mhurhangee/ep-ind-claims huggingface dataset:
A method for producing a plant, comprising: a step of growing at least one plant selected from the group consisting of a sweet potato and crown daisies; and a step of subjecting the grown plant to nutriculture using a culture solution; wherein the content of each of a nitrate ion and a phosphate ion in the culture solution is less than 10 ppm by mass with respect to a total mass of the culture solution, wherein the culture solution contains a metal ion of at least one metal selected from the group consisting of B, Mn, Zn, Cu, and Mo, wherein, in a case where the culture solution contains one type of the metal ion, a content of the metal ion is 20 ppb by mass or more and 1.0 ppm by mass or less with respect to a total mass of the culture solution; and wherein, in a case where the culture solution contains two or more types of the metal ions, the content of each of the metal ions is 20 ppb by mass or more and 1.0 ppm by mass or less with respect to the total mass of the culture solution. a step of growing at least one plant selected from the group consisting of a sweet potato and crown daisies; and a step of subjecting the grown plant to nutriculture using a culture solution; wherein the content of each of a nitrate ion and a phosphate ion in the culture solution is less than 10 ppm by mass with respect to a total mass of the culture solution, wherein the culture solution contains a metal ion of at least one metal selected from the group consisting of B, Mn, Zn, Cu, and Mo, wherein, in a case where the culture solution contains one type of the metal ion, a content of the metal ion is 20 ppb by mass or more and 1.0 ppm by mass or less with respect to a total mass of the culture solution; and wherein, in a case where the culture solution contains two or more types of the metal ions, the content of each of the metal ions is 20 ppb by mass or more and 1.0 ppm by mass or less with respect to the total mass of the culture solution.
An alkaline detergent and rinsing composition comprising: from 45 wt-% to 75 wt-% of an alkalinity source comprising an alkali metal carbonate; and at least two nonionic surfactants, wherein said nonionic surfactants comprise from 1 wt-% to 10 wt-% of the alkaline detergent composition of a C10-C12 alcohol alkoxylate with 15 to 25 moles of alkyl oxide and from 1 wt-% to 10 wt-% of the alkaline detergent composition of an EO/PO copolymer represented by the formula y x y, where x is in the range of 5 to 50, y is in the range of 1 to 50, and x plus y is in the range of 6 to 200; and from 5 wt-% to 50 wt-% of a builder selected from the group consisting of condensed phosphates, alkali metal silicates and metasilicates, phosphonates and aminocarboxylic acids; wherein said composition performs both a cleaning and rinsing function. from 45 wt-% to 75 wt-% of an alkalinity source comprising an alkali metal carbonate; and at least two nonionic surfactants, wherein said nonionic surfactants comprise from 1 wt-% to 10 wt-% of the alkaline detergent composition of a C10-C12 alcohol alkoxylate with 15 to 25 moles of alkyl oxide and from 1 wt-% to 10 wt-% of the alkaline detergent composition of an EO/PO copolymer represented by the formula y x y, where x is in the range of 5 to 50, y is in the range of 1 to 50, and x plus y is in the range of 6 to 200; and from 5 wt-% to 50 wt-% of a builder selected from the group consisting of condensed phosphates, alkali metal silicates and metasilicates, phosphonates and aminocarboxylic acids; wherein said composition performs both a cleaning and rinsing function.
A radio frequency signal acquisition and source location system, comprising: a first signal acquisition and source location module comprising an RF transceiver coupled to an antenna, the antenna provided with a electronic steering circuit; the antenna operative to launch an interrogation signal, the interrogation signal steerable through a zone by an electronic steering circuit; and a processor operatively coupled to the RF transceiver and the electronic steering circuit; the processor provided with a data storage for storing a signal data record for each of at least one response signal(s) received by the RF transceiver(s); the signal data record including a signal identification, a received signal strength indicator and an RF signal direction along which respective signal(s) are received by the antenna, the RF signal direction derived from the electronic steering circuit; and a position logic operative upon the data record(s) to derive a first three dimensional signal origin location within the zone of each response signal characterized in that the antenna is a phased array steerable antenna; the position logic applying a curve fitting routine between at least three points to define a sphere and therefrom a center point and designating the calculated sphere center point as the three dimensional signal origin location. a first signal acquisition and source location module comprising an RF transceiver coupled to an antenna, the antenna provided with a electronic steering circuit; the antenna operative to launch an interrogation signal, the interrogation signal steerable through a zone by an electronic steering circuit; and a processor operatively coupled to the RF transceiver and the electronic steering circuit; the processor provided with a data storage for storing a signal data record for each of at least one response signal(s) received by the RF transceiver(s); the signal data record including a signal identification, a received signal strength indicator and an RF signal direction along which respective signal(s) are received by the antenna, the RF signal direction derived from the electronic steering circuit; and a position logic operative upon the data record(s) to derive a first three dimensional signal origin location within the zone of each response signal characterized in that the antenna is a phased array steerable antenna; the position logic applying a curve fitting routine between at least three points to define a sphere and therefrom a center point and designating the calculated sphere center point as the three dimensional signal origin location.
