mhurhangee/ep-ind-claims huggingface dataset:
Method for cooling IR emitters in a heating device used for warming preforms before processing the preforms in a stretch blow molding device, whereby IR emitters are arranged on at least one sidewall of the heating device parallel to the transport direction of the preforms, whereby at least one back reflector is arranged on the side of the IR emitters averting the preforms, whereby the preforms to be warmed comprise a mouth region and a longitudinal axis and whereby the mouth region of the preforms is cooled with a first coolant flow, characterized in that a second vertical coolant flow (51, 54) passes between the IR emitters and the at least one back reflector, whereby this second coolant flow (51, 54) is at least partially branched off from the horizontal first coolant flow and / or whereby this second coolant flow (51, 54) is united with the horizontal first coolant flow, whereby the second coolant flow (51, 54) runs parallel to the longitudinal axis of the preforms.
Skin and/or mucous membrane penetrating microemulsion comprising: - 50 to 80% w/w of an oil phase, - 2 to 40 % w/w of a mixture of one or several W/O emulsifiers and one or several O/W emulsifiers at a ratio of 1:5 to 1:1, - 5 to 40 % w/w of honey, royal jelly, propolis and/or perga - 0.01 to 30 % w/w of co-emulsifiers, wherein the co-emulsifiers originate from the group of phospholipids - 1 to 20 % w/w of water or an aqueous solution and - 0.01 to 30 % w/w of one or several water-soluble or fat-soluble active ingredients, wherein the active ingredients are selected from the group: analgetics, local anesthetics, antiphlogistics, antirheumatics, glucocorticoids, antibiotics, antimycotics, virustatics, immunosuppressive agents, phytopharmaceuticals, antihistamines, chemotherapeutics, blood circulation stimulants, steroids, immunomodulators, antipsoriatics, keratolytics, hormones, alkaloids, hormones, ceramides. - 50 to 80% w/w of an oil phase, - 2 to 40 % w/w of a mixture of one or several W/O emulsifiers and one or several O/W emulsifiers at a ratio of 1:5 to 1:1, - 5 to 40 % w/w of honey, royal jelly, propolis and/or perga - 0.01 to 30 % w/w of co-emulsifiers, wherein the co-emulsifiers originate from the group of phospholipids - 1 to 20 % w/w of water or an aqueous solution and - 0.01 to 30 % w/w of one or several water-soluble or fat-soluble active ingredients,
A method for manufacturing a grain-oriented electrical steel sheet, comprising the steps of: rolling a steel slab containing 0.08 mass percent or less of carbon, 2.0-8.0 mass percent of Si, and 0.005-3.0 mass percent of Mn into a cold-rolled steel sheet; subsequently performing decarburizing annealing of the cold-rolled steel sheet if desired; subsequently applying an annealing separator to the cold-rolled steel sheet if desired; performing secondary-recrystallization annealing of the cold-rolled steel sheet; and subsequently performing purification annealing of the cold-rolled steel sheet, wherein the steel slab contains less than 100 ppm of Al and not more than 50 ppm each of N, S, and Se, the purification annealing is performed at 1050°C or more, and the partial pressure of hydrogen in the atmosphere is adjusted to 0.4 atm or less in a temperature range above 1170°C for a purification annealing conducted at a temperature above 1170°C, or 0.8 atm or less in a temperature range of 1050°C or more for a purification annealing conducted at a temperature of 1170°C or less, and wherein the gas used to adjust the hydrogen partial pressure is an inert gas. rolling a steel slab containing 0.08 mass percent or less of carbon, 2.0-8.0 mass percent of Si, and 0.005-3.0 mass percent of Mn into a cold-rolled steel sheet; subsequently performing decarburizing annealing of the cold-rolled steel sheet if desired; subsequently applying an annealing separator to the cold-rolled steel sheet if desired; performing secondary-recrystallization annealing of the cold-rolled steel sheet; and subsequently performing purification annealing of the cold-rolled steel sheet, wherein the steel slab contains less than 100 ppm of Al and not more than 50 ppm each of N, S, and Se, the purification annealing is performed at 1050°C or more, and the partial pressure of hydrogen in the atmosphere is adjusted to 0.4 atm or less in a temperature range above 1170°C for a purification annealing conducted at a temperature above 1170°C, or 0.8 atm or less in a temperature range of 1050°C or more for a purification annealing conducted at a temperature of 1170°C or less, and wherein the gas used to adjust the hydrogen partial pressure is an inert gas.
