mhurhangee/patent-ind-claim-en huggingface dataset:
A method for producing an adeno-associated virus (AAV) particle comprising an oversized recombinant AAV (rAAV) genome, the method comprising a) culturing an AAV producer cell line under conditions to generate rAAV particles, wherein the AAV producer cell line comprises i) nucleic acid encoding AAV rep and cap genes, and ii) an oversized rAAV genome, wherein the oversized rAAV genome is between 5.4 kb and 6.7 kb or 5.4 kb and 6 kb; b) providing AAV helper functions, optionally wherein the AAV helper functions are provided by adenovirus, HSV, or baculovirus; and c) collecting the rAAV particles comprising oversized rAAV genomes, optionally between 48 hours and 96 hours after the provision of helper functions, and wherein the nucleic acid encoding AAV rep and cap genes and the oversized rAAV genome are stably integrated into the genome of the producer cell line. a) culturing an AAV producer cell line under conditions to generate rAAV particles, wherein the AAV producer cell line comprises i) nucleic acid encoding AAV rep and cap genes, and ii) an oversized rAAV genome, wherein the oversized rAAV genome is between 5.4 kb and 6.7 kb or 5.4 kb and 6 kb; i) nucleic acid encoding AAV rep and cap genes, and ii) an oversized rAAV genome, wherein the oversized rAAV genome is between 5.4 kb and 6.7 kb or 5.4 kb and 6 kb; b) providing AAV helper functions, optionally wherein the AAV helper functions are provided by adenovirus, HSV, or baculovirus; and c) collecting the rAAV particles comprising oversized rAAV genomes, optionally between 48 hours and 96 hours after the provision of helper functions, and
A heat exchanger comprising: a plurality of flat tubes that each have a cross-sectional shape perpendicular to a direction of flow of refrigerant with a width direction that extends in an air flow direction; and a plurality of heat transfer fins each having a plurality of notches configured to receive the plurality of flat tubes, the plurality of notches being along the width direction of the plurality of flat tubes, the plurality of heat transfer fins including at least three standing portions provided on a peripheral portion of each of the plurality of notches for forming gaps between adjacent heat transfer fins, and the at least three standing portions being arranged so as not to face each other across a reference line that extends in the width direction through a perpendicular center portion of the flat tube; wherein each of the plurality of heat transfer fins includes, in the notch, a plurality of the standing portions on each of two long sides that face each other across the reference line; characterized in that in each of the plurality of heat transfer fins, when viewed from an air flow direction, a height at which intervals between the standing portions disposed on one of the long sides of the notch and the standing portions disposed on the other of the long sides of the notch is at a minimum is less than half of a height of the standing portion. a plurality of flat tubes that each have a cross-sectional shape perpendicular to a direction of flow of refrigerant with a width direction that extends in an air flow direction; and a plurality of heat transfer fins each having a plurality of notches configured to receive the plurality of flat tubes, the plurality of notches being along the width direction of the plurality of flat tubes, the plurality of heat transfer fins including at least three standing portions provided on a peripheral portion of each of the plurality of notches for forming gaps between adjacent heat transfer fins, and the at least three standing portions being arranged so as not to face each other across a reference line that extends in the width direction through a perpendicular center portion of the flat tube; wherein each of the plurality of heat transfer fins includes, in the notch, a plurality of the standing portions on each of two long sides that face each other across the reference line; characterized in that in each of the plurality of heat transfer fins, when viewed from an air flow direction, a height at which intervals between the standing portions disposed on one of the long sides of the notch and the standing portions disposed on the other of the long sides of the notch is at a minimum is less than half of a height of the standing portion.
