mhurhangee/ep-ind-claims huggingface dataset:
An additive supply device for an internal combustion engine, comprising: a tank that stores additive; a pump that delivers the additive in the tank; a supply passage through which the additive delivered from the pump is supplied to an exhaust passage of the internal combustion engine; a tank heating section that heats the additive in the tank; a pump heating section that heats the additive in the pump; a passage heating section that heats the additive in the supply passage; a pressure detecting section that detects the pressure of the additive in the supply passage; a remaining amount detecting section that detects a remaining amount of the additive in the tank; a heating controller (80, 300) that is configured to exert heating control of the tank heating section, the pump heating section, and the passage heating section; and a signal output section, wherein, in a case in which the pump is configured to be operated to supply the additive to the exhaust passage after the heating control of the tank heating section, the pump heating section, and the passage heating section is started, characterized in that the signal output section is configured to output a signal indicating an abnormality in the tank heating section if the additive pressure detected by the pressure detecting section is reduced during supply of the additive and the additive remaining amount detected by the remaining amount detecting section indicates the presence of the additive remaining in the tank. a tank that stores additive; a pump that delivers the additive in the tank; a supply passage through which the additive delivered from the pump is supplied to an exhaust passage of the internal combustion engine; a tank heating section that heats the additive in the tank; a pump heating section that heats the additive in the pump; a passage heating section that heats the additive in the supply passage; a pressure detecting section that detects the pressure of the additive in the supply passage; a remaining amount detecting section that detects a remaining amount of the additive in the tank; a heating controller (80, 300) that is configured to exert heating control of the tank heating section, the pump heating section, and the passage heating section; and a signal output section, wherein, in a case in which the pump is configured to be operated to supply the additive to the exhaust passage after the heating control of the tank heating section, the pump heating section, and the passage heating section is started, characterized in that the signal output section is configured to output a signal indicating an abnormality in the tank heating section if the additive pressure detected by the pressure detecting section is reduced during supply of the additive and the additive remaining amount detected by the remaining amount detecting section indicates the presence of the additive remaining in the tank.
A method, comprising: determining a block error rate of a multicast channel; determining a number of packets that serves as basis to compute the block error rate of the multicast channel;: encoding the number of packets using an uneven encoding format comprising a plurality of granularities and a plurality of number of packets thresholds differentiating the plurality of granularities, wherein the granularity increases as the number of packets increases, encoding the block error rate of the multicast channel independently from the number of packets; and transmitting together with the block error rate of the multicast channel the number of packets in a report to allow a network to evaluate the reliability of the block error rate of the multicast channel based on the number of packets. determining a block error rate of a multicast channel; determining a number of packets that serves as basis to compute the block error rate of the multicast channel;: encoding the number of packets using an uneven encoding format comprising a plurality of granularities and a plurality of number of packets thresholds differentiating the plurality of granularities, wherein the granularity increases as the number of packets increases, encoding the block error rate of the multicast channel independently from the number of packets; and transmitting together with the block error rate of the multicast channel the number of packets in a report to allow a network to evaluate the reliability of the block error rate of the multicast channel based on the number of packets. encoding the number of packets using an uneven encoding format comprising a plurality of granularities and a plurality of number of packets thresholds differentiating the plurality of granularities, wherein the granularity increases as the number of packets increases, encoding the block error rate of the multicast channel independently from the number of packets; and transmitting together with the block error rate of the multicast channel the number of packets in a report to allow a network to evaluate the reliability of the block error rate of the multicast channel based on the number of packets.
