mhurhangee/patent-ind-claim-en huggingface dataset:
Circuit breaker, comprising - a first and a second breaker terminal , - a bimetal stripe , - a first conduction line , - a switch with a first and a second contact , wherein the first conduction line is electrically coupled to the first breaker terminal and to the first contact of the switch , - a triggering device mechanically coupling the bimetal stripe to the switch , - a magnet connected to at least one of the bimetal stripe , the triggering device and the switch , - a detection device comprising a magnetic field sensor configured to detect a magnetic field of the magnet and a control circuit connected to the magnetic field sensor , and - a first housing which at least encloses the bimetal stripe , the first conduction line , the switch , the triggering device and the magnet , characterized in that the first conduction line is wound around the bimetal stripe , wherein the circuit breaker comprises a second housing which at least encloses the detection device , and wherein the magnetic field sensor is outside of the first housing and is configured to detect a movement of the magnet inside the first housing . - a first and a second breaker terminal , - a bimetal stripe , - a first conduction line , - a switch with a first and a second contact , wherein the first conduction line is electrically coupled to the first breaker terminal and to the first contact of the switch , - a triggering device mechanically coupling the bimetal stripe to the switch , - a magnet connected to at least one of the bimetal stripe , the triggering device and the switch , - a detection device comprising a magnetic field sensor configured to detect a magnetic field of the magnet and a control circuit connected to the magnetic field sensor , and - a first housing which at least encloses the bimetal stripe , the first conduction line , the switch , the triggering device and the magnet , the first conduction line is wound around the bimetal stripe , wherein the circuit breaker comprises a second housing which at least encloses the detection device , and wherein the magnetic field sensor is outside of the first housing and is configured to detect a movement of the magnet inside the first housing .
A heterophasic propylene copolymer having a. Overall ethylene content between 5-20 wt% measured with FTIR b. MFI between 3 and 25 (g/10 min) measured according to ISO 1133-1:2011 at 230 0 C and 2.16 kg, c. 20 °C xylene soluble fraction (CXS) between 8 and 30 (wt%), wherein the CXS is determined according to ISO 16152, d. a BTT according to the formula: BTT ≤ 65 - 10* (CXS/MFI), wherein the BTT is determined according to ISO 180/4A. wherein the wt% is defined relative to the total of the composition. a. Overall ethylene content between 5-20 wt% measured with FTIR b. MFI between 3 and 25 (g/10 min) measured according to ISO 1133-1:2011 at 230 0 C and 2.16 kg, c. 20 °C xylene soluble fraction (CXS) between 8 and 30 (wt%), wherein the CXS is determined according to ISO 16152, d. a BTT according to the formula: BTT ≤ 65 - 10* (CXS/MFI), wherein the BTT is determined according to ISO 180/4A.
A device for detecting nucleic acids comprising at least two heatable sample blocks and a reaction cartridge containing the base and at least one film sealing the base characterized in that the film moreover comprises surfaces that are not connected to the base and said surfaces form at least two reaction chambers , wherein the one reaction chamber comprises an optical detection unit for the detection of nucleic acids and a test strip is located in the second reaction chamber for the detection of nucleic acids.
An active material having a composition represented by Na x M y Si 46 , wherein M is a metal element other than Na and x and y satisfy 2.9 ≤ x, 0 ≤ y, y ≤ x and 2.9 ≤ x + y ≤ 7.1, the active material comprising a crystal phase of a Type I silicon clathrate.
A solar powered aircraft comprising: an electric-powered engine propulsion system; one or more first wings attached parallel to the lateral axis of the aircraft, wherein the first wings are configured to produce lift in a first direction when the aircraft is moving in a second direction that is substantially perpendicular to the first direction, wherein the first wings are configured to also produce a centripetal force when the aircraft is banking while moving in the second direction; one or more second wings affixed and oriented substantially perpendicular to the first wings , a solar power system comprising a plurality of solar cells affixed to one or more wings of the aircraft, wherein the solar power system is configured to capture sunlight, convert the captured sunlight to electricity, and provide the electricity to the engine propulsion system, characterized in that the second wings are rotatable with respect to the vertical axis of the aircraft, and wherein the second wings are configured to produce a counter force in a third direction that is substantially perpendicular to both the first direction and the second direction, wherein the counter force reduces the centripetal force when the aircraft is banking, wherein a rotation of the second wings produces lift in a desired direction while the aircraft is in motion. an electric-powered engine propulsion system; one or more first wings attached parallel to the lateral axis of the aircraft, wherein the first wings are configured to produce lift in a first direction when the aircraft is moving in a second direction that is substantially perpendicular to the first direction, wherein the first wings are configured to also produce a centripetal force when the aircraft is banking while moving in the second direction; one or more second wings affixed and oriented substantially perpendicular to the first wings , a solar power system comprising a plurality of solar cells affixed to one or more wings of the aircraft, wherein the solar power system is configured to capture sunlight, convert the captured sunlight to electricity, and provide the electricity to the engine propulsion system, characterized in that the second wings are rotatable with respect to the vertical axis of the aircraft, and wherein the second wings are configured to produce a counter force in a third direction that is substantially perpendicular to both the first direction and the second direction, wherein the counter force reduces the centripetal force when the aircraft is banking, wherein a rotation of the second wings produces lift in a desired direction while the aircraft is in motion.