A computer-implemented method for deploying an application in a computer network comprising: determining information about a reliability of a predetermined first deployment for the application; determining information about a reliability of a predetermined second deployment for the application; comparing the information about the reliability of the first deployment with the information about the reliability of the second deployment; selecting the first deployment or the second deployment for deploying the application in the computer network depending on the result of the comparison, characterized in that the information about the reliability of the respective predetermined deployment is determined by : generating respective failure states for a plurality of components for deploying the application according to the respective predetermined deployment; determining information about a reachability of the plurality of components depending on the generated failure states; and determining the information about the reliability of the respective predetermined deployment depending on the information about the reachability. determining information about a reliability of a predetermined first deployment for the application; determining information about a reliability of a predetermined second deployment for the application; comparing the information about the reliability of the first deployment with the information about the reliability of the second deployment; selecting the first deployment or the second deployment for deploying the application in the computer network depending on the result of the comparison, characterized in that the information about the reliability of the respective predetermined deployment is determined by : generating respective failure states for a plurality of components for deploying the application according to the respective predetermined deployment; determining information about a reachability of the plurality of components depending on the generated failure states; and determining the information about the reliability of the respective predetermined deployment depending on the information about the reachability. generating respective failure states for a plurality of components for deploying the application according to the respective predetermined deployment; determining information about a reachability of the plurality of components depending on the generated failure states; and determining the information about the reliability of the respective predetermined deployment depending on the information about the reachability.
A method for determining a flow rate and a temperature of a fluid at a selected position in a district heating or cooling utility distribution network, the utility distribution network comprising a plurality of interconnected distribution lines and smart utility meters (M) arranged to register the energy delivered at consumer premisses situated along the distribution lines, the utility meters (M) are connected to a Head End System (HES) 104 using an Advanced Metering Infrastructure the method comprising the steps of: - collecting meter data time series (MD) from the smart utility meters (M) using the Advanced Metering Infrastructure, - calculating the temperature and the flow rate (QT_EST) at the selected position based on; - flow and temperature information derived from the collected meter data time series (MD), - topology of the utility distribution network, including lengths of the distribution lines, and - heat transfer coefficients of the distribution lines; characterized in that the meter data times series (MD) collected from the utility meters comprises at least: - an accumulated volume (V), and - an integrated flow-temperature product (ε) calculated by the meter, and in that the derived flow and temperature information include: - an average flow (Q_AVG) derived from the collected meter data time series (MD) as Q n = V n − V n − 1 Δt , and - a volume weighted temperature (T_VOL) derived from the collected meter data time series (MD) as T n = ε n − ε n − 1 V n − V n − 1 . - collecting meter data time series (MD) from the smart utility meters (M) using the Advanced Metering Infrastructure, - calculating the temperature and the flow rate (QT_EST) at the selected position based on; - flow and temperature information derived from the collected meter data time series (MD), - topology of the utility distribution network, including lengths of the distribution lines, and - heat transfer coefficients of the distribution lines; - flow and temperature information derived from the collected meter data time series (MD), - topology of the utility distribution network, including lengths of the distribution lines, and - heat transfer coefficients of the distribution lines; - an accumulated volume (V), and - an integrated flow-temperature product (ε) calculated by the meter, - an average flow (Q_AVG) derived from the collected meter data time series (MD) as Q n = V n − V n − 1 Δt , and - a volume weighted temperature (T_VOL) derived from the collected meter data time series (MD) as T n = ε n − ε n − 1 V n − V n − 1 .
A method for controlling motion of a legged robot executed by an electronic device , the legged robot comprising a plurality of foot ends , and the method comprising: determining (S501), according to state data of the legged robot at a start moment in a preset period, a candidate landing point of each foot end in the preset period; determining (S502), according to the state data at the start moment and the candidate landing point of each foot end, a first correlation between a center-of-mass position change parameter, a candidate landing point , and a foot end contact force; determining (S503), under constraint of a constraint condition set, a target center-of-mass position change parameter, a target step order, and a target landing point that satisfy the first correlation, the constraint condition set comprising a constraint condition used for constraining a step order; and controlling (S504), according to the target center-of-mass position change parameter, the target step order, and the target landing point, motion of the legged robot in the preset period. determining (S501), according to state data of the legged robot at a start moment in a preset period, a candidate landing point of each foot end in the preset period; determining (S502), according to the state data at the start moment and the candidate landing point of each foot end, a first correlation between a center-of-mass position change parameter, a candidate landing point , and a foot end contact force; determining (S503), under constraint of a constraint condition set, a target center-of-mass position change parameter, a target step order, and a target landing point that satisfy the first correlation, the constraint condition set comprising a constraint condition used for constraining a step order; and controlling (S504), according to the target center-of-mass position change parameter, the target step order, and the target landing point, motion of the legged robot in the preset period.
