mhurhangee/patent-ind-claim-en huggingface dataset:
Clutch actuator device which is arranged in a drive train between an internal combustion engine and a manual shift transmission of a motor vehicle; with an input shaft which is connected rotationally secured to the internal combustion engine ; with an output shaft which is connected rotationally secured to the manual shift transmission ; wherein the input shaft is connected rotationally secured to an input plate support ; that the output shaft is connected rotationally secured to an output plate support ; that the input plate support supports input plates ; that the output plate support supports output plates ; and that the input plates and the output plates can be charged and cooled with oil , with a spring assembly and a pump actuator arrangement , wherein a friction lock-up of the input plates and the output plates is cleared by means of the spring assembly and is produced by means of the pump actuator arrangement ; or that a friction lock-up of the input plates and the output plates is produced by means of the spring assembly and is cleared by means of the pump actuator arrangement , with a clutch pedal sensor for detecting a foot force acting on a clutch pedal, and with a clutch control , characterized in that if the foot force acting on the clutch pedal is detected by a clutch pedal sensor , a positive electric clutch pedal signal is emitted by the clutch pedal sensor ; that the positive electric clutch pedal signal is transmitted to the clutch control ; that a negative electric actuator signal is generated by the clutch control for a positive electric clutch pedal signal ; that the negative electric actuator signal is transmitted to an electric motor ; and that an oil pump is driven by the electric motor for a transmitted negative electric actuator signal so that the input plates and the output plates are not in friction lock-up.
Ground anchor element with - an elongated tension member , which is provided for insertion into an anchor hole in the ground, and - at least one rod element , which is arranged spirally around the tension member , characterised in that - the rod element is formed as a flexible tube or a flexible hose, respectively from a plastic material, and - the flexible tube or the flexible hose of the plastic material is wound around the tension member , whereby a spacer device is formed on an outer side of the tension member for spacing the tension member with respect to a surrounding in the anchor hole. - an elongated tension member , which is provided for insertion into an anchor hole in the ground, and - at least one rod element , which is arranged spirally around the tension member , characterised in that - the rod element is formed as a flexible tube or a flexible hose, respectively from a plastic material, and - the flexible tube or the flexible hose of the plastic material is wound around the tension member , whereby a spacer device is formed on an outer side of the tension member for spacing the tension member with respect to a surrounding in the anchor hole.
A method for wireless fault-tolerant synchronization of clocks of node computers in a distributed real-time system, which distributed real-time system comprises a number of arenas , wherein in each arena a plurality of node computers and one or more base stations are arranged, and wherein the node computers communicate with the base station or base stations by means of time-triggered wireless data messages, wherein GNS designates a Global Navigation System, characterized in that in each arena there is provided at least one Global Navigation System Signal Generator, GNSSG , wherein all GNSSGs communicate with each other by means of time-triggered messages via a wired time-triggered communication system, ZKS, and wherein each GNSSG transmits at least one GNS message exactly at the beginning of each full and half minute of the global time of the time controlled communication system provided by the ZKS, hereinafter referred to as ZKS time, and wherein a node computer disciplines an oscillator of its clock with at least one received GNS message, thus participating in the global ZKS time, and wherein, according to a schedule individually established a priori for each node computer and each base station , trigger signals for transmission of time-triggered data messages between the node computers and the base stations through one or preferably several wireless bidirectional data channels are derived from the advancement of the global ZKS time.
An apparatus comprising a processor and a memory for storing instructions to be executed by the processor , wherein the processor is configured to determine transmit power for each antenna element ( 31 to 34 ) of an antenna array for beamforming by determining a weight vector comprising a weight for each antenna element ( 31 to 34) according to a specific beamforming procedure, to detect whether at least one of the plurality of antenna elements ( 31 to 34) is saturated, wherein an antenna element is saturated when the determined transmit power for this antenna element is higher than a threshold, and, when it is detected that there is at least one saturated antenna element, to adjust the transmit power for each antenna element ( 31 to 34 ) of the antenna array such that a part of the transmit power allocated to the at least one saturated antenna element is reallocated to at least one antenna element of the antenna array which is not saturated based on the weight vector determined according to the specific beamforming procedure. wherein the processor is further configured, upon adjusting the transmit power for each unsaturated antenna element, to calculate an adjustment factor based on a weight vector determined by the specific beamforming procedure and on a weight of the saturated antenna element, and to calculate the adjusted weight of the at least one unsaturated antenna element based on the following formula: U 0 , i ′ = ρ i U 0 , i , i ∈ A , ρ i = ∑ i ∈ A ‖ U 0 , i ‖ 2 + ‖ U 0 , j ‖ 2 − C ∑ i ∈ A ‖ U 0 , i ‖ 2 , where j is the saturated antenna element index, U 0 , i ′ is the adjusted weight of the antenna element i, ρ i is the adjustment factor, U 0 , i is the weight determined by the specific beamforming procedure, U 0 is the weight vector determined by the specific beamforming procedure, U 0 , j is the weight of the saturated antenna element, C is the per-antenna element transmit power capability, and A is a subset of all antenna elements i with j ∉ A.