Use of a marker set comprising at least three substances chosen from the group consisting of 3-hydroxy isovalerate, acetyl carnitine, alanine, citrate, dimethylamine, glucose, glucuronate, hippurate, lactate, malonate, methyl guanidine, methyl malonate, methyl succinate, p-cresol, phenyl acetate, phenylacetylglycine, phenylacetylglutamine, taurine, trigonelline, and urea, in an in vitro method for determining the risk of kidney rejection of an individual after having obtained a kidney donation by urine analysis, with the provision that the marker set comprises alanine.
Method for determining the installation position of a sensor module in a vehicle, specifically whether the sensor module is installed with its longitudinal axis longitudinally or transversely in the vehicle, wherein the sensor module has a longitudinal acceleration sensor for measuring a module longitudinal acceleration (L_sens) in the direction of the longitudinal axis of the sensor module and/or a transverse acceleration sensor for measuring a module transverse acceleration (Q_sens) transversely with respect to the longitudinal axis of the sensor module, wherein a measured module longitudinal acceleration (L_sens) and/or a measured module transverse acceleration (Q_sens) are/is compared with a vehicle longitudinal acceleration (L_rad) and/or a vehicle transverse acceleration (Q_gier) while the vehicle is travelling, characterized in that the vehicle longitudinal acceleration (L_rad) is calculated from wheel speeds of the vehicle and/or using the position data of satellite navigation system and/or using data of radar system mounted in the vehicle and/or wherein the vehicle transverse acceleration (Q_gier) is calculated from a vehicle speed and a yaw rate of the vehicle or from wheel speeds of the vehicle, and at least one degree of correspondence which represents correspondence between a measured module acceleration (L_sens, Q_sens) and a calculated vehicle acceleration (L_rad, Q_gier) is determined on the basis of the comparison, and the installation position of the sensor module is determined on the basis of the degree of correspondence.
A high-low-voltage conversion star multi-phase variable-frequency drive system, comprising a phase-shifting transformer, rectifying circuits, inverter circuits, a multi-phase motor, primary windings of the phase-shifting transformer being connected with an alternating-current power source, and secondary windings of the phase-shifting transformer being connected with the rectifying circuits, wherein the number of the secondary windings is the same as the number of the rectifying circuits, one secondary winding is connected with one rectifying circuit, and output ends of the rectifying circuits are connected with the inverter circuits; the high-low-voltage conversion star multi-phase variable-frequency drive system being characterized in that the system further comprises a control circuit connected with the phase-shifting transformer, the rectifying circuits, the inverter circuits and the multi-phase motor; all rectifying circuits are in common-ground connection to form a common-ground direct-current power source; the number of the inverter circuits is the same as the number of phases of a stator of the multi-phase motor, one inverter circuit is connected with one end of one motor stator winding and the other ends of the motor stator windings are mutually connected to form a multi-phase star winding; and the number of the rectifying circuits is the same as the number of the inverter circuits and one rectifying circuit is connected with one inverter circuit; or the number of the inverter circuits is k times of the number of the rectifying circuits. the high-low-voltage conversion star multi-phase variable-frequency drive system being characterized in that the system further comprises a control circuit connected with the phase-shifting transformer, the rectifying circuits, the inverter circuits and the multi-phase motor; all rectifying circuits are in common-ground connection to form a common-ground direct-current power source; the number of the inverter circuits is the same as the number of phases of a stator of the multi-phase motor, one inverter circuit is connected with one end of one motor stator winding and the other ends of the motor stator windings are mutually connected to form a multi-phase star winding; and the number of the rectifying circuits is the same as the number of the inverter circuits and one rectifying circuit is connected with one inverter circuit; or the number of the inverter circuits is k times of the number of the rectifying circuits.
