mhurhangee/patent-ind-claim-en huggingface dataset:
A method in a user equipment, UE, for transmitting on a first allocated physical uplink control channel, PUCCH, resource, the method comprising: receiving, at the UE, a downlink control channel carrying a PUCCH resource indicator, wherein the downlink control channel is associated with a demodulation reference signal, DMRS, antenna port; mapping the PUCCH resource indicator to a first offset; determining a second offset based on a position of the received downlink control channel normalized by a first value; determining an index of the DMRS antenna port associated with the downlink control channel; determining a third offset based on the determined index of the DMRS antenna port; mapping a linear combination of the first, second, and third offsets to an index identifying the first allocated PUCCH resource; and transmitting a PUCCH on the first allocated PUCCH resource. receiving, at the UE, a downlink control channel carrying a PUCCH resource indicator, wherein the downlink control channel is associated with a demodulation reference signal, DMRS, antenna port; mapping the PUCCH resource indicator to a first offset; determining a second offset based on a position of the received downlink control channel normalized by a first value; determining an index of the DMRS antenna port associated with the downlink control channel; determining a third offset based on the determined index of the DMRS antenna port; mapping a linear combination of the first, second, and third offsets to an index identifying the first allocated PUCCH resource; and transmitting a PUCCH on the first allocated PUCCH resource.
A method of processing satellite navigation system data, said method comprising: deriving predicted ephemeris data and clock correction values for a plurality of satellites using predicted positions of said satellites at selected times; compressing the predicted ephemeris data and clock correction values into coefficients and constants using time dependent functions; converting said coefficients and constants of ephemeris data into respective first scaled values, converting residuals comprising differences between said predicted ephemeris data and values calculated using the respective time dependent function into respective second scaled values, and converting said coefficients and constants of clock correction values into respective third scaled values, said converting performed with respective scaling factors selected such that coefficients reconstructed from said first scaled values have more precision than residuals reconstructed from said second scaled values, wherein each coefficient and constant is represented as the product of a scaled value and a respective scaling factor; and storing said scaled values and scaling factors in a computer-readable memory for later reconstructing the predicted ephemeris data and clock correction values by a client device, wherein said scaling factors are provided to the client device less frequently than said scaled values. deriving predicted ephemeris data and clock correction values for a plurality of satellites using predicted positions of said satellites at selected times; compressing the predicted ephemeris data and clock correction values into coefficients and constants using time dependent functions; converting said coefficients and constants of ephemeris data into respective first scaled values, converting residuals comprising differences between said predicted ephemeris data and values calculated using the respective time dependent function into respective second scaled values, and converting said coefficients and constants of clock correction values into respective third scaled values, said converting performed with respective scaling factors selected such that coefficients reconstructed from said first scaled values have more precision than residuals reconstructed from said second scaled values, wherein each coefficient and constant is represented as the product of a scaled value and a respective scaling factor; and storing said scaled values and scaling factors in a computer-readable memory for later reconstructing the predicted ephemeris data and clock correction values by a client device, wherein said scaling factors are provided to the client device less frequently than said scaled values.
An arrangement comprising a device (2; 102) for securing a first module (4; 104) and a second module (6; 106) in a space (7; 107) between a first mount (8; 108) and a second mount (10; 110), the device (2; 102) comprising: the first module (4;104) and the second module (6; 106), and a biasing apparatus (12; 112) for urging the first module (4; 104) and the second module (6; 106) away from each other, thereby urging the first module (4; 104) against the first mount (8; 108) and urging the second module (6; 106) against the second mount (10; 110), and characterised by comprising: a release apparatus (14; 114) for moving the first module (4; 104) and the second module (6; 106) toward each other, thereby moving the first module (4; 104) away from the first mount (8; 108) and moving the second module (6; 106) away from the second mount (10; 110); wherein the arrangement further comprises the first mount and the second mount , wherein the first and second mounts define the space which is configured to receive and hold the device , and wherein the arrangement comprises a first heat sink thermally coupled to the first mount . the first module (4;104) and the second module (6; 106), and a biasing apparatus (12; 112) for urging the first module (4; 104) and the second module (6; 106) away from each other, thereby urging the first module (4; 104) against the first mount (8; 108) and urging the second module (6; 106) against the second mount (10; 110), and characterised by comprising: a release apparatus (14; 114) for moving the first module (4; 104) and the second module (6; 106) toward each other, thereby moving the first module (4; 104) away from the first mount (8; 108) and moving the second module (6; 106) away from the second mount (10; 110); wherein the arrangement further comprises the first mount and the second mount , wherein the first and second mounts define the space which is configured to receive and hold the device , and wherein the arrangement comprises a first heat sink thermally coupled to the first mount .
