mhurhangee/ep-ind-claims huggingface dataset:
Apparatus for obtaining information enabling a determination of a maximum power point of a power source comprising: means for discharging (Rdis, Co, Lo) energy stored in an inductor (LU1, L1) linked to the power source, means for monitoring voltage values on the inductor (LU1, L1) linked to the power source only after the discharging of the energy stored in the inductor by the means for discharging in order to obtain information enabling the determination of the maximum power point of the power source, characterised in that the apparatus further comprises: the voltage means for obtaining a value of the current going through the inductor during the monitoring of the voltage values on the inductor, wherein the current going through the inductor is derived from the voltage values obtained during the monitoring of the voltage values on the inductor. means for discharging (Rdis, Co, Lo) energy stored in an inductor (LU1, L1) linked to the power source, means for monitoring voltage values on the inductor (LU1, L1) linked to the power source only after the discharging of the energy stored in the inductor by the means for discharging in order to obtain information enabling the determination of the maximum power point of the power source, characterised in that the apparatus further comprises: the voltage means for obtaining a value of the current going through the inductor during the monitoring of the voltage values on the inductor, wherein the current going through the inductor is derived from the voltage values obtained during the monitoring of the voltage values on the inductor. the voltage means for obtaining a value of the current going through the inductor during the monitoring of the voltage values on the inductor, wherein the current going through the inductor is derived from the voltage values obtained during the monitoring of the voltage values on the inductor.
A section of a packaging line for beverage containers, which section comprises: - a shrinking tunnel, via which shrinking tunnel thermoplastic packaging material can be shrunk onto assemblies of beverage containers in order to produce packs, as well as - at least one manipulator, which manipulator is preferably designed for the clamping and/or form-fitting reception and handling of packs produced via the shrinking tunnel, characterized in that - the at least one manipulator is located downstream of the packs, directly following the shrinking tunnel, so that no horizontal conveying device is arranged between the at least one manipulator and the shrinking tunnel as a further station or working device, as the case may be. - a shrinking tunnel, via which shrinking tunnel thermoplastic packaging material can be shrunk onto assemblies of beverage containers in order to produce packs, as well as - at least one manipulator, which manipulator is preferably designed for the clamping and/or form-fitting reception and handling of packs produced via the shrinking tunnel, characterized in that - the at least one manipulator is located downstream of the packs, directly following the shrinking tunnel, so that no horizontal conveying device is arranged between the at least one manipulator and the shrinking tunnel as a further station or working device, as the case may be.
A formation vehicle comprising: a leading vehicle; a first intermediate vehicle coupled to the leading vehicle; a trailing vehicle; a third intermediate vehicle coupled to the trailing vehicle; a second intermediate vehicle coupled between the first intermediate vehicle and the third intermediate vehicle; first inter-vehicle body damper devices provided between the leading vehicle and the first intermediate vehicle and between the trailing vehicle and the third intermediate vehicle; and further inter-vehicle body damper devices (A2, A3) provided at both ends in a longitudinal direction of the second intermediate vehicle, characterised in that the first inter-vehicle body damper devices each include two up-down dampers (4a, 4b) and a left-right damper which bridge respectively between the leading vehicle and the first intermediate vehicle and between the trailing vehicle and the third intermediate vehicle, and the further inter-vehicle body damper device includes, at each end in the longitudinal direction of the second intermediate vehicle, an up-down damper (4a, 4b) and a left-right damper which bridge each end of the second intermediate vehicle and the respective vehicle (30a, 30c) coupled thereto. a leading vehicle; a first intermediate vehicle coupled to the leading vehicle; a trailing vehicle; a third intermediate vehicle coupled to the trailing vehicle; a second intermediate vehicle coupled between the first intermediate vehicle and the third intermediate vehicle; first inter-vehicle body damper devices provided between the leading vehicle and the first intermediate vehicle and between the trailing vehicle and the third intermediate vehicle; and further inter-vehicle body damper devices (A2, A3) provided at both ends in a longitudinal direction of the second intermediate vehicle, characterised in that the first inter-vehicle body damper devices each include two up-down dampers (4a, 4b) and a left-right damper which bridge respectively between the leading vehicle and the first intermediate vehicle and between the trailing vehicle and the third intermediate vehicle, and the further inter-vehicle body damper device includes, at each end in the longitudinal direction of the second intermediate vehicle, an up-down damper (4a, 4b) and a left-right damper which bridge each end of the second intermediate vehicle and the respective vehicle (30a, 30c) coupled thereto.