A distortion reducing system comprising: a display having a lens arranged to view an image; an image mapping module , in communication with an image input source , to map a received image onto one or more of a plurality of distortion meshes; a radial aberration compensation module , in communication with the image mapping module , to compensate for radial distortions within the received image using at least one of the one or more of the plurality of distortion meshes and output a radially corrected image; a chromatic aberration compensation module , in communication with the image mapping module , to compensate for chromatic distortions within the received image using at least one of the one or more of the plurality of distortion meshes and output a chromatically corrected image; and a blending module , in communication with the radial aberration compensation module and the chromatic aberration compensation module , to adaptively blend the radially corrected image and the chromatically corrected image rendered from the one or more of the plurality of distortion meshes into a composite corrected image to reduce distortions within the received image , and output the composite corrected image to be viewed via the display . a display having a lens arranged to view an image; an image mapping module , in communication with an image input source , to map a received image onto one or more of a plurality of distortion meshes; a radial aberration compensation module , in communication with the image mapping module , to compensate for radial distortions within the received image using at least one of the one or more of the plurality of distortion meshes and output a radially corrected image; a chromatic aberration compensation module , in communication with the image mapping module , to compensate for chromatic distortions within the received image using at least one of the one or more of the plurality of distortion meshes and output a chromatically corrected image; and a blending module , in communication with the radial aberration compensation module and the chromatic aberration compensation module , to adaptively blend the radially corrected image and the chromatically corrected image rendered from the one or more of the plurality of distortion meshes into a composite corrected image to reduce distortions within the received image , and output the composite corrected image to be viewed via the display .
Tool turret, in particular intended for use with a machine tool, having a pivotable tool disc , which has on its outer circumference a plurality of receptacles for holders provided with machining tools, said holders being attached to the tool disc in an exchangeable manner by means of a fixing device and, each swivelled into a working position, permit the assigned machining tool to be driven by means of a drive , which for this purpose can be coupled to a driven shaft of the respective holder by means of a coupling device , characterised in that the clamping device can be actuated by means of this drive when said drive is disengaged while the machining tool is stopped, and in that the clamping device has a pawl arrangement with control pawls and latching pawls which are assigned to each other in pairs and can be actuated by an actuating device in such a manner that, in their latched position, they connect a holder to the tool disc and, in their released position, release this holder .
An indoor unit of a wall-mounted air conditioner, characterized by comprising: a housing, comprising: a chassis defining an air duct having an air outlet; a face frame ; and an installation plate disposed at one end of the air outlet extending in an up-down direction of the air outlet, wherein the one end of the air outlet is along a length direction of the air outlet; a motor assembly disposed at a side of the installation plate opposite to the air outlet; a first extending plate disposed on the chassis , extended along the air outlet and disposed above the motor assembly , wherein the first extending plate , the installation plate, and the face frame define an accommodating space comprising an opening opposite to the installation plate; and a rats-proof plate disposed on an inner surface of the face frame and extending rearwardly, wherein the rats-proof plate is configured to cover at least a part of the opening , and wherein the motor assembly is disposed between the rats-proof plate and the air outlet. a housing, comprising: a chassis defining an air duct having an air outlet; a face frame ; and an installation plate disposed at one end of the air outlet extending in an up-down direction of the air outlet, wherein the one end of the air outlet is along a length direction of the air outlet; a chassis defining an air duct having an air outlet; a face frame ; and an installation plate disposed at one end of the air outlet extending in an up-down direction of the air outlet, wherein the one end of the air outlet is along a length direction of the air outlet; a motor assembly disposed at a side of the installation plate opposite to the air outlet; a first extending plate disposed on the chassis , extended along the air outlet and disposed above the motor assembly , wherein the first extending plate , the installation plate, and the face frame define an accommodating space comprising an opening opposite to the installation plate; and a rats-proof plate disposed on an inner surface of the face frame and extending rearwardly, wherein the rats-proof plate is configured to cover at least a part of the opening , and wherein the motor assembly is disposed between the rats-proof plate and the air outlet. wherein the rats-proof plate is configured to cover at least a part of the opening , and wherein the motor assembly is disposed between the rats-proof plate and the air outlet.
