mhurhangee/patent-ind-claim-en huggingface dataset:
Battery system , comprising: a plurality of battery cells connected in series; a plurality of balancing circuits , each balancing circuit being connected in parallel to one of the plurality of battery cells and comprising a bleed resistor connected in series with a balancing switch ; a control unit comprising a balancing controller , the balancing controller being configured to output an individual control signal for each of the balancing switches , characterized in that each balancing switch is configured to be set non-conductive in response to a control signal received by the balancing controller and to be set conductive in the absence of the control signal, and the balancing controller and the balancing switches are configured for providing balancing between the battery cells and each balancing switch is configured to provide an auto-discharge functionality at the end of life of the battery system , wherein at the end of life of battery system , the power produced by the battery cells is not sufficient to operate the control unit . a plurality of battery cells connected in series; a plurality of balancing circuits , each balancing circuit being connected in parallel to one of the plurality of battery cells and comprising a bleed resistor connected in series with a balancing switch ; a control unit comprising a balancing controller , the balancing controller being configured to output an individual control signal for each of the balancing switches , characterized in that each balancing switch is configured to be set non-conductive in response to a control signal received by the balancing controller and to be set conductive in the absence of the control signal, and the balancing controller and the balancing switches are configured for providing balancing between the battery cells and each balancing switch is configured to provide an auto-discharge functionality at the end of life of the battery system , wherein at the end of life of battery system , the power produced by the battery cells is not sufficient to operate the control unit .
A hydrostatic transmission pedal stroke limiter , comprising: a range shift lever having at least a low range gear and a high range gear; a hydrostatic transmission actuator arm connected to a foot pedal that pivots a trunnion arm on a hydrostatic transmission ; a stop connected through a linkage to the range shift lever and limiting the travel of the hydrostatic transmission actuator arm when the range shift lever is in the low gear range; the linkage being between the range shift lever and the stop , the linkage including a cross shaft extending at least partially across a tractor frame ; the range shift lever pivoting the stop to a position limiting travel of the hydrostatic transmission actuator arm if the range shift lever is in a low gear range position. a range shift lever having at least a low range gear and a high range gear; a hydrostatic transmission actuator arm connected to a foot pedal that pivots a trunnion arm on a hydrostatic transmission ; a stop connected through a linkage to the range shift lever and limiting the travel of the hydrostatic transmission actuator arm when the range shift lever is in the low gear range; the linkage being between the range shift lever and the stop , the linkage including a cross shaft extending at least partially across a tractor frame ; the range shift lever pivoting the stop to a position limiting travel of the hydrostatic transmission actuator arm if the range shift lever is in a low gear range position.
A real-time location system comprises: - a plurality of positioning transceiver systems configured to determine, for each positioning transceiver system , its corresponding position, relative to a global coordinate system, during set up of the real-time location system ; - a tag transceiver with location marker programmer configured to determine the location of the tag transceiver relative to global position coordinates and configured to: - provide global coordinate location information for programming a plurality of location markers with location information; - receive user-friendly location information that is a user supplied name of the location; and - program the plurality of location markers with location information; - the plurality of location markers programmed by the tag transceiver with location marker programmer , the plurality of location markers being programmed with location information of the locations that the location markers are affixed to around a site, and the user-friendly location information; - a mobile tracking system configured to read location information from nearby location markers that are placed around the site; and - a mobile monitoring and display system configured to receive signals from the mobile tracking system to display status and geo coordinates of the mobile tracking system . - a plurality of positioning transceiver systems configured to determine, for each positioning transceiver system , its corresponding position, relative to a global coordinate system, during set up of the real-time location system ; - a tag transceiver with location marker programmer configured to determine the location of the tag transceiver relative to global position coordinates and configured to: - provide global coordinate location information for programming a plurality of location markers with location information; - receive user-friendly location information that is a user supplied name of the location; and - program the plurality of location markers with location information; - provide global coordinate location information for programming a plurality of location markers with location information; - receive user-friendly location information that is a user supplied name of the location; and - program the plurality of location markers with location information; - the plurality of location markers programmed by the tag transceiver with location marker programmer , the plurality of location markers being programmed with location information of the locations that the location markers are affixed to around a site, and the user-friendly location information; - a mobile tracking system configured to read location information from nearby location markers that are placed around the site; and - a mobile monitoring and display system configured to receive signals from the mobile tracking system to display status and geo coordinates of the mobile tracking system .