Propulsion assembly for an aircraft, having a longitudinal direction and having: - a chassis, - a gearbox comprising an output shaft, said shaft bearing a propeller, and - a propulsion system having at least the following propulsion elements: at least one electric motor, each of the at least one electric motor having a drive shaft mechanically coupled to the gearbox, at least one fuel cell configured to electrically power said at least one electric motor, and at least one tank configured to supply said at least one fuel cell with dihydrogen, said propulsion assembly being characterized in that the chassis has a T-shaped profile with a horizontal structure and a vertical structure, in that the gearbox is fastened to the front of the chassis by first fastening means, and in that the propulsion elements (154a-c) are fastened beneath the horizontal structure and against the vertical structure by second fastening means. - a chassis, - a gearbox comprising an output shaft, said shaft bearing a propeller, and - a propulsion system having at least the following propulsion elements: at least one electric motor, each of the at least one electric motor having a drive shaft mechanically coupled to the gearbox, at least one fuel cell configured to electrically power said at least one electric motor, and at least one tank configured to supply said at least one fuel cell with dihydrogen,
An organic solvent dispersion comprising an organic solvent and flaky titanium oxide particles dispersed therein, characterized in that the organic solvent dispersion has, in a UV-visible absorption spectrum, an optical absorption peak in the wavelength range of 250 to 280 nm and no optical 1 absorption peak in the wavelength range of 300 to 800 nm.
Method for triggered acquisition of a measured data set of a target object in a plurality of single measurements by means of a magnetic resonance system, having the following method steps: - detecting a cyclical signal, which describes a cyclical change in at least part of the target object, - continued automatic identification of cycles of the cyclical signal, - automatic determination of a mean duration L m of the identified cycles as at least one property of the cyclical signal, - specification of a reference duration TR prot as a reference value of an acquisition parameter, characterised in that, the following method steps are carried out - automatic determination of whether, in a particular identified cycle of the cyclical signal, triggering of one of the single measurements is permitted, as a function of the mean duration L m and the reference duration TR prot, wherein the smallest whole number n ≥ 1 is determined, so an n-multiple of the determined mean duration L m is longer than the specified reference duration TR prot, and - acquisition of the measured data set of the target object in a plurality of single measurements, wherein triggering of the single measurements is permitted only in each n th cycle of the cyclical signal. - detecting a cyclical signal, which describes a cyclical change in at least part of the target object, - continued automatic identification of cycles of the cyclical signal, - automatic determination of a mean duration L m of the identified cycles as at least one property of the cyclical signal, - specification of a reference duration TR prot as a reference value of an acquisition parameter, characterised in that, the following method steps are carried out - automatic determination of whether, in a particular identified cycle of the cyclical signal, triggering of one of the single measurements is permitted, as a function of the mean duration L m and the reference duration TR prot, wherein the smallest whole number n ≥ 1 is determined, so an n-multiple of the determined mean duration L m is longer than the specified reference duration TR prot, and - acquisition of the measured data set of the target object in a plurality of single measurements, wherein triggering of the single measurements is permitted only in each n th cycle of the cyclical signal.
A zinc (Zn) alloy plated steel material, comprising: a base steel and a Zn alloy plating layer, the Zn alloy plating layer including, by wt%, aluminum (Al): 0.1% to 5.0%, magnesium (Mg): 0.1% to 5.0%, Zn as a residual component, and inevitable impurities, wherein between the base steel and the Zn alloy plating layer, a lower interface layer formed on the base steel and having a fine structure and an upper interface layer formed on the lower interface layer and having a network-type structure or an island-type structure are provided, wherein a centerline arithmetical average roughness (Ra) of the base steel is in a range of 0.8 μm to 1.2 μm, a ten point median height (Rz) is in a range of 7.5 μm to 15.5 μm, and a maximum height roughness (Rmax) is in a range of 8 μm to 16.5 μm. a base steel and a Zn alloy plating layer, the Zn alloy plating layer including, by wt%, aluminum (Al): 0.1% to 5.0%, magnesium (Mg): 0.1% to 5.0%, Zn as a residual component, and inevitable impurities, wherein between the base steel and the Zn alloy plating layer, a lower interface layer formed on the base steel and having a fine structure and an upper interface layer formed on the lower interface layer and having a network-type structure or an island-type structure are provided, wherein a centerline arithmetical average roughness (Ra) of the base steel is in a range of 0.8 μm to 1.2 μm, a ten point median height (Rz) is in a range of 7.5 μm to 15.5 μm, and a maximum height roughness (Rmax) is in a range of 8 μm to 16.5 μm.
