mhurhangee/patent-ind-claim-en huggingface dataset:
An angled infusion set adapted to be secured to a skin surface, the angled infusion set comprising: a hub comprising: a body member having a first end and a second end and a bore extending from said first end to said second end; a needle or cannula disposed in said bore such that a distal end of said needle or cannula extends beyond said first end of said body member and an elongated slot is formed in a lower surface of the body member extending rearwardly from the first end , said elongated slot opening into said bore, said needle or cannula being disposed in said slot, characterised in that the body member further comprises a rounded protrusion surrounding said elongated slot so when the needle is bent in any direction, the needle bends around the rounded protrusion , thereby allowing more bend cycles of the needle before it fractures because the stress in the needle is reduced by the increased bend radius provided by the rounded protrusion . a hub comprising: a body member having a first end and a second end and a bore extending from said first end to said second end; a needle or cannula disposed in said bore such that a distal end of said needle or cannula extends beyond said first end of said body member and an elongated slot is formed in a lower surface of the body member extending rearwardly from the first end , said elongated slot opening into said bore, said a body member having a first end and a second end and a bore extending from said first end to said second end; a needle or cannula disposed in said bore such that a distal end of said needle or cannula extends beyond said first end of said body member and an elongated slot is formed in a lower surface of the body member extending rearwardly from the first end , said elongated slot opening into said bore, said needle or cannula being disposed in said slot, characterised in that the body member further comprises a rounded protrusion surrounding said elongated slot so when the needle is bent in any direction, the needle bends around the rounded protrusion , thereby allowing more bend cycles of the needle before it fractures because the stress in the needle is reduced by the increased bend radius provided by the rounded protrusion .
A relay node for a communication system in which a mobility management entity, MME, is a core network node affected by overload, the relay node comprising: means for receiving, from a donor base station , an overload start message including an identity of the affected core network node and an information element to indicate an overload action to be performed; means for using the identity of the overload affected core network node to selectively apply an overload procedure represented by said overload start message in respect of user equipment associated with the relay node. means for receiving, from a donor base station , an overload start message including an identity of the affected core network node and an information element to indicate an overload action to be performed; means for using the identity of the overload affected core network node to selectively apply an overload procedure represented by said overload start message in respect of user equipment associated with the relay node.
Floor panel of the type which comprises at least a substrate and a top layer provided on this substrate , wherein said top layer comprises a motif ; wherein the floor panel comprises at least at two opposite edges (5-6) coupling means , with which two of such floor panels can be locked to each other in horizontal direction (H1) as well as in vertical direction (V1); wherein said coupling means substantially are made as a tongue-in-groove coupling, which is provided with locking parts (18-19); wherein said tongue-in-groove coupling realizes said locking in vertical direction (V1), whereas said locking parts (18-19) are provided for realizing said locking in horizontal direction (H1); characterized in that said substrate substantially consists of a foamed synthetic material board having an average density of more than 300 kilograms per cubic meter; that said coupling means substantially are realized in the foamed synthetic material board; that at least one pair of horizontally active locking surfaces (20-21) of the coupling means is realized in the substrate ; that the top layer is composed of at least a back layer , which consists of a vinyl compound, the motif , which is formed by a printed synthetic material film provided on the back layer , and a transparent or translucent wear layer ; that the back layer has a thickness which is 45 percent or more of the overall thickness of the top layer ; and that the top layer is glued to the substrate .
A structured substrate comprising: a substrate body having an active side , the substrate body including reaction cavities that open along the active side and interstitial regions that separate the reaction cavities ; and an ensemble amplifier positioned within each of the reaction cavities , the ensemble amplifier including a plurality of nanostructures configured to at least one of amplify electromagnetic energy that propagates into the corresponding reaction cavity or amplify electromagnetic energy that is generated within the corresponding reaction cavity ; wherein the ensemble amplifier is a polarized amplifier that is configured to preferentially respond to electromagnetic energy of a predetermined polarization; wherein the electromagnetic energy is light energy; and wherein the reaction cavities include a first set of reaction cavities and a second set of reaction cavities , the first set of reaction cavities preferentially responding to a first polarized light over a second polarized light and the second set of reaction cavities preferentially responding to the second polarized light over the first polarized light. a substrate body having an active side , the substrate body including reaction cavities that open along the active side and interstitial regions that separate the reaction cavities ; and an ensemble amplifier positioned within each of the reaction cavities , the ensemble amplifier including a plurality of nanostructures configured to at least one of amplify electromagnetic energy that propagates into the corresponding reaction cavity or amplify electromagnetic energy that is generated within the corresponding reaction cavity ; wherein the ensemble amplifier is a polarized amplifier that is configured to preferentially respond to electromagnetic energy of a predetermined polarization; wherein the electromagnetic energy is light energy; and wherein the reaction cavities include a first set of reaction cavities and a second set of reaction cavities , the first set of reaction cavities preferentially responding to a first polarized light over a second polarized light and the second set of reaction cavities preferentially responding to the second polarized light over the first polarized light.