An apparatus for automatic amplifier gain setting of an optical amplifier, said apparatus comprising: an optical channel counter, OCC, unit configured to detect a number of channels present in an optical transmission spectrum; a determination unit configured to determine an average power per channel calculated by dividing a measured total power of a signal input and/or signal output of the optical amplifier by the number of channels detected by said optical channel counter, OCC, unit; and a gain adjustment unit configured to adjust the amplifier gain of said optical amplifier automatically depending on a calculated power difference between a predetermined desired power per channel and the determined average power per channel provided by said determination unit. an optical channel counter, OCC, unit configured to detect a number of channels present in an optical transmission spectrum; a determination unit configured to determine an average power per channel calculated by dividing a measured total power of a signal input and/or signal output of the optical amplifier by the number of channels detected by said optical channel counter, OCC, unit; and a gain adjustment unit configured to adjust the amplifier gain of said optical amplifier automatically depending on a calculated power difference between a predetermined desired power per channel and the determined average power per channel provided by said determination unit.
A fluid cooled cold plate (40;40';40") for an electronic device comprising: a main coolant passage having a first cross-sectional area taken laterally in a direction perpendicular to the flow direction; characterized by finned coolant passages each having a second cross-sectional area taken laterally in a direction perpendicular to the flow direction, wherein the second area is smaller than the first area and the finned coolant passages are located downstream from the main coolant passage; a branch fluidly connecting the main coolant passage with the finned coolant passage, wherein the branch is oriented such that a fluid is turned 90° or more when passing into the branch from the main coolant passage; and a coolant bypass passage in fluid communication with the main coolant passage to form a continuous straight passage located fluidically parallel to the finned coolant passage. a main coolant passage having a first cross-sectional area taken laterally in a direction perpendicular to the flow direction; characterized by finned coolant passages each having a second cross-sectional area taken laterally in a direction perpendicular to the flow direction, wherein the second area is smaller than the first area and the finned coolant passages are located downstream from the main coolant passage; a branch fluidly connecting the main coolant passage with the finned coolant passage, wherein the branch is oriented such that a fluid is turned 90° or more when passing into the branch from the main coolant passage; and a coolant bypass passage in fluid communication with the main coolant passage to form a continuous straight passage located fluidically parallel to the finned coolant passage.
A device for coating a surface of a product, comprising: means for providing a liquid comprising reagents required for coating; transport means (102, 104, 113; 130, 134) configured to effect a relative movement between a surface of the product to be coated and the liquid, while the surface of the product to be coated is in contact with the liquid such that the surface to be coated remains in contact with the liquid for a predetermined period of time so as to cause coating thereof, the transport means further being configured to effect the relative movement of the surface to be coated continuously and without reversing the direction of movement along a heated plate (113; 130; 134); characterized in that the heated plate (113; 130; 134) comprises bores implemented to generate an air cushion between the heated plate and the product on which the product is transported; and wherein the device is implemented to coat a band-shaped product on one side. means for providing a liquid comprising reagents required for coating; transport means (102, 104, 113; 130, 134) configured to effect a relative movement between a surface of the product to be coated and the liquid, while the surface of the product to be coated is in contact with the liquid such that the surface to be coated remains in contact with the liquid for a predetermined period of time so as to cause coating thereof, the transport means further being configured to effect the relative movement of the surface to be coated continuously and without reversing the direction of movement along a heated plate (113; 130; 134); characterized in that the heated plate (113; 130; 134) comprises bores implemented to generate an air cushion between the heated plate and the product on which the product is transported; and
A filter device comprising: a housing; a plurality of resonators inside the housing; a wall inside the housing between a first of the resonators and a second of the resonators, wherein an average thickness of the wall is 3.0 mm or thinner; an outer cover on the housing; adhesive tape that attaches the outer cover to the housing; a tuning cover between the resonators and the outer cover; and a plurality of cleaning holes in the tuning cover. a housing; a plurality of resonators inside the housing; a wall inside the housing between a first of the resonators and a second of the resonators, wherein an average thickness of the wall is 3.0 mm or thinner; an outer cover on the housing; adhesive tape that attaches the outer cover to the housing; a tuning cover between the resonators and the outer cover; and a plurality of cleaning holes in the tuning cover.