An assembly comprising a quick-coupling device and a thermal lance, wherein the coupling device does not require external elements for coupling, wherein the thermal lance is for fusion cutting and/or piercing, for example, for piercing and opening tapping passages in melting furnaces that use plugs made of clay or mixtures of, inter alia, alumina, silica and carbon, the coupling device comprising a hollow cylinder having bevelled ends and two circular internal grooves (2, 3) at each end of said device; wherein the first groove from each end of the coupling device is referred to as pressure ring groove, and wherein a hardened and tempered steel pressure ring is placed in each pressure ring groove; wherein the second groove closer to the center of the coupling device is referred to as O-ring groove, and wherein an O-ring with a hardness suitable for generating a good seal is placed in each O-ring groove; wherein the coupling device is configured to be coupled with the thermal lance, the thermal lance comprising an inverted conical end and, immediately before the start of said inverted conical end, the lance has a smooth and cylindrical surface which has an annular external groove that allows assuring the fitting between the lance and the coupling device through the insertion of the pressure ring in said annular external groove. wherein the first groove from each end of the coupling device is referred to as pressure ring groove, and wherein a hardened and tempered steel pressure ring is placed in each pressure ring groove; wherein the second groove closer to the center of the coupling device is referred to as O-ring groove, and wherein an O-ring with a hardness suitable for generating a good seal is placed in each O-ring groove; wherein the coupling device is configured to be coupled with the thermal lance, the thermal lance comprising an inverted conical end and, immediately before the start of said inverted conical end, the lance has a smooth and cylindrical surface which has an annular external groove that allows assuring the fitting between the lance and the coupling device through the insertion of the pressure ring in said annular external groove.
A method for synthesizing a diamond using a diamond synthesis machine, comprising: receiving, by a processor, a time series of images of a diamond during synthesis within a diamond synthesis machine, each of the time series of images captured within a time period; executing, by the processor, a diamond state prediction machine learning model using the time series of images to obtain a predicted data object, the predicted data object indicating a predicted state of the diamond within the diamond synthesis machine at a time subsequent to the time period, wherein the diamond state prediction machine learning model is trained based on a chronological series of images corresponding to a set of images of previously synthesized diamonds; detecting, by the processor, a predicted defect in the diamond based on the predicted data object of the diamond; and adjusting by the processor, operation of the diamond synthesis machine responsive to detecting the defect. receiving, by a processor, a time series of images of a diamond during synthesis within a diamond synthesis machine, each of the time series of images captured within a time period; executing, by the processor, a diamond state prediction machine learning model using the time series of images to obtain a predicted data object, the predicted data object indicating a predicted state of the diamond within the diamond synthesis machine at a time subsequent to the time period, wherein the diamond state prediction machine learning model is trained based on a chronological series of images corresponding to a set of images of previously synthesized diamonds; detecting, by the processor, a predicted defect in the diamond based on the predicted data object of the diamond; and adjusting by the processor, operation of the diamond synthesis machine responsive to detecting the defect.
A fan nacelle comprising: a metallic fan containment case; and a nacelle inlet secured to the metallic fan containment case by permanent fastening elements (92,94), wherein the fan containment case includes forward and aft ends (72,74) axially spaced from one another and first and second flanges (78,8 0) at the forward end, wherein the nacelle inlet includes first and second walls (82,84) respectively secured to the first and second flanges (78,80) by the permanent fastening elements (92,94), characterised in that a mount, configured to attach to a pylon of an aircraft, is provided at the aft end, the aft end being configured to be secured to a flow exit guide vane. a metallic fan containment case; and a nacelle inlet secured to the metallic fan containment case by permanent fastening elements (92,94), wherein the fan containment case includes forward and aft ends (72,74) axially spaced from one another and first and second flanges (78,8 0) at the forward end, wherein the nacelle inlet includes first and second walls (82,84) respectively secured to the first and second flanges (78,80) by the permanent fastening elements (92,94), characterised in that a mount, configured to attach to a pylon of an aircraft, is provided at the aft end, the aft end being configured to be secured to a flow exit guide vane.
