mhurhangee/ep-ind-claims huggingface dataset:
A charging control method, comprising: controlling a first rectifier to rectify an input first alternating current AC to output a voltage with a first ripple waveform; outputting a control signal to a switch unit, such that the switch unit modulates the voltage with the first ripple waveform based on the control signal, and the modulated voltage is applied to a primary winding of a transformer to output a plurality of voltages with ripple waveforms via a plurality of secondary windings of the transformer; controlling a compositing unit to composite the plurality of voltages with ripple waveforms to output a second alternating current AC for charging a device to be charged, wherein for each cycle of the alternating current AC, an absolute value of a peak voltage of a positive half is greater than that of a trough voltage of a negative half; and adjusting a duty ratio of the control signal. controlling a first rectifier to rectify an input first alternating current AC to output a voltage with a first ripple waveform; outputting a control signal to a switch unit, such that the switch unit modulates the voltage with the first ripple waveform based on the control signal, and the modulated voltage is applied to a primary winding of a transformer to output a plurality of voltages with ripple waveforms via a plurality of secondary windings of the transformer; controlling a compositing unit to composite the plurality of voltages with ripple waveforms to output a second alternating current AC for charging a device to be charged, wherein for each cycle of the alternating current AC, an absolute value of a peak voltage of a positive half is greater than that of a trough voltage of a negative half; and adjusting a duty ratio of the control signal.
An apparatus for multi-core processing, the apparatus comprising: a memory controller; a first processor core of a first type to execute program code; a second processor core of a second type different from the first type; and a code distribution module to (i) determine, while the first processor core executes the program code, one or more performance metrics of the first processor core and one or more performance metrics of the second processor core indicative of execution of the program code by the second processor core and (ii) switch execution of the program code from the first processor core to the second processor core in response to a determination that the one or more performance metrics of the second processor core are better than the one or more performance metrics of the first processor core; wherein determining the performance metrics of the second processing core comprises executing a plurality of pieces of code on both the first processing core and the second processing core, collecting the respective performance information and statistics of the first and second processing cores while executing the pieces of code, and determining a best fit function F such that differences between F, performace information and statistics of the first processing core, and the performance of the second processing core are minimized. a memory controller; a first processor core of a first type to execute program code; a second processor core of a second type different from the first type; and a code distribution module to (i) determine, while the first processor core executes the program code, one or more performance metrics of the first processor core and one or more performance metrics of the second processor core indicative of execution of the program code by the second processor core and (ii) switch execution of the program code from the first processor core to the second processor core in response to a determination that the one or more performance metrics of the second processor core are better than the one or more performance metrics of the first processor core; wherein determining the performance metrics of the second processing core comprises executing a plurality of pieces of code on both the first processing core and the second processing core, collecting the respective performance information and statistics of the first and second processing cores while executing the pieces of code, and determining a best fit function F such that differences between F, performace information and statistics of the first processing core, and the performance of the second processing core are minimized.
An aircraft comprising a passenger cabin and a system, the system comprising: a vestibule disposed in the passenger cabin of the aircraft, the vestibule including at least one staircase for accessing at least one passenger rest cabin, each of the at least one passenger rest cabin implemented above or below the passenger cabin of the aircraft; at least one external view camera configured to capture images outside of the aircraft; and a plurality of passenger rest compartments implemented in the at least one passenger rest cabin, each of the plurality of the passenger rest compartments including a bed and a passenger service unit, PSU,; wherein each of the plurality of the passenger rest compartments further includes a display, wherein for each of the plurality of the passenger rest compartments the display is configured to be a virtual window configured to present at least a portion of the images outside of the aircraft; and wherein each of the plurality of passenger rest compartments further includes at least one sensor (912, 914) configured to detect a position of an occupant's head, wherein for each of the plurality of passenger rest compartments, the display is configured to be the virtual window configured to present at least the portion of the images outside of the aircraft based on the detected position of the occupant's head. a vestibule disposed in the passenger cabin of the aircraft, the vestibule including at least one staircase for accessing at least one passenger rest cabin, each of the at least one passenger rest cabin implemented above or below the passenger cabin of the aircraft; at least one external view camera configured to capture images outside of the aircraft; and a plurality of passenger rest compartments implemented in the at least one passenger rest cabin, each of the plurality of the passenger rest compartments including a bed and a passenger service unit, PSU,; wherein each of the plurality of the passenger rest compartments further includes a display, wherein for each of the plurality of the passenger rest compartments the display is configured to be a virtual window configured to present at least a portion of the images outside of the aircraft; and wherein each of the plurality of passenger rest compartments further includes at least one sensor (912, 914) configured to detect a position of an occupant's head, wherein for each of the plurality of passenger rest compartments, the display is configured to be the virtual window configured to present at least the portion of the images outside of the aircraft based on the detected position of the occupant's head.
