mhurhangee/ep-ind-claims huggingface dataset:
A direct-current interrupter comprising: a current-carrying path comprising a first switch and a second switch connected in series and a resistor connected in parallel to the second switch, the first switch having a predetermined first withstand voltage property and switching between conduction and non-conduction of current by using no semiconductor switch, the second switch having a second withstand voltage property lower in withstand voltage property than the first withstand voltage property and switching between conduction and non-conduction of current by using no semiconductor switch, and the resistor protecting the second switch from a voltage to be applied to the second switch; and a current-interrupting path connected in parallel to the current-carrying path and comprising a semiconductor switch and a current source connected in series and a non-linear resistor connected in parallel to a series connection of the semiconductor switch and the current source. a current-carrying path comprising a first switch and a second switch connected in series and a resistor connected in parallel to the second switch, the first switch having a predetermined first withstand voltage property and switching between conduction and non-conduction of current by using no semiconductor switch, the second switch having a second withstand voltage property lower in withstand voltage property than the first withstand voltage property and switching between conduction and non-conduction of current by using no semiconductor switch, and the resistor protecting the second switch from a voltage to be applied to the second switch; and a current-interrupting path connected in parallel to the current-carrying path and comprising a semiconductor switch and a current source connected in series and a non-linear resistor connected in parallel to a series connection of the semiconductor switch and the current source.
A handover method in satellite communications that uses a satellite constellation in a non-geosynchronous satellite orbit -based communications system, comprising: obtaining, by a terminal device, ephemeris information of first satellite base stations, wherein the first satellite base stations are satellite base stations that cover the terminal device; wherein the ephemeris information includes an angle of inclination of an orbital plane of the satellite, a right ascension of an ascending node, a semi-major axis of an orbital ellipse, an eccentricity of the orbital ellipse, an angular distance of a perigee, a moment at which the satellite passes the perigee; determining, by the terminal device based on the ephemeris information, a destination satellite base station to which the terminal device needs to hand over; determining, by the terminal device based on the determined destination satellite base station, a first time at which the terminal device is to hand over to the destination satellite base station; and handing over, by the terminal device based on the determined first time, to a destination cell served by the destination satellite base station. obtaining, by a terminal device, ephemeris information of first satellite base stations, wherein the first satellite base stations are satellite base stations that cover the terminal device; wherein the ephemeris information includes an angle of inclination of an orbital plane of the satellite, a right ascension of an ascending node, a semi-major axis of an orbital ellipse, an eccentricity of the orbital ellipse, an angular distance of a perigee, a moment at which the satellite passes the perigee; determining, by the terminal device based on the ephemeris information, a destination satellite base station to which the terminal device needs to hand over; determining, by the terminal device based on the determined destination satellite base station, a first time at which the terminal device is to hand over to the destination satellite base station; and handing over, by the terminal device based on the determined first time, to a destination cell served by the destination satellite base station.
A device for damping thermoacoustic oscillations in a combustion chamber, comprising a Helmholtz resonator, which has a resonating volume which is connectable with the combustion chamber comprising means for adjusting a flow (14,20) of cooling air into the resonator volume, wherein - cooling (14,20) air is introduced into the resonator volume through several openings (12A,12B) located on the resonator and whereby the cross-section of said openings (12A,12B) is adjustable so that the openings (12A,12B) can be completely closed in order to alter the number of effective openings. - cooling (14,20) air is introduced into the resonator volume through several openings (12A,12B) located on the resonator and whereby the cross-section of said openings (12A,12B) is adjustable so that the openings (12A,12B) can be completely closed in order to alter the number of effective openings.
An electromagnetic relay comprising: a fixed spring (32; 33) having a hole (32d; 33c) penetrating therethrough; a fixed contact (34; 35) inserted into the hole (32d; 33c); a movable spring; and a movable contact provided on the movable spring so as to make contact with the fixed contact (34; 35), characterised in that: a first surface (32b; 33a) of the fixed spring (32; 33) opposite a second surface thereof facing the movable spring has a recess (32e; 33d), the recess (32e; 33d) being formed in a stepped shape around an entire outer edge of the hole (32d; 33c), and a portion (34a; 35a), inserted into the hole (32d; 33c), of the fixed contact (34; 35) is swaged to extend in the recess (32e; 33d), so that the swaged portion (34a; 35a) of the fixed contact (34; 35) with the first surface (32b; 33a) of the fixed spring (32; 33) is flat, and so that the fixed contact (34; 35) is securely attached to the fixed spring (32; 33). a fixed spring (32; 33) having a hole (32d; 33c) penetrating therethrough; a fixed contact (34; 35) inserted into the hole (32d; 33c); a movable spring; and a movable contact provided on the movable spring so as to make contact with the fixed contact (34; 35), a first surface (32b; 33a) of the fixed spring (32; 33) opposite a second surface thereof facing the movable spring has a recess (32e; 33d), the recess (32e; 33d) being formed in a stepped shape around an entire outer edge of the hole (32d; 33c), and a portion (34a; 35a), inserted into the hole (32d; 33c), of the fixed contact (34; 35) is swaged to extend in the recess (32e; 33d), so that the swaged portion (34a; 35a) of the fixed contact (34; 35) with the first surface (32b; 33a) of the fixed spring (32; 33) is flat, and so that the fixed contact (34; 35) is securely attached to the fixed spring (32; 33).
