mhurhangee/patent-ind-claim-en huggingface dataset:
A steering control apparatus for a steering system to which a motor torque that reciprocates a wheel turning shaft of a steering mechanism is applied by an actuator that uses a motor as a drive source, the steering control apparatus comprising a controller configured to: compute a torque command value that is a target value of the motor torque that the motor outputs; when an absolute value of a rotation angle of a rotary shaft exceeds a steering angle threshold for the steering system , compute a steering angle limit value that reduces with an increase in the absolute value of the rotation angle, the rotation angle of the rotary shaft being convertible to a wheel steering angle of a steered wheel coupled to the wheel turning shaft ; set a limit value to less than or equal to the steering angle limit value, the limit value being an upper limit of an absolute value of the torque command value; control the motor such that the motor torque follows the torque command value whose absolute value is limited to less than or equal to the limit value; compute a basic command value based on a steering torque; when the absolute value of the rotation angle exceeds the steering angle threshold, compute a damping control amount such that the damping control amount increases with an increase in an excess of an angular velocity of the rotary shaft over a first upper limit angular velocity set according to the absolute value of the rotation angle; and compute the torque command value based on a value obtained by combining the basic command value and the damping control amount such that an absolute value of the basic command value is reduced. compute a torque command value that is a target value of the motor torque that the motor outputs; when an absolute value of a rotation angle of a rotary shaft exceeds a steering angle threshold for the steering system , compute a steering angle limit value that reduces with an increase in the absolute value of the rotation angle, the rotation angle of the rotary shaft being convertible to a wheel steering angle of a steered wheel coupled to the wheel turning shaft ; set a limit value to less than or equal to the steering angle limit value, the limit value being an upper limit of an absolute value of the torque command value; control the motor such that the motor torque follows the torque command value whose absolute value is limited to less than or equal to the limit value; compute a basic command value based on a steering torque; when the absolute value of the rotation angle exceeds the steering angle threshold, compute a damping control amount such that the damping control amount increases with an increase in an excess of an angular velocity of the rotary shaft over a first upper limit angular velocity set according to the absolute value of the rotation angle; and compute the torque command value based on a value obtained by combining the basic command value and the damping control amount such that an absolute value of the basic command value is reduced.
A distributed architecture for multi-nodal control of functions in an aircraft cabin , comprising: a processor ; a controller operatively connected to the processor ; a passenger-controlled IO node operatively connected to the controller ; and a crew-controlled IO node operatively connected to the controller ; wherein the controller controls at least one controllable parameter in response to inputs received from at least one of the passenger-controlled IO node and the crew-controlled IO node , wherein the at least one controllable parameter comprises at least one of light intensity in the aircraft cabin , color of light in the aircraft cabin , temperature in the aircraft cabin , and a degree of openness of a window shade in the aircraft cabin , and wherein the controller includes a command hierarchy to prioritize inputs received from the passenger-controlled IO node and the crew-controlled IO node to prevent conflicts between the inputs, the distributed architecture being characterized in that the command hierarchy prioritizes inputs received from the passenger-controlled IO node and the crew-controlled IO node based on an operation mode of the aircraft, said operation mode being determined via a data exchange with an avionic system of the aircraft. a processor ; a controller operatively connected to the processor ; a passenger-controlled IO node operatively connected to the controller ; and a crew-controlled IO node operatively connected to the controller ; wherein the controller controls at least one controllable parameter in response to inputs received from at least one of the passenger-controlled IO node and the crew-controlled IO node , wherein the at least one controllable parameter comprises at least one of light intensity in the aircraft cabin , color of light in the aircraft cabin , temperature in the aircraft cabin , and a degree of openness of a window shade in the aircraft cabin , and wherein the controller includes a command hierarchy to prioritize inputs received from the passenger-controlled IO node and the crew-controlled IO node to prevent conflicts between the inputs, the distributed architecture being characterized in that the command hierarchy prioritizes inputs received from the passenger-controlled IO node and the crew-controlled IO node based on an operation mode of the aircraft, said operation mode being determined via a data exchange with an avionic system of the aircraft.