A front-side type image sensor, including: - a substrate successively comprising, from its rear side to its front side, a P- type doped semiconducting support substrate, an electrically insulating layer and a semiconducting layer called an active layer, and - a matrix array of photodiodes in the active layer of said substrate, characterised in that the substrate comprises, between the support substrate and the electrically insulating layer, a P+ type doped semiconducting epitaxial layer located immediately at the rear of the electrically insulating layer, wherein the thickness of said epitaxial layer is between 0.1 and 3 μm and said epitaxial layer is configured to be biased at a lower voltage than the active layer. - a substrate successively comprising, from its rear side to its front side, a P- type doped semiconducting support substrate, an electrically insulating layer and a semiconducting layer called an active layer, and - a matrix array of photodiodes in the active layer of said substrate,
A photocurable resin composition comprising: an N-vinyl amide compound represented by the following formula: wherein R 1 and R 2 are each independently a hydrogen atom or hydrocarbon group having 1 to 5 carbon atoms, or R 1 and R 2 may be bonded together to form a hydrocarbon group having 2 to 6 carbon atoms.; a polyfunctional (meth)acrylate monomer represented by the following formula: wherein R 4 and R 5 are each independently a hydrogen atom or methyl group, R 3 is a trivalent to hexavalent organic residue, "a" is an integer of 0 to 3, and "b" is an integer of 3 to 6.; a photopolymerization initiator; and a compound having a 2,2,6,6-tetramethyl-4-piperidyl skeleton and represented by the following formula as a radical scavenger; wherein R 9 and R 10 are each independently a hydrogen atom or methyl group, and "e" is an integer of 5 to 12. an N-vinyl amide compound represented by the following formula: wherein R 1 and R 2 are each independently a hydrogen atom or hydrocarbon group having 1 to 5 carbon atoms, or R 1 and R 2 may be bonded together to form a hydrocarbon group having 2 to 6 carbon atoms.; a polyfunctional (meth)acrylate monomer represented by the following formula: wherein R 4 and R 5 are each independently a hydrogen atom or methyl group, R 3 is a trivalent to hexavalent organic residue, "a" is an integer of 0 to 3, and "b" is an integer of 3 to 6.; a photopolymerization initiator; and a compound having a 2,2,6,6-tetramethyl-4-piperidyl skeleton and represented by the following formula as a radical scavenger; wherein R 9 and R 10 are each independently a hydrogen atom or methyl group, and "e" is an integer of 5 to 12.
A method for controlling a laundry machine, comprising: a first rotation comprising rotating a stationary drum in a first direction by a predetermined rotation angle within 180 degrees; and a second rotation comprising rotating the drum, in a second direction opposite to the first direction, at least one revolution, characterized in that the predetermined rotation angle of the drum in the first rotation changes according to a quantity of laundry (m) input into the drum, and the sensing of the quantity of laundry (m) is carried out by determining a frequency with which current applied to a motor, which drives the drum, rises to a current limit, namely a current limit frequency, during the first rotation of the drum. a first rotation comprising rotating a stationary drum in a first direction by a predetermined rotation angle within 180 degrees; and a second rotation comprising rotating the drum, in a second direction opposite to the first direction, at least one revolution, characterized in that the predetermined rotation angle of the drum in the first rotation changes according to a quantity of laundry (m) input into the drum, and the sensing of the quantity of laundry (m) is carried out by determining a frequency with which current applied to a motor, which drives the drum, rises to a current limit, namely a current limit frequency, during the first rotation of the drum.
A plasma delivery tip of a medical grade plasma generating device, the device configured for intrabody delivery of said tip through a working channel, comprising: a gas delivery lumen defined within a circumferential wall and having a proximal-to-distal axis, and along which a flow of ionization gas flows to a distal aperture of the gas delivery lumen; a discharge electrode, separated from said flow by a dielectric barrier, which transmits a high voltage to the flow of ionization gas when attached to a high voltage source; and a one way valve, positioned between the discharge electrode and the distal aperture to prevent proximal ingress of contamination to a longitudinal position of the discharge electrode along the proximal-to-distal axis, thereby preventing liquid contamination in a plasma generation region of the plasma delivery tip. a gas delivery lumen defined within a circumferential wall and having a proximal-to-distal axis, and along which a flow of ionization gas flows to a distal aperture of the gas delivery lumen; a discharge electrode, separated from said flow by a dielectric barrier, which transmits a high voltage to the flow of ionization gas when attached to a high voltage source; and a one way valve, positioned between the discharge electrode and the distal aperture to prevent proximal ingress of contamination to a longitudinal position of the discharge electrode along the proximal-to-distal axis, thereby preventing liquid contamination in a plasma generation region of the plasma delivery tip.
A lift-type cleaning device for a floor washer, a cleaning tool for cleaning a floor being disposed on the floor washer, and the lift-type cleaning device comprising a bucket for containing water, wherein a drying member and a driver which are kept static during spin-drying are disposed in the bucket, and the cleaning tool is matched with the drying member; the driver is connected with the drying member and is able to control the drying member to rise; during cleaning, the drying member is located below; and during drying, the drying member is driven by the driver to rise and is then maintained above.