A method of manufacturing an aircraft interior panel comprising a core (22; 32) sandwiched between first (24; 34) and second (26; 36) skins, wherein both of the first and second skins are formed from natural fibres containing fire-retardant and set within an inorganic thermoset resin, thereby forming a fire-resistant sustainable aircraft interior panel, the method comprising: (a) impregnating the natural fibres with fire retardant to form fire-resistant natural fibres ; (b) impregnating the fire-resistant natural fibres with inorganic thermoset resin ; (c) laying up the resin-impregnated natural fibres to sandwich the core thereby forming a stack of the core sandwiched between the resin-impregnated natural fibres ; and (d) curing the stack to form the fire resistant sustainable aircraft interior panel that comprises the core sandwiched between the first and second skins, characterized in that the curing step comprises: (d1) raising the temperature of the stack to a first temperature that is equal to or greater than a minimum activation temperature of the inorganic thermoset resin that initiates the curing reaction and less than the boiling point of water in the stack ; (d2) holding the stack at the first temperature ; (d3) raising the temperature of the stack to a second temperature that is equal to or greater than the boiling point of water in the stack ; and (d4) cooling the stack to reduce the temperature of the stack from the second temperature . (a) impregnating the natural fibres with fire retardant to form fire-resistant natural fibres ; (b) impregnating the fire-resistant natural fibres with inorganic thermoset resin ; (c) laying up the resin-impregnated natural fibres to sandwich the core thereby forming a stack of the core sandwiched between the resin-impregnated natural fibres ; and (d) curing the stack to form the fire resistant sustainable aircraft interior panel that comprises the core sandwiched between the first and second skins, characterized in that the curing step comprises: (d1) raising the temperature of the stack to a first temperature that is equal to or greater than a minimum activation temperature of the inorganic thermoset resin that initiates the curing reaction and less than the boiling point of water in the stack ; (d2) holding the stack at the first temperature ; (d3) raising the temperature of the stack to a second temperature that is equal to or greater than the boiling point of water in the stack ; and (d4) cooling the stack to reduce the temperature of the stack from the second temperature . (d1) raising the temperature of the stack to a first temperature that is equal to or greater than a minimum activation temperature of the inorganic thermoset resin that initiates the curing reaction and less than the boiling point of water in the stack ; (d2) holding the stack at the first temperature ; (d3) raising the temperature of the stack to a second temperature that is equal to or greater than the boiling point of water in the stack ; and (d4) cooling the stack to reduce the temperature of the stack from the second temperature .
A multiphase current measuring apparatus for measuring currents of a multiconductor current system with N current phases which are carried along N current conductors where N >2, comprising N -1 magnetoresistive gradient sensors for determining a magnetic field strength difference in a measurement plane between conductor currents of adjacent current conductors , characterised in that at least one bypass conductor of at least one of the further, non-immediately adjacent current conductors is arranged with respect to each magnetoresistive gradient sensor , wherein the at least one bypass conductor is designed to compensate a DC field component of the conductor currents of the two adjacent current conductors .
A laminate film comprising: a resin layer (I) which is formed from a fluororesin composition (B); and a resin layer (II) which is formed from a resin composition (C) containing an acid anhydride copolymer (C-1) including a monomer unit of styrene and acrylic rubber particles (C-2); wherein a glass transition temperature, as determined in accordance with the description, of the acid anhydride copolymer (C-1) is 50°C or higher and 105°C or lower, and the resin composition (C) forming the resin layer (II) has an acid anhydride group for exhibiting adhesiveness with a base material and the resin layer (II) is a bonding layer for facing an adherend side and the resin layer (I) is a surface layer for opposing the adherend side. a resin layer (I) which is formed from a fluororesin composition (B); and a resin layer (II) which is formed from a resin composition (C) containing an acid anhydride copolymer (C-1) including a monomer unit of styrene and acrylic rubber particles (C-2); wherein a glass transition temperature, as determined in accordance with the description, of the acid anhydride copolymer (C-1) is 50°C or higher and 105°C or lower, and the resin composition (C) forming the resin layer (II) has an acid anhydride group for exhibiting adhesiveness with a base material and the resin layer (II) is a bonding layer for facing an adherend side and the resin layer (I) is a surface layer for opposing the adherend side.
Spinach plant comprising a single dominant gene which confers resistance to Peronospora farinosa f. sp. spinaciae races Pfs1, Pfs2, Pfs3, Pfs4, Pfs5, Pfs6, Pfs9, Pfs11, Pfs12, Pfs13 and UA4410, wherein the gene is obtainable by introgression from a plant grown from seeds of which a representative sample was deposited with the NCIMB under NCIMB accession number 41857.