A thin-plate modular horseshoe-type permanent magnet rotor for a motor, the rotor comprising: a main shaft; a magnetically non-conductive shaft axially coupled to an outer circumference of the main shaft; an iron core circumferentially divided into four equal parts and coupled to an outer circumferential surface of the magnetically non-conductive shaft; first core fixing means for pressing and fixing both circumferential side ends of each part of the iron core to the magnetically non-conductive shaft along four boundaries of the iron core; magnets attached to an outer surface of the iron core in eight radial directions; a pole plate core circumferentially divided into four equal parts coupled to surround the magnets, wherein each part of the pole plate core is coupled to magnets attached in two radial directions to two adjacent parts of the iron core; second core fixing means for pressing and fixing both circumferential ends of each part of the pole plate core to the iron core, boundary guide pins consisting of plate members coupled to the iron core and the pole plate core to form a wall outside the first core fixing means in an axial direction. a main shaft; a magnetically non-conductive shaft axially coupled to an outer circumference of the main shaft; an iron core circumferentially divided into four equal parts and coupled to an outer circumferential surface of the magnetically non-conductive shaft; first core fixing means for pressing and fixing both circumferential side ends of each part of the iron core to the magnetically non-conductive shaft along four boundaries of the iron core; magnets attached to an outer surface of the iron core in eight radial directions; a pole plate core circumferentially divided into four equal parts coupled to surround the magnets, wherein each part of the pole plate core is coupled to magnets attached in two radial directions to two adjacent parts of the iron core; second core fixing means for pressing and fixing both circumferential ends of each part of the pole plate core to the iron core, boundary guide pins consisting of plate members coupled to the iron core and the pole plate core to form a wall outside the first core fixing means in an axial direction.
Radial turbomachine having a radial diffuser channel with a diaphragm, the main flow direction through which runs radially from the inside outward, a deflecting channel, which connects to the radial diffuser channel downstream thereof and the main flow direction through which is deflected from radially outward to radially inward, and a return flow channel, which connects to the deflecting channel downstream thereof and the main flow direction through which runs radially from the outside inward, wherein the diaphragm has a first outer surface section having a convex shape for delimiting the deflecting channel, wherein at least one consumption-gas removal channel, which opens into the deflecting channel, is provided in the diaphragm so that, if the main flow in the deflecting channel contains solid or liquid particles, consumption gas can be removed as a low-particulate gas of a main flow from said main flow through the consumption-gas removal channel, wherein the radial turbomachine has a return flow channel and an inner casing which is shaped and arranged in such a way that the inner casing, together with a third outer surface section of the diaphragm, forms the return flow channel, wherein at least one guide vane is arranged in the return flow channel, which guide vane bridges the return flow channel, characterized in that the consumption-gas removal channel is routed from the diaphragm to the inner casing.