A gearbox for actuating at least one component of a vehicle seat comprising: a housing defining an interior, an output pulley rotatably coupled to said housing, and an output cable coupled to said output pulley, characterized by an input pulley rotatably coupled to said housing; a sun gear attached to one of said pulleys (18, 20); a ring gear coupled to said housing and disposed about said sun gear; a plurality of planetary gears attached to the other of said pulleys (18, 20) and operably engaged with said sun gear and said ring gear; an input cable coupled to said input pulley with said input cable having a neutral state and an activated state, wherein said input cable rotates said input pulley in a first direction when said input cable moves from said neutral state to said activated state; wherein said output cable has a locked state and an unlocked state, wherein said output cable moves from said locked state to said unlocked state when said output pulley rotates in said first direction in response to said rotation of said input pulley in said first direction; and a biasing member operatively connected to said output pulley to rotate said output pulley in a second direction opposite of said first direction to move said input cable from said activated state to said neutral state. a housing defining an interior, an output pulley rotatably coupled to said housing, and an output cable coupled to said output pulley, characterized by an input pulley rotatably coupled to said housing; a sun gear attached to one of said pulleys (18, 20); a ring gear coupled to said housing and disposed about said sun gear; a plurality of planetary gears attached to the other of said pulleys (18, 20) and operably engaged with said sun gear and said ring gear; an input cable coupled to said input pulley with said input cable having a neutral state and an activated state, wherein said input cable rotates said input pulley in a first direction when said input cable moves from said neutral state to said activated state; wherein said output cable has a locked state and an unlocked state, wherein said output cable moves from said locked state to said unlocked state when said output pulley rotates in said first direction in response to said rotation of said input pulley in said first direction; and a biasing member operatively connected to said output pulley to rotate said output pulley in a second direction opposite of said first direction to move said input cable from said activated state to said neutral state.
An automatic pressing jig apparatus that closely contacts a lead assembly and a bus bar provided in a battery module to each other, the automatic pressing jig apparatus comprising: a plurality of contacting units configured to simultaneously press each of a plurality of bus bars provided in the battery module and press an end of the lead assembly from a top of the plurality of bus bars to prevent the lead assembly from protruding from a surface of the plurality of bus bars; a pair of pressing units (250, 260) connected to the plurality of contacting units and configured to adjust a pressing force of the plurality of contacting units with respect to the plurality of bus bars; a support frame supporting the pair of pressing units (250, 260); and a distance adjusting unit connected to the support frame and configured to ascend or descend the support frame to move the plurality of contacting units away from or close to the battery module. a plurality of contacting units configured to simultaneously press each of a plurality of bus bars provided in the battery module and press an end of the lead assembly from a top of the plurality of bus bars to prevent the lead assembly from protruding from a surface of the plurality of bus bars; a pair of pressing units (250, 260) connected to the plurality of contacting units and configured to adjust a pressing force of the plurality of contacting units with respect to the plurality of bus bars; a support frame supporting the pair of pressing units (250, 260); and a distance adjusting unit connected to the support frame and configured to ascend or descend the support frame to move the plurality of contacting units away from or close to the battery module.
A catalytic site-introduced functional separator for a lithium-sulfur battery comprising a base separator; and a catalytic site-containing coating layer located on the surface of the base separator; wherein the catalytic site contains a continuous bond of transition metal-nitrogen-carbon; wherein the content of the catalytic site-containing coating layer is 1 to 200 μ g/cm 2 relative to the surface area of the base separator.
