mhurhangee/patent-ind-claim-en huggingface dataset:
A method for manufacturing an electrochemical gas sensor for sensing a target gas, comprising the steps of - providing a substrate supporting an arrangement comprising a thin film of a thickness s ≤ 5μm arranged between a sensing electrode configured to chemically interact with the target gas and a reference electrode facing the substrate , wherein the thin film is selected from the group consisting of SixOy, SixNy, SiOxNy, Al2O3, BaZrO3, and LaAlO3, or any combination thereof, wherein the sensing electrode is porous at least for the target gas and comprises a compound selected from the group consisting of sodium salts, lithium salts, sodium hydroxides, and lithium hydroxides, wherein the thin film is an electronically non-conducting and ionically non-conducting ceramic or glass, - and heating the arrangement to an annealing temperature (T1) for irreversibly turning the thin film into an ionic conductor by incorporating mobile ions released from the sensing electrode in response to the heating. - providing a substrate supporting an arrangement comprising a thin film of a thickness s ≤ 5μm arranged between a sensing electrode configured to chemically interact with the target gas and a reference electrode facing the substrate , wherein the thin film is selected from the group consisting of SixOy, SixNy, SiOxNy, Al2O3, BaZrO3, and LaAlO3, or any combination thereof, wherein the sensing electrode is porous at least for the target gas and comprises a compound selected from the group consisting of sodium salts, lithium salts, sodium hydroxides, and lithium hydroxides, wherein the thin film is an electronically non-conducting and ionically non-conducting ceramic or glass, - and heating the arrangement to an annealing temperature (T1) for irreversibly turning the thin film into an ionic conductor by incorporating mobile ions released from the sensing electrode in response to the heating.
Method for producing a scintillator nanocomposite comprising nanoparticles with scintillating properties and a diameter between 10 and 50 nanometer and a first matrix material, said method comprising the steps of: - introducing the nanoparticles into 1,4-butanediol as a first dispersing medium to form a stable suspension, wherein the 1,4-butanediol is used both as a dispersing medium and as a precursor to the first matrix material; and - curing the dispersing medium to form the first matrix material without having to remove the dispersing medium. - introducing the nanoparticles into 1,4-butanediol as a first dispersing medium to form a stable suspension, wherein the 1,4-butanediol is used both as a dispersing medium and as a precursor to the first matrix material; and - curing the dispersing medium to form the first matrix material without having to remove the dispersing medium.
A method of controlling a machine comprising; obtaining one or more images of an object , at least part of which comprises a patterned marker having a detectable pattern arranged thereon; calculating the position and orientation of the object in space from the appearance of the patterned marker in the one or more images; and changing a position and orientation of the machine in accordance with the calculated position and orientation of the object in space; wherein calculating the position and orientation of the object in space comprises: generating a projected image of the patterned marker according to a mathematical model describing the patterned marker, imaging means and light rays travelling from the patterned marker to the imaging means; and matching the projected image of the patterned marker to the patterned marker in the one or more images of the object. obtaining one or more images of an object , at least part of which comprises a patterned marker having a detectable pattern arranged thereon; calculating the position and orientation of the object in space from the appearance of the patterned marker in the one or more images; and changing a position and orientation of the machine in accordance with the calculated position and orientation of the object in space; wherein calculating the position and orientation of the object in space comprises: generating a projected image of the patterned marker according to a mathematical model describing the patterned marker, imaging means and light rays travelling from the patterned marker to the imaging means; and matching the projected image of the patterned marker to the patterned marker in the one or more images of the object. generating a projected image of the patterned marker according to a mathematical model describing the patterned marker, imaging means and light rays travelling from the patterned marker to the imaging means; and matching the projected image of the patterned marker to the patterned marker in the one or more images of the object.