A floating floor panel, comprising a core of a plastic material, and a mechanical locking system for locking the floor panel to adjacent floor panels horizontally and vertically at its long and short sides through angling and/or snapping, characterised in that the floor panel further comprises a resilient surface arranged on said core , the resilient surface comprising a transparent, hard and durable wear layer of plastic material, a reinforcement layer made of an elastic material, which is both moisture proof and sound-absorbing, and an intermediate decorative layer of plastic film or decorative patterns printed directly on an underside of the transparent wear layer or on an upper side of the elastic reinforcement layer , a joint seal at least at one of the adjoining joint edge portions of the floor panels, the joint seal adapted to counteract penetration of moisture along the joint surfaces of the joint edges between adjoining floor panels , the joint seal made of an elastic sealing material, is secured in the floor panel and formed simultaneously with the forming of the locking system of the floor panels, and adapted to be elastically deformed when the floor panel is joined with the similar floor panel. a core of a plastic material, and a mechanical locking system for locking the floor panel to adjacent floor panels horizontally and vertically at its long and short sides through angling and/or snapping, characterised in that the floor panel further comprises a resilient surface arranged on said core , the resilient surface comprising a transparent, hard and durable wear layer of plastic material, a reinforcement layer made of an elastic material, which is both moisture proof and sound-absorbing, and an intermediate decorative layer of plastic film or decorative patterns printed directly on an underside of the transparent wear layer or on an upper side of the elastic reinforcement layer , a joint seal at least at one of the adjoining joint edge portions of the floor panels, the joint seal adapted to counteract penetration of moisture along the joint surfaces of the joint edges between adjoining floor panels , the joint seal made of an elastic sealing material, is secured in the floor panel and formed simultaneously with the forming of the locking system of the floor panels, and adapted to be elastically deformed when the floor panel is joined with the similar floor panel.
A method for determining the binding affinity of the binding sites of a bivalent full length antibody of the human IgG1 subclass to a homo-multimeric antigen comprising the following steps: - incubating a mixture comprising the antibody and lysine-gingipain of Porphyromonas gingivalis or an enzymatically active fragment thereof at a pH of 7.5 to 8.5, in the presence of a reducing agent, at a temperature of 30 °C to 42°C, for a time of 10 min. to 240 min. to cleave the antibody into Fabs and Fc-region, and - determining the binding affinity of the Fabs of the antibody for its antigen using surface plasmon resonance by directly applying the incubated reaction mixture obtained in the previous step in the surface plasmon resonance method and thereby determining the binding affinity of the binding sites of the bivalent full length antibody of the human IgG1 subclass, wherein the incubated mixture is used for the determination of the binding affinity without intermediate purification. - incubating a mixture comprising the antibody and lysine-gingipain of Porphyromonas gingivalis or an enzymatically active fragment thereof at a pH of 7.5 to 8.5, in the presence of a reducing agent, at a temperature of 30 °C to 42°C, for a time of 10 min. to 240 min. to cleave the antibody into Fabs and Fc-region, and - determining the binding affinity of the Fabs of the antibody for its antigen using surface plasmon resonance by directly applying the incubated reaction mixture obtained in the previous step in the surface plasmon resonance method and thereby determining the binding affinity of the binding sites of the bivalent full length antibody of the human IgG1 subclass,
Self-propelling device , in particular a cleaning device for cleaning a floor , such as a vacuum and/or sweeping robot, comprising one or more light sensors (6 to 8), characterised in that a preamplifier element is provided and a phase-sensitive detector element and a central control element , in that a signal supplied by the light sensor (6 to 8) is checked with regard to a signal pattern specified by the central control element , and in that this signal, with regard to controlling the device , is linked to the orientation of the relevant light sensor (6 to 8) when a plurality of light sensors (6 to 8) are arranged or to the angular orientation of a light sensor .
A bacterial strain of Lactiplantibacillus plantarum Provege, deposited on 24 August, 2021 with DSMZ under number DSM 33989.
Turbofan engine for a civil supersonic aircraft, which turbofan engine has: - an engine inlet which is provided and configured to slow down the incoming air during supersonic flight to speeds below the speed of sound, - a multiple-stage fan which is arranged behind the engine inlet , - a core engine which comprises a compressor , a combustion chamber and a turbine , - a primary flow duct which leads through the core engine, - a secondary flow duct which leads past the core engine, - an adjustable convergent-divergent thrust nozzle which configures a nozzle throat area and a nozzle outlet area , at least the nozzle throat area being adjustable, - the thrust nozzle having a front, upstream non-adjustable region and a rear, downstream adjustable region , and - a thrust reverser which has thrust reverser doors and is integrated into the adjustable convergent-divergent thrust nozzle , characterized in that the thrust reverser including the thrust reverser doors which deflect the gas stream in the case of a thrust reversal is integrated into the front, non-adjustable region of the thrust nozzle . - an engine inlet which is provided and configured to slow down the incoming air during supersonic flight to speeds below the speed of sound, - a multiple-stage fan which is arranged behind the engine inlet , - a core engine which comprises a compressor , a combustion chamber and a turbine , - a primary flow duct which leads through the core engine, - a secondary flow duct which leads past the core engine, - an adjustable convergent-divergent thrust nozzle which configures a nozzle throat area and a nozzle outlet area , at least the nozzle throat area being adjustable, - the thrust nozzle having a front, upstream non-adjustable region and a rear, downstream adjustable region , and - a thrust reverser which has thrust reverser doors and is integrated into the adjustable convergent-divergent thrust nozzle ,
An electronic device comprising: at least one environmental sensor configured to obtain air flowing in from outside of the electronic device; a plurality of openings formed in the electronic device; and a duct formed between the at least one environmental sensor and at least two of the plurality of openings, characterised in that at least one of the at least two openings has a bump configured to change a direction of air which flows along an outer surface of the electronic device. at least one environmental sensor configured to obtain air flowing in from outside of the electronic device; a plurality of openings formed in the electronic device; and a duct formed between the at least one environmental sensor and at least two of the plurality of openings, characterised in that at least one of the at least two openings has a bump configured to change a direction of air which flows along an outer surface of the electronic device.