A method comprising: providing an optical component having one or more damage sites, wherein each of the one or more damage sites is characterized by a pit with material missing from a surface of the optical component; focusing a laser beam from a laser at a location within a first damage site, from among the one or more damage sites, the laser beam being characterized by an output power and a beam diameter at any instant in time, the laser beam being directed through an optical window in a nozzle and focused to a desired spot and size by the laser; setting the output power of the laser beam to a first output power; heating an area of the optical component at the location to a first temperature using the laser beam at the first output power; using the nozzle to receive a precursor gas, and to provide the precursor gas coaxial to the laser beam, at the location; and depositing a first predetermined amount of material only at the area heated by the laser beam so as to at least partially fill the first damage site with the first predetermined amount of material. providing an optical component having one or more damage sites, wherein each of the one or more damage sites is characterized by a pit with material missing from a surface of the optical component; focusing a laser beam from a laser at a location within a first damage site, from among the one or more damage sites, the laser beam being characterized by an output power and a beam diameter at any instant in time, the laser beam being directed through an optical window in a nozzle and focused to a desired spot and size by the laser; setting the output power of the laser beam to a first output power; heating an area of the optical component at the location to a first temperature using the laser beam at the first output power; using the nozzle to receive a precursor gas, and to provide the precursor gas coaxial to the laser beam, at the location; and depositing a first predetermined amount of material only at the area heated by the laser beam so as to at least partially fill the first damage site with the first predetermined amount of material.
Seal arrangement for sealing two spaces which are arranged adjacently with respect to one another in the axial direction and are to be sealed with respect to one another, comprising a first machine element , a second machine element and a sealing ring , the first machine element being enclosed by the second machine element at a radial spacing, and the sealing ring being arranged in the gap which is formed by way of the radial spacing, the sealing ring having at least one dynamically loaded first sealing lip which sealingly encloses a surface to be sealed of the first machine element , the sealing ring being arranged in an installation space of the second machine element , and the sealing ring having a first and a second end side , of which the first end side axially faces the first space to be sealed and the second end side axially faces the second space to be sealed, it being possible for the first space to be loaded with a relative positive pressure, in relation to the second space , the second end side being configured as a first contact face of the sealing ring , the second machine element having a second contact face on the side which axially faces the first contact face , and the first and the second contact face making contact with one another in a bearing manner, characterized in that the first and the second contact face are of congruent configuration with respect to one another in a production-induced manner, in that the contact faces are configured in each case as an oblique plane in such a way that, in the case of a movement of the sealing ring axially in the direction of the second space , a relative movement of the two contact faces on one another takes place at the same time, and the internal diameter of the at least one sealing lip sealingly encloses the surface to be sealed with an increasing radial prestress, the contact faces in each case enclosing an angle (α 1 , α 2 ) which is from 5° to 45° with an imaginary radial plane which intersects the contact faces .
A cleaning composition, comprising: 1) at least one chelating agent in an amount of from 0.01 % to 0.5% by weight of the composition, the chelating agent being a polyaminopolycarboxylic acid; 2) at least one organic solvent selected from the group consisting of water soluble alcohols, water soluble ketones, water soluble esters, and water soluble ethers, the at least one organic solvent being in an amount of 2% to 20% by weight of the composition; 3) at least one monocarboxylic acid containing a primary or secondary amino group and at least one additional basic group containing nitrogen, wherein the primary or secondary amino group is not directly bonded to nor part of another nitrogen containing basic group, the at least one monocarboxylic acid being in an amount of from 0.02% to 2% by weight of the composition; 4) at least one metal corrosion inhibitor, the metal corrosion inhibitor being a substituted or unsubstituted benzotriazole and in an amount of from 0.05% to 2% by weight of the composition; and 5) water in an amount of from 78% to 98% by weight of the composition; wherein the pH of the composition is between 7 and 9; wherein the polyaminopolycarboxylic acid is selected from the group consisting of mono- or polyalkylene polyamine polycarboxylic acids, polyaminoalkane polycarboxylic acids, polyaminoalkanol polycarboxylic acids, and hydroxyalkylether polyamine polycarboxylic acids; and wherein the monocarboxylic acid is a compound of Structure (I): (R 3 NH)C(R 1 )(R 2 )CO 2 H (I), wherein each of R 1 and R 2 , independently, is a hydrogen atom, C 1 -C 4 alkyl, or a group having at least one nitrogen-containing basic group; and R 3 is a hydrogen atom, C 1 -C 10 alkyl, or a group having at least one nitrogen-containing basic group; wherein at least one of R 1 , R 2 , and R 3 is a group having at least one nitrogen-containing basic group. 