A compound which is 1-N'-(4-fluorophenyl)-1-N-[4-[7-methoxy-6-(methylcarbamoyl)quinolin-4-yl]oxyphenyl]cyclopropane-1,1-dicarboxamide: or a pharmaceutically acceptable salt thereof.
Method for an emergency braking of an elevator car , in which method: a first emergency braking procedure is activated for braking the elevator car at a first deceleration (a 1 ) if the speed (v) of the elevator car exceeds a first limit value (v lim1 ) for permitted speed, characterized in that a second emergency braking procedure is further activated for braking the elevator car at a second deceleration (a 2 ) that is greater than the first deceleration (a 1 ), if the speed (v) of the elevator car exceeds a second limit value (V lim2 ) for permitted speed that is greater than the first limit value (v lim1 ) for permitted speed, wherein the first limit value (v lim1 ) for permitted speed is increased in the proximity of a terminal floor. a first emergency braking procedure is activated for braking the elevator car at a first deceleration (a 1 ) if the speed (v) of the elevator car exceeds a first limit value (v lim1 ) for permitted speed, characterized in that a second emergency braking procedure is further activated for braking the elevator car at a second deceleration (a 2 ) that is greater than the first deceleration (a 1 ), if the speed (v) of the elevator car exceeds a second limit value (V lim2 ) for permitted speed that is greater than the first limit value (v lim1 ) for permitted speed, wherein the first limit value (v lim1 ) for permitted speed is increased in the proximity of a terminal floor.
A spacecraft comprising: a spacecraft bus; a set of thrusters for changing a pose of the spacecraft , wherein at least two thrusters are mounted on a gimbaled boom assembly connecting the two thrusters with the spacecraft bus, such that the two thrusters are coupled thrusters sharing the same gimbal angle; a set of momentum exchange devices for absorbing disturbance torques acting on the spacecraft ; and a model predictive controller (MPC) to produce a solution for controlling thrusters of the spacecraft by optimizing a cost function over a receding horizon using a model of dynamics of the spacecraft effecting a pose of the spacecraft and a model of dynamics of the momentum exchange devices of the spacecraft effecting an orientation of the spacecraft ; a modulator to modulate magnitudes of the thrust of the coupled thrusters determined by the MPC as pulse signals specifying ON and OFF states of each of the coupled thruster , such that the ON states of the coupled thrusters sharing the same gimbal angle do not intersect in time; and a thruster controller to operate the thrusters according to their corresponding pulse signals. a spacecraft bus; a set of thrusters for changing a pose of the spacecraft , wherein at least two thrusters are mounted on a gimbaled boom assembly connecting the two thrusters with the spacecraft bus, such that the two thrusters are coupled thrusters sharing the same gimbal angle; a set of momentum exchange devices for absorbing disturbance torques acting on the spacecraft ; and a model predictive controller (MPC) to produce a solution for controlling thrusters of the spacecraft by optimizing a cost function over a receding horizon using a model of dynamics of the spacecraft effecting a pose of the spacecraft and a model of dynamics of the momentum exchange devices of the spacecraft effecting an orientation of the spacecraft ; a modulator to modulate magnitudes of the thrust of the coupled thrusters determined by the MPC as pulse signals specifying ON and OFF states of each of the coupled thruster , such that the ON states of the coupled thrusters sharing the same gimbal angle do not intersect in time; and a thruster controller to operate the thrusters according to their corresponding pulse signals.
A biopharmaceutical agent including a 37 kDa/67 kDa laminin receptor precursor/ high affinity laminin receptor (LRP/LR) and/or a fragment thereof for use in the treatment and/or prevention of obesity, wherein the LRP/LR and/or the fragment thereof being for administration to a target cell of a subject in need thereof, wherein the target cell is at least one of the following group: endothelial cells of blood vessels, smooth muscles cells of blood vessels, pancreatic cells including alpha (α) cells, beta (β) cells, delta (δ), and gamma (γ) cells, such that in use administration of the biopharmaceutical agent reduces lipid content in the target cell, and wherein the fragment is set forth in SEQ ID NO: 4 or SEQ ID NO: 5.
