mhurhangee/patent-ind-claim-en huggingface dataset:
An injector assembly adapted to be disposed in a combustion stage of a combustion turbine engine, the combustion stage fluidly coupled to receive a cross-flow of combustion products , the injector assembly comprising: a reactant-guiding structure arranged to convey a flow of reactants to admix with the cross-flow of combustion products; and means for injecting a flow of air arranged to condition interaction of the flow of reactants with the cross-flow of combustion products, wherein the injector assembly is designed to generate a shielding flow of air to form a boundary of air flow that surrounds the flow of reactants , as the flow of reactants is admitted in the combustion stage, wherein the boundary of air flow that surrounds the flow of reactants is effective to transitorily shield the flow of reactants conveyed to the combustion stage from the cross-flow of combustion products, and thus provide an ignition delay to the flow of reactants injected into the combustion stage, an injector assembly body comprising an inner wall and an outer wall that define a passageway having an inlet side and an outlet side , the passageway defined by the inner wall and the outer wall of the injector assembly body effective to inject the flow of air into the combustion stage, characterized in that the outlet side of the passageway comprises a varying cross-sectional profile along a perimeter of the outlet side of the passageway so that a velocity and a volume of the flow of air have a desired variation along the perimeter of the outlet side of the passageway. a reactant-guiding structure arranged to convey a flow of reactants to admix with the cross-flow of combustion products; and means for injecting a flow of air arranged to condition interaction of the flow of reactants with the cross-flow of combustion products, wherein the injector assembly is designed to generate a shielding flow of air to form a boundary of air flow that surrounds the flow of reactants , as the flow of reactants is admitted in the combustion stage, wherein the boundary of air flow that surrounds the flow of reactants is effective to transitorily shield the flow of reactants conveyed to the combustion stage from the cross-flow of combustion products, and thus provide an ignition delay to the flow of reactants injected into the combustion stage, an injector assembly body comprising an inner wall and an outer wall that define a passageway having an inlet side and an outlet side , the passageway defined by the inner wall and the outer wall of the injector assembly body effective to inject the flow of air into the combustion stage, characterized in that the outlet side of the passageway comprises a varying cross-sectional profile along a perimeter of the outlet side of the passageway so that a velocity and a volume of the flow of air have a desired variation along the perimeter of the outlet side of the passageway.
A footwear scanning system comprising: a platform configured to contact footwear to be scanned; an antenna array configured to transmit electromagnetic waves through the platform into the footwear and to receive electromagnetic waves from the footwear and the platform ; a transceiver coupled with antennas of the antenna array and configured to apply electrical signals to at least one of the antennas to generate the transmitted electromagnetic waves and to receive electrical signals from at least another of the antennas corresponding to the electromagnetic waves received by the another of the antennas; processing circuitry configured to process the received electrical signals from the transceiver to provide information regarding contents within the footwear; and characterized in that the platform comprises a conformal support surface configured to contact and support soles of the footwear and to conform to different surface features of the soles of the footwear ; and wherein the conformal support surface comprises a retention layer over a plurality of movable members . a platform configured to contact footwear to be scanned; an antenna array configured to transmit electromagnetic waves through the platform into the footwear and to receive electromagnetic waves from the footwear and the platform ; a transceiver coupled with antennas of the antenna array and configured to apply electrical signals to at least one of the antennas to generate the transmitted electromagnetic waves and to receive electrical signals from at least another of the antennas corresponding to the electromagnetic waves received by the another of the antennas; processing circuitry configured to process the received electrical signals from the transceiver to provide information regarding contents within the footwear; and characterized in that the platform comprises a conformal support surface configured to contact and support soles of the footwear and to conform to different surface features of the soles of the footwear ; and
An additive composition for silica compounded rubber composition comprising a glycerin fatty acid ester, wherein: the glycerin fatty acid ester is an ester of a glycerin and two or more fatty acids, a fatty acid component which is the most among the two or more fatty acids constituting the glycerin fatty acid ester being 10 to 90 mass% of all fatty acids; and a monoester component is contained in an amount of 85 to 98 mass% in the glycerin fatty acid ester. the glycerin fatty acid ester is an ester of a glycerin and two or more fatty acids, a fatty acid component which is the most among the two or more fatty acids constituting the glycerin fatty acid ester being 10 to 90 mass% of all fatty acids; and a monoester component is contained in an amount of 85 to 98 mass% in the glycerin fatty acid ester.