An anti-reflective film comprising: a hard coating layer; and a low-refractive layer containing a binder resin and hollow inorganic nanoparticles and solid inorganic nanoparticles which are dispersed in the binder resin, wherein the low-refractive layer includes a first layer containing at least 70 vol% of the entire solid inorganic nanoparticles and a second layer containing at least 70 vol% of the entire hollow inorganic nanoparticles, and at the time of fitting polarization ellipticity measured by ellipsometry for the second layer included in the low-refractive layer using a Cauchy model represented by the following General Equation 1, the second layer satisfies the following conditions: A is 1.0 to 1.50, B is 0 to 0.00 7 , and C is 0 to 1*10 -3 : n λ = A + B λ 2 + C λ 4 in General Equation 1, n(λ) is a refractive index at a wavelength of λ, λ is in a range of 300 nm to 1800nm, and A, B, and C are Cauchy parameters, wherein the first layer has a thickness of 1 nm to 50 nm and the second layer has a thickness of 5nm to 30 nm or 120 nm to 300 nm and the thicknesses of the two layers and the Cauchy parameters A, B and C are measured as detailed in the description. a hard coating layer; and a low-refractive layer containing a binder resin and hollow inorganic nanoparticles and solid inorganic nanoparticles which are dispersed in the binder resin, wherein the low-refractive layer includes a first layer containing at least 70 vol% of the entire solid inorganic nanoparticles and a second layer containing at least 70 vol% of the entire hollow inorganic nanoparticles, and at the time of fitting polarization ellipticity measured by ellipsometry for the second layer included in the low-refractive layer using a Cauchy model represented by the following General Equation 1, the second layer satisfies the following conditions: A is 1.0 to 1.50, B is 0 to 0.00 7 , and C is 0 to 1*10 -3 : n λ = A + B λ 2 + C λ 4 in General Equation 1, n(λ) is a refractive index at a wavelength of λ, λ is in a range of 300 nm to 1800nm, and A, B, and C are Cauchy parameters, wherein the first layer has a thickness of 1 nm to 50 nm and the second layer has a thickness of 5nm to 30 nm or 120 nm to 300 nm and the thicknesses of the two layers and the Cauchy parameters A, B and C are measured as detailed in the description. in General Equation 1, n(λ) is a refractive index at a wavelength of λ, λ is in a range of 300 nm to 1800nm, and A, B, and C are Cauchy parameters, wherein the first layer has a thickness of 1 nm to 50 nm and the second layer has a thickness of 5nm to 30 nm or 120 nm to 300 nm and the thicknesses of the two layers and the Cauchy parameters A, B and C are measured as detailed in the description.
