosure , each retaining element having a substantially annular open general shape undulating radially so as to be in contact alternately with an inner surface of the enclosure and an opposite bearing surface of said support means , said radial undulations being configured to block said support means radially with respect to said enclosure.
A computer-implemented method comprising: identifying a first performance metric associated with processing a current workload at a graphics processing unit, GPU , for a number of consecutive measurement cycles, wherein the number of consecutive measurement cycles includes a current measurement cycle and at least one previous measurement cycle; identifying that the first performance metric is lower than a performance metric threshold for the number of consecutive measurement cycles; determining that the number of consecutive measurement cycles exceeds a minimum hysteresis number, wherein the minimum hysteresis number comprises an up-hysteresis level defining a minimum number of consecutive cycles that the first performance metric must be maintained at or above the performance metric threshold before increasing a power level of the GPU, and a down-hysteresis level defining a minimum number of consecutive cycles that the first performance metric must be maintained below the performance metric threshold before decreasing the power level of the GPU; determining , based on data representative of a current computing environment processing the current workload, an estimated optimization to be applied to the GPU for a future measurement cycle; and characterised by adjusting , based on the estimated optimization, a power level setting at the GPU to a power savings optimized setting by increasing the up-hysteresis level and decreasing the down-hysteresis level for the future measurement cycle. identifying a first performance metric associated with processing a current workload at a graphics processing unit, GPU , for a number of consecutive measurement cycles, wherein the number of consecutive measurement cycles includes a current measurement cycle and at least one previous measurement cycle; identifying that the first performance metric is lower than a performance metric threshold for the number of consecutive measurement cycles; determining that the number of consecutive measurement cycles exceeds a minimum hysteresis number, wherein the minimum hysteresis number comprises an up-hysteresis level defining a minimum number of consecutive cycles that the first performance metric must be maintained at or above the performance metric threshold before increasing a power level of the GPU, and a down-hysteresis level defining a minimum number of consecutive cycles that the first performance metric must be maintained below the performance metric threshold before decreasing the power level of the GPU; determining , based on data representative of a current computing environment processing the current workload, an estimated optimization to be applied to the GPU for a future measurement cycle; and characterised by adjusting , based on the estimated optimization, a power level setting at the GPU to a power savings optimized setting by increasing the up-hysteresis level and decreasing the down-hysteresis level for the future measurement cycle.
A method of attaching a hose coupling to a first end of a reinforced bonded hose , the method comprising: skiving the first end of the reinforced hose to expose at least one reinforcing layer of a plurality of reinforcing layers of the reinforced hose ; and positioning the skived first end of the reinforced hose in an inner cavity of the hose coupling ; the method characterized by : introducing a vacuum into the inner cavity through a vent port in the hose coupling ; and introducing a bonding agent into the cavity through an injection port in the hose coupling , wherein the bonding agent is drawn by the vacuum into at least one reinforcing layer of the plurality of reinforcing layers of the reinforced hose . skiving the first end of the reinforced hose to expose at least one reinforcing layer of a plurality of reinforcing layers of the reinforced hose ; and positioning the skived first end of the reinforced hose in an inner cavity of the hose coupling ; introducing a vacuum into the inner cavity through a vent port in the hose coupling ; and introducing a bonding agent into the cavity through an injection port in the hose coupling , wherein the bonding agent is drawn by the vacuum into at least one reinforcing layer of the plurality of reinforcing layers of the reinforced hose .
A cellobiohydrolase 1 variant comprising an amino acid sequence having a sequence identity of at least 80% with SEQ ID NO: 2 and comprising an amino acid substitution at position N209 corresponding to positions 1 to 526 of SEQ ID NO 2, wherein said substitution is N209D or N209E.
A sheet for an aerosol-generating substrate of an aerosol-generating article, the sheet comprising fibrous material, one or more nicotine salts and a binder, wherein at least about 20% by weight of the one or more nicotine salts are monoprotic and wherein the sheet has a binder content of less than about 8% by weight on a dry weight basis.
A method for communication between a first network element and a second network element, wherein the first network element generates data and the second network elements uses the data generated by the first network element, the method comprising: receiving , by the first network element, a request message of the second network element, wherein the request message comprises one or more to-be-collected data types and one or more sizes of one or more requested buffer queues, the one or more data types comprise a first type, the sizes of the one or more requested buffer queues comprise a size of a requested first buffer queue, and the first buffer queue corresponds to the first type; determining , by the first network element, an actual size of the first buffer queue based on at least one of the sizes of the one or more requested buffer queues, wherein the actual size of the first buffer queue is less than or equal to the size of the requested first buffer queue; and sending , by the first network element, a response message for the request message to the second network element, wherein the response message comprises an identifier of the first buffer queue and the actual size of the first buffer queue. receiving , by the first network element, a request message of the second network element, wherein the request message comprises one or more to-be-collected data types and one or more sizes of one or more requested buffer queues, the one or more data types comprise a first type, the sizes of the one or more requested buffer queues comprise a size of a requested first buffer queue, and the first buffer queue corresponds to the first type; determining , by the first network element, an actual size of the first buffer queue based on at least one of the sizes of the one or more requested buffer queues, wherein the actual size of the first buffer queue is less than or equal to the size of the requested first buffer queue; and sending , by the first network element, a response message for the request message to the second network element, wherein the response message comprises an identifier of the first buffer queue and the actual size of the first buffer queue.
An aircraft control system , comprising: a processor; and a non-volatile computer readable storage medium having stored therein computer-executable components executable by the processor, the computer-executable components comprising: a mapping component configured to map noise-restricted areas of a flight path defined by respective relative positions of an aircraft to ground noise restriction locations; and a noise abatement component that configured to compute a thrust and to control the aircraft in the noise restriction locations, wherein the thrust computed by the noise abatement component facilitates operation of the aircraft while retaining noise below a defined noise level, wherein the noise abatement component is configured to compute the thrust and to control the aircraft in the noise restriction locations based on a line-of-sight distance from the aircraft to a geographical point of interest. a processor; and a non-volatile computer readable storage medium having stored therein computer-executable components executable by the processor, the computer-executable components comprising: a mapping component configured to map noise-restricted areas of a flight path defined by respective relative positions of an aircraft to ground noise restriction locations; and a noise abatement component that configured to compute a thrust and to control the aircraft in the noise restriction locations, wherein the thrust computed by the noise abatement component facilitates operation of the aircraft while retaining noise below a defined noise level, wherein the noise abatement component is configured to compute the thrust and to control the aircraft in the noise restriction locations based on a line-of-sight distance from the aircraft to a geographical point of interest. a mapping component configured to map noise-restricted areas of a flight path defined by respective relative positions of an aircraft to ground noise restriction locations; and a noise abatement component that configured to compute a thrust and to control the aircraft in the noise restriction locations, wherein the thrust computed by the noise abatement component facilitates operation of the aircraft while retaining noise below a defined noise level, wherein the noise abatement component is configured to compute the thrust and to control the aircraft in the noise restriction locations based on a line-of-sight distance from the aircraft to a geographical point of interest.