mhurhangee/patent-ind-claim-en huggingface dataset:
An organic light emitting device comprising: a first electrode; a second electrode provided opposite to the first electrode; a one or more-layered organic material layer including an emission layer provided between the first electrode and the second electrode; a secondary electrode provided on a top, a bottom, or a side surface of the first electrode and electrically connected to the first electrode, the secondary electrode having a mesh structure; and an insulation layer provided between the secondary electrode and the one or more-layered organic material layer, wherein the insulation layer is formed on the secondary electrode, and a width of the insulation layer is 10 μ m or more greater than a line width of the secondary electrode, and wherein each of meshes of the secondary electrode configures a pixel of the organic light emitting device, a sheet resistance of the first electrode is 5,000 Ω/□ or more, and a multiplication of the sheet resistance of the first electrode and an area of one pixel is 3,200 V cm 2 /A or less, and wherein the secondary electrode is located in a non-emissive area, and the insulation layer is provided in the non-emissive area. a first electrode; a second electrode provided opposite to the first electrode; a one or more-layered organic material layer including an emission layer provided between the first electrode and the second electrode; a secondary electrode provided on a top, a bottom, or a side surface of the first electrode and electrically connected to the first electrode, the secondary electrode having a mesh structure; and an insulation layer provided between the secondary electrode and the one or more-layered organic material layer, wherein the insulation layer is formed on the secondary electrode, and a width of the insulation layer is 10 μ m or more greater than a line width of the secondary electrode, and wherein each of meshes of the secondary electrode configures a pixel of the organic light emitting device, a sheet resistance of the first electrode is 5,000 Ω/□ or more, and a multiplication of the sheet resistance of the first electrode and an area of one pixel is 3,200 V cm 2 /A or less, and wherein the secondary electrode is located in a non-emissive area, and the insulation layer is provided in the non-emissive area.
An intermediate transfer member (ITM), comprising: one or more flexible layers comprising an outer layer for receiving ink droplets to form an ink image thereon, and for transferring the ink image to a target substrate; and one or more markers, at least one of the markers comprising: (i) a structure engraved in at least one of the one or more flexible layers at a respective marking location along the ITM, and (ii) filled with a filling material, which fills at least part of the structure, and changes one or both of an optical property and a magnetic property of the ITM. one or more flexible layers comprising an outer layer for receiving ink droplets to form an ink image thereon, and for transferring the ink image to a target substrate; and one or more markers, at least one of the markers comprising: (i) a structure engraved in at least one of the one or more flexible layers at a respective marking location along the ITM, and (ii) filled with a filling material, which fills at least part of the structure, and changes one or both of an optical property and a magnetic property of the ITM.
A system for facilitating an enhanced video pipeline in order to improve color perception, the system comprises: a first source configured to generate a first video stream , a second source configured to generate a second video stream , and a computing device , wherein the computing device is configured to superpose the first video stream onto the second video stream , thereby generating an output video stream , and wherein the computing device is further configured to calculate weighting factors for individual pixels or discrete pixel sets of adjacent individual pixels of the output video stream by analyzing the first video stream and/or the second video stream , characterized in that, the system further comprises a memory configured to store pre-calculated color manipulation matrices , and the computing device is further configured to utilize the weighting factors in order to determine the percentage of the pre-calculated color manipulation matrices so as to obtain a final color matrix for the output video stream and to obtain an altered color accordingly. a first source configured to generate a first video stream , a second source configured to generate a second video stream , and a computing device , wherein the computing device is configured to superpose the first video stream onto the second video stream , thereby generating an output video stream , and wherein the computing device is further configured to calculate weighting factors for individual pixels or discrete pixel sets of adjacent individual pixels of the output video stream by analyzing the first video stream and/or the second video stream , characterized in that, the system further comprises a memory configured to store pre-calculated color manipulation matrices , and the computing device is further configured to utilize the weighting factors in order to determine the percentage of the pre-calculated color manipulation matrices so as to obtain a final color matrix for the output video stream and to obtain an altered color accordingly.