A gas turbine engine , comprising: a fan section including a fan nacelle arranged at least partially about a fan ; an aft nacelle (68B;68C) moveable relative to the fan nacelle ; a core engine including a compressor section and a turbine section arranged within a core cowling , the turbine section configured to drive the fan , the fan nacelle and the aft nacelle (68B;68C) arranged at least partially about the core cowling to define a bypass flow path ; a thrust reverser configured to selectively communicate a portion of fan bypass airflow (B) from the bypass flow path when in a thrust reversal mode; and a controller in communication with the core engine and the thrust reverser , wherein the controller is configured to: receive position information of the thrust reverser and engine power information of the core engine ; cause the core engine to deny an engine power request during the thrust reversal mode when at least one criterion is met; and respond to the engine power request when the at least one predetermined criterion is not met, wherein the at least one criterion is a predetermined criterion and includes an engine reverse power threshold and a predefined time limit relating to the engine reverse power threshold. a fan section including a fan nacelle arranged at least partially about a fan ; an aft nacelle (68B;68C) moveable relative to the fan nacelle ; a core engine including a compressor section and a turbine section arranged within a core cowling , the turbine section configured to drive the fan , the fan nacelle and the aft nacelle (68B;68C) arranged at least partially about the core cowling to define a bypass flow path ; a thrust reverser configured to selectively communicate a portion of fan bypass airflow (B) from the bypass flow path when in a thrust reversal mode; and a controller in communication with the core engine and the thrust reverser , wherein the controller is configured to: receive position information of the thrust reverser and engine power information of the core engine ; cause the core engine to deny an engine power request during the thrust reversal mode when at least one criterion is met; and respond to the engine power request when the at least one predetermined criterion is not met, wherein the at least one criterion is a predetermined criterion and includes an engine reverse power threshold and a predefined time limit relating to the engine reverse power threshold. receive position information of the thrust reverser and engine power information of the core engine ; cause the core engine to deny an engine power request during the thrust reversal mode when at least one criterion is met; and respond to the engine power request when the at least one predetermined criterion is not met, wherein the at least one criterion is a predetermined criterion and includes an engine reverse power threshold and a predefined time limit relating to the engine reverse power threshold.
A cutting tool comprising: a first lever having a first end and a second end , wherein the first lever defines a first handle portion towards the first end of the first lever ; a second lever having a first end and a second end , wherein the second lever defines a second handle portion towards the first end of the second lever , and wherein the second lever is pivotally coupled to the first lever at a pivot point ; a first cutting edge defined by the first lever between the pivot point and the second end of the first lever ; a support surface defined by the second lever between the pivot point and the second end of the second lever such that the first cutting edge and the support surface are adapted to perform a first cutting action therebetween; an element rotatably coupled with one or more of the first lever and the second lever such that the element removably rests on the support surface of the second lever ; and characterized in that: the first cutting edge and the element are adapted to perform a second cutting action therebetween when the element rests on the support surface of the second lever ; and wherein the second cutting action is a cutting action similar to one performed by the bypass secateurs, where one cutting blade bypasses the adjacent part on the other lever during the cutting action. a first lever having a first end and a second end , wherein the first lever defines a first handle portion towards the first end of the first lever ; a second lever having a first end and a second end , wherein the second lever defines a second handle portion towards the first end of the second lever , and wherein the second lever is pivotally coupled to the first lever at a pivot point ; a first cutting edge defined by the first lever between the pivot point and the second end of the first lever ; a support surface defined by the second lever between the pivot point and the second end of the second lever such that the first cutting edge and the support surface are adapted to perform a first cutting action therebetween; an element rotatably coupled with one or more of the first lever and the second lever such that the element removably rests on the support surface of the second lever ; and characterized in that: the first cutting edge and the element are adapted to perform a second cutting action therebetween when the element rests on the support surface of the second lever ; and wherein the second cutting action is a cutting action similar to one performed by the bypass secateurs, where one cutting blade bypasses the adjacent part on the other lever during the cutting action. the first cutting edge and the element are adapted to perform a second cutting action therebetween when the element rests on the support surface of the second lever ; and wherein the second cutting action is a cutting action similar to one performed by the bypass secateurs, where one cutting blade bypasses the adjacent part on the other lever during the cutting action.