Automated live cell microscope, comprising a sample holding frame arranged in the housing of the microscope, comprising an apparatus for sterilizing a sample space of the live cell microscope comprising a UV-C sterilization unit emitting ultraviolet light with a wavelength of 280 nm to 100 nm (UV-C radiation) and comprising attachment, operating and control elements for fixing, and introducing the movement of, the sample holding frame, characterized in that the UV-C sterilization unit is arranged in a manner traversable through the sample space in the live cell microscope for the purposes of sterilization.
A method for enabling download of verified vehicle manoeuvres (M1, M2), the method comprising: recording, in a database, a manoeuvre (M1, M2) as having been performed by a first vehicle at a location and according to a set of conditions of the first vehicle and a set of conditions of the location; assigning an assessment score to the manoeuvre (M1, M2) upon the manoeuvre (M1, M2) having been tested for at least one second vehicle, wherein the manoeuvre (M1, M2) is tested under test conditions given by the location, the set of conditions of the first vehicle and the set of conditions of the location, wherein aspects relating to safety concepts which could occur whilst the manoeuvre (M1, M2) is performed by at least one third vehicle are taken into consideration when testing the manoeuvre (M1, M2) for the at least one second vehicle such that such effects do not impact the safety of the manoeuvre (M1, M2) as performed by the at least third vehicle, wherein the assessment score is assigned upon review of a report issued in response to the manoeuvre (M1, M2) having been tested for the at least one second vehicle, wherein the assessment score is based on an outcome of the review, and wherein the manoeuvre (M1, M2) is edited when tested for the at least one second vehicle; determining the manoeuvre (M1, M2) to be verified only when the assessment score is above a threshold value; and enabling download of the manoeuvre (M1, M2) from the database to the at least one third vehicle only in case the manoeuvre (M1, M2) is verified recording, in a database, a manoeuvre (M1, M2) as having been performed by a first vehicle at a location and according to a set of conditions of the first vehicle and a set of conditions of the location; assigning an assessment score to the manoeuvre (M1, M2) upon the manoeuvre (M1, M2) having been tested for at least one second vehicle, wherein the manoeuvre (M1, M2) is tested under test conditions given by the location, the set of conditions of the first vehicle and the set of conditions of the location, wherein aspects relating to safety concepts which could occur whilst the manoeuvre (M1, M2) is performed by at least one third vehicle are taken into consideration when testing the manoeuvre (M1, M2) for the at least one second vehicle such that such effects do not impact the safety of the manoeuvre (M1, M2) as performed by the at least third vehicle, wherein the assessment score is assigned upon review of a report issued in response to the manoeuvre (M1, M2) having been tested for the at least one second vehicle, wherein the assessment score is based on an outcome of the review, and wherein the manoeuvre (M1, M2) is edited when tested for the at least one second vehicle; determining the manoeuvre (M1, M2) to be verified only when the assessment score is above a threshold value; and enabling download of the manoeuvre (M1, M2) from the database to the at least one third vehicle only in case the manoeuvre (M1, M2) is verified
A method for displaying traffic information on a traffic display unit onboard a first aircraft, comprising: acquiring data representing a current position, current climb rate, current groundspeed, current heading, current track, and current bank angle of the first aircraft; calculating a future position and a future heading/track of the first aircraft that would result were the first aircraft to continue to fly from its current position at its current climb rate, current groundspeed and current bank angle for a specified time or distance; displaying a first symbol that indicates the current position and current heading/track of the first aircraft relative to a frame of reference; displaying a second symbol that indicates the future position and future heading/track of the first aircraft relative to the frame of reference; characterized in that the method further comprises: displaying a curved line that indicates possible future positions of the first aircraft were the first aircraft to fly from its current position with its current heading/track at different possible bank angles for the specified time or distance. acquiring data representing a current position, current climb rate, current groundspeed, current heading, current track, and current bank angle of the first aircraft; calculating a future position and a future heading/track of the first aircraft that would result were the first aircraft to continue to fly from its current position at its current climb rate, current groundspeed and current bank angle for a specified time or distance; displaying a first symbol that indicates the current position and current heading/track of the first aircraft relative to a frame of reference; displaying a second symbol that indicates the future position and future heading/track of the first aircraft relative to the frame of reference; characterized in that the method further comprises: displaying a curved line that indicates possible future positions of the first aircraft were the first aircraft to fly from its current position with its current heading/track at different possible bank angles for the specified time or distance. displaying a curved line that indicates possible future positions of the first aircraft were the first aircraft to fly from its current position with its current heading/track at different possible bank angles for the specified time or distance.