A thermoplastic resin composition comprising: a graft copolymer, which is prepared by graft-polymerizing an aromatic vinyl-based monomer and a vinyl cyan-based monomer onto an acrylic rubber polymer having an average particle diameter of 50.0 nm to 90.0 nm; a matrix copolymer, which includes a C 1 -C 3 alkyl (meth)acrylate-based monomer unit, an aromatic vinyl-based monomer unit and a vinyl cyan-based monomer unit; and an additive, which includes a polymer including a C 1 -C 3 alkyl (meth)acrylate-based monomer unit, wherein the average particle diameter of the acrylic rubber polymer is referring to an arithmetic average particle diameter in the particle size distribution as measured by a dynamic light scattering method, that is, an average particle diameter in the scattering intensity distribution. a graft copolymer, which is prepared by graft-polymerizing an aromatic vinyl-based monomer and a vinyl cyan-based monomer onto an acrylic rubber polymer having an average particle diameter of 50.0 nm to 90.0 nm; a matrix copolymer, which includes a C 1 -C 3 alkyl (meth)acrylate-based monomer unit, an aromatic vinyl-based monomer unit and a vinyl cyan-based monomer unit; and an additive, which includes a polymer including a C 1 -C 3 alkyl (meth)acrylate-based monomer unit, wherein the average particle diameter of the acrylic rubber polymer is referring to an arithmetic average particle diameter in the particle size distribution as measured by a dynamic light scattering method, that is, an average particle diameter in the scattering intensity distribution.
A method comprising: welding a first end of a base to a first end of a first work piece having a first content of a metallic element, the base having a same content of the metallic element as the first work piece ; depositing a first weld layer on a second end of the base opposite the first end ; depositing a second weld layer between the first weld layer and a second end of a second work piece to couple the first work piece to the second work piece , the second work piece having a second content of the metallic element higher than the first content, the first weld layer having a third content of the metallic element higher than the first content and lower than the second content, and the second weld layer having a fourth content of the metallic element higher than the third content and lower than the second content; and before the deposition of the second weld layer , depositing a third weld layer on the first weld layer , the second weld layer to be deposited between the third weld layer and the second end of the second work piece , the third weld layer having a fifth content of the metallic element higher than the third content and lower than the fourth content. welding a first end of a base to a first end of a first work piece having a first content of a metallic element, the base having a same content of the metallic element as the first work piece ; depositing a first weld layer on a second end of the base opposite the first end ; depositing a second weld layer between the first weld layer and a second end of a second work piece to couple the first work piece to the second work piece , the second work piece having a second content of the metallic element higher than the first content, the first weld layer having a third content of the metallic element higher than the first content and lower than the second content, and the second weld layer having a fourth content of the metallic element higher than the third content and lower than the second content; and before the deposition of the second weld layer , depositing a third weld layer on the first weld layer , the second weld layer to be deposited between the third weld layer and the second end of the second work piece , the third weld layer having a fifth content of the metallic element higher than the third content and lower than the fourth content.