Method of manufacturing a pressure tank , comprising an inner container and an outer layer made of a fiber material, which is wound around the inner container ; characterized by the following steps: a) providing an inner container with a cylindrical central portion , having two opposite end portions the openings of which are each closed by a dome-shaped pole cap portion (21;22); b) attaching a retention device with several protruding retention elements (44;45) in the area of an end portion of the central portion , the retention device being axially spaced from the opening of the end portion; c) manufacturing a pole cap reinforcement by winding fiber material around at least part of the pole cap portion (21;22) and the end portion with the retention device, the fiber material being guided around the protruding retention elements (44;45) of the retention device with reversal of direction; d) winding a circumferential winding around the end portion with the pole cap reinforcement , the circumferential winding being positioned between the opening of the end portion and the retention device; e) cutting the fiber material of the pole cap reinforcement between the retention device and the circumferential winding ; f) removing the retention device; g) manufacturing an outer layer by winding fiber material, the outer layer enclosing the central portion and the pole cap portions (21;22) of the inner container . a) providing an inner container with a cylindrical central portion , having two opposite end portions the openings of which are each closed by a dome-shaped pole cap portion (21;22); b) attaching a retention device with several protruding retention elements (44;45) in the area of an end portion of the central portion , the retention device being axially spaced from the opening of the end portion; c) manufacturing a pole cap reinforcement by winding fiber material around at least part of the pole cap portion (21;22) and the end portion with the retention device, the fiber material being guided around the protruding retention elements (44;45) of the retention device with reversal of direction; d) winding a circumferential winding around the end portion with the pole cap reinforcement , the circumferential winding being positioned between the opening of the end portion and the retention device; e) cutting the fiber material of the pole cap reinforcement between the retention device and the circumferential winding ; f) removing the retention device; g) manufacturing an outer layer by winding fiber material, the outer layer enclosing the central portion and the pole cap portions (21;22) of the inner container .
A fabrication method for fabricating a part by selective melting or selective sintering of powder beds by high energy beam, the method comprising the following steps: a) providing a material in the form of powder particles ; b) depositing a first powder layer of said material on a build support ; c) scanning at least one region of said first layer with the beam so as to heat the powder of said region locally to a temperature higher than the sintering temperature of the powder, such that the particles of said powder as melted or sintered in this way in said region form at least a first single-piece element ; d) laying a second powder layer of said material on said first powder layer ; e) scanning at least one region of said second layer with the beam so as to heat the powder of this region to a temperature higher than the sintering temperature of the powder, so that the particles of powder as sintered or melted in this way form at least one second single-piece element ; and f) repeating steps d) and e) for each new powder layer to be laid over a preceding layer until the part has been completely formed; said method being characterized in that the powder comprises a grain size distribution that is multimodal and in that , between steps a) and b), said powder is continuously preheated to a preheat temperature T p lying in the range 80°C to 150°C and an inert gas is caused to flow through said powder so as to diminish the air humidity adsorbed on the surface of the powder particles . a) providing a material in the form of powder particles ; b) depositing a first powder layer of said material on a build support ; c) scanning at least one region of said first layer with the beam so as to heat the powder of said region locally to a temperature higher than the sintering temperature of the powder, such that the particles of said powder as melted or sintered in this way in said region form at least a first single-piece element ; d) laying a second powder layer of said material on said first powder layer ; e) scanning at least one region of said second layer with the beam so as to heat the powder of this region to a temperature higher than the sintering temperature of the powder, so that the particles of powder as sintered or melted in this way form at least one second single-piece element ; and f) repeating steps d) and e) for each new powder layer to be laid over a preceding layer until the part has been completely formed; said method being characterized in that the powder comprises a grain size distribution that is multimodal and in that , between steps a) and b), said powder is continuously preheated to a preheat temperature T p lying in the range 80°C to 150°C and an inert gas is caused to flow through said powder so as to diminish the air humidity adsorbed on the surface of the powder particles .
Casing for distributing electrical power for an aircraft comprising a frame containing at least one power connector formed of one or more rails capable of cooperating with an end of a power plate , the power connector being configured such that the rails receive one or more distribution bars of the power plate at the end , said power plate comprising at least one switching element for an electrical energy distribution plate.
Single-edged milling tool having a shaft section and having a machining section , wherein a face cutting edge is formed on an end of the machining section , said end facing away from the shaft section , and said face cutting edge extends in a radial direction from an outer end at an outer peripheral edge up to an inner end that is arranged spaced apart from the outer peripheral edge and close to the axis of rotation, characterized in that the face cutting edge comprises on its outer end that is facing the outer peripheral edge a planar portion in which the face cutting edge has a constant planar distance to a reference plane that in the shaft section extends perpendicular to the axis of rotation , and said face cutting edge comprises an oblique portion that adjoins the planar portion and extends up to the inner end and in said oblique portion the face cutting edge has a smaller distance than the planar distance to the reference plane .
An optical spectroscopy system, comprising: a light transmission unit for emitting light to a specific region of a subject using a plurality of light sources, wherein the light emitted from the plurality of light sources is code-modulated using Walsh codes; and a light reception unit for detecting light coming through the specific region, wherein the light is demodulated using the Walsh codes to distinguish the light sources, wherein the light reception unit comprises a pipelinestructured matched filter for extracting one piece of data for each bit period by accumulating input signals in a continuous time domain using a reference clock used for the light emission as a sampling clock. a light transmission unit for emitting light to a specific region of a subject using a plurality of light sources, wherein the light emitted from the plurality of light sources is code-modulated using Walsh codes; and a light reception unit for detecting light coming through the specific region, wherein the light is demodulated using the Walsh codes to distinguish the light sources, wherein the light reception unit comprises a pipelinestructured matched filter for extracting one piece of data for each bit period by accumulating input signals in a continuous time domain using a reference clock used for the light emission as a sampling clock.