A method of performing fractional subframe transmission in a wireless communication system, comprising: in response to detecting that a channel becomes available; performing the fractional subframe transmission from a target position, wherein the target position is any one of at least one potential position predefined in a subframe, wherein each of the at least one potential position corresponds to a symbol of the subframe periodically. in response to detecting that a channel becomes available; performing the fractional subframe transmission from a target position, wherein the target position is any one of at least one potential position predefined in a subframe, wherein each of the at least one potential position corresponds to a symbol of the subframe periodically.
An air conditioner, comprising: an outdoor unit comprising an enhanced vapor compression mechanism and an outdoor heat exchanger; an indoor unit comprising a first heat exchanger and a first throttle regulator ; a discharge pipe connected to a discharge side of the compression mechanism, a low-pressure suction pipe connected to a low-pressure suction side of the compression mechanism, a first piping connecting the discharge pipe , the outdoor heat exchanger, the first throttle regulator , and the first heat exchanger in sequence, and a second piping connecting the first heat exchanger and the low-pressure suction pipe , thus forming a refrigerant circuit; a first switching device capable of switching between: a first switching state of the first switching device , in which the first switching device causes the first piping to communicate with the suction pipe and causes the second piping to communicate with the discharge pipe ; and a second switching state of the first switching device , in which the first switching device causes the first piping to communicate with the discharge pipe and causes the second piping to communicate with the suction pipe; and an economizer arranged on the first piping between the outdoor heat exchanger and the first throttle device; a first refrigerant flow path arranged in the economizer and connected to the first piping through a refrigerant bridge ; and a second refrigerant flow path arranged in the economizer , one end of the second refrigerant flow path communicating with the first piping through a liquid pickup pipe and the other end of the second refrigerant flow path communicating with both a medium-pressure suction port of the compressor and the suction pipe through a return pipe , wherein refrigerant flow directions in the first refrigerant flow path and the second refrigerant flow path are opposite; characterised in that the return pipe comprises a return pipe body, a first communication pipe , and a second communication pipe ; one end of the first communication pipe communicates with the return pipe body and the other end of the first communication pipe communicates with the medium-pressure suction port of the compressor ; the return pipe body or the first communication pipe is provided with a first control valve ; and one end of the second communication pipe communicates with the return pipe body and the other end of the second communication pipe communicates with the suction pipe, and the second communication pipe is provided with a second control valve .
A method comprising: applying a first light pulse to a hydrocarbon fluid sample at a first angle-of-incidence; detecting an intensity of a first fluorescence emission as the intensity of the first fluorescence emission fades; applying a second light pulse to the hydrocarbon fluid sample at a second angle-of-incidence different from the first angle-of-incidence; detecting an intensity of a second fluorescence emission as the intensity of the second fluorescence emission fades; comparing , by a processor, the fading of the first fluorescence emission with the fading of the second fluorescence emission; and determining a specific gravity of the hydrocarbon fluid sample based on a ratio calculated based on a comparison of the fading of the first fluorescence emission and the fading of the second fluorescence emission. applying a first light pulse to a hydrocarbon fluid sample at a first angle-of-incidence; detecting an intensity of a first fluorescence emission as the intensity of the first fluorescence emission fades; applying a second light pulse to the hydrocarbon fluid sample at a second angle-of-incidence different from the first angle-of-incidence; detecting an intensity of a second fluorescence emission as the intensity of the second fluorescence emission fades; comparing , by a processor, the fading of the first fluorescence emission with the fading of the second fluorescence emission; and determining a specific gravity of the hydrocarbon fluid sample based on a ratio calculated based on a comparison of the fading of the first fluorescence emission and the fading of the second fluorescence emission.
An aerosol generation device comprising: a heater configured to heat an outer periphery of a smoking article comprising an aerosol source, and a control part configured to control the heater ; wherein the control part is configured to control the heater in such a manner that a delivery profile of aerosol in a predetermined suction allowable period comprises one or more maximum values in a period between a start point (T2) and an end point (T7) in the suction allowable period, wherein the smoking article comprises an aerosol existing region including the aerosol source, and an aerosol non-existing region positioned downstream the aerosol existing region in the direction of flow of generated aerosol; characterized in that , when the smoking article is inserted into the aerosol generation device , a heating part of the heater is arranged to extend from the aerosol existing region of the smoking article to the aerosol non-existing region of the smoking article . a heater configured to heat an outer periphery of a smoking article comprising an aerosol source, and a control part configured to control the heater ; wherein the control part is configured to control the heater in such a manner that a delivery profile of aerosol in a predetermined suction allowable period comprises one or more maximum values in a period between a start point (T2) and an end point (T7) in the suction allowable period, wherein the smoking article comprises an aerosol existing region including the aerosol source, and an aerosol non-existing region positioned downstream the aerosol existing region in the direction of flow of generated aerosol; characterized in that , when the smoking article is inserted into the aerosol generation device , a heating part of the heater is arranged to extend from the aerosol existing region of the smoking article to the aerosol non-existing region of the smoking article .