Optical element for influencing the light emission of lamps, in particular for influencing the light emission of one or more LEDs , wherein the optical element consists of a translucent material and has at least one surface region which serves as a light-refracting light-exit surface of the optical element , wherein the surface region has a structure which was produced by remelting the optical element or a tool used to manufacture the optical element with corresponding shaping, preferably an injection molding tool, by means of a laser, wherein the structure is divided into at least two sub-regions (10 1 , 10 2 ...), the respective structures of which have a different geometry, wherein these structures continuously merge into one other at common boundaries of the sub-regions (10 1 , 10 2 ...), and wherein the structures of the at least the two sub-regions (10 1 , 10 2 ...) each has a continuous, in particular a continuous and differentiable, wave-like shape at least in a first direction, wherein • the wave-like structure has a wavelength (λ) in the range of approximately 50-500 μm and/or • the wave-like structure has elevated regions with a height (h) in the range of approximately 5-100 μm, wherein the sub-regions (10 1 , 10 2 ...) differ in terms of their wavelength (λ) and in terms of the height (h) of the elevated regions. wherein the surface region has a structure which was produced by remelting the optical element or a tool used to manufacture the optical element with corresponding shaping, preferably an injection molding tool, by means of a laser, wherein the structure is divided into at least two sub-regions (10 1 , 10 2 ...), the respective structures of which have a different geometry, wherein these structures continuously merge into one other at common boundaries of the sub-regions (10 1 , 10 2 ...), and wherein the structures of the at least the two sub-regions (10 1 , 10 2 ...) each has a continuous, in particular a continuous and differentiable, wave-like shape at least in a first direction, wherein • the wave-like structure has a wavelength (λ) in the range of approximately 50-500 μm and/or • the wave-like structure has elevated regions with a height (h) in the range of approximately 5-100 μm, • the wave-like structure has a wavelength (λ) in the range of approximately 50-500 μm and/or • the wave-like structure has elevated regions with a height (h) in the range of approximately 5-100 μm, wherein the sub-regions (10 1 , 10 2 ...) differ in terms of their wavelength (λ) and in terms of the height (h) of the elevated regions.
A cross member (TS) made from extruded aluminium for attaching an electrical drive machine (ME) of a vehicle, and including at least two hollow longitudinal areas which are hollowed out during the extrusion phase, characterized in that these two hollow longitudinal areas are, subsequently to the extrusion phase, filled with solid added material thus forming at least two solid longitudinal areas (ZLj), in which there are defined at selected locations holes (TF) suitable for permitting an attaching of said electrical drive machine (ME) and/or of an equipment of the said vehicle, and/or a coupling of the said cross member (TS) to structural elements (ES1, ES2) of the said vehicle.
An augmented mirror comprising: a partially silvered mirror surface ; a screen underneath the mirrored surface; a camera ; and a computation module configured to receive visual information from the camera, process the information, and display one or more images on the display screen based upon the processed information; wherein the field of view over which visual information is processed by the computational module is reduced to visual information from within a visual corridor , the visual corridor corresponding to a subset of the field of view of the camera; characterised in that the mirror comprises lighting panels, the lighting panels controlled by the computational module wherein the computation module is configured to gradually illuminate the lighting panels as a user moves towards an optimal position in which to use the mirror, wherein the lighting panels indicate to the user when the user is in the optimal position or is approaching an optimal position for interaction with the mirror. a partially silvered mirror surface ; a screen underneath the mirrored surface; a camera ; and a computation module configured to receive visual information from the camera, process the information, and display one or more images on the display screen based upon the processed information; wherein the field of view over which visual information is processed by the computational module is reduced to visual information from within a visual corridor , the visual corridor corresponding to a subset of the field of view of the camera; characterised in that the mirror comprises lighting panels, the lighting panels controlled by the computational module wherein the computation module is configured to gradually illuminate the lighting panels as a user moves towards an optimal position in which to use the mirror, wherein the lighting panels indicate to the user when the user is in the optimal position or is approaching an optimal position for interaction with the mirror.
A power distribution system for an aircraft on the ground, comprising: a preconditioned air unit , operably coupleable to the aircraft on the ground and configured to receive at least a first portion of a predetermined maximum input power provided by a power supply ; at least one ground power unit , electrically coupleable to the aircraft on the ground and configured to receive at least a second portion of said predetermined maximum input power provided by said power supply , and a controller, adapted to monitor at least one parameter of the power consumed by any one of said preconditioned air unit and said at least one ground power unit , and control the power consumption of at least said preconditioned air unit so that the total power consumption of said preconditioned air unit and said at least one ground power unit does not exceed said predetermined maximum input power; wherein said predetermined maximum input power is provided via a single power line between said power supply and an input port of said preconditioned air unit , wherein said predetermined maximum input power is a maximum acceptable power consumption. a preconditioned air unit , operably coupleable to the aircraft on the ground and configured to receive at least a first portion of a predetermined maximum input power provided by a power supply ; at least one ground power unit , electrically coupleable to the aircraft on the ground and configured to receive at least a second portion of said predetermined maximum input power provided by said power supply , and a controller, adapted to monitor at least one parameter of the power consumed by any one of said preconditioned air unit and said at least one ground power unit , and control the power consumption of at least said preconditioned air unit so that the total power consumption of said preconditioned air unit and said at least one ground power unit does not exceed said predetermined maximum input power; wherein said predetermined maximum input power is provided via a single power line between said power supply and an input port of said preconditioned air unit , wherein said predetermined maximum input power is a maximum acceptable power consumption.