A method for evaluating an effective component content (C) of a reducing agent for engine exhaust gas processing arranged in a container in which a heat transfer provision arrangement is provided, comprising the steps of: - determining (s410) a prevailing volume (V) of said reducing agent in said container ; - determining (s420) a prevailing temperature (T1) of said reducing agent; - determining (s430) a prevailing temperature (T2) of said heat transfer provision arrangement ; and - determining (s440) a prevailing temperature (T3) of a medium surrounding said container , characterized by the steps of: - for a predetermined time period, determining (s450) a mean temperature change rate (Tprim) for said reducing agent; and - determining (s460) said effective component content (C) of said reducing agent on the basis of said mean temperature change rate (Tprim), said prevailing volume (V) of said reducing agent, said prevailing temperature (T1) of said reducing agent, said prevailing temperature (T2) of said heat transfer provision arrangement and said prevailing temperature (T3) of said medium surrounding said container . - determining (s410) a prevailing volume (V) of said reducing agent in said container ; - determining (s420) a prevailing temperature (T1) of said reducing agent; - determining (s430) a prevailing temperature (T2) of said heat transfer provision arrangement ; and - determining (s440) a prevailing temperature (T3) of a medium surrounding said container , - for a predetermined time period, determining (s450) a mean temperature change rate (Tprim) for said reducing agent; and - determining (s460) said effective component content (C) of said reducing agent on the basis of said mean temperature change rate (Tprim), said prevailing volume (V) of said reducing agent, said prevailing temperature (T1) of said reducing agent, said prevailing temperature (T2) of said heat transfer provision arrangement and said prevailing temperature (T3) of said medium surrounding said container .
A wall mountable connector for securing a thermostat to a wall, the wall mountable connector comprising: a housing having a front side and a back side , the back side is configured to be mountable to a wall; the housing defining a field wire receiving cavity including a field wire aperture extending through the back side of the housing and into the field wire receiving cavity in order to receive one or more field wires; a connection block positioned alongside the field wire receiving cavity , the connection block configured to electrically connect to one or more field wires; a front side of the field wire receiving cavity is open to allow a user to gain access and electrically connect one or more field wires in the field wire receiving cavity to the connection block; characterized by a door movable between a closed position and an open position, wherein in the closed position, the door is situated along the front side of the field wire receiving cavity and covers the field wire receiving cavity. a housing having a front side and a back side , the back side is configured to be mountable to a wall; the housing defining a field wire receiving cavity including a field wire aperture extending through the back side of the housing and into the field wire receiving cavity in order to receive one or more field wires; a connection block positioned alongside the field wire receiving cavity , the connection block configured to electrically connect to one or more field wires; a front side of the field wire receiving cavity is open to allow a user to gain access and electrically connect one or more field wires in the field wire receiving cavity to the connection block; characterized by a door movable between a closed position and an open position, wherein in the closed position, the door is situated along the front side of the field wire receiving cavity and covers the field wire receiving cavity.
A method for processing a network failure, executed by a device which is applicable in a Bluetooth player, wherein the Bluetooth player is a playing device having a Bluetooth function and a network access function, the method comprises: establishing a failure identifier database, the failure identifier database being configured to store failure identifiers corresponding to various network failures; acquiring (110; 220) a failure identifier corresponding to the network failure, when detecting the network failure; and adding (120; 230) the failure identifier to a Bluetooth broadcast frame sent by the Bluetooth player, and sending the Bluetooth broadcast frame to a user terminal, such that the user terminal determines the network failure of the Bluetooth player according to the failure identifier in the Bluetooth broadcast frame and processes the network failure. establishing a failure identifier database, the failure identifier database being configured to store failure identifiers corresponding to various network failures; acquiring (110; 220) a failure identifier corresponding to the network failure, when detecting the network failure; and adding (120; 230) the failure identifier to a Bluetooth broadcast frame sent by the Bluetooth player, and sending the Bluetooth broadcast frame to a user terminal, such that the user terminal determines the network failure of the Bluetooth player according to the failure identifier in the Bluetooth broadcast frame and processes the network failure.
Locating system, in particular a hand-held locating device, comprising at least one hand-guided locating sensor (11a; 11b; 11c) provided for capturing locating data concerning objects to be located (13a; 13b; 13c) concealed below an examination surface (12a; 12b; 12c), comprising a position sensor (14a; 14b; 14c) provided for capturing position data assignable to the locating data, comprising an evaluation unit (15a; 15b; 15c) provided for determining at least two-dimensional map information from the locating data and the position data and for providing said at least two-dimensional map information, comprising at least one data source (25a; 25b; 25c) provided for providing data concerning a modification of the at least two-dimensional map information, wherein the data source (25a; 25b; 25c) has a buffer memory (18a; 18b; 18c) at least for the locating data, characterized in that the data source (25a; 25b; 25c) comprises an image recognition module (34a; 34b; 34c) provided for evaluating locating data of the locating sensor (11a; 11b; 11c) which are stored in the buffer memory and for extracting structural properties of the locating data, wherein the image recognition module (34a; 34b; 34c) provides the evaluation unit with the structural properties as geometric object data, wherein the evaluation unit is provided for superimposing the locating data on the geometric object data.