1) at least one chelating agent in an amount of from 0.01 % to 0.5% by weight of the composition, the chelating agent being a polyaminopolycarboxylic acid; 2) at least one organic solvent selected from the group consisting of water soluble alcohols, water soluble ketones, water soluble esters, and water soluble ethers, the at least one organic solvent being in an amount of 2% to 20% by weight of the composition; 3) at least one monocarboxylic acid containing a primary or secondary amino group and at least one additional basic group containing nitrogen, wherein the primary or secondary amino group is not directly bonded to nor part of another nitrogen containing basic group, the at least one monocarboxylic acid being in an amount of from 0.02% to 2% by weight of the composition; 4) at least one metal corrosion inhibitor, the metal corrosion inhibitor being a substituted or unsubstituted benzotriazole and in an amount of from 0.05% to 2% by weight of the composition; and 5) water in an amount of from 78% to 98% by weight of the composition;
A tablet comprising: (i) not less than 25 mass % of N-(4-(1-(2,6-difluorobenzyl)-5-((dimethylamino)methyl)-3-(6-methoxy-3-pyridazinyl)-2,4-dioxo-1,2,3,4-tetrahydrothieno[2,3-d]pyrimidin-6-yl)phenyl)-N'-methoxyurea or a salt thereof; and (ii) D-mannitol particles having an average particle size of 60 - 500 μm. (i) not less than 25 mass % of N-(4-(1-(2,6-difluorobenzyl)-5-((dimethylamino)methyl)-3-(6-methoxy-3-pyridazinyl)-2,4-dioxo-1,2,3,4-tetrahydrothieno[2,3-d]pyrimidin-6-yl)phenyl)-N'-methoxyurea or a salt thereof; and (ii) D-mannitol particles having an average particle size of 60 - 500 μm.
Fixed-wing flying drone comprising: - a fuselage consisting of a single central body ; - a wing assembly consisting of: - a front aerofoil defined by a wing surface A1, a wing span E1 and a chord C1, with A1 = E1 x C1; - a rear aerofoil defined by a wing surface A2, a wing span E2 and a chord C2, with A2 = E2 x C2; the rear aerofoil being offset in height and length on the fuselage with respect to the front aerofoil, the front aerofoil and the rear aerofoil being straight aerofoils; - propulsion means supplied at least by electric accumulators and/or photovoltaic cells; - photovoltaic cells covering mainly the upper faces of the front aerofoil and of the rear aerofoil; characterised in that : - the front aerofoil is directly attached on a lower height of the central body, extending from the central body, and exhibits a zero or negative dihedron; - the rear aerofoil is attached directly on an upper height of the central body, extending from this central body, and exhibits a zero or positive dihedron; - E1 > E2, and C2 > C1; - the wing surface A2 is equal to the wing surface A1. - a fuselage consisting of a single central body ; - a wing assembly consisting of: - a front aerofoil defined by a wing surface A1, a wing span E1 and a chord C1, with A1 = E1 x C1; - a rear aerofoil defined by a wing surface A2, a wing span E2 and a chord C2, with A2 = E2 x C2; the rear aerofoil being offset in height and length on the fuselage with respect to the front aerofoil, the front aerofoil and the rear aerofoil being straight aerofoils; - a front aerofoil defined by a wing surface A1, a wing span E1 and a chord C1, with A1 = E1 x C1; - a rear aerofoil defined by a wing surface A2, a wing span E2 and a chord C2, with A2 = E2 x C2; the rear aerofoil being offset in height and length on the fuselage with respect to the front aerofoil, the front aerofoil and the rear aerofoil being straight aerofoils; - propulsion means supplied at least by electric accumulators and/or photovoltaic cells; - photovoltaic cells covering mainly the upper faces of the front aerofoil and of the rear aerofoil; - the front aerofoil is directly attached on a lower height of the central body, extending from the central body, and exhibits a zero or negative dihedron; - the rear aerofoil is attached directly on an upper height of the central body, extending from this central body, and exhibits a zero or positive dihedron; - E1 > E2, and C2 > C1; - the wing surface A2 is equal to the wing surface A1.
Manual dosing device , in particular pipette , having a main body and having a fluid-dispensing unit which is connected to the main body , wherein the manual dosing device has a grip which is releasably fastened to the main body of the manual dosing device and is removable therefrom and/or is exchangeable, wherein the grip is of hook-shaped form at its upper end , which is adjacent to a head end of the main body , characterized in that the grip comprises a grip shell which at least partially surrounds the main body in the position of use.
A steer-by-wire system , comprising a first control device , which controls at least one steering actuator , and at least one second control device , which controls at least one actuator on a steering handle , in order to generate a haptic torque, wherein a sensor system for detecting a steering wheel angle is associated with the second control device , wherein the first control device is connected to a first bus system and the second control device is connected to a second bus system , characterized in that the two bus systems are connected to one another via a gateway control device and the first control device and the second control device are directly connected with one another via a third bus system .
A knob assembly, comprising: a knob configured to be rotatably installed; a knob ring configured to surround the knob and be rotated independently from the knob ; characterized by at least one spring (S1, S2) configured to provide an elastic force for returning the knob ring toward an initial position when the knob ring is rotated to a position spaced apart from the initial position; and at least one magnetic force provider (M1, M2) configured to provide a magnetic force for moving the knob ring to the initial position when the knob ring is at a position adjacent to the initial position. a knob configured to be rotatably installed; a knob ring configured to surround the knob and be rotated independently from the knob ; characterized by at least one spring (S1, S2) configured to provide an elastic force for returning the knob ring toward an initial position when the knob ring is rotated to a position spaced apart from the initial position; and at least one magnetic force provider (M1, M2) configured to provide a magnetic force for moving the knob ring to the initial position when the knob ring is at a position adjacent to the initial position.
A honeycomb filter comprising a plurality of cells for allowing exhaust gas to flow therethrough, the cells including exhaust gas introduction cells and exhaust gas emission cells, and porous cell walls defining rims of the plurality of cells, the exhaust gas introduction cells each having an open end at an exhaust gas introduction side and a plugged end at an exhaust gas emission side, the exhaust gas emission cells each having an open end at the exhaust gas emission side and a plugged end at the exhaust gas introduction side, wherein an oxidation catalyst is supported inside the cell walls in an amount of 5 to 60 g/L; the exhaust gas introduction cells and the exhaust gas emission cells each have a uniform cross sectional shape except for the plugged portion in a direction perpendicular to the longitudinal direction of the cells thoroughly from the end at the exhaust gas introduction side to the end at the exhaust gas emission side; the exhaust gas emission cells have a larger average cross sectional area in a direction perpendicular to the longitudinal direction than the exhaust gas introduction cells in a direction perpendicular to the longitudinal direction; and the total volume of the exhaust gas introduction cells is larger than the total volume of the exhaust gas emission cells, wherein each exhaust gas emission cell is adjacently surrounded fully by the exhaust gas introduction cells across the porous cell walls, the exhaust gas introduction cells include first exhaust gas introduction cells and second exhaust gas introduction cells each having a larger cross sectional area than each first exhaust gas introduction cell in a direction perpendicular to the longitudinal direction of the cells, each exhaust gas emission cell has a cross sectional area equal in size to each second exhaust gas introduction cell in a direction perpendicular to the longitudinal direction of the cells, in the cross section perpendicular to the longitudinal direction of the cells, the exhaust gas introduction cells and the exhaust gas emission cells are each polygonal, and a side forming the cross sectional shape of each first exhaust gas introduction cell faces one of the exhaust gas emission cells, a side forming the cross sectional shape of each second exhaust gas introduction cell faces one of the exhaust gas emission cells, and the side of the first exhaust gas introduction cell is longer than the side of the second exhaust gas introduction cell, and wherein, in the cross section perpendicular to the longitudinal direction of the cells, the exhaust gas emission cells are each octagonal, the first exhaust gas introduction cells are each square, and the second exhaust gas introduction cells are each octagonal.
An information communication system, comprising: a first transmission system configured to transmit information in a direction from a first communication device to a second communication device ; and a second transmission system configured to transmit information in a direction opposite to the direction of the first transmission system , wherein part of transmission information is received as received information in each of the first transmission system and the second transmission system ; wherein each of the first communication device and the second communication device includes a transmitter configured to transmit transmission information to another communication device, a receiver configured to receive received information from the another communication device, switching means for, at a time of parameter adjustment of the transmitter, turning back a transmission signal outputted from the transmitter and making the transmission signal be inputted to the receiver in the own device, and a parameter adjustment means for adjusting a transmission parameter of the transmitter based on a received signal of the receiver in the own device having received the signal that is turned back. a first transmission system configured to transmit information in a direction from a first communication device to a second communication device ; and a second transmission system configured to transmit information in a direction opposite to the direction of the first transmission system , wherein part of transmission information is received as received information in each of the first transmission system and the second transmission system ; wherein each of the first communication device and the second communication device includes a transmitter configured to transmit transmission information to another communication device, a receiver configured to receive received information from the another communication device, switching means for, at a time of parameter adjustment of the transmitter, turning back a transmission signal outputted from the transmitter and making the transmission signal be inputted to the receiver in the own device, and a parameter adjustment means for adjusting a transmission parameter of the transmitter based on a received signal of the receiver in the own device having received the signal that is turned back.