A double-cylinder circular hosiery knitting machine with device for tensioning the manufacture during its production, comprising a supporting structure which is provided with a footing for resting on the ground and supports, so as to allow rotation about its vertically oriented axis, a lower needle cylinder and an upper needle cylinder which can be positioned, during the production of the manufacture, above and coaxially with respect to said lower needle cylinder; said lower needle cylinder and said upper needle cylinder being actuatable with a rotary motion about their axes (4, 6) with respect to said supporting structure; a device for tensioning the manufacture during its production being accommodated inside said needle cylinders (5, 7); said device for tensioning the manufacture comprising means for retaining the manufacture proximate to the region where knitting is formed by the needles accommodated in said needle cylinders (5, 7) and a tensioning tube, which is accommodated in said upper needle cylinder and is movable on command along the axis of said upper needle cylinder; the lower end of said tensioning tube being engageable, by sliding along the axis of said upper needle cylinder, with the region of the manufacture being formed that lies from said retention means to the needles; said retention means having a size suitable to allow the movement of said tensioning tube about said retention means, means for the translational motion of said tensioning tube along the axis of said upper needle cylinder being provided, characterized in that said retention means comprise a suction tube, which is accommodated internally and coaxially to said lower needle cylinder, and an element for locking the manufacture, which faces the upper end of said suction tube and is supported by said upper needle cylinder, said locking element being movable on command along the axis of said upper needle cylinder to engage or disengage the upper end of said suction tube.
A method for increasing a growth characteristic of a plant or increasing nutrient use efficiency of a plant, or improving a plant's ability to overcome stress comprising applying a composition comprising ketosuccinamate, dimeric ketosuccinamate, 3-carbamoyl-2,4-dihydroxy-6-oxopiperidine-2,4-dicarboxylate; 4-amino-2,4-dioxobutanoic acid; -4-oxo-2-azetidinecarboxylic acid; -4-oxo-2-azetidinecarboxylic acid; 4,8-dioxo-1,5-diazocane-2,6-dicarboxylic acid; or 2,6-dihydroxy-4,8-dioxo-1,5-diazocane-2,6-dicarboxylic acid, or a salt thereof, to the plant or to a propagation material of the plant.
Method for producing a vehicle pneumatic tyre with a tyre bead, in the case of which method tyre components for configuring the tyre bead are fed to a tyre building drum, are laid onto the latter, and are joined to one another in the region of the ends, the tyre components comprising at least one rubber strip and strip-shaped textile strips (11b, 11c), characterized in that, before they are fed to the tyre building drum, the tyre components are cut to form portions in the required length, are laid on one another, and are connected to one another to form a combination component, and the combination component is subsequently fed to the tyre building drum.