A pharmaceutical composition comprising (a) a nucleic acid active pharmaceutical ingredient (API); (b) a compound having the following Formula II: (c) a DSPE lipid comprising a polyethyleneglycol (PEG) region, a multibranched PEG region, a methoxypolyethyleneglycol (mPEG) region, a carbonyl-methoxypolyethyleneglycol region, or a polyglycerine region; (d) a sterol lipid; and (e) one or more neutral lipids. (a) a nucleic acid active pharmaceutical ingredient (API); (b) a compound having the following Formula II: (c) a DSPE lipid comprising a polyethyleneglycol (PEG) region, a multibranched PEG region, a methoxypolyethyleneglycol (mPEG) region, a carbonyl-methoxypolyethyleneglycol region, or a polyglycerine region; (d) a sterol lipid; and (e) one or more neutral lipids.
A defect inspection device, comprising: a flying body capable of freely moving in the space; an inspection means for inspecting a wall of an inspection target area of an inspection structure provided on the flying body ; an arm means to which the inspection means is attached at one end; and a first directing means having a rotation shaft for controlling a direction of the inspection means by rotating the arm means ; an imaging means which is provided on the flying body and captures images of the inspection target area of the inspection structure; and a second directing means for controlling a direction of capturing images performed by the imaging means , by rotating the imaging means , wherein the first directing means is mounted on the flying body so as to be biased away in any direction from a horizontal center or center of gravity of the flying body , wherein the second directing means is mounted on the flying body so as to be biased away in the direction opposite to the direction in which the first directing means is mounted, wherein a first balance adjustment means is provided for adjusting a mass balance so that the flying body is balanced at the center position or the center of gravity position, wherein the rotation shaft is arranged at the position of a center of gravity of an object, wherein said object comprises the inspection means , the arm means , and a second balance adjustment means . a flying body capable of freely moving in the space; an inspection means for inspecting a wall of an inspection target area of an inspection structure provided on the flying body ; an arm means to which the inspection means is attached at one end; and a first directing means having a rotation shaft for controlling a direction of the inspection means by rotating the arm means ; an imaging means which is provided on the flying body and captures images of the inspection target area of the inspection structure; and a second directing means for controlling a direction of capturing images performed by the imaging means , by rotating the imaging means , wherein the first directing means is mounted on the flying body so as to be biased away in any direction from a horizontal center or center of gravity of the flying body , wherein the second directing means is mounted on the flying body so as to be biased away in the direction opposite to the direction in which the first directing means is mounted, wherein a first balance adjustment means is provided for adjusting a mass balance so that the flying body is balanced at the center position or the center of gravity position, wherein the rotation shaft is arranged at the position of a center of gravity of an object, wherein said object comprises the inspection means , the arm means , and a second balance adjustment means .
A method of wireless communication, comprising: communicating , by a first wireless communication device with a second wireless communication device, a first configuration indicating a plurality of bandwidth parts in a frequency band , the frequency band including at least a first set of resource blocks interlaced with a second set of resource blocks across the plurality of bandwidth parts, wherein the first set of resource block and the second set of resource blocks for the plurality of bandwidth parts are defined in respect to a common resource block, and wherein the first configuration further indicates the lowest-frequency subcarrier of the lowest indexed resource block of the plurality of resource blocks with respect to a frequency location; and communicating , by the first wireless communication device with the second wireless communication device, a first communication signal using at least a portion of the first set of resource blocks within a first bandwidth part of the plurality of bandwidth parts based on a first listen-before-talk, LBT, result. communicating , by a first wireless communication device with a second wireless communication device, a first configuration indicating a plurality of bandwidth parts in a frequency band , the frequency band including at least a first set of resource blocks interlaced with a second set of resource blocks across the plurality of bandwidth parts, wherein the first set of resource block and the second set of resource blocks for the plurality of bandwidth parts are defined in respect to a common resource block, and wherein the first configuration further indicates the lowest-frequency subcarrier of the lowest indexed resource block of the plurality of resource blocks with respect to a frequency location; and communicating , by the first wireless communication device with the second wireless communication device, a first communication signal using at least a portion of the first set of resource blocks within a first bandwidth part of the plurality of bandwidth parts based on a first listen-before-talk, LBT, result.
