mhurhangee/ep-ind-claims huggingface dataset:
A method for verifying the speed of a vehicle A among a number of vehicles adapted to communicate with one another by V2V (vehicle-to-vehicle) communication or to communicate between vehicle and infrastructure by V2I (vehicle-to-infrastructure) communication, which method comprises - monitoring vehicle A's speed and generating a speed signal V A which presents the vehicle's speed; - generating a reference signal S ref which contains information about a speed V B of at least one other vehicle B; - determining a location P A for vehicle A; - determining a location P B for vehicle B; - determining a location difference between the location P A for vehicle A and the location P B for vehicle B over a period of time t; - comparing the location difference with a predetermined threshold value Tp over the period of time t and determining if the location difference has not changed more than the predetermined threshold value Tp over the period of time t; - generating a location verification signal S p which represents said comparison over the period of time t; - verifying vehicle A's speed based on said speed signal V A, reference signal S ref and location verification signal S p; - generating a verification signal S v on the basis of said verifying. - monitoring vehicle A's speed and generating a speed signal V A which presents the vehicle's speed; - generating a reference signal S ref which contains information about a speed V B of at least one other vehicle B; - determining a location P A for vehicle A; - determining a location P B for vehicle B; - determining a location difference between the location P A for vehicle A and the location P B for vehicle B over a period of time t; - comparing the location difference with a predetermined threshold value Tp over the period of time t and determining if the location difference has not changed more than the predetermined threshold value Tp over the period of time t; - generating a location verification signal S p which represents said comparison over the period of time t; - verifying vehicle A's speed based on said speed signal V A, reference signal S ref and location verification signal S p; - generating a verification signal S v on the basis of said verifying.
An aircraft comprising a hybrid propulsion system comprising; an inboard gas turbine engine (10a, 10c) and an outboard gas turbine engine (10b, 10d), each gas turbine engine comprising a propulsor (12a, 12b) and an electric machine (32a, 32b) coupled to one or more engine shaft (24a, 24b); an electrical interconnection between the electric machine of the inboard gas turbine engine and the electric machine of the outboard gas turbine engine; and a controller configured to transfer electrical power between the inboard gas turbine engine electrical machine and the outboard gas turbine engine electrical machine when a thrust setting change is selected; the controller is configured to transfer electrical power from the electric machine of the inboard gas turbine engine acting as a generator to the electric machine of the outboard gas turbine engine acting as a motor; and characterised in that: the controller is configured to transfer electric power from the electric machine of the inboard gas turbine engine to the electric machine of the outboard gas turbine engine when one or more of the following conditions are met: the aircraft is at an altitude greater than a predetermined minimum; the current engine thrust is between a predetermined minimum and a predetermined maximum; and an increased or reduced thrust setting is selected. an inboard gas turbine engine (10a, 10c) and an outboard gas turbine engine (10b, 10d), each gas turbine engine comprising a propulsor (12a, 12b) and an electric machine (32a, 32b) coupled to one or more engine shaft (24a, 24b); an electrical interconnection between the electric machine of the inboard gas turbine engine and the electric machine of the outboard gas turbine engine; and a controller configured to transfer electrical power between the inboard gas turbine engine electrical machine and the outboard gas turbine engine electrical machine when a thrust setting change is selected; the controller is configured to transfer electrical power from the electric machine of the inboard gas turbine engine acting as a generator to the electric machine of the outboard gas turbine engine acting as a motor; and characterised in that: the controller is configured to transfer electric power from the electric machine of the inboard gas turbine engine to the electric machine of the outboard gas turbine engine when one or more of the following conditions are met: the aircraft is at an altitude greater than a predetermined minimum; the current engine thrust is between a predetermined minimum and a predetermined maximum; and an increased or reduced thrust setting is selected. the aircraft is at an altitude greater than a predetermined minimum; the current engine thrust is between a predetermined minimum and a predetermined maximum; and an increased or reduced thrust setting is selected.