Wind turbine having a wind rotor, a generator that is driven thereby and has a converter for generating electric power that is delivered to a grid by way of a connection line, a converter controller that has a first control channel for controlling the delivery of power to the grid and for exciting the generator, and a second control channel, different from the first control channel, characterized in that the second control channel is configured as a field-oriented controller and, to this end, has a dedicated coordinate transformation unit that is configured so as to be sub-synchronous and, to this end, is provided with a revolving coordinate system (θ SS) having a frequency that is lower than the grid frequency (θ) in absolute terms.
An electrode for an electric double layer capacitor, comprising a polarizing electrode layer formed from polarizing electrode materials; a conductive adhesive; and a sheet current collector, wherein the polarizing electrode materials include porous carbon particles, an auxiliary conductive agent, a tungsten oxide powder, and a binder; and the conductive adhesive containing a conductive material and a binder; characterized in that the binder contained in the conductive adhesive is a poly-N-vinylacetamide (PNVA)-based binder, and the polarizing electrode layer has a porosity in a range of 40% to 90% and/or an average pore size of 0.1 μm to 5 μm.
Piston accumulator, having an accumulator housing and a separating piston guided so as to be longitudinally movable therein, which separates a liquid side from a gas side in the accumulator housing, wherein, despite a piston seal on the separating piston, liquid passes unintentionally from the liquid side to the gas side, wherein, to enlarge the volume of the gas side, the separating piston has the shape of a shell, the inner cavity of which extends from the piston crown with its open end to the piston end on the gas side, characterised in that, by means of a return device (28; 92), the fluid which has passed over is at least partially returned from the gas side of the accumulator housing to the liquid side thereof.
A channel assembly for fluid conduits, comprising a base profile and a cover profile that is removably fixed to said base profile to form with the latter a closed-section channel intended for housing therein at least one fluid conduit extending longitudinally into said channel, said base profile being formed by a plate that is configured for being fixed to a wall, or to any other flat support, parallel to a main plane of said plate, said plate constituting a bottom wall of said channel and lacking side walls that constitute the side walls of said channel, and said cover profile having a U-shaped cross section with two opposite walls (6, 7) and a transverse wall constituting respective side walls and an upper wall of said channel, respectively, characterized in that said base profile is provided with at least one fin projecting from said plate into said channel, said fin extending in the longitudinal direction of said channel and comprising a wall orthogonal to said main plane of said plate, said wall of the fin being perforated with a plurality of through openings distributed along said fin, each of said through openings having a closed contour and forming an eyelet for the passage of a zip tie which is not part of said channel assembly, and in that said base profile is provided with a plurality of transverse weakening lines distributed along said base profile, each of said weakening lines extending partially into said bottom wall and partially into said fin.
An aircraft, comprising: fuselage having a nose, a main section aft of the nose in an axial direction and a tail aft of the main section in the axial direction; an engine nacelle partially embedded in the tail and comprising a boundary layer ingestion propulsor with an inlet directly adjacent to the fuselage; and a nozzle element disposed upstream from the inlet; characterised in that the nozzle element is configured to accelerate boundary flows flowing toward an interior side of the engine nacelle; and in that the nozzle element has a step-wise curvature along the axial direction and an annular curvature about a longitudinal axis of the fuselage. fuselage having a nose, a main section aft of the nose in an axial direction and a tail aft of the main section in the axial direction; an engine nacelle partially embedded in the tail and comprising a boundary layer ingestion propulsor with an inlet directly adjacent to the fuselage; and a nozzle element disposed upstream from the inlet; characterised in that the nozzle element is configured to accelerate boundary flows flowing toward an interior side of the engine nacelle; and in that the nozzle element has a step-wise curvature along the axial direction and an annular curvature about a longitudinal axis of the fuselage.
A method performed by a base station, BS, for performing communication in a wireless communication system, the method comprising: receiving, from a user equipment, UE, multiple input multiple output, MIMO, capability of the UE; transmitting, to the UE, information about a number of antenna ports for a serving cell; identifying a number of bits for a rank indication, RI, based on a maximum number of layers for spatial multiplexing for the UE; and receiving, from the UE, the RI using the identified number of bits for the RI, wherein the maximum number of layers for spatial multiplexing is determined based on a smaller between the number of antenna ports and a number of layers corresponding to the MIMO capability of the UE for a frequency band in a corresponding band combination, in case that the BS identifies that the UE is configured with a first transmission mode among a plurality of transmission modes. receiving, from a user equipment, UE, multiple input multiple output, MIMO, capability of the UE; transmitting, to the UE, information about a number of antenna ports for a serving cell; identifying a number of bits for a rank indication, RI, based on a maximum number of layers for spatial multiplexing for the UE; and receiving, from the UE, the RI using the identified number of bits for the RI, wherein the maximum number of layers for spatial multiplexing is determined based on a smaller between the number of antenna ports and a number of layers corresponding to the MIMO capability of the UE for a frequency band in a corresponding band combination, in case that the BS identifies that the UE is configured with a first transmission mode among a plurality of transmission modes.