A centrifugal fan impeller, comprising a hub and a plurality of fan blades distributed around the periphery of the hub ; and wherein each fan blade comprises a first blade section and a second blade section connected with the first blade section ; each first blade section is in a backward blade form; and each second blade section is in a forward blade form; characterized in that each fan blade further comprises a connecting blade section which smoothly connects the first blade section with the second blade section , the connecting blade section is a linear segment by which the first blade section is connected with the second blade section . wherein each fan blade comprises a first blade section and a second blade section connected with the first blade section ; each first blade section is in a backward blade form; and each second blade section is in a forward blade form; characterized in that each fan blade further comprises a connecting blade section which smoothly connects the first blade section with the second blade section , the connecting blade section is a linear segment by which the first blade section is connected with the second blade section .
A compound represented by the following formula or a pharmaceutically acceptable salt thereof; wherein R A is -CH 2 -CZ 1 Z 2 (COX) or -CH=CZ 1 (COX), Z 1 and Z 2 are each independently a hydrogen atom or a fluorine atom, X is OR 4 or NR 5 R 6 , R 4 is a hydrogen atom, an alkyl group having 1 - 6 carbon atoms or a substituted alkyl group having 1 - 6 carbon atoms, R 5 is a hydrogen atom, an alkyl group having 1 - 6 carbon atoms or a substituted alkyl group having 1 - 6 carbon atoms, R 6 is a hydrogen atom, an alkyl group having 1 - 6 carbon atoms, a substituted alkyl group having 1 - 6 carbon atoms, an alkylsulfonyl group having 1 - 6 carbon atoms, a substituted alkylsulfonyl group having 1 - 6 carbon atoms, an arylsulfonyl group having 6 - 10 carbon atoms or a substituted arylsulfonyl group having 6 - 10 carbon atoms; Y is CH 2 , S or O; A-B is a carbon-carbon single bond or a carbon-carbon double bond; a hydroxy group bonded by a wavy line is a hydroxy group having α-configuration, β-configuration or a mixed configuration of α-configuration and β-configuration; R 1 and R 2 are each independently a hydrogen atom, an alkyl group having 1 - 3 carbon atoms or a substituted alkyl group having 1 - 3 carbon atoms; n is an integer of 0 - 2; R 3 is an alkyl group having 2 - 3 carbon atoms or a cycloalkyl group having 3 - 5 carbon atoms. R A is -CH 2 -CZ 1 Z 2 (COX) or -CH=CZ 1 (COX), Z 1 and Z 2 are each independently a hydrogen atom or a fluorine atom, X is OR 4 or NR 5 R 6 , R 4 is a hydrogen atom, an alkyl group having 1 - 6 carbon atoms or a substituted alkyl group having 1 - 6 carbon atoms, R 5 is a hydrogen atom, an alkyl group having 1 - 6 carbon atoms or a substituted alkyl group having 1 - 6 carbon atoms, R 6 is a hydrogen atom, an alkyl group having 1 - 6 carbon atoms, a substituted alkyl group having 1 - 6 carbon atoms, an alkylsulfonyl group having 1 - 6 carbon atoms, a substituted alkylsulfonyl group having 1 - 6 carbon atoms, an arylsulfonyl group having 6 - 10 carbon atoms or a substituted arylsulfonyl group having 6 - 10 carbon atoms; Y is CH 2 , S or O; A-B is a carbon-carbon single bond or a carbon-carbon double bond; a hydroxy group bonded by a wavy line is a hydroxy group having α-configuration, β-configuration or a mixed configuration of α-configuration and β-configuration; R 1 and R 2 are each independently a hydrogen atom, an alkyl group having 1 - 3 carbon atoms or a substituted alkyl group having 1 - 3 carbon atoms; n is an integer of 0 - 2; R 3 is an alkyl group having 2 - 3 carbon atoms or a cycloalkyl group having 3 - 5 carbon atoms.