An optical product comprising a composite coating, deposited on a substrate, that includes multiple bilayers having a first layer and a second layer, each provided with a binding group component which together form a complementary binding group pair, the multiple bilayers comprising, in sequence: at least one bilayer a) comprising in at least one of the first and second layer a first pigment or pigment blend that, when formed into a bilayer, exhibits a color reflection value that is less than about 2.5; at least one bilayer b) comprising in at least one of the first and second layer a pigment or pigment blend that, when formed into a bilayer, selectively blocks visible light in a wavelength range of interest; and at least one bilayer c) comprising in at least one of the first and second layer a second pigment or pigment blend that, when formed into a bilayer, exhibits a color reflection value that is less than about 2.5, and that may be the same as or different than the first pigment or pigment blend, wherein the optical product selectively blocks visible light in the wavelength range of interest, while exhibiting a color reflection value that is less than about 2.5, wherein the color reflection value is calculated from the formula sqrt[(a*) 2 + (b*) 2]. at least one bilayer a) comprising in at least one of the first and second layer a first pigment or pigment blend that, when formed into a bilayer, exhibits a color reflection value that is less than about 2.5; at least one bilayer b) comprising in at least one of the first and second layer a pigment or pigment blend that, when formed into a bilayer, selectively blocks visible light in a wavelength range of interest; and at least one bilayer c) comprising in at least one of the first and second layer a second pigment or pigment blend that, when formed into a bilayer, exhibits a color reflection value that is less than about 2.5, and that may be the same as or different than the first pigment or pigment blend, wherein the optical product selectively blocks visible light in the wavelength range of interest, while exhibiting a color reflection value that is less than about 2.5, wherein the color reflection value is calculated from the formula sqrt[(a*) 2 + (b*) 2].
A personal care composition comprising: a) an effective amount of Zinc Pyrithione; b) an effective amount of an iron chelator or a material which chelates iron, wherein the iron chelator or a material which chelates iron is selected from the group consisting of EDDHMA Zinc salt, Maltol Zinc salt, EDDHA Zinc salt, Benzohydroxamic acid Zinc salt, Thiomaltol Zinc salt and 1,2-Dimethyl-3-hydroxy-4-pyridone Zinc salt; wherein the Zinc salt of EDDHA and EDDHMA has a stoichiometry zinc to ligand of 1:1 or 2:1; wherein EDDHA is selected from the group consisting of o,o-EDDHA (ethylenediamine-N,N'-di(2-hydroxyphenyl acetic acid), and o,p-EDDHA (ethylenediamine-N-(2-hydroxyphenyl acetic acid)-N' -(4-hydroxyphenylacetic acid)); wherein EDDHMA is selected from the group consisting of o,o-EDDHMA (ethylenediamine-N,N' -di(2-hydroxy-4-methylphenyl acetic acid)), and o,o'-EDDHMA (ethylenediamine-N -(2-hydroxy -4-methylphenyl acetic acid)-N' -(2-hydroxy-6-methylphenylacetic acid)); wherein the combination of the iron chelator and the pyrithione or a polyvalent metal salt of a pyrithione has a fractional inhibitor concentration of less than or equal to 0.5 according to the Fractional Inhibitor Concentration Test Method as disclosed herein in the present application. a) an effective amount of Zinc Pyrithione; b) an effective amount of an iron chelator or a material which chelates iron, wherein the iron chelator or a material which chelates iron is selected from the group consisting of EDDHMA Zinc salt, Maltol Zinc salt, EDDHA Zinc salt, Benzohydroxamic acid Zinc salt, Thiomaltol Zinc salt and 1,2-Dimethyl-3-hydroxy-4-pyridone Zinc salt; wherein the Zinc salt of EDDHA and EDDHMA has a stoichiometry zinc to ligand of 1:1 or 2:1; wherein EDDHA is selected from the group consisting of o,o-EDDHA (ethylenediamine-N,N'-di(2-hydroxyphenyl acetic acid), and o,p-EDDHA (ethylenediamine-N-(2-hydroxyphenyl acetic acid)-N' -(4-hydroxyphenylacetic acid)); wherein EDDHMA is selected from the group consisting of o,o-EDDHMA (ethylenediamine-N,N' -di(2-hydroxy-4-methylphenyl acetic acid)), and o,o'-EDDHMA (ethylenediamine-N -(2-hydroxy -4-methylphenyl acetic acid)-N' -(2-hydroxy-6-methylphenylacetic acid)); wherein the combination of the iron chelator and the pyrithione or a polyvalent metal salt of a pyrithione has a fractional inhibitor concentration of less than or equal to 0.5 according to the Fractional Inhibitor Concentration Test Method as disclosed herein in the present application.