A system for manufacturing components by melting and resolidifiying powdered materials, the system comprising: a concentrated energy source for selectively melting the powdered material; and a simulation and control system comprising a computing device, and a non-transitory computer readable storage medium containing instructions that, when executed, cause the simulation and control system to: scan the concentrated energy source across the powdered material to create a melt pool; calculate an average melt pool temperature based on a signal from a thermal imaging device using a Canny edge detection algorithm or a connected contour labeling algorithm; estimate a temperature profile of the material by simulating a result of previous scanning of the concentrated energy source across the powdered material; and control at least one of a power output, scan speed of the concentrated energy source with a feedback controller to obtain a desired temperature of the melt pool, using the temperature profile and the calculated average melt pool temperature as inputs to the feedback controller. a concentrated energy source for selectively melting the powdered material; and a simulation and control system comprising a computing device, and a non-transitory computer readable storage medium containing instructions that, when executed, cause the simulation and control system to: scan the concentrated energy source across the powdered material to create a melt pool; calculate an average melt pool temperature based on a signal from a thermal imaging device using a Canny edge detection algorithm or a connected contour labeling algorithm; estimate a temperature profile of the material by simulating a result of previous scanning of the concentrated energy source across the powdered material; and control at least one of a power output, scan speed of the concentrated energy source with a feedback controller to obtain a desired temperature of the melt pool, using the temperature profile and the calculated average melt pool temperature as inputs to the feedback controller. scan the concentrated energy source across the powdered material to create a melt pool; calculate an average melt pool temperature based on a signal from a thermal imaging device using a Canny edge detection algorithm or a connected contour labeling algorithm; estimate a temperature profile of the material by simulating a result of previous scanning of the concentrated energy source across the powdered material; and control at least one of a power output, scan speed of the concentrated energy source with a feedback controller to obtain a desired temperature of the melt pool, using the temperature profile and the calculated average melt pool temperature as inputs to the feedback controller.
A pacing system , comprising: a signal generator configured to generate a pacing signal; and an electromechanical switch having a plurality of outputs that are configured to be coupled to a plurality of electrodes inserted into a heart of a patient, each output configured to deliver the pacing signal to a respective electrode, wherein the electromechanical switch is configured to route the pacing signal to no more than a single selected one of the outputs at any given time, so as to pace the heart using no more than a single selected one of the electrodes, wherein the electromechanical switch comprises: a substrate patterned with multiple contacts arranged in an array, wherein each contact in the array is coupled to a respective output of the plurality of outputs, a moving switch , which is configured to move over the array of contacts and to establish electrical contact with one contact only at any given time, and a motor configured to move the moving switch. a signal generator configured to generate a pacing signal; and an electromechanical switch having a plurality of outputs that are configured to be coupled to a plurality of electrodes inserted into a heart of a patient, each output configured to deliver the pacing signal to a respective electrode, wherein the electromechanical switch is configured to route the pacing signal to no more than a single selected one of the outputs at any given time, so as to pace the heart using no more than a single selected one of the electrodes, a substrate patterned with multiple contacts arranged in an array, wherein each contact in the array is coupled to a respective output of the plurality of outputs, a moving switch , which is configured to move over the array of contacts and to establish electrical contact with one contact only at any given time, and a motor configured to move the moving switch.
A light measurement system comprising: • a light source (a) to be measured, which is any device capable of producing light, and • a pre-calibrated light measuring sensor (c) placed at a known distance from said light source, including • a control system (d) adapted to obtain data from said sensor (c) and to rotate said light source (a) around an axis over time and to save a series of light measurements obtained by said light measuring sensor (c) while the light source (a) is rotated, thereby obtaining an angular light distribution in one plane of complete light output distribution field (b) of said light source (a), • characterized in that said control system (d) is adapted to calculate from said angular light output distribution measurement in one plane the total combined light output corresponding to the total amount of light output by said light source (a) based on information about the shape of the light field and at which orientation the light source was measured as derived from a previous reference measurement of the same light source and/or based on a default or user or preselected light distribution field information matching said light source. • a light source (a) to be measured, which is any device capable of producing light, and • a pre-calibrated light measuring sensor (c) placed at a known distance from said light source, including • a control system (d) adapted to obtain data from said sensor (c) and to rotate said light source (a) around an axis over time and to save a series of light measurements obtained by said light measuring sensor (c) while the light source (a) is rotated, thereby obtaining an angular light distribution in one plane of complete light output distribution field (b) of said light source (a), • characterized in that said control system (d) is adapted to calculate from said angular light output distribution measurement in one plane the total combined light output corresponding to the total amount of light output by said light source (a) based on information about the shape of the light field and at which orientation the light source was measured as derived from a previous reference measurement of the same light source and/or based on a default or user or preselected light distribution field information matching said light source.