Underwater machine tool comprising a tool holder having a removable hub for receiving at least one rotating tool, such as a milling tool, a saw, a drill bit and the like, the tool holder having a preferably cylindrically formed carrier body for receiving the removable hub, which is formed from a hub flange for receiving tools and a hub ring protruding centrally from the hub flange, it being possible to arrange the preferably centrally formed hub ring on the carrier body and to arrange said ring to be releasable and lockable by means of a locking device, characterised in that the at least one locking device has, in the tool holder, an unlatching bolt received in a pressurisable chamber, and a blocking bolt aligned with the unlatching bolt is received in the hub ring and can preferably be biased at its end remote from the tool holder by a spring element and has, on its front end facing the tool holder, a latching bolt, which in a latching position engages in a latching formation on the carrier body and cooperates with a cam on the front end of the blocking bolt, said cam being formed in such a way that, when the unlatching piston is deployed in the hub direction under the pressurisation, the piston presses the blocking bolt into the hub ring and the latching bolt is moved out of the latching formation by the cam, in such a way that the removable hub is releasable from the tool holder.
A dish washing machine, comprising: a main body; a washing tank provided inside the main body; and a fixed nozzle assembly (320, 360) fixed in one side of the washing tank and configured to jet washing water, wherein the fixed nozzle assembly includes, a nozzle body having a jet nozzle configured to jet washing water; and a nozzle front cover combined with a front surface of the nozzle body, and wherein the nozzle front cover includes a guide rib provided to cover a combining portion formed between the combined nozzle front cover and the front surface of the nozzle body, to reduce introduction of a foreign substance into the combining portion of the nozzle front cover and the front surface of the nozzle body, characterised in that the guide rib is separated a predetermined interval from the nozzle body and covers at least a part of one side surface of the nozzle body. a main body; a washing tank provided inside the main body; and a fixed nozzle assembly (320, 360) fixed in one side of the washing tank and configured to jet washing water, wherein the fixed nozzle assembly includes, a nozzle body having a jet nozzle configured to jet washing water; and a nozzle front cover combined with a front surface of the nozzle body, and wherein the nozzle front cover includes a guide rib provided to cover a combining portion formed between the combined nozzle front cover and the front surface of the nozzle body, to reduce introduction of a foreign substance into the combining portion of the nozzle front cover and the front surface of the nozzle body, characterised in that the guide rib is separated a predetermined interval from the nozzle body and covers at least a part of one side surface of the nozzle body.
A needle shield remover, comprising: a needle cap; a carrier sheath (6.2) axially slidably disposed in the needle cap and adapted to engage a needle shield disposed on a needle; and a grip (6.1), characterized in that the grip (6.1) is transversely slidably disposed in the needle cap and adapted to engage the carrier sheath (6.2) along an abutting surface angled relative to a central axis of the needle cap to displace the carrier sheath (6.2) and the needle shield axially relative to the needle cap. a needle cap; a carrier sheath (6.2) axially slidably disposed in the needle cap and adapted to engage a needle shield disposed on a needle; and a grip (6.1), characterized in that the grip (6.1) is transversely slidably disposed in the needle cap and adapted to engage the carrier sheath (6.2) along an abutting surface angled relative to a central axis of the needle cap to displace the carrier sheath (6.2) and the needle shield axially relative to the needle cap.