Method for generating decks of sheet elements , comprising the steps of positioning a set of numerous sheet elements onto a transport surface of a transport device one after another such that the sheet elements are partly overlapping with their adjacent sheet elements , wherein the transport device has a transport direction (T), and wherein the last sheet element of the set with respect to the transport direction (T) is positioned to be the lowermost sheet element of the set, and the other sheet elements being positioned so that their rear end lies onto the front ends of the sheet element being adjacent in counter-transport direction, so as to form a row (R) of overlapping sheet elements , moving the row (R) of overlapping sheet elements in the transport direction (T), and moving the overlapping sheet elements against a stop member , which is firstly contacted by the uppermost sheet element , until the lowermost sheet element is completely shifted underneath an adjacent sheet element , and wherein the stop member is moved in the transport direction (T) with a lower velocity than a velocity of the transport surface. positioning a set of numerous sheet elements onto a transport surface of a transport device one after another such that the sheet elements are partly overlapping with their adjacent sheet elements , wherein the transport device has a transport direction (T), and wherein the last sheet element of the set with respect to the transport direction (T) is positioned to be the lowermost sheet element of the set, and the other sheet elements being positioned so that their rear end lies onto the front ends of the sheet element being adjacent in counter-transport direction, so as to form a row (R) of overlapping sheet elements , moving the row (R) of overlapping sheet elements in the transport direction (T), and moving the overlapping sheet elements against a stop member , which is firstly contacted by the uppermost sheet element , until the lowermost sheet element is completely shifted underneath an adjacent sheet element , and wherein the stop member is moved in the transport direction (T) with a lower velocity than a velocity of the transport surface.
Diagnostic system for a lubrication circuit of an internal combustion engine of a vehicle, the system comprising: - a viscometer for detecting the viscosity of a lubricating liquid of the lubrication circuit, - a temperature sensor suitable for detecting the temperature of the lubricating liquid, - means for acquiring the date of last replacement of the lubricating liquid, - means for determining a condition of use of the engine , - a database capable of storing viscosity reference values for at least a given temperature of the lubricating liquid, a given date of last replacement of the lubricating liquid and a given condition of use of the engine , and - a control unit capable of acquiring the state of the lubricating liquid, given by the viscosity detected for a given lubricating liquid condition, which includes the lubricating liquid temperature and the date of last replacement of the lubricating liquid, and for a given condition of use of the engine , and capable of assessing the state of the lubricating liquid by comparing the detected viscosity of the lubricating liquid with the viscosity reference values stored in the database in the same or similar condition of lubricating liquid temperature, date of last replacement of the lubricating liquid and use of the engine , characterized in that the control unit is configured to autonomously activate an addition of additives to the lubricating liquid, said additives being dispensable by a suitable additive tank connected to the lubrication circuit. - a viscometer for detecting the viscosity of a lubricating liquid of the lubrication circuit, - a temperature sensor suitable for detecting the temperature of the lubricating liquid, - means for acquiring the date of last replacement of the lubricating liquid, - means for determining a condition of use of the engine , - a database capable of storing viscosity reference values for at least a given temperature of the lubricating liquid, a given date of last replacement of the lubricating liquid and a given condition of use of the engine , and - a control unit capable of acquiring the state of the lubricating liquid, given by the viscosity detected for a given lubricating liquid condition, which includes the lubricating liquid temperature and the date of last replacement of the lubricating liquid, and for a given condition of use of the engine , and capable of assessing the state of the lubricating liquid by comparing the detected viscosity of the lubricating liquid with the viscosity reference values stored in the database in the same or similar condition of lubricating liquid temperature, date of last replacement of the lubricating liquid and use of the engine ,
A method for defending against threats using an aerial defense system having a plurality of defensive aircraft , the method comprising the steps of: identifying a detected threat; identifying a first defensive aircraft from said plurality of defensive aircraft that is within a first predetermined distance of the detected threat; sending, via a targeting system, a launch command message to the first defensive aircraft , wherein the launch command message comprises a location and trajectory of the detected threat; steering the first defensive aircraft toward the detected threat under an external guidance mode; switching the first defensive aircraft from the external guidance mode to a local guidance mode when the first defensive aircraft is within a predetermined range of the detected threat, wherein the first defensive aircraft is configured to navigate during local guidance mode using an onboard sensor payload; and engaging the detected threat using the first defensive aircraft . identifying a detected threat; identifying a first defensive aircraft from said plurality of defensive aircraft that is within a first predetermined distance of the detected threat; sending, via a targeting system, a launch command message to the first defensive aircraft , wherein the launch command message comprises a location and trajectory of the detected threat; steering the first defensive aircraft toward the detected threat under an external guidance mode; switching the first defensive aircraft from the external guidance mode to a local guidance mode when the first defensive aircraft is within a predetermined range of the detected threat, wherein the first defensive aircraft is configured to navigate during local guidance mode using an onboard sensor payload; and engaging the detected threat using the first defensive aircraft .