A method for forming a thin film between a pair of annular seal rings (3, 4; or 23, 24) and a rotatable runner (15, 35, or 67) within a circumferential seal assembly (1 or 21) comprising the steps of: (a) communicating a source flow into a feed groove communicable with at least two grooves, said feed groove and said grooves are disposed along an outer annular surface of said rotatable runner (15, 35 or 67), each said groove has an upstream end at an intersection between said groove and said feed groove and a downstream end; (b) separating said source flow at said upstream ends into each said groove to form a longitudinal flow therein; (c) redirecting said longitudinal flow via interaction with a base shoulder interposed between a pair of base walls to form an outward radial flow adjacent to said base shoulder, said base walls disposed between a pair of side walls, said base walls arranged along said groove to decrease depthwise in the direction opposite to rotation of said rotatable runner (15, 35 or 67); and (d) redirecting said longitudinal flow via interaction with a side shoulder along at least one said side wall to form a lateral flow in the direction of another said side wall, said lateral flow and said outward radial flow perpendicular to one another and to said longitudinal flow. (a) communicating a source flow into a feed groove communicable with at least two grooves, said feed groove and said grooves are disposed along an outer annular surface of said rotatable runner (15, 35 or 67), each said groove has an upstream end at an intersection between said groove and said feed groove and a downstream end; (b) separating said source flow at said upstream ends into each said groove to form a longitudinal flow therein; (c) redirecting said longitudinal flow via interaction with a base shoulder interposed between a pair of base walls to form an outward radial flow adjacent to said base shoulder, said base walls disposed between a pair of side walls, said base walls arranged along said groove to decrease depthwise in the direction opposite to rotation of said rotatable runner (15, 35 or 67); and (d) redirecting said longitudinal flow via interaction with a side shoulder along at least one said side wall to form a lateral flow in the direction of another said side wall, said lateral flow and said outward radial flow perpendicular to one another and to said longitudinal flow.
An unmanned aerial vehicle system, comprising: a line capture body having a line slot, the line slot having an open end and a closed end; a retainer having a first lobe, a second lobe, and a third lobe, and being positioned proximate the line slot, the retainer being pivotable relative to the line capture body among three positions: a first position in which the first and third lobes (1052a; 1052c) are positioned on opposite sides of the line slot and the second lobe is positioned over the line slot; a second position in which the first lobe is positioned over the line slot and the second and third lobes (1052b; 1052c) are clear of the line slot; and a third position in which the first and second lobes (1052a; 1052b) are positioned over the line slot and the third lobe is positioned clear of the line slot; and a biasing device coupled between the line capture body and the retainer to bias the retainer toward the first position. a line capture body having a line slot, the line slot having an open end and a closed end; a retainer having a first lobe, a second lobe, and a third lobe, and being positioned proximate the line slot, the retainer being pivotable relative to the line capture body among three positions: a first position in which the first and third lobes (1052a; 1052c) are positioned on opposite sides of the line slot and the second lobe is positioned over the line slot; a second position in which the first lobe is positioned over the line slot and the second and third lobes (1052b; 1052c) are clear of the line slot; and a third position in which the first and second lobes (1052a; 1052b) are positioned over the line slot and the third lobe is positioned clear of the line slot; and a biasing device coupled between the line capture body and the retainer to bias the retainer toward the first position. a first position in which the first and third lobes (1052a; 1052c) are positioned on opposite sides of the line slot and the second lobe is positioned over the line slot; a second position in which the first lobe is positioned over the line slot and the second and third lobes (1052b; 1052c) are clear of the line slot; and a third position in which the first and second lobes (1052a; 1052b) are positioned over the line slot and the third lobe is positioned clear of the line slot; and a biasing device coupled between the line capture body and the retainer to bias the retainer toward the first position.
A system, comprising: an electrosurgical generator configured to output energy; a tuner coupled to an electrosurgical generator and including at least one tuning circuit configured to provide a simulated tissue load having a variable complex impedance for the electrosurgical generator; and a controller coupled to the electrosurgical generator for diagnostic testing thereof, the controller including stored data pertaining to a plurality of complex impedance values, the controller being in operable communication with the tuner for varying a complex impedance of the load, the controller configured to adjust the tuner to at least one of the plurality of impedance values during diagnostic testing of the electrosurgical generator. an electrosurgical generator configured to output energy; a tuner coupled to an electrosurgical generator and including at least one tuning circuit configured to provide a simulated tissue load having a variable complex impedance for the electrosurgical generator; and a controller coupled to the electrosurgical generator for diagnostic testing thereof, the controller including stored data pertaining to a plurality of complex impedance values, the controller being in operable communication with the tuner for varying a complex impedance of the load, the controller configured to adjust the tuner to at least one of the plurality of impedance values during diagnostic testing of the electrosurgical generator.