A method of forming a silicon material for use in anodes of batteries, the method comprising: reacting a metal or a mixture of multiple metals with silicon (Si) in a solid state reaction to form a metal silicide; performing a CO 2 -thermic oxidation process on the formed metal silicide with carbon dioxide to form a composite of one or more metal oxides, silicon, and carbon; and contacting the formed composite of one or more metal oxides, silicon, and carbon with an acid to remove the one or more metal oxides from the composite to produce particles of the silicon material individually having: a crystalline silicon formed in the CO 2 -thermic oxidation process; and pores in the crystalline silicon, the pores corresponding to the removed metal oxide by the acid and having surfaces coated with the carbon from the performed CO 2 -thermic oxidation process, wherein reacting the metal or the mixture of multiple metals with silicon includes reacting one of magnesium (Mg), calcium (Ca), or barium (Ba) with silicon (Si); and performing the CO 2 -thermic oxidation process includes performing the CO 2 -termic oxidation process with one of magnesium silicide (Mg 2 Si), calcium (CaSi 2), and barium silicide (BaSi 2) and wherein in case Mg is present, Mg is at least 10 wt % more in excess of silicon. reacting a metal or a mixture of multiple metals with silicon (Si) in a solid state reaction to form a metal silicide; performing a CO 2 -thermic oxidation process on the formed metal silicide with carbon dioxide to form a composite of one or more metal oxides, silicon, and carbon; and contacting the formed composite of one or more metal oxides, silicon, and carbon with an acid to remove the one or more metal oxides from the composite to produce particles of the silicon material individually having: a crystalline silicon formed in the CO 2 -thermic oxidation process; and pores in the crystalline silicon, the pores corresponding to the removed metal oxide by the acid and having surfaces coated with the carbon from the performed CO 2 -thermic oxidation process,
A method of processing an image for diagnosing a cutaneous lesion using a cutaneous image, comprising the steps of: (a) obtaining a first detail image made by performing a first component separation filter, which is a first edge preserving smoothing filter configured to highlight a periphery of an edge of the cutaneous image, on a brightness component of the cutaneous image characterized by (b) obtaining a second detail image made by performing a second component separation filter, which is a second edge preserving smoothing filter configured to attenuate a periphery of an edge of the cutaneous image, on the brightness component of the cutaneous image, the second component separation filter having properties different from those of the first component separation filter; and (c) generating a third detail image based on the first detail image and the second detail image; (d) newly generating a third base image based on the third detail image; and (e) combining the third detail image with the third base image to restore a brightness component and generate a highlighted image. (a) obtaining a first detail image made by performing a first component separation filter, which is a first edge preserving smoothing filter configured to highlight a periphery of an edge of the cutaneous image, on a brightness component of the cutaneous image characterized by (b) obtaining a second detail image made by performing a second component separation filter, which is a second edge preserving smoothing filter configured to attenuate a periphery of an edge of the cutaneous image, on the brightness component of the cutaneous image, the second component separation filter having properties different from those of the first component separation filter; and (c) generating a third detail image based on the first detail image and the second detail image; (d) newly generating a third base image based on the third detail image; and (e) combining the third detail image with the third base image to restore a brightness component and generate a highlighted image.
A method for manufacturing a laminate of mutually stacked metal parts (10; 11) by means of a multi-layer blanking process, wherein in the multi-layer blanking process successively several layered sets (16; 16-1, 16-2, 16-s) of such metal parts (10; 11) are cut from a layered basic material, in which subsequently the laminate is assembled from several such sets (16; 16-1, 16-2, 16-s) of the metal parts (10; 11), by stacking these, and in which, prior to the multi-layer blanking process, the individual layers of the layered basic material are interconnected by plastically deforming them, whereby a bulge is formed on the layered basic material within the outer circumference of the, still to be cut, metal parts (10; 11), characterized in that the metal parts (10; 11) are provided with a hole that is cut in the multi-layer blanking process and that extends completely through the layered basic material and in that when the laminate is assembled, the bulge of a first set (16; 16-1) of the metal parts (10; 11) is inserted into the hole of a second set (16; 16-2) of the metal parts (10; 11).
Method for processing planar XPS or EBS plastic foam boards, the planar XPS or EBS plastic foam boards having: ▪ a front surface and a back surface opposite the front surface, ▪ an initial thickness (D 1) delimited by the front and back surface (11, 12), the method comprising the pressing of the planar XPS or EBS plastic foam boards in the thickness direction thereof and the pressing □ causing a reversible compression and an irreversible compression of the planar XPS or EBS plastic foam boards, the thickness being (D 3) immediately after the pressing operation and the thickness of the planar XPS or EBS plastic foam boards assuming the value (D 2) after the removal of the pressing surfaces, where (D 3) < (D 2) < (D 1). characterised in that the method comprises a heating of the supplied XPS or EBS plastic foam boards before the pressing, the heating of the XPS or EBS plastic foam boards being carried out in such a way that the XPS or EBS plastic foam boards have a surface temperature in a range between 50°C and 75°, and in that the foam cells are not destroyed by the pressing, but compressed and deformed. ▪ a front surface and a back surface opposite the front surface, ▪ an initial thickness (D 1) delimited by the front and back surface (11, 12), □ causing a reversible compression and an irreversible compression of the planar XPS or EBS plastic foam boards, the thickness being (D 3) immediately after the pressing operation and the thickness of the planar XPS or EBS plastic foam boards assuming the value (D 2) after the removal of the pressing surfaces, where (D 3) < (D 2) < (D 1).