Internal combustion engine comprising: - a combustion chamber, - a fresh air intake line that opens into the combustion chamber, - an exhaust line for exhausting burnt gases from the combustion chamber, which comprises at least one catalyst and means for heating the gases that are situated on a first side of the catalyst , - a vacuum pump that has an inlet and that is designed to establish, in said inlet , an air pressure below atmospheric pressure, characterized in that it has: - a preheating line that communicates at a first end with said inlet of the vacuum pump , which opens at a second end into the exhaust line , on a second side of the catalyst , and that has an air reserve and means for isolating the air reserve that are able to open or close the preheating line on either side of the air reserve , and - an air intake line that, at one end, communicates with the outside, and, at another end, opens into the exhaust line , on the side opposite the catalyst with respect to the heating means . - a combustion chamber, - a fresh air intake line that opens into the combustion chamber, - an exhaust line for exhausting burnt gases from the combustion chamber, which comprises at least one catalyst and means for heating the gases that are situated on a first side of the catalyst , - a vacuum pump that has an inlet and that is designed to establish, in said inlet , an air pressure below atmospheric pressure, characterized in that it has: - a preheating line that communicates at a first end with said inlet of the vacuum pump , which opens at a second end into the exhaust line , on a second side of the catalyst , and that has an air reserve and means for isolating the air reserve that are able to open or close the preheating line on either side of the air reserve , and - an air intake line that, at one end, communicates with the outside, and, at another end, opens into the exhaust line , on the side opposite the catalyst with respect to the heating means .
A method for receiving a demodulation reference signal, DMRS, based-downlink data channel by a user equipment , UE, in a long term evolution, LTE, communication system, the method comprising: receiving, from a network, a downlink control channel; and receiving the DMRS based-downlink data channel from the network based on the downlink control channel, wherein, when the downlink control channel includes a downlink control information, DCI, format 2D or the downlink control channel includes a DCI format 1A, antenna ports for the DMRS are not assumed to be quasi co-located with antenna ports for a channel status information-reference signal, CSI-RS, unless: when the downlink control channel includes the DCI format 2D, the antenna ports for the DMRS can be assumed to be quasi co-located with the antenna ports for the CSI-RS, and quasi co-location between DMRS and CSI-RS information is indicated by radio resource control, RRC, signalling; and when the downlink control channel includes the DCI format 1A, antenna port 7 for DMRS can be assumed to be quasi co-located with specific antenna ports for the CSI-RS, and the quasi co-location between DMRS and CSI-RS information is indicated by the RRC signalling. receiving, from a network, a downlink control channel; and receiving the DMRS based-downlink data channel from the network based on the downlink control channel, wherein, when the downlink control channel includes a downlink control information, DCI, format 2D or the downlink control channel includes a DCI format 1A, antenna ports for the DMRS are not assumed to be quasi co-located with antenna ports for a channel status information-reference signal, CSI-RS, unless: when the downlink control channel includes the DCI format 2D, the antenna ports for the DMRS can be assumed to be quasi co-located with the antenna ports for the CSI-RS, and quasi co-location between DMRS and CSI-RS information is indicated by radio resource control, RRC, signalling; and when the downlink control channel includes the DCI format 1A, antenna port 7 for DMRS can be assumed to be quasi co-located with specific antenna ports for the CSI-RS, and the quasi co-location between DMRS and CSI-RS information is indicated by the RRC signalling. when the downlink control channel includes the DCI format 2D, the antenna ports for the DMRS can be assumed to be quasi co-located with the antenna ports for the CSI-RS, and quasi co-location between DMRS and CSI-RS information is indicated by radio resource control, RRC, signalling; and when the downlink control channel includes the DCI format 1A, antenna port 7 for DMRS can be assumed to be quasi co-located with specific antenna ports for the CSI-RS, and the quasi co-location between DMRS and CSI-RS information is indicated by the RRC signalling.
A set for filtering an air flow (I) for a motor vehicle comprising a filter box into which an air inlet opens, a filter box cover between which a filter element is interposed, the filter set comprising an element for splitting the airflow circulating in the filter box , the element comprising (i) an external shell having a geometry adapted to form a cyclonic air flow (II), and (ii) acoustic attenuation means comprising at least one chamber defining a resonance volume inside the element , characterized in that the element is disposed upstream of the filter element and in that the external shell has a substantially Gaussian geometry.