A method of controlling flight of an unmanned aerial vehicle, UAV, said method comprising: collecting a first set of images corresponding to different fields of view of an environment around the UAV using multiple image capture devices while traversing a flight path , the multiple image capture devices having different fields of view relative to one another; extracting a first set of feature points from the first set of images while traversing the flight path ; constructing a two - or three-dimensional map of the environment using the first set of feature points and making the map accessible to the UAV; collecting a second set of images corresponding to different fields of view using the multiple image capture devices while traversing a return path , wherein the flight path starts at a starting point and terminates at an end location , and wherein the return path starts at the end location and terminates at the starting point ; and generating a signal that causes the UAV to traverse the return path using the map and based on comparing the first set of feature points extracted during the flight path with a second set of feature points extracted from the second set of images. collecting a first set of images corresponding to different fields of view of an environment around the UAV using multiple image capture devices while traversing a flight path , the multiple image capture devices having different fields of view relative to one another; extracting a first set of feature points from the first set of images while traversing the flight path ; constructing a two - or three-dimensional map of the environment using the first set of feature points and making the map accessible to the UAV; collecting a second set of images corresponding to different fields of view using the multiple image capture devices while traversing a return path , wherein the flight path starts at a starting point and terminates at an end location , and wherein the return path starts at the end location and terminates at the starting point ; and generating a signal that causes the UAV to traverse the return path using the map and based on comparing the first set of feature points extracted during the flight path with a second set of feature points extracted from the second set of images.
A poppet valve for a piston compressor, comprising a cage , a valve body with a multiplicity of inlet ducts , wherein each inlet duct opens into a valve seat , and comprising a multiplicity of closing elements which are movable in an axial direction (A), wherein each inlet duct is assigned a closing element , and wherein the valve seat is arranged so as to be situated opposite the associated closing element in the axial direction (A) in such a way that the valve seat is closable by the closing element , wherein a spring is arranged between the cage and the closing element in order to subject the closing element to a preload force directed toward the valve seat , wherein the closing element comprises a closing head and a guide section , wherein the closing head and the guide section follow one another in the axial direction (A), wherein the closing head has a face side which widens in the axial direction (A) in the direction toward the guide section up to a maximum circumference , wherein the maximum circumference has a circumference central point (M F ), characterized in that on the cage , there is arranged a guide part which extends in the axial direction (A), which extends at least partially inside the closing element, and in that the closing element is guided movably in the axial direction (A) on the guide part , in that the closing element , proceeding from the guide section , has a guide interior space which extends in the axial direction (A) into the interior of the closing element in the direction of the closing head and in which the guide part also extends, , and in that the guide interior extends at least so far in the direction towards the closing head that the circumferential centre (M F ) comes to lie within the guide interior .
Method for printing a substrate using an aerosol jet comprising metallic nanoparticles, the method comprising implementation of the following successive steps: a) a step to prepare a solution comprising said metallic nanoparticles, using a solution comprising at least one metallic precursor of said metallic nanoparticles, and at least one reducing agent of the precursor(s), b) a step to generate an aerosol containing metallic nanoparticles, by continuous feed of an aerosol generation device with the solution obtained in step a), c) a step to print the substrate using a print head continuously supplied with the aerosol obtained in step b). a) a step to prepare a solution comprising said metallic nanoparticles, using a solution comprising at least one metallic precursor of said metallic nanoparticles, and at least one reducing agent of the precursor(s), b) a step to generate an aerosol containing metallic nanoparticles, by continuous feed of an aerosol generation device with the solution obtained in step a), c) a step to print the substrate using a print head continuously supplied with the aerosol obtained in step b).
Device for handling laboratory samples, comprising at least one gripper movable from above over a sample and comprising multiple fingers arranged around an axis (S), which fingers are pushable against the sample for gripping the sample, as well as an actuator mechanism for moving the fingers in order to grip or to dump the sample, wherein each finger is elastically displaceable radially to the axis (S), wherein the gripper has at least two gripper hands and wherein the gripper hands are arranged at a common carrier , characterized in that the fingers of the at least two gripper hands have different gripping diameters for gripping samples with different sample diameters.