A turbine, comprising: a turbine casing provided with a combustor for combusting fuel and generating combustion gas, the combustor having an inlet pipe penetrating the turbine casing so as to introduce the generated combustion gas into the turbine casing; a turbine rotor accommodated in the turbine casing, the turbine rotor being rotated by the combustion gas as a working fluid CO 2; stator blades provided in the turbine casing; rotor blades provided at the turbine rotor, the working fluid CO 2 being supplied to the rotor blades and stator blades after flowing in the inlet pipe of the combustor; and a sleeve provided at the turbine casing, and accommodating the inlet pipe therein, wherein the sleeve is thicker than the inlet pipe, and a cooling fluid CO 2 whose temperature is lower than the working fluid CO 2 and whose pressure is higher than the working fluid CO 2, is introduced from outside of the turbine casing into a cooling fluid passage between an outer peripheral surface of the inlet pipe and an inner peripheral surface of the sleeve and the rotor blades and the stator blades are cooled by the cooling fluid CO 2 which is supplied after it flows between the inlet pipe and the sleeve. a turbine casing provided with a combustor for combusting fuel and generating combustion gas, the combustor having an inlet pipe penetrating the turbine casing so as to introduce the generated combustion gas into the turbine casing; a turbine rotor accommodated in the turbine casing, the turbine rotor being rotated by the combustion gas as a working fluid CO 2; stator blades provided in the turbine casing; rotor blades provided at the turbine rotor, the working fluid CO 2 being supplied to the rotor blades and stator blades after flowing in the inlet pipe of the combustor; and a sleeve provided at the turbine casing, and accommodating the inlet pipe therein, wherein the sleeve is thicker than the inlet pipe, and a cooling fluid CO 2 whose temperature is lower than the working fluid CO 2 and whose pressure is higher than the working fluid CO 2, is introduced from outside of the turbine casing into a cooling fluid passage between an outer peripheral surface of the inlet pipe and an inner peripheral surface of the sleeve and the rotor blades and the stator blades are cooled by the cooling fluid CO 2 which is supplied after it flows between the inlet pipe and the sleeve.
Instrument for penetrating an anatomical structure, in particular a bony structure, having a lateral surface and a distal end, the penetration instrument comprising an exploration device for monitoring penetration of the penetration instrument in the anatomical structure, the device comprising: - at least two electrodes (3, 4) disposed on the penetration instrument, - a voltage source supplying said electrodes (3, 4) and - a means for measuring impedance between said electrodes (3, 4), - an angular locating means formed by at least one of said electrodes being locally flush, i.e. partially and discontinuously, with a peripheral surface of said penetration instrument, - a means for locating the position of said at least one electrode, wherein the flushing electrode has a contact surface locally flush, i.e. partially and discontinuously, with the lateral surface of the penetration instrument, the contact surface of said flushing electrode, being in a position offset from a longitudinal axis of said instrument, the penetration instrument being characterised in that said at least two electrodes (3, 4) comprise a plurality of aligned electrodes (3, 4, 7, 8, 9) as an angular locating means, said aligned electrodes (3, 4, 7, 8, 9) being fixed and angularly spaced, and in that the impedance measuring means supplies a corresponding signal to each of said flushing electrodes (3, 4, 7, 8,9). - at least two electrodes (3, 4) disposed on the penetration instrument, - a voltage source supplying said electrodes (3, 4) and - a means for measuring impedance between said electrodes (3, 4), - an angular locating means formed by at least one of said electrodes being locally flush, i.e. partially and discontinuously, with a peripheral surface of said penetration instrument, - a means for locating the position of said at least one electrode,