A tissue bonding implantation device , comprising: a drainage tube having an internal surface and an external surface; an inflatable balloon connected to the drainage tube , on the external surface of the drainage tube ; a balloon inflation conduit in fluid communication with the inflatable balloon , the balloon inflation conduit extends through the drainage tube from the inflatable balloon ; an external cap connected to the drainage tube and the balloon inflation conduit , the cap having a first sealable opening in fluid communication with the drainage tube and a second sealable opening in fluid communication with the balloon inflation conduit ; characterized in that the tissue bonding implantation device further comprises an anchor formed of a central cylinder connected to a flange , wherein the anchor includes a central channel through the central cylinder and an internal balloon inflation void along the central channel , wherein the internal balloon inflation void is configured so that when the inflatable balloon is lodged in the internal balloon inflation void and expanded via inflation through the second sealable opening of the external cap and the balloon inflation conduit the inflatable balloon fills the internal balloon inflation void and secures the inflatable balloon to the anchor , to retain the drainage tube with the anchor . a drainage tube having an internal surface and an external surface; an inflatable balloon connected to the drainage tube , on the external surface of the drainage tube ; a balloon inflation conduit in fluid communication with the inflatable balloon , the balloon inflation conduit extends through the drainage tube from the inflatable balloon ; an external cap connected to the drainage tube and the balloon inflation conduit , the cap having a first sealable opening in fluid communication with the drainage tube and a second sealable opening in fluid communication with the balloon inflation conduit ; characterized in that the tissue bonding implantation device further comprises an anchor formed of a central cylinder connected to a flange , wherein the anchor includes a central channel through the central cylinder and an internal balloon inflation void along the central channel , wherein the internal balloon inflation void is configured so that when the inflatable balloon is lodged in the internal balloon inflation void and expanded via inflation through the second sealable opening of the external cap and the balloon inflation conduit the inflatable balloon fills the internal balloon inflation void and secures the inflatable balloon to the anchor , to retain the drainage tube with the anchor .
An aerosol delivery device (10; 210; 310; 410) comprising: an airflow inlet (19; 242; 330; 414); a mouthpiece region having an outlet (20; 230; 331; 415), wherein the mouthpiece region is removably attached to the aerosol delivery device; an airflow passage extending between the airflow inlet and the outlet; a slot to receive a cartridge, wherein the cartridge includes a substance placed over a vapor element, wherein the vapor element comprising an electrically-resistive heating support configured to, when activated, vaporize the substance to produce a condensation aerosol; a battery to provide power; a microcontroller chip (428; 438) coupled to the battery to receive power and configured to regulate the vapor element, wherein, in response to each inhalation, the microcontroller chip is configured to activate the vapor element to release a respective dose of the condensation aerosol of the substance; characterised by : a USB connector or the like configured to draw power from an external device or an A/C power adapter to charge the battery; and an electrical contact configured to provide electrical communication between the microcontroller chip and the cartridge. an airflow inlet (19; 242; 330; 414); a mouthpiece region having an outlet (20; 230; 331; 415), wherein the mouthpiece region is removably attached to the aerosol delivery device; an airflow passage extending between the airflow inlet and the outlet; a slot to receive a cartridge, wherein the cartridge includes a substance placed over a vapor element, wherein the vapor element comprising an electrically-resistive heating support configured to, when activated, vaporize the substance to produce a condensation aerosol; a battery to provide power; a microcontroller chip (428; 438) coupled to the battery to receive power and configured to regulate the vapor element, wherein, in response to each inhalation, the microcontroller chip is configured to activate the vapor element to release a respective dose of the condensation aerosol of the substance; characterised by : a USB connector or the like configured to draw power from an external device or an A/C power adapter to charge the battery; and an electrical contact configured to provide electrical communication between the microcontroller chip and the cartridge. a USB connector or the like configured to draw power from an external device or an A/C power adapter to charge the battery; and an electrical contact configured to provide electrical communication between the microcontroller chip and the cartridge.
A composition comprising (i) a hydrofluorothermoplastic polymer, wherein the hydrofluorothermoplastic polymer is derived from: (a) 50-85 mol% tetrafluoroethene; (b) 2-15 mol% hexafluoropropene; (c) 10-35 mol% vinylidene fluoride; and (d) 0.1 to 5 mol% of a bromine-containing monomer; and (ii) a perhalogenated thermoplastic polymer having a melting point of 150 to 315 °C with the ratio of the hydrofluorothermoplastic polymer to the perhalogenated thermoplastic polymer on a mass to mass basis of 10:90 and 90:10. (i) a hydrofluorothermoplastic polymer, wherein the hydrofluorothermoplastic polymer is derived from: (a) 50-85 mol% tetrafluoroethene; (b) 2-15 mol% hexafluoropropene; (c) 10-35 mol% vinylidene fluoride; and (d) 0.1 to 5 mol% of a bromine-containing monomer; and (a) 50-85 mol% tetrafluoroethene; (b) 2-15 mol% hexafluoropropene; (c) 10-35 mol% vinylidene fluoride; and (d) 0.1 to 5 mol% of a bromine-containing monomer; and (ii) a perhalogenated thermoplastic polymer having a melting point of 150 to 315 °C with the ratio of the hydrofluorothermoplastic polymer to the perhalogenated thermoplastic polymer on a mass to mass basis of 10:90 and 90:10.