A power tool (11A; 11B) comprising: a rotational force generating device having a rotational drive shaft ; and a rotational driven shaft (36; 36B; 36C) coupled to the rotational drive shaft via a transmission mechanism , so that the rotation of the rotational drive shaft is transmitted to the rotational driven shaft (36; 36B; 36C) via the transmission mechanism , the rotational driven shaft (36; 36B; 36C) being a separate member from the rotational drive shaft ; characterized in that the rotational driven shaft (36; 36B; 36C) is rotatably supported by at least three bearings (37, 381, 382; 37B, 381B, 382B; 371C, 372C, 381C, 382C), the power tool further comprises a tool main body (13A; 13B) comprising a gear housing and a motor housing , wherein the rotational force generating device is disposed in the motor housing and the rotational driven shaft is disposed in the gear housing and the at least three bearings are mounted to the gear housing , or comprising a motor housing and the rotational force generating device and the rotational driven shaft (36B; 36C) are disposed in the motor housing and the at least three bearings (37B, 381B, 382B; 371C, 372C, 381C, 382C) are mounted to the motor housing , and the power tool further comprises a machining tool (14; 14B) for machining a workpiece, wherein the machining tool (14; 14B) is mounted to a mount portion of the rotational driven shaft (36; 36B; 36C), and two (381, 382; 381B, 382B; 381C, 382C) of the at least three bearings are arranged side by side on a side of a portion of the rotational driven shaft where the machining tool is attached. a rotational force generating device having a rotational drive shaft ; and a rotational driven shaft (36; 36B; 36C) coupled to the rotational drive shaft via a transmission mechanism , so that the rotation of the rotational drive shaft is transmitted to the rotational driven shaft (36; 36B; 36C) via the transmission mechanism , the rotational driven shaft (36; 36B; 36C) being a separate member from the rotational drive shaft ; characterized in that the rotational driven shaft (36; 36B; 36C) is rotatably supported by at least three bearings (37, 381, 382; 37B, 381B, 382B; 371C, 372C, 381C, 382C), the power tool further comprises a tool main body (13A; 13B) comprising a gear housing and a motor housing , wherein the rotational force generating device is disposed in the motor housing and the rotational driven shaft is disposed in the gear housing and the at least three bearings are mounted to the gear housing , or comprising a motor housing and the rotational force generating device and the rotational driven shaft (36B; 36C) are disposed in the motor housing and the at least three bearings (37B, 381B, 382B; 371C, 372C, 381C, 382C) are mounted to the motor housing , and the power tool further comprises a machining tool (14; 14B) for machining a workpiece, wherein the machining tool (14; 14B) is mounted to a mount portion of the rotational driven shaft (36; 36B; 36C), and two (381, 382; 381B, 382B; 381C, 382C) of the at least three bearings are arranged side by side on a side of a portion of the rotational driven shaft where the machining tool is attached.
A control module for use with a plurality of wellbore tools , the control module comprising: a power source ; a logic circuit operably coupled to the power source ; wherein the logic circuit is operably coupled to the plurality of wellbore tools through a topmost wellbore tool (200 1 ) of the plurality of wellbore tools ; characterized in that the logic circuit is configured to, in response to an initiation condition: for each wellbore tool (200 i ) of the plurality of wellbore tools in a sequential order from a bottommost wellbore tool (200 N ) to the topmost wellbore tool (200 1 ), determine whether a return signal, a current draw, or a voltage change of the wellbore tool (200 i ) is within an operation range; in response to a determination that the return signal, the current draw, or the voltage change is within the operation range, initiate the wellbore tool (200 i ); and in response to a determination that the return signal, the current draw, or the voltage change is outside the operation range, skip initiation of the wellbore tool (200 i ). a power source ; a logic circuit operably coupled to the power source ; wherein the logic circuit is operably coupled to the plurality of wellbore tools through a topmost wellbore tool (200 1 ) of the plurality of wellbore tools ; characterized in that the logic circuit is configured to, in response to an initiation condition: for each wellbore tool (200 i ) of the plurality of wellbore tools in a sequential order from a bottommost wellbore tool (200 N ) to the topmost wellbore tool (200 1 ), determine whether a return signal, a current draw, or a voltage change of the wellbore tool (200 i ) is within an operation range; in response to a determination that the return signal, the current draw, or the voltage change is within the operation range, initiate the wellbore tool (200 i ); and in response to a determination that the return signal, the current draw, or the voltage change is outside the operation range, skip initiation of the wellbore tool (200 i ). for each wellbore tool (200 i ) of the plurality of wellbore tools in a sequential order from a bottommost wellbore tool (200 N ) to the topmost wellbore tool (200 1 ), determine whether a return signal, a current draw, or a voltage change of the wellbore tool (200 i ) is within an operation range; in response to a determination that the return signal, the current draw, or the voltage change is within the operation range, initiate the wellbore tool (200 i ); and in response to a determination that the return signal, the current draw, or the voltage change is outside the operation range, skip initiation of the wellbore tool (200 i ).