A hydrogen purity monitor comprising: a first fuel cell configured to generate electrical current from the electrochemical reaction of hydrogen and oxidant, having a first fuel inlet configured to receive hydrogen from a first hydrogen source (16, 27); a second fuel cell configured to generate electrical current from the electrochemical reaction of hydrogen and oxidant, having a second fuel inlet configured to receive hydrogen from a second hydrogen source; a control system configured to apply an electrical load to each fuel cell and determine an electrical output of each fuel cell, the control system including a comparator for comparing the electrical outputs of the first and second fuel cells; and a purity monitor output configured to give an indication of hydrogen purity based on an output of the comparator. a first fuel cell configured to generate electrical current from the electrochemical reaction of hydrogen and oxidant, having a first fuel inlet configured to receive hydrogen from a first hydrogen source (16, 27); a second fuel cell configured to generate electrical current from the electrochemical reaction of hydrogen and oxidant, having a second fuel inlet configured to receive hydrogen from a second hydrogen source; a control system configured to apply an electrical load to each fuel cell and determine an electrical output of each fuel cell, the control system including a comparator for comparing the electrical outputs of the first and second fuel cells; and a purity monitor output configured to give an indication of hydrogen purity based on an output of the comparator.
A method for controlling a menu on a mobile communications device (100, 101, 200) having a display with an idle mode background image (400, 500, 600, 700), comprising receiving a first user input from an input control device (202, 350), relating said user input to an area of said idle mode background image (402, 404, 406, 502, 504, 506, 602, 604, 606, 702, 704, 706), determining an application which is linked to said area of said idle mode background image, superposing an application icon (410, 614, 714) associated with said linked application corresponding to said area of said idle mode background image related to said first user input over at least a part of said idle mode background image, and in response to a second user input comprising a selection of said area, executing said linked application.
An injectable insulin formulation comprising an effective amount of a dissolution/stabilizing agent selected from acetic acid, ascorbic acid, citric acid, glutamic acid, aspartic acid, succinic acid, fumaric acid, maleic acid, adipic acid, and salts thereof; an effective amount of a zinc chelator; and one or more magnesium compounds, wherein the insulin concentration is 100, 200, 400 or 500 UmL, wherein the one or more magnesium compounds comprises an inorganic magnesium salt, and wherein the concentration of the one or more magnesium compounds is 0.1 to 10 mg/ml.
A method for optimizing operation of a wind farm, the method comprising: monitoring, via one or more sensors, one or more wake parameters for wind turbines in the wind farm; developing a farm-level wake model for the interacting wind turbines based at least partially on the monitored wake parameters; and controlling the interacting wind turbines based on the farm-level wake model; characterized in that the method further comprises identifying at least two interacting wind turbines from the wind turbines based on the monitored wake parameters; and determining a wake offset angle between the interacting wind turbines as a function of at least an average wind direction and a wake meandering component, the wake meandering component corresponding to a shift in a wave track due to lateral components of wind speed; wherein developing the farm-level wake model comprises developing a farm-level wake model for the interacting wind turbines based at least partially on the monitored wake parameters and the wake offset angle. monitoring, via one or more sensors, one or more wake parameters for wind turbines in the wind farm; developing a farm-level wake model for the interacting wind turbines based at least partially on the monitored wake parameters; and controlling the interacting wind turbines based on the farm-level wake model; characterized in that the method further comprises identifying at least two interacting wind turbines from the wind turbines based on the monitored wake parameters; and determining a wake offset angle between the interacting wind turbines as a function of at least an average wind direction and a wake meandering component, the wake meandering component corresponding to a shift in a wave track due to lateral components of wind speed; wherein developing the farm-level wake model comprises developing a farm-level wake model for the interacting wind turbines based at least partially on the monitored wake parameters and the wake offset angle.
An endoscopic surgical device configured to fire a surgical anchor into target tissue, the surgical device comprising; a handle assembly including: a handle housing; a trigger operatively connected to the handle housing, the trigger including at least a fully un-actuated position; and a drive mechanism actuatable by the trigger; and an endoscopic assembly including: a proximal end portion extending from the handle assembly; a distal end portion configured to support an end effector; and a rotatable inner actuation shaft extending from the handle assembly and into the distal end portion of the endoscopic assembly, the inner actuation shaft being connected to the drive mechanism of the handle assembly such that an actuation of the trigger results in a rotation of the inner actuation shaft to fire a surgical anchor of the surgical device, characterized in that said surgical device further comprises a timing system associating the trigger with the drive mechanism, wherein the timing system includes: a raceway formed in a surface of the trigger, the raceway defining a plurality of steps along a length thereof; and a deflectable arm having a distal first end disposed within the raceway and operatively associated with the steps thereof, and a second end connected to the handle housing, wherein the distal end of the deflectable arm rides through the raceway when the trigger is actuated to maintain a timing of an actuation stroke of the trigger with an actuation of the drive mechanism to fire a single surgical anchor upon a single stroke of the trigger from the fully un-actuated position, to a fully actuated position, to the fully un-actuated position. a handle housing; a trigger operatively connected to the handle housing, the trigger including at least a fully un-actuated position; and a drive mechanism actuatable by the trigger; and a proximal end portion extending from the handle assembly; a distal end portion configured to support an end effector; and a rotatable inner actuation shaft extending from the handle assembly and into the distal end portion of the endoscopic assembly, the inner actuation shaft being connected to the drive mechanism of the handle assembly such that an actuation of the trigger results in a rotation of the inner actuation shaft to fire a surgical anchor of the surgical device, a raceway formed in a surface of the trigger, the raceway defining a plurality of steps along a length thereof; and a deflectable arm having a distal first end disposed within the raceway and operatively associated with the steps thereof, and a second end connected to the handle housing, wherein the distal end of the deflectable arm rides through the raceway when the trigger is actuated to maintain a timing of an actuation stroke of the trigger with an actuation of the drive mechanism to fire a single surgical anchor upon a single stroke of the trigger from the fully un-actuated position, to a fully actuated position, to the fully un-actuated position.
