mhurhangee/patent-ind-claim-en huggingface dataset:
A method for manufacturing one or more 3D products in a single batch by additive manufacturing using a layer-by-layer technique, said method comprising the steps of; a) setting a first thickness (Tr) of a reference layer ; b) setting a second thickness (T2) as a multiple of an integer and said first thickness (Tr) of said reference layer c) forming a first material layer having said second thickness (T2); d) performing a binding action on said first material layer; wherein steps c) and d) are performed one or more times, thereby forming a first zone in said batch; and e) setting a third thickness, said third thickness being a multiple of an integer and said first thickness (Tr) of said reference layer ; f) forming a second material layer having said third thickness; g) performing a binding action on said second material layer; wherein steps f) and g) are performed one or more times, thereby forming a second zone in said batch, said first zone and said second zone sharing a same X-Y plane; and wherein said material layer thickness of said second zone is different from said material layer thickness of said first zone, whereby a resolution of said second zone is different from a resolution of said first zone. a) setting a first thickness (Tr) of a reference layer ; b) setting a second thickness (T2) as a multiple of an integer and said first thickness (Tr) of said reference layer c) forming a first material layer having said second thickness (T2); d) performing a binding action on said first material layer; wherein steps c) and d) are performed one or more times, thereby forming a first zone in said batch; and e) setting a third thickness, said third thickness being a multiple of an integer and said first thickness (Tr) of said reference layer ; f) forming a second material layer having said third thickness; g) performing a binding action on said second material layer;
A method of identifying dental consumables including at least one of a dental blank and a dental tool equipped into a dental tool machine , the method comprising: a step of colliding the dental tool with the dental blank or a dental blank holder of the dental tool machine ; a step of detecting a signal indicative of the collision, characterized by further comprising: a step of analyzing the detected signal through trained artificial intelligence; and a step of identifying the type including the material and the geometrical properties and the condition of at least one of the dental consumables based on the analysis. a step of colliding the dental tool with the dental blank or a dental blank holder of the dental tool machine ; a step of detecting a signal indicative of the collision, characterized by further comprising: a step of analyzing the detected signal through trained artificial intelligence; and a step of identifying the type including the material and the geometrical properties and the condition of at least one of the dental consumables based on the analysis. a step of analyzing the detected signal through trained artificial intelligence; and a step of identifying the type including the material and the geometrical properties and the condition of at least one of the dental consumables based on the analysis.
An adhesive composition comprising: (a) at least one isocyanate component, and (b) at least one polyol component, wherein the polyol component comprises (bi) at least one first polyol compound, (bii) 0.1 to 3 wt% of, based on the weight of the adhesive composition, at least one second polyol compound having a functionality of greater than 2 and an equivalent weight of less than 200, which is glycerin; and (biii) at least one chain extender, wherein the chain extender comprises an aliphatic diol with an equivalent weight of less than 200. (a) at least one isocyanate component, and (b) at least one polyol component, wherein the polyol component comprises (bi) at least one first polyol compound, (bii) 0.1 to 3 wt% of, based on the weight of the adhesive composition, at least one second polyol compound having a functionality of greater than 2 and an equivalent weight of less than 200, which is glycerin; and (biii) at least one chain extender, wherein the chain extender comprises an aliphatic diol with an equivalent weight of less than 200.
A method of manufacturing a wood-based panel provided with a decor comprising the steps: (a) applying at least one first layer of at least one powdered resin to at least one side of a wood-based panel and melting-on the at least one applied layer of powdered resin; a1) applying at least one undercoat to the melted-on resin powder layer; a2) applying of at least one primer layer to the at least one undercoat; b) applying at least one decorative layer by means of a direct printing process; c) applying at least one further, second layer of at least one powdered resin to the at least one imprinted decorative layer and melting-on the at least one layer of powdered resin spread on the decorative layer. d) uniformly sprinkling abrasion-resistant particles onto the powdered resin layer applied in step c). e) applying at least one further, third layer of at least one powdered resin to the layer of abrasion-resistant particles and melting-on the applied third layer of powdered resin, f) sprinkling glass beads onto the at least one further, third melted-on layer of powdered resin, whereon the glass beads used have a diameter of 60-120 μm, preferably 80-90 μm, and the amount of scattered glass beads is 5 to 30 g/m 2 , preferably 8 to 20 g/m 2 , more preferably 8 to 15 g/m 2 , g) applying at least one further, fourth layer of at least one powdered resin to the layer of glass beads and melting-on the applied fourth layer of powdered resin, h) pressing the layered structure. (a) applying at least one first layer of at least one powdered resin to at least one side of a wood-based panel and melting-on the at least one applied layer of powdered resin; a1) applying at least one undercoat to the melted-on resin powder layer; a2) applying of at least one primer layer to the at least one undercoat; a1) applying at least one undercoat to the melted-on resin powder layer; a2) applying of at least one primer layer to the at least one undercoat; b) applying at least one decorative layer by means of a direct printing process; c) applying at least one further, second layer of at least one powdered resin to the at least one imprinted decorative layer and melting-on the at least one layer of powdered resin spread on the decorative layer. d) uniformly sprinkling abrasion-resistant particles onto the powdered resin layer applied in step c). e) applying at least one further, third layer of at least one powdered resin to the layer of abrasion-resistant particles and melting-on the applied third layer of powdered resin, f) sprinkling glass beads onto the at least one further, third melted-on layer of powdered resin, whereon the glass beads used have a diameter of 60-120 μm, preferably 80-90 μm, and the amount of scattered glass beads is 5 to 30 g/m 2 , preferably 8 to 20 g/m 2 , more preferably 8 to 15 g/m 2 , g) applying at least one further, fourth layer of at least one powdered resin to the layer of glass beads and melting-on the applied fourth layer of powdered resin, h) pressing the layered structure.