An optical connector comprising: a housing having a first end and a second end positioned at opposite ends of an optical axis of the housing; a chamber disposed in an interior volume of the housing such that the optical axis of the housing passes through the chamber, a light source coupled to the first end of the housing wherein, when the light source is powered on, divergent light from the light source propagates through the chamber; characterised in that the chamber tapers from the first end of the housing to the second end of the housing such that a first diameter of the chamber at the first end of the housing is larger than a second diameter of the chamber at the second end of the housing; and the chamber has a reflecting material positioned on a sidewall of the chamber so that the divergent light from the light source that propagates through the chamber is reflected by the reflecting material to concentrate the light proximate the second end of the housing. a housing having a first end and a second end positioned at opposite ends of an optical axis of the housing; a chamber disposed in an interior volume of the housing such that the optical axis of the housing passes through the chamber, a light source coupled to the first end of the housing wherein, when the light source is powered on, divergent light from the light source propagates through the chamber; characterised in that the chamber tapers from the first end of the housing to the second end of the housing such that a first diameter of the chamber at the first end of the housing is larger than a second diameter of the chamber at the second end of the housing; and the chamber has a reflecting material positioned on a sidewall of the chamber so that the divergent light from the light source that propagates through the chamber is reflected by the reflecting material to concentrate the light proximate the second end of the housing.
"Cold-walls"-type combustion chamber fitted with a burner comprising at least one oxidant inlet and at least one fuel inlet , the oxidant and fuel inlets opening separately into the chamber at a distance suitable for establishing combustion which is highly diluted by internal recirculation of the combustion products towards the burner zone, and a device for stabilizing the dilute combustion characterized in that it comprises a heating element designed to heat, during steady operating conditions, the combustion products in order to sustain self-ignition conditions, said heating element being positioned in the area for diluting the fuel with combustion products in recirculation, firstly, and the oxidant with combustion products, secondly, and surrounding the set of oxidant and fuel jets before their area of contact .
A compressor, including a compressor housing , a scroll compressor unit that is arranged in the compressor housing and has a first, stationary compressor body and a second compressor body that is movable in relation to the stationary compressor body , whereof first and second scroll vanes , in the shape of a circle involute, engage in one another to form compressor chambers when the second compressor body is moved in relation to the first compressor body on an orbital path , an axial guide that supports the movable compressor body to prevent movements in the direction parallel to a centre axis of the stationary compressor body and, in the event of movements, guides it in the direction transverse to the centre axis , a drive motor that drives an eccentric drive for the scroll compressor unit , wherein the eccentric drive has an entrainer that is driven by the drive motor , that revolves on a path about a centre axis of a drive shaft and that cooperates with an entrainer receptacle in the second compressor body , and a coupling that prevents the second compressor body from rotating freely, wherein the coupling that prevents free rotation has at least two coupling element sets that include at least two coupling elements , and wherein one of the coupling elements is formed by a pin body , wherein one of the coupling elements takes the form of an annular body arranged in a cylindrical receptacle , characterised in that the compressor body base of the second compressor body is provided with pockets that have openings facing the cylindrical receptacles of the coupling element sets . a compressor housing , a scroll compressor unit that is arranged in the compressor housing and has a first, stationary compressor body and a second compressor body that is movable in relation to the stationary compressor body , whereof first and second scroll vanes , in the shape of a circle involute, engage in one another to form compressor chambers when the second compressor body is moved in relation to the first compressor body on an orbital path , an axial guide that supports the movable compressor body to prevent movements in the direction parallel to a centre axis of the stationary compressor body and, in the event of movements, guides it in the direction transverse to the centre axis , a drive motor that drives an eccentric drive for the scroll compressor unit , wherein the eccentric drive has an entrainer that is driven by the drive motor , that revolves on a path about a centre axis of a drive shaft and that cooperates with an entrainer receptacle in the second compressor body , and a coupling that prevents the second compressor body from rotating freely, wherein the coupling that prevents free rotation has at least two coupling element sets that include at least two coupling elements , and wherein one of the coupling elements is formed by a pin body , wherein one of the coupling elements takes the form of an annular body arranged in a cylindrical receptacle , characterised in that the compressor body base of the second compressor body is provided with pockets that have openings facing the cylindrical receptacles of the coupling element sets .