An oral cavity washing device that washes an oral cavity with a liquid, the oral cavity washing device comprising: a housing ; a storage space having a tubular shape and being located in the housing , the storage space being configured to store the liquid; and a pump housed in the housing to discharge the liquid stored in the storage space , wherein the housing includes: a peripheral wall section constituting at least part of a peripheral wall of the storage space and having a supply port for supplying the liquid from outside the housing into the storage space ; and a lid disposed at one end of the storage space to be able to entirely open and close a largest opening that is larger in area than any other opening in the housing , characterized in that an inner peripheral surface of the storage space is formed into a conical shape such that a cross-sectional area orthogonal to the axial direction thereof gradually decreases with an advancement in the axial direction from the lid to a division top section positioned at the other end of the storage space . a housing ; a storage space having a tubular shape and being located in the housing , the storage space being configured to store the liquid; and a pump housed in the housing to discharge the liquid stored in the storage space , wherein the housing includes: a peripheral wall section constituting at least part of a peripheral wall of the storage space and having a supply port for supplying the liquid from outside the housing into the storage space ; and a lid disposed at one end of the storage space to be able to entirely open and close a largest opening that is larger in area than any other opening in the housing , characterized in that an inner peripheral surface of the storage space is formed into a conical shape such that a cross-sectional area orthogonal to the axial direction thereof gradually decreases with an advancement in the axial direction from the lid to a division top section positioned at the other end of the storage space . a peripheral wall section constituting at least part of a peripheral wall of the storage space and having a supply port for supplying the liquid from outside the housing into the storage space ; and a lid disposed at one end of the storage space to be able to entirely open and close a largest opening that is larger in area than any other opening in the housing , characterized in that an inner peripheral surface of the storage space is formed into a conical shape such that a cross-sectional area orthogonal to the axial direction thereof gradually decreases with an advancement in the axial direction from the lid to a division top section positioned at the other end of the storage space .
A composition that comprises 0.0001% to 1% of a SIRT6 activating peptide and 0.0001% - 0.05% of 8-Oxoguanine glycosylase, by weight of the composition, wherein the SIRT6 activating peptide is incorporated into the composition in the form of yeast extract, with the peptide being a component of the extract and wherein the SIRT 6 activating peptide is (SEQ ID No. 1) G-A-G-V-S-A-E-NH 2 Gly-Ala-Gly-Val-Ser-Ala-Glu-NH 2 .
A surgical cassette manifold , comprising: a front housing , a rear housing , a gasket , and a tubing segment , wherein the gasket is coupled with the rear housing, and wherein upon assembly of the surgical cassette manifold, at least a portion of the gasket is located between the front housing and the rear housing, wherein the rear housing comprises a first lower tube connection and a second lower tube connection , wherein the first lower tube connection is configured and dimensioned to couple with a first end of the tubing segment and the second lower tube connection is configured and dimensioned to couple with a second end of the tubing segment thereby creating a first portion of a peristaltic pump, wherein the first lower tube connection and second lower tube connection have an in flow and out flow path on a same axis. a front housing , a rear housing , a gasket , and a tubing segment , wherein the gasket is coupled with the rear housing, and wherein upon assembly of the surgical cassette manifold, at least a portion of the gasket is located between the front housing and the rear housing, wherein the rear housing comprises a first lower tube connection and a second lower tube connection , wherein the first lower tube connection is configured and dimensioned to couple with a first end of the tubing segment and the second lower tube connection is configured and dimensioned to couple with a second end of the tubing segment thereby creating a first portion of a peristaltic pump, wherein the first lower tube connection and second lower tube connection have an in flow and out flow path on a same axis.