A resin composition comprising a polyacetal resin (A), a salt (B) consisting of a carboxylic acid and an alkaline-earth metal, and a rubber-containing graft polymer (C), wherein when 2 parts by mass of the salt (B) consisting of a carboxylic acid and an alkaline-earth metal is dissolved in 18 parts by mass of deionized water comprising a nonionic dispersant, the obtained solution has pH 8 to 12 as measured at 25 °C, characterized in that the amount of formaldehyde in an ISO-527 type 1A test piece formed by injection molding the resin composition at a molding temperature of 205°C according to a VDA 275 test is 0.10 ppm or less and the weight reduction rate of the resin composition measured by TG-DTA, after the resin composition has been retained under the air at 230°C for 20 minutes, is 4% or less, and wherein, or characterized in that the content of sodium and potassium in the resin composition is 200 ppm or less, or characterized in that , if salt (B) and the rubber-containing graft polymer (C) are comprised in a powder (X), the content of sodium and potassium in the powder (X) is 1500 ppm or less. a polyacetal resin (A), a salt (B) consisting of a carboxylic acid and an alkaline-earth metal, and a rubber-containing graft polymer (C), wherein when 2 parts by mass of the salt (B) consisting of a carboxylic acid and an alkaline-earth metal is dissolved in 18 parts by mass of deionized water comprising a nonionic dispersant, the obtained solution has pH 8 to 12 as measured at 25 °C, characterized in that the amount of formaldehyde in an ISO-527 type 1A test piece formed by injection molding the resin composition at a molding temperature of 205°C according to a VDA 275 test is 0.10 ppm or less and the weight reduction rate of the resin composition measured by TG-DTA, after the resin composition has been retained under the air at 230°C for 20 minutes, is 4% or less, and wherein, or characterized in that the content of sodium and potassium in the resin composition is 200 ppm or less, or characterized in that , if salt (B) and the rubber-containing graft polymer (C) are comprised in a powder (X), the content of sodium and potassium in the powder (X) is 1500 ppm or less.
A p-type oxide semiconductor, comprising: a metal oxide containing thallium (Tl) in a +1 valent state, wherein the metal oxide does not contain a Cu element and the metal oxide contains excess oxygen or the metal oxide contains anions having smaller ionic valency than oxygen.
Method for processing an image for an identity document, said method comprising steps consisting in: - dividing a greyscale source image into a predetermined grid comprising a set of rectangular blocks of N pixels ∗ M pixels, each block corresponding to at least 4 pixels of the source image, - applying an error diffusion dithering algorithm to the source image divided into blocks, then, for each block: - determining the average luminous intensity of the block, - selecting, from a set of predetermined cells in a lookup table, a cell that has an average luminous intensity corresponding to the average luminous intensity of the block, - said set of predetermined cells comprising a plurality of individual cells, - each individual cell comprising a unique pattern stored in a memory, and - replacing the block with the selected cell, the method further comprising a step of encoding a message in the source image divided into blocks, the method being characterized in that the encoding step comprises, for a given average-luminous-intensity value, a step consisting in: - establishing a correspondence between the position of a cell inside a super-cell and a binary value of the message to be encoded. - dividing a greyscale source image into a predetermined grid comprising a set of rectangular blocks of N pixels ∗ M pixels, each block corresponding to at least 4 pixels of the source image, - applying an error diffusion dithering algorithm to the source image divided into blocks, - determining the average luminous intensity of the block, - selecting, from a set of predetermined cells in a lookup table, a cell that has an average luminous intensity corresponding to the average luminous intensity of the block, - said set of predetermined cells comprising a plurality of individual cells, - each individual cell comprising a unique pattern stored in a memory, and - replacing the block with the selected cell, - establishing a correspondence between the position of a cell inside a super-cell and a binary value of the message to be encoded.
An industrial truck having a lift mast with at least one mast lift stage driven by at least one mast lift cylinder and with a free lift stage driven by at least one free lift cylinder , with which a load receiving means can be displaced along the lift mast , comprising a hydraulic system for supplying the at least one mast lift cylinder and the at least one free lift cylinder with a hydraulic fluid , wherein the hydraulic system is designed to at least at times simultaneously actuate the at least one mast lift cylinder and the at least one free lift cylinder in load lifting operation and/or in load lowering operation, wherein the hydraulic system for unloading the at least one mast lift cylinder and the at least one free lift cylinder in load lowering operation comprises a first hydraulic return line and a second hydraulic return line , characterized in that the first and the second hydraulic return line are fluidically coupled to one another via a third connecting line in which a third lowering valve is integrated.
A method of routing an autonomous vehicle , the method comprising: maneuvering the vehicle along a route in a first lane using map information identifying a first plurality of nodes (A-D) representing locations within a first lane and a second plurality of nodes (E-H) representing locations within a second lane different from the first lane; while maneuvering, determining when the vehicle should make a lane change to follow the route by assessing a cost of connecting a pair of nodes comprising a first node of the first plurality of nodes and a second node of a second plurality of nodes; when it is determined that the vehicle is unable to change lanes between a location represented by the first node and a location represented by the second node, increasing a cost for changing lanes between the location represented by the first node and the location represented by the second node; based on increasing the cost, identifying a different pair of nodes for effecting the lane change, the different pair of nodes comprising a node from the first plurality of nodes and a node from the second plurality of nodes; and maneuvering the vehicle to make the lane change between the nodes of the different pair of nodes. maneuvering the vehicle along a route in a first lane using map information identifying a first plurality of nodes (A-D) representing locations within a first lane and a second plurality of nodes (E-H) representing locations within a second lane different from the first lane; while maneuvering, determining when the vehicle should make a lane change to follow the route by assessing a cost of connecting a pair of nodes comprising a first node of the first plurality of nodes and a second node of a second plurality of nodes; when it is determined that the vehicle is unable to change lanes between a location represented by the first node and a location represented by the second node, increasing a cost for changing lanes between the location represented by the first node and the location represented by the second node; based on increasing the cost, identifying a different pair of nodes for effecting the lane change, the different pair of nodes comprising a node from the first plurality of nodes and a node from the second plurality of nodes; and maneuvering the vehicle to make the lane change between the nodes of the different pair of nodes.