An induction heating type cooktop, comprising: a case ; an upper plate coupled to a top of the case and configured to support a target heating object; a working coil disposed inside the case and configured to heat the target heating object; a thin film disposed at a top surface of the upper plate or a bottom surface of the upper plate ; and an insulator disposed between the bottom surface of the upper plate and the working coil , wherein the thin film comprises: a plurality of sub-thin films that are arranged about a central portion of the working coil , each of the plurality of sub-thin films defining a closed loop surrounding the central portion of the working coil , characterised by a heat conduction member that is arranged in a predetermined pattern and contacts at least one of the plurality of sub-thin films . a case ; an upper plate coupled to a top of the case and configured to support a target heating object; a working coil disposed inside the case and configured to heat the target heating object; a thin film disposed at a top surface of the upper plate or a bottom surface of the upper plate ; and an insulator disposed between the bottom surface of the upper plate and the working coil , wherein the thin film comprises: a plurality of sub-thin films that are arranged about a central portion of the working coil , each of the plurality of sub-thin films defining a closed loop surrounding the central portion of the working coil , characterised by a heat conduction member that is arranged in a predetermined pattern and contacts at least one of the plurality of sub-thin films . a plurality of sub-thin films that are arranged about a central portion of the working coil , each of the plurality of sub-thin films defining a closed loop surrounding the central portion of the working coil , characterised by a heat conduction member that is arranged in a predetermined pattern and contacts at least one of the plurality of sub-thin films .
Membrane arrangement for an outlet opening of a designated hollow body with an interior space for a medium and the outlet opening for the medium , - with a membrane , which in a designated mounting position (M) can be attached to the hollow body , closing the outlet opening in a media-sealing manner, and at the same time is designed to bulge increasingly away from the interior space as the internal pressure (PI) increases, - with a cutting means , which in the mounting position (M) can be attached to the hollow body and at the same time is arranged beyond the membrane with respect to the interior space , - wherein, in the mounting position (M), the membrane and the cutting means are in a relative position (R) in relation to one another in which, up to an internal pressure (PI) at the level of a limit pressure (PG), the cutting means does not lie against the membrane and, when the limit pressure (PG) is exceeded, the cutting means lies against the membrane , while producing a cutting effect that severs the membrane , - wherein the cutting means is designed in the manner of a cannula , which at a pointed end tapers towards the membrane in at least one cutting tip and has an outlet channel and a wall surrounding said outlet channel, - wherein, when the membrane is severed, the medium can be made to pass through the outlet opening by means of the outlet channel , - wherein, when the membrane is severed, the outlet opening is at least partially open for the medium to pass through by means of the outlet channel . - with a membrane , which in a designated mounting position (M) can be attached to the hollow body , closing the outlet opening in a media-sealing manner, and at the same time is designed to bulge increasingly away from the interior space as the internal pressure (PI) increases, - with a cutting means , which in the mounting position (M) can be attached to the hollow body and at the same time is arranged beyond the membrane with respect to the interior space , - wherein, in the mounting position (M), the membrane and the cutting means are in a relative position (R) in relation to one another in which, up to an internal pressure (PI) at the level of a limit pressure (PG), the cutting means does not lie against the membrane and, when the limit pressure (PG) is exceeded, the cutting means lies against the membrane , while producing a cutting effect that severs the membrane , - wherein the cutting means is designed in the manner of a cannula , which at a pointed end tapers towards the membrane in at least one cutting tip and has an outlet channel and a wall surrounding said outlet channel, - wherein, when the membrane is severed, the medium can be made to pass through the outlet opening by means of the outlet channel , - wherein, when the membrane is severed, the outlet opening is at least partially open for the medium to pass through by means of the outlet channel .
A discharge arrangement for horizontal filtration equipment , the discharge arrangement comprising a conveyor configured to be provided below the horizontal filtration equipment for receiving discharge material discharged from the horizontal filtration equipment , and a drive for driving the conveyor , characterized in that the drive is configured to enable driving the conveyor in two opposite directions, such that material provided on the conveyor can be discharged at either a first end or a second end depending on the direction in which the conveyor is driven, and that the discharge arrangement further comprises a control unit configured to control the drive to drive the conveyor alternatively in a first direction, which is a direction directed towards the first end , such that the conveyor is configured to discharge material provided on the conveyor at the first end , and in a second direction, which is a direction directed towards the second end , such that the conveyor is configured to discharge material provided on the conveyor at the second end . a conveyor configured to be provided below the horizontal filtration equipment for receiving discharge material discharged from the horizontal filtration equipment , and a drive for driving the conveyor , characterized in that the drive is configured to enable driving the conveyor in two opposite directions, such that material provided on the conveyor can be discharged at either a first end or a second end depending on the direction in which the conveyor is driven, and that the discharge arrangement further comprises a control unit configured to control the drive to drive the conveyor alternatively in a first direction, which is a direction directed towards the first end , such that the conveyor is configured to discharge material provided on the conveyor at the first end , and in a second direction, which is a direction directed towards the second end , such that the conveyor is configured to discharge material provided on the conveyor at the second end .