A thiazolone derivative of N6022 having the following characteristic structure: , or a pharmaceutically acceptable salt thereof.
An aircraft with a fuselage for accommodating at least one pilot and/or a payload, in particular air freight and/or at least one passenger, and having at least one ducted propeller drive comprising: - a propeller having a hub body and a plurality of rotor blades uniformly distributed about the outer circumference of the hub body which are invariably connected to the hub body , wherein the propeller is rotatable about a drive axis (A) and its drive power is supplied via a driveshaft arranged substantially radially to the hub body of the propeller ; - a shell housing extending coaxially about the drive axis (A) of the propeller which accommodates the propeller and which, particularly in concert with the hub body , defines an outlet cross section of the ducted propeller drive at a propulsion outlet side ; and - at least one drive mechanism providing drive power to the ducted propeller drive which is at least partly arranged in the fuselage and/or at least partly external of the fuselage and/or at least partly in at least one bearing surface of the aircraft , particularly in sound-suppressed manner; characterized in that the hub body on the propulsion outlet side of the ducted propeller drive has an axially displaceable central body of varying tapering cross-section, particularly on the propulsion outlet side , wherein the outlet cross section of the ducted propeller drive can be regulated by axial displacement of the central body and the drive mechanism of the ducted propeller drive comprises a control device and is configured to keep the rotational speed of the propeller of the ducted propeller drive substantially constant during flight, in particular in support of lower noise emissions, by adjusting the delivered drive power and in concert with the axially displaceable central body. - a propeller having a hub body and a plurality of rotor blades uniformly distributed about the outer circumference of the hub body which are invariably connected to the hub body , wherein the propeller is rotatable about a drive axis (A) and its drive power is supplied via a driveshaft arranged substantially radially to the hub body of the propeller ; - a shell housing extending coaxially about the drive axis (A) of the propeller which accommodates the propeller and which, particularly in concert with the hub body , defines an outlet cross section of the ducted propeller drive at a propulsion outlet side ; and - at least one drive mechanism providing drive power to the ducted propeller drive which is at least partly arranged in the fuselage and/or at least partly external of the fuselage and/or at least partly in at least one bearing surface of the aircraft , particularly in sound-suppressed manner;
Ion beam sputtering apparatus comprising: an ion source configured to generate a hollow ion beam along a beam axis that is located in a hollow part of the beam; and a sputtering target having a target body that defines at least one target surface , the target body comprising sputterable particles, the target body being located relative to the ion source so that the ion beam hits the at least one target surface to sputter particles from the target body towards a surface of an object to be modified; wherein the target body is shaped so that the particles sputtered towards a surface to be modified are generally sputtered from the sputtering target in radially extending sputter directions relative to the beam axis, the sputter directions extending towards the beam axis; wherein the target body has a target passage that extends through the target body, the target passage having an ion beam inlet for the ion beam and a particle outlet for sputtered particles to exit the target passage towards a surface to be modified; wherein a cross sectional area of the particle outlet, in a plane perpendicular to the beam axis, is substantially smaller than a cross sectional area of a hollow portion of the ion beam. an ion source configured to generate a hollow ion beam along a beam axis that is located in a hollow part of the beam; and a sputtering target having a target body that defines at least one target surface , the target body comprising sputterable particles, the target body being located relative to the ion source so that the ion beam hits the at least one target surface to sputter particles from the target body towards a surface of an object to be modified; wherein the target body is shaped so that the particles sputtered towards a surface to be modified are generally sputtered from the sputtering target in radially extending sputter directions relative to the beam axis, the sputter directions extending towards the beam axis; wherein the target body has a target passage that extends through the target body, the target passage having an ion beam inlet for the ion beam and a particle outlet for sputtered particles to exit the target passage towards a surface to be modified; wherein a cross sectional area of the particle outlet, in a plane perpendicular to the beam axis, is substantially smaller than a cross sectional area of a hollow portion of the ion beam.
Magazine release/holding device of a firearm, comprising a magazine holding element and a magazine release slide for transferring the magazine holding element from a magazine holding position thereof into a magazine release position thereof and vice versa, at least one replaceable actuating handle , which projects from one side of a grip or housing of the firearm, being provided on the magazine release slide , wherein the at least one actuating handle can be replaced and mounted on the magazine release slide without tools, for which purpose the magazine release slide comprises at least one guide element for guiding at least one counter guide in or on the actuating handle when it is mounted and removed, characterised in that the guide is provided perpendicularly to the longitudinal axis of the magazine release slide.
A heat exchanger comprising a base plate and at least one heat exchanger fin (100; 600), whereby the base plate comprises a mounting surface and a contact surface , opposite the mounting surface , whereby the at least one heat exchanger fin (100; 600) comprises a fin base , a fin tip and a channel system that is provided between the fin base and the fin tip and that is under vacuum and has a working fluid therein, whereby the fin base of the at least one heat exchanger fin (100; 600) is attached to the mounting surface of the base plate for heat transfer between the base plate and the at least one heat exchanger fin (100; 600), whereby the channel system is at least divided into a first part included in a first portion of the heat exchanger fin (100; 600) and a second part included in a second portion (113; 