An exhaust gas aftertreatment system for dosing reducing agent into an exhaust stream, the system comprising a diesel emission fluid reservoir, a reactor for generating an ammonia solution from diesel emission fluid in the diesel emission fluid reservoir, a doser configured to discharge controlled amounts of the ammonia solution into an exhaust stream moving through the exhaust gas aftertreatment system, a heating system configured to manage temperatures within the doser, the heating system including a passive doser heat exchanger configured to withdraw heat from exhaust gasses passing through the exhaust aftertreatment system and heat passageways through the doser, an active doser heating element configured to produce heat from electrical energy supplied to the heating system and heat passageways through the doser, and a heating system controller configured to selectively apply heat from the active doser heating element to manage the temperature of the ammonia solution moving in passageways through the doser, a NOx sensor configured to detect the amount of NOx carried in an exhaust stream entering the exhaust aftertreatment system, a doser controller configured to inject the ammonia solution at a predetermined reaction flow rate into the exhaust stream based at least in part on the amount of NOx detected wherein the reactor is an ammonium carbamate reactor and the ammonia solution is ammonium carbamate, an ammonium carbamate reservoir configured to store aqueous ammonium carbamate generated by the ammonium carbamate reactor, and a reservoir level sensor configured to detect an amount of aqueous ammonium carbamate solution in the ammonium carbamate reservoir, wherein the doser controller is configured to inject aqueous ammonium carbamate solution at a relief flow rate into the exhaust stream greater than the predetermined reaction flow rate when the amount of aqueous ammonium carbamate solution in the ammonium carbamate reservoir is greater than a predetermined amount.
A propulsion system for an aircraft comprising: an electric power source; an electric propulsion assembly comprising an electric motor and a propulsor, the propulsor powered by the electric motor; and a high-voltage electric power bus electrically connecting the electric power source to the electric propulsion assembly; wherein the electric power source is configured to provide electrical power to the high-voltage electric power bus; the high-voltage electric power bus comprises a high-voltage cable configured to transfer the electric power to the electric propulsion assembly at a voltage exceeding 800 volts; the high-voltage cable comprises: a conductor; a semi-conductive conductor screen enclosing the conductor; an insulation layer enclosing the conductor screen; and a semi-conductive insulator screen enclosing the insulation layer; the conductor is a braided conductor; and the conductor screen fills air gaps on an outer surface of the braided conductor. an electric power source; an electric propulsion assembly comprising an electric motor and a propulsor, the propulsor powered by the electric motor; and a high-voltage electric power bus electrically connecting the electric power source to the electric propulsion assembly; wherein the electric power source is configured to provide electrical power to the high-voltage electric power bus; the high-voltage electric power bus comprises a high-voltage cable configured to transfer the electric power to the electric propulsion assembly at a voltage exceeding 800 volts; the high-voltage cable comprises: a conductor; a semi-conductive conductor screen enclosing the conductor; an insulation layer enclosing the conductor screen; and a semi-conductive insulator screen enclosing the insulation layer; a conductor; a semi-conductive conductor screen enclosing the conductor; an insulation layer enclosing the conductor screen; and a semi-conductive insulator screen enclosing the insulation layer; the conductor is a braided conductor; and the conductor screen fills air gaps on an outer surface of the braided conductor.
Gas pipe unit assembly having a particle filter, for a heat exchanger for gas, very especially for engine exhaust gases, the gas pipe unit being able to be fixed to one end of a heat exchanger block such that it remains in fluidic communication with the latter in order for the gases to pass through it and the particle filter being coupled to the gas pipe unit in order to filter the exhaust gases that pass through it, characterized in that said particle filter is interchangeable, said filter being mounted in a removable manner in said gas pipe unit, said gas pipe unit comprising at least one flange for connecting to a gas recirculation line, and said particle filter being mounted in a removable manner on said connecting flange and disposed so as to filter the gases that pass through it and pass through a through-opening in the connecting flange.