A method of processing for alarm clearing for alarm occurred in an apparatus having a processor and a transceiver, characterized by comprising, at the processor: (a) receiving a hardware interrupt request for an alarm occurring from the transceiver when a parameter associated with the transceiver for the alarm exceeds a threshold value (S402, S502); (b) determining the parameter for the alarm (S404, S504); (c) obtaining a current value of the parameter from the transceiver by software polling (S408, S514); (d) obtaining the threshold value for the parameter from the transceiver by software polling (S410, S516); (e) determining whether the current value is below the threshold value (S412, S520, S522); and (f) processing an alarm clearing for the alarm when the current value is below the threshold value (S416, S524). (a) receiving a hardware interrupt request for an alarm occurring from the transceiver when a parameter associated with the transceiver for the alarm exceeds a threshold value (S402, S502); (b) determining the parameter for the alarm (S404, S504); (c) obtaining a current value of the parameter from the transceiver by software polling (S408, S514); (d) obtaining the threshold value for the parameter from the transceiver by software polling (S410, S516); (e) determining whether the current value is below the threshold value (S412, S520, S522); and (f) processing an alarm clearing for the alarm when the current value is below the threshold value (S416, S524).
An input generation system operable to generate motion data for a gaze tracking system, the system comprising: an input receiving unit operable to receive one or more non-gaze inputs; an input processing unit operable to generate motion data in dependence upon the received inputs, wherein the motion data comprises simulated gaze information; and an output unit operable to output the generated motion data, wherein the one or more inputs comprises information that is used to characterise the simulated gaze information, characterised in that the simulated gaze information comprises simulated eye motion for at least one eye. an input receiving unit operable to receive one or more non-gaze inputs; an input processing unit operable to generate motion data in dependence upon the received inputs, wherein the motion data comprises simulated gaze information; and an output unit operable to output the generated motion data, wherein the one or more inputs comprises information that is used to characterise the simulated gaze information, characterised in that the simulated gaze information comprises simulated eye motion for at least one eye.
Ship (1; 11) with a deckhouse as at least one superstructure, having an engine room with at least one driving engine and having at least one fuel tank for liquefied gas, wherein the fuel tank for liquefied gas is provided in the area of the deckhouse or a superstructure below the main deck of the ship (1; 11), wherein the fuel tank for liquefied gas is arranged as a tank that has been premanufactured outside of the ship in a fuel room which is provided directly adjacent to the engine room, characterised in that a) the fuel tank is designed as a type-C tank, b) a gas operation room is arranged directly adjacent to the fuel room, c) the fuel room, the gas operation room and the engine room are arranged directly adjacent to each other, d) the fuel tank has a connecting dome which is connected by connecting lines to the gas operation room arranged directly adjacent to the fuel room, e) the type-C tank with its connecting dome is arranged projecting into the gas operation room, f) the deckhouse is provided asymmetrically with respect to the ship's longitudinal axis with a free space towards the more distant ship's side, or the deckhouse has in the upper area a bridge arranged asymmetrically with respect to the ship's longitudinal axis at a distance from one side of the ship, h) at least one boil-off mast is provided to discharge hazardous fluid such as vaporised liquefied gas, and i) the boil-off mast is guided upwards, projecting over the deckhouse including bridge, in the outer area of the deckhouse or spaced apart from it in the free space. a) the fuel tank is designed as a type-C tank, b) a gas operation room is arranged directly adjacent to the fuel room, c) the fuel room, the gas operation room and the engine room are arranged directly adjacent to each other, d) the fuel tank has a connecting dome which is connected by connecting lines to the gas operation room arranged directly adjacent to the fuel room, e) the type-C tank with its connecting dome is arranged projecting into the gas operation room, f) the deckhouse is provided asymmetrically with respect to the ship's longitudinal axis with a free space towards the more distant ship's side, or the deckhouse has in the upper area a bridge arranged asymmetrically with respect to the ship's longitudinal axis at a distance from one side of the ship, h) at least one boil-off mast is provided to discharge hazardous fluid such as vaporised liquefied gas, and i) the boil-off mast is guided upwards, projecting over the deckhouse including bridge, in the outer area of the deckhouse or spaced apart from it in the free space.