A drug eluting stent comprising: - a stent framework; - an electro-grafted coating of poly-butyl methacrylate disposed on the stent framework, wherein the coating promotes proliferation and adhesion of the endothelial cells to ensure the full recolonization of the stent by endothelial cells; - a drug hosting biodegradable polymer coating disposed on the electro-grafted coating. - a stent framework; - an electro-grafted coating of poly-butyl methacrylate disposed on the stent framework, wherein the coating promotes proliferation and adhesion of the endothelial cells to ensure the full recolonization of the stent by endothelial cells; - a drug hosting biodegradable polymer coating disposed on the electro-grafted coating.
A method for producing a sole plate, comprising the following steps: a. providing a mixture of a polymer melt and of a foaming agent, b. injecting the mixture into a mold; and c. solidifying at least a first portion of the sole plate without foaming and at least a second portion of the sole plate after foaming inside the mold, d. wherein the mixture comprises a polymer having an average molecular mass corresponding to a viscosity number ≥ 130 ml/g, preferably ≥ 170 ml/g, more preferably ≥ 190 ml/g and most preferably ≥225 ml/g, wherein the viscosity number is determined via solution viscometry according to the ISO 307 standard; e. wherein the mold (110, 210) comprises at least a first and a second cavity, wherein foaming inside the second cavity is induced by increasing the volume of the second cavity such that the mixture (120, 220) solidifies inside the first cavity essentially without foaming while the mixture (120, 220) at least partially undergoes foaming inside the second cavity. a. providing a mixture of a polymer melt and of a foaming agent, b. injecting the mixture into a mold; and c. solidifying at least a first portion of the sole plate without foaming and at least a second portion of the sole plate after foaming inside the mold, d. wherein the mixture comprises a polymer having an average molecular mass corresponding to a viscosity number ≥ 130 ml/g, preferably ≥ 170 ml/g, more preferably ≥ 190 ml/g and most preferably ≥225 ml/g, wherein the viscosity number is determined via solution viscometry according to the ISO 307 standard; e. wherein the mold (110, 210) comprises at least a first and a second cavity, wherein foaming inside the second cavity is induced by increasing the volume of the second cavity such that the mixture (120, 220) solidifies inside the first cavity essentially without foaming while the mixture (120, 220) at least partially undergoes foaming inside the second cavity.
A method enabling continuous estimation of air-fuel ratio in an internal combustion engine's cylinder, said engine comprising a plurality of cylinders, at least one richness measurement sensor, a plurality of injectors connected to the cylinders, a flow meter, said method including the steps consisting of: • measuring a richness signal by means of the richness sensor. • calculating a simple richness model (Φ_Calc) corresponding to the quotient of the flow of injected fuel (qlnj) on the flow of intake air (Qair), multiplied by the stoichiometric ratio (γ), characterized in that said method further includes the steps consisting of: • identifying and quantifying the possible dispersions and deviations of richness on stabilised points of operation by means of at least one deviation identifier from the signal constituting the richness model (Φ_Calc) and from the measured richness signal carried at the input of this deviation identifier, a mapping of the richness deviations in the engine field being realized by the deviation identifier, by teach-in of these possible deviations; • identifying and quantifying the possible transient dispersions and richness deviations by means of at least one supplementary deviation identifier consisting of a Kalman filter from the measured richness signal and from the model richness signal of the sensor, • correcting continuously the calculated richness (Φ_Calc) by using the deviation read in the mapping for directly correcting the model richness input signal of the Kalman filter or by using the deviation read in the mapping for the a priori status of the Kalman filter. • measuring a richness signal by means of the richness sensor. • calculating a simple richness model (Φ_Calc) corresponding to the quotient of the flow of injected fuel (qlnj) on the flow of intake air (Qair), multiplied by the stoichiometric ratio (γ), • identifying and quantifying the possible dispersions and deviations of richness on stabilised points of operation by means of at least one deviation identifier from the signal constituting the richness model (Φ_Calc) and from the measured richness signal carried at the input of this deviation identifier, a mapping of the richness deviations in the engine field being realized by the deviation identifier, by teach-in of these possible deviations; • identifying and quantifying the possible transient dispersions and richness deviations by means of at least one supplementary deviation identifier consisting of a Kalman filter from the measured richness signal and from the model richness signal of the sensor, • correcting continuously the calculated richness (Φ_Calc) by using the deviation read in the mapping for directly correcting the model richness input signal of the Kalman filter or by using the deviation read in the mapping for the a priori status of the Kalman filter.