A spiral membrane element, comprising: a layered body which comprises a composite semipermeable membrane having a porous support and a separating functional layer on/over a surface of the porous support, a supply-side flow-channel member , and a permeation-side flow-channel member ; a perforated central pipe around which the layered body is wound; and a sealing portion that prevents a supply-side flow-channel from being mixed with a permeation-side flow-channel; the porous support of the composite semipermeable membrane having a thickness of 70 μm to 120 μm; the permeation-side flow-channel member comprising a tricot knitted fabric having a plurality of ribs each formed by repeating loops in a linear form in a longitudinal direction, and a plurality of grooves present between the ribs ; the permeation-side flow-channel member having a membrane support index of 60 to 135, the membrane support index being calculated in accordance with "the number (wale) of grooves per 25-mm" × {rib width (mm)/groove width (mm)}, and the permeation-side flow-channel member having a flow-channel index of 0.02 to 0.039 (mm 2 ), the flow-channel index being calculated in accordance with {groove width (mm) × groove depth (mm) × "the number (wale) of grooves per 25-mm"}/"the number (course) of loops forming ribs per 25-mm". the porous support of the composite semipermeable membrane having a thickness of 70 μm to 120 μm; the permeation-side flow-channel member comprising a tricot knitted fabric having a plurality of ribs each formed by repeating loops in a linear form in a longitudinal direction, and a plurality of grooves present between the ribs ; the permeation-side flow-channel member having a membrane support index of 60 to 135, the membrane support index being calculated in accordance with "the number (wale) of grooves per 25-mm" × {rib width (mm)/groove width (mm)}, and the permeation-side flow-channel member having a flow-channel index of 0.02 to 0.039 (mm 2 ), the flow-channel index being calculated in accordance with {groove width (mm) × groove depth (mm) × "the number (wale) of grooves per 25-mm"}/"the number (course) of loops forming ribs per 25-mm".
An electrical device , comprising: a reconfigurable integrated circuit , comprising: paired top electrodes and bottom electrodes separated from each other by an active layer , wherein: the top electrodes are distributed in two or more rows parallel to a major planar surface of the active layer, each of the rows of top electrodes having different separation distances from the active layer along a dimension perpendicular to the major plane, the bottom electrodes are distributed in two or more rows parallel to the major plane of the active layer, each of the rows of bottom electrodes having different separation distances from the active layer along the dimension perpendicular to the major plane, and a resistivity state of portions of the active layer are independently changeable by a voltage applied to one or more of the paired top and bottom electrodes. the top electrodes are distributed in two or more rows parallel to a major planar surface of the active layer, each of the rows of top electrodes having different separation distances from the active layer along a dimension perpendicular to the major plane, the bottom electrodes are distributed in two or more rows parallel to the major plane of the active layer, each of the rows of bottom electrodes having different separation distances from the active layer along the dimension perpendicular to the major plane, and a resistivity state of portions of the active layer are independently changeable by a voltage applied to one or more of the paired top and bottom electrodes.
An apparatus for network manager, NM , in a New Radio, NR, network, or Long Term Evolution, LTE, network, the apparatus comprising: at least one processor configured to: request a network functions virtualization orchestrator ,NFVO , via a network service ,NS, update request, including a nslnstanceld parameter and an updateType parameter, to remove a physical network function ,PNF, part from an NS instance with updateType set to RemovePnf, or add a new PNF part to the NS instance with updateType set to AddPnf, as indicated by parameters in the NS update request.
A braking system for an aircraft operable to apply one or more aircraft wheel brakes according to at least one of a plurality of wheel brake control functions, the braking system comprising: an aircraft speed indicator ; and a controller configured to: control a wheel braking operation of the aircraft according to at least a first wheel brake control function if the aircraft speed indicated by the aircraft speed indicator exceeds a speed threshold; control the wheel braking operation of the aircraft according to at least a second wheel brake control function if the aircraft speed does not exceed the speed threshold; characterized in that the controller is configured to select a brake wear reduction function or a thermal oxidation harmonising function as the second wheel brake control function. an aircraft speed indicator ; and a controller configured to: control a wheel braking operation of the aircraft according to at least a first wheel brake control function if the aircraft speed indicated by the aircraft speed indicator exceeds a speed threshold; control the wheel braking operation of the aircraft according to at least a second wheel brake control function if the aircraft speed does not exceed the speed threshold; characterized in that the controller is configured to select a brake wear reduction function or a thermal oxidation harmonising control a wheel braking operation of the aircraft according to at least a first wheel brake control function if the aircraft speed indicated by the aircraft speed indicator exceeds a speed threshold; control the wheel braking operation of the aircraft according to at least a second wheel brake control function if the aircraft speed does not exceed the speed threshold; characterized in that the controller is configured to select a brake wear reduction function or a thermal oxidation harmonising function as the second wheel brake control function.