A two-shaft gas turbine comprising: a compressor having an intake equipped with an inlet guide vane; a combustor having a plurality of fuel systems capable of being supplied with fuels independently of one another and generating combustion gas by combusting the fuels from the fuel systems and air compressed by the compressor; a high-pressure turbine coupled coaxially with the compressor and rotated by the combustion gas from the combustor to drive the compressor; a low-pressure turbine having a shaft structure independent of the high-pressure turbine and rotated by exhaust gas from the high-pressure turbine to drive a load; an air extraction channel for extracting the air compressed by the compressor to outside the gas turbine; an injection flow channel for feeding the air extracted through the air extraction channel back to the combustor; and a controller configured to control a flow rate of the fuel supplied to each of the fuel systems based on an air flow rate of the compressor, on a flow rate of the fuel supplied to the combustor, and on a temperature of the air in the injection flow channel wherein, at the time of start-up that is a stage of operation at partial rotating speed under no load condition of the gas turbine, the controller controls a timing at which a fuel system starting to be supplied anew with the fuel is added from among the fuel systems based on the air flow rate of the compressor, on the flow rate of the fuel supplied to the combustor, and on the temperature of the air in the injection flow channel. a compressor having an intake equipped with an inlet guide vane; a combustor having a plurality of fuel systems capable of being supplied with fuels independently of one another and generating combustion gas by combusting the fuels from the fuel systems and air compressed by the compressor; a high-pressure turbine coupled coaxially with the compressor and rotated by the combustion gas from the combustor to drive the compressor; a low-pressure turbine having a shaft structure independent of the high-pressure turbine and rotated by exhaust gas from the high-pressure turbine to drive a load; an air extraction channel for extracting the air compressed by the compressor to outside the gas turbine; an injection flow channel for feeding the air extracted through the air extraction channel back to the combustor; and a controller configured to control a flow rate of the fuel supplied to each of the fuel systems based on an air flow rate of the compressor, on a flow rate of the fuel supplied to the combustor, and on a temperature of the air in the injection flow channel wherein, at the time of start-up that is a stage of operation at partial rotating speed under no load condition of the gas turbine, the controller controls a timing at which a fuel system starting to be supplied anew with the fuel is added from among the fuel systems based on the air flow rate of the compressor, on the flow rate of the fuel supplied to the combustor, and on the temperature of the air in the injection flow channel.
A method of wireless communication by a core network entity, comprising: by the core network entity, sending a request for a device identifier of a user equipment, UE, to the UE; by the core network entity, receiving a response message including the device identifier of the UE from the UE using a security association established between the UE and the core network entity, wherein the security association is established during an authentication and tunnel setup procedure between the UE and the core network entity; and by the core network entity, determining to maintain, establish, terminate or prevent a connection between the UE and a core network through wireless local area network, WLAN, access based on the device identifier of the UE included in the response message. by the core network entity, sending a request for a device identifier of a user equipment, UE, to the UE; by the core network entity, receiving a response message including the device identifier of the UE from the UE using a security association established between the UE and the core network entity, wherein the security association is established during an authentication and tunnel setup procedure between the UE and the core network entity; and by the core network entity, determining to maintain, establish, terminate or prevent a connection between the UE and a core network through wireless local area network, WLAN, access based on the device identifier of the UE included in the response message.
Edible pourable water-in-oil emulsion suitable for shallow frying comprising: • 40 to 90 wt. % liquid oil; • 5 to 55 wt. % of water; • 1 to 20 wt. % of plant sterol esters; • 0.5 to 8 wt. % of hardstock fat; • 0.05 to 5 wt. % of sodium chloride, potassium chloride or a combination thereof; • one or more coloring agents; • 0.01 to 3 wt. % of water-in-oil promoting emulsifier. • 40 to 90 wt. % liquid oil; • 5 to 55 wt. % of water; • 1 to 20 wt. % of plant sterol esters; • 0.5 to 8 wt. % of hardstock fat; • 0.05 to 5 wt. % of sodium chloride, potassium chloride or a combination thereof; • one or more coloring agents; • 0.01 to 3 wt. % of water-in-oil promoting emulsifier.