Compound of formula 1 wherein X is selected from O, S or Se; R 1 and R 2 are independently selected from the group consisting of C 6 to C 18 aryl group and C 5 to C 18 heteroaryl group, wherein each of R 1 and R 2 may independently be unsubstituted or substituted with at least one C 1 to C 12 alkyl group or C 1 to C 12 alkoxy group, preferably C 1 to C 4 alkyl group or C 1 to C 4 alkoxy group; and each R 3, R 4, R 5, and R 6 are independently selected from the group consisting of H, C 1 to C 12 alkyl group or C 1 to C 12 alkoxy group, preferably H, C 1 to C 4 alkyl group or C 1 to C 4 alkoxy group. X is selected from O, S or Se; R 1 and R 2 are independently selected from the group consisting of C 6 to C 18 aryl group and C 5 to C 18 heteroaryl group, wherein each of R 1 and R 2 may independently be unsubstituted or substituted with at least one C 1 to C 12 alkyl group or C 1 to C 12 alkoxy group, preferably C 1 to C 4 alkyl group or C 1 to C 4 alkoxy group; and each R 3, R 4, R 5, and R 6 are independently selected from the group consisting of H, C 1 to C 12 alkyl group or C 1 to C 12 alkoxy group, preferably H, C 1 to C 4 alkyl group or C 1 to C 4 alkoxy group.
Use of a polymeric composition containing a polymer matrix and at least two mineral fillers of different types chosen from oxides, sulfates, carbonates, phosphates and silicates, uniformly dispersed in the polymer matrix, having properties of absorption and/or emission in the far infrared region ranging from 2 μ m to 20 μ m, for preventing or reducing wrinkles and/or age spots of the skin, characterized in that the polymeric composition is in the form of particles dispersed in a cosmetic composition.
A method for performing a reaction in a reverse flow reactor, comprising: reacting a fuel mixture comprising fuel, 0.1 vol% or more of O 2, and a diluent under combustion conditions in a combustion zone within a reverse flow reactor to form a flue gas and to heat a conversion zone to an average conversion zone temperature of 400°C or more, the conversion zone comprising a catalyst composition; and exposing a reactant stream comprising 5.0 vol% to 50 vol% CO 2, 20 vol% or more H 2, and a ratio of H 2 to CO 2 of 2.0 or more, to the catalyst composition in the conversion zone under reverse water gas shift reaction conditions to form a product stream comprising H 2 O and CO, a direction of flow for the reactant stream within the reaction zone being reversed relative to a direction of flow for the fuel mixture.
A system comprising a preform and a mould for producing a bottle, the preform comprising: - a neck finish (N.F.) comprising a support ledge (S.L.), a thread and a sealing ring (S.R.); - an area under the support ledge (U.S.L.); and - a body preform; - wherein the internal profile of the preform has a diameter reduction, - wherein the external profile of the preform is tangentially connected in the area under the support ledge to the lower part of the support ledge forming a one fourth of a ring; the system being characterized in - the diameter reduction starting downwardly from the neck at a level that is higher than the level of the support ledge (S.L.); and - wherein the mould in the area corresponding to the area under the support ledge has a concave ring that partially follows the profile of the preform in the area under the support ledge (U.L.S.). - a neck finish (N.F.) comprising a support ledge (S.L.), a thread and a sealing ring (S.R.); - an area under the support ledge (U.S.L.); and - a body preform; - wherein the internal profile of the preform has a diameter reduction, - wherein the external profile of the preform is tangentially connected in the area under the support ledge to the lower part of the support ledge forming a one fourth of a ring; - the diameter reduction starting downwardly from the neck at a level that is higher than the level of the support ledge (S.L.); and - wherein the mould in the area corresponding to the area under the