A computer implemented method of detecting malicious code in a software application executing with a runtime environment in a computer system, the method comprising: receiving a definition of one or more runtime exception trigger conditions , each trigger condition defining criteria for the runtime environment to enter a software exception state and having associated a definition of a resulting state of the runtime environment having entered the exception state; monitoring the runtime environment to detect the satisfaction of a detected trigger condition by the runtime environment and, in response to a determination that the runtime environment fails to enter a resulting state associated with the detected trigger condition, identifying the software application as including malicious code. receiving a definition of one or more runtime exception trigger conditions , each trigger condition defining criteria for the runtime environment to enter a software exception state and having associated a definition of a resulting state of the runtime environment having entered the exception state; monitoring the runtime environment to detect the satisfaction of a detected trigger condition by the runtime environment and, in response to a determination that the runtime environment fails to enter a resulting state associated with the detected trigger condition, identifying the software application as including malicious code.
Compound for use in therapeutically treating heart failure in a subject having heart failure, wherein the compound is selected from the croup consisting of -N-[1-ethyl-1-(4-ethylphenyl)propyl]-2,7,7-trimethyl-5-phenyl-4,5,6,7-tetrahydropyrazolo[1,5-a]pyrimidine-3-carboxamide, -N-[1-ethyl-1-(4-methoxyphenyl)propyl]-2,7,7-trimethyl-5-phenyl-4,5,6,7-tetrahydropyrazolo[1,5-a]pyrimidine-3-carboxamide, -N-[1-ethyl-1-(4-ethylphenyl)propyl]-5-(2-fluorophenyl)-2,7,7-trimethyl-4,5,6,7-tetrahydropyrazolo[1,5-a]pyrimidine-3-carboxamide and salts thereof.
A method for monitoring a tool rotation of a survey tool within a wellbore during a gyrocompassing survey measurement, the method comprising: receiving a first plurality of signals from at least one accelerometer module of the survey tool, the first plurality of signals indicative of measurements of the Earth's gravitation vector taken by the at least one accelerometer module during the gyrocompassing survey measurement; using the first plurality of signals to calculate a tool face rate of change of the survey tool with respect to the wellbore during the gyrocompassing survey measurement; receiving a second plurality of signals from at least one gyroscopic sensor module of the survey tool, the second plurality of signals indicative of the total rotation rate to which the survey tool is subjected during the gyrocompassing survey measurement; and using the second plurality of signals to calculate the total rotation rate to which the survey tool is subjected during the gyrocompassing survey measurement; and compensating for the tool rotation of the survey tool during the gyrocompassing survey measurement by subtracting the tool face rate of change from a total rotation rate to which the survey tool is subjected during the gyrocompassing survey measurement. receiving a first plurality of signals from at least one accelerometer module of the survey tool, the first plurality of signals indicative of measurements of the Earth's gravitation vector taken by the at least one accelerometer module during the gyrocompassing survey measurement; using the first plurality of signals to calculate a tool face rate of change of the survey tool with respect to the wellbore during the gyrocompassing survey measurement; receiving a second plurality of signals from at least one gyroscopic sensor module of the survey tool, the second plurality of signals indicative of the total rotation rate to which the survey tool is subjected during the gyrocompassing survey measurement; and using the second plurality of signals to calculate the total rotation rate to which the survey tool is subjected during the gyrocompassing survey measurement; and compensating for the tool rotation of the survey tool during the gyrocompassing survey measurement by subtracting the tool face rate of change from a total rotation rate to which the survey tool is subjected during the gyrocompassing survey measurement.
Lithium cobalt oxide powder for use as an active positive electrode material in lithium-ion batteries having a d50 of more than 15 μm, a specific surface area (BET) of less than 0.2 m 2 /g. an OH - content measured by acid-base titration between 0.010 and 0.015 wt%, more preferably between 0.0125 and 0.015, said powder being characterized in that it has a Li to Co atomic ratio between 0.980 and less than 1.000, more preferably of less than 0.999.