A resource allocation method, comprising: updating a fairness parameter at a current moment according to a fairness parameter at a previous moment, an edge-to-average ratio at the previous moment, and a preset critical value, wherein the edge-to-average ratio is a ratio of an average cell edge throughput to an average system throughput, and the fairness parameter is not less than zero; obtaining, according to average user throughputs of users at the previous moment, the fairness parameter at the current moment, and channel conditions of the users at the current moment, an allocation scheme that maximizes system utility; and performing resource allocation according to the allocation scheme that maximizes the system utility, so that the edge-to-average ratio at the current moment is closer to the preset critical value when compared with the edge-to-average ratio at the previous moment. updating a fairness parameter at a current moment according to a fairness parameter at a previous moment, an edge-to-average ratio at the previous moment, and a preset critical value, wherein the edge-to-average ratio is a ratio of an average cell edge throughput to an average system throughput, and the fairness parameter is not less than zero; obtaining, according to average user throughputs of users at the previous moment, the fairness parameter at the current moment, and channel conditions of the users at the current moment, an allocation scheme that maximizes system utility; and performing resource allocation according to the allocation scheme that maximizes the system utility, so that the edge-to-average ratio at the current moment is closer to the preset critical value when compared with the edge-to-average ratio at the previous moment.
Insert for a mould for vulcanising tyres for vehicle wheels, comprising: - a main body arranged to be received in a seat formed on a moulding surface of said mould, - a base surface arranged to integrate said moulding surface in the region of said seat when said main body is received in said seat, - a plurality of projections and/or recesses formed on said base surface on the opposite side to said main body, wherein at least one part of said base surface and of said plurality of projections and/or recesses is defined on a plate removably applied to said main body, characterized in that a ridge is defined along a perimeter edge of said main body facing said plate, on which ridge a peripheral rim of said plate is supported. - a main body arranged to be received in a seat formed on a moulding surface of said mould, - a base surface arranged to integrate said moulding surface in the region of said seat when said main body is received in said seat, - a plurality of projections and/or recesses formed on said base surface on the opposite side to said main body, wherein at least one part of said base surface and of said plurality of projections and/or recesses is defined on a plate removably applied to said main body, characterized in that a ridge is defined along a perimeter edge of said main body facing said plate, on which ridge a peripheral rim of said plate is supported.
A system for delivering insufflation gas to a body cavity of a patient during a surgical procedure, comprising: a) an insufflator for delivering insufflation gas to the body cavity of a patient through a flow path and a recirculation pump communicating with the flow path, wherein the flow path is configured to communicate with a pneumatically sealed trocar; b) a vacuum source and a suction device connected to the vacuum source for removing solid, liquids and gases from the body cavity during the surgical procedure; c) a conduit providing communication between the vacuum source and the suction device; d) a flow meter communicating with the conduit for measuring an amount of gas flowing through the conduit that has been removed from the body cavity by use of the suction device; and e) a controller operatively connected to the flow meter for receiving a flow measurement from the flow meter to determine when the suction device is in use and an amount of insufflation gas needed to be delivered to the body cavity by the insufflator to compensate for the gas removed from the body cavity by the suction device, wherein the vacuum source is a vacuum pump communicating with the suction device through the conduit, and wherein the controller is adapted and configured to communicate with the recirculation pump to adjust an amount of gas circulating through the system by way of the pneumatically sealed trocar so as to maintain a stable pneumoperitoneum within the body cavity when the suction device is used during the surgical procedure, and wherein the vacuum pump is operatively connected to and controlled by the controller. a) an insufflator for delivering insufflation gas to the body cavity of a patient through a flow path and a recirculation pump communicating with the flow path, wherein the flow path is configured to communicate with a pneumatically sealed trocar; b) a vacuum source and a suction device connected to the vacuum source for removing solid, liquids and gases from the body cavity during the surgical procedure; c) a conduit providing communication between the vacuum source and the suction device; d) a flow meter communicating with the conduit for measuring an amount of gas flowing through the conduit that has been removed from the body cavity by use of the suction device; and e) a controller operatively connected to the flow meter for receiving a flow measurement from the flow meter to determine when the suction device is in use and an amount of insufflation gas needed to be delivered to the body cavity by the insufflator to compensate for the gas removed from the body cavity by the suction device, wherein the vacuum source is a vacuum pump communicating with the suction device through the conduit, and wherein the controller is adapted and configured to communicate with the recirculation pump to adjust an amount of gas circulating through the system by way of the pneumatically sealed trocar so as to maintain a stable pneumoperitoneum within the body cavity when the suction device is used during the surgical procedure, and wherein the vacuum pump is operatively connected to and controlled by the controller.