A heat exchanger, comprising: a first header and a second header, flat tubes each divided into a first straight segment connected to the first header, a second straight segment connected to the second header and a twisted segment connected between the first straight segment and the second straight segment, along a length direction of the flat tube; and fins disposed between adjacent first straight segments and between adjacent second straight segments, wherein the flat tube is bent at the twisted segment around a first bending axis to provide a first bending portion, and the first bending axis is parallel to axial directions of the first header and the second header, characterised in that the first header and the second header are bent around at least one second bending axis to provide at least one second bending portion, the first header is located at an outer bending side of the second bending portion and the second header is located at an inner bending side of the second bending portion, and the second bending axis is orthogonal to the axial directions of the first header and the second header and parallel to length directions of the first straight segment and the second straight segment and a length of the second header being less than a length of the first header. a first header and a second header, flat tubes each divided into a first straight segment connected to the first header, a second straight segment connected to the second header and a twisted segment connected between the first straight segment and the second straight segment, along a length direction of the flat tube; and fins disposed between adjacent first straight segments and between adjacent second straight segments, wherein the flat tube is bent at the twisted segment around a first bending axis to provide a first bending portion, and the first bending axis is parallel to axial directions of the first header and the second header, characterised in that the first header and the second header are bent around at least one second bending axis to provide at least one second bending portion, the first header is located at an outer bending side of the second bending portion and the second header is located at an inner bending side of the second bending portion, and the second bending axis is orthogonal to the axial directions of the first header and the second header and parallel to length directions of the first straight segment and the second straight segment and a length of the second header being less than a length of the first header.
An electronic device comprising: an enclosure formed of a plurality of layers cooperating to define an interior cavity, comprising: a first layer, formed of a first material and defining: a user input surface of the enclosure; and a first portion of a continuous side surface of the enclosure; a second layer, positioned below the first layer, the second layer comprising a circuit board, the circuit board: formed of a second material different from the first material; and defining a second portion of the continuous side surface of the enclosure; and a third layer, formed of a third material different from the first and second materials, positioned below the second layer and defining: a bottom surface of the enclosure; and a third portion of the continuous side surface of the enclosure; a battery positioned in the interior cavity of the enclosure and operably coupled to the circuit board; and a camera positioned at least partially in the interior cavity and operably coupled to the circuit board. an enclosure formed of a plurality of layers cooperating to define an interior cavity, comprising: a first layer, formed of a first material and defining: a user input surface of the enclosure; and a first portion of a continuous side surface of the enclosure; a second layer, positioned below the first layer, the second layer comprising a circuit board, the circuit board: formed of a second material different from the first material; and defining a second portion of the continuous side surface of the enclosure; and a third layer, formed of a third material different from the first and second materials, positioned below the second layer and defining: a bottom surface of the enclosure; and a third portion of the continuous side surface of the enclosure; a first layer, formed of a first material and defining: a user input surface of the enclosure; and a first portion of a continuous side surface of the enclosure; a user input surface of the enclosure; and a first portion of a continuous side surface of the enclosure; a second layer, positioned below the first layer, the second layer comprising a circuit board, the circuit board: formed of a second material different from the first material; and defining a second portion of the continuous side surface of the enclosure; and formed of a second material different from the first material; and defining a second portion of the continuous side surface of the enclosure; and a third layer, formed of a third material different from the first and second materials, positioned below the second layer and defining: a bottom surface of the enclosure; and a third portion of the continuous side surface of the enclosure; a battery positioned in the interior cavity of the enclosure and operably coupled to the circuit board; and a camera positioned at least partially in the interior cavity and operably coupled to the circuit board.