A dental machine tool, especially a dental milling machine , comprising a tool especially exchangeable via a tool bench , and a workpiece holder for receiving a workpiece such as a dental blank made of ceramic, composite or plastic such as PMMA, and comprising a housing , which is closable during machining by the machine tool, and comprising a vacuum connection on the housing , characterized in that a plurality of air nozzles mounted on or in the housing are provided, wherein at least one of the air nozzles is directed towards the workpiece and/or the workpiece holder and/or the tool and/or the tool bench and/or a shim of a front flap of the machine tool, and is provided with at least one electrode for generating an electric field in the region of the workpiece or in front thereof, and in that at least one nozzle, with the at least one electrode, is directed towards that side of the workpiece or of the workpiece holder , where the tool processes the workpiece by machining, wherein the air supply and/or voltage at the air nozzles is adjustable to adjust the deionization effect.
An antenna , wherein the antenna comprises: a balun structure ; a radiation structure , disposed on the balun structure ; and a coupling structure , disposed on the radiation structure , wherein the coupling structure is configured to eliminate or mitigate an interference current, to reduce radiation of the antenna associated with the interference current; wherein the coupling structure is an L-shaped stub, the L-shaped stub comprises a first stub and a second stub , one end of the first stub and one end of the second stub are connected to form an L shape, the end of the first stub is electrically connected to the end of the second stub , the L-shaped stub is electrically connected to the radiation structure through the other end of the first stub , and the other end of the second stub is not connected; characterized in that two adjacent L-shaped stubs with opposite directions are combined into one T-shaped stub. a balun structure ; a radiation structure , disposed on the balun structure ; and a coupling structure , disposed on the radiation structure , wherein the coupling structure is configured to eliminate or mitigate an interference current, to reduce radiation of the antenna associated with the interference current; wherein the coupling structure is an L-shaped stub, the L-shaped stub comprises a first stub and a second stub , one end of the first stub and one end of the second stub are connected to form an L shape, the end of the first stub is electrically connected to the end of the second stub , the L-shaped stub is electrically connected to the radiation structure through the other end of the first stub , and the other end of the second stub is not connected; characterized in that two adjacent L-shaped stubs with opposite directions are combined into one T-shaped stub.
An apparatus comprising: an inlet fluid feed plate ; a base plate ; and a plurality of intermediate plates positioned between the inlet fluid feed plate and the base plate , wherein each of the plurality of intermediate plates comprises: a first end , a second end , a first side , and a second side ; a distribution channel proximal to the first end ; and a gathering channel proximal to the second end , wherein: the distribution channel extends between the first side and the second side of the intermediate plate ; and the gathering channel extends between the first side and the second side of the intermediate plate . an inlet fluid feed plate ; a base plate ; and a plurality of intermediate plates positioned between the inlet fluid feed plate and the base plate , wherein each of the plurality of intermediate plates comprises: a first end , a second end , a first side , and a second side ; a distribution channel proximal to the first end ; and a gathering channel proximal to the second end , wherein: the distribution channel extends between the first side and the second side of the intermediate plate ; and the gathering channel extends between the first side and the second side of the intermediate plate . a first end , a second end , a first side , and a second side ; a distribution channel proximal to the first end ; and a gathering channel proximal to the second end , wherein: the distribution channel extends between the first side and the second side of the intermediate plate ; and the gathering channel extends between the first side and the second side of the intermediate plate . the distribution channel extends between the first side and the second side of the intermediate plate ; and the gathering channel extends between the first side and the second side of the intermediate plate .
Method for locating a vehicle , the vehicle comprising a device having an environment sensor system by means of which the access authorization of a user to the vehicle and its position are determined, the device being indirectly or directly connected to a loudspeaker which generates acoustic signals in order to navigate the user along a route to the location of the vehicle if access authorization is granted, characterized in that the entry of the user into the vehicle is voice-assisted by means of the loudspeaker , which is directly connected to the device , by describing entry-relevant states of the vehicle , namely "The door is opening" or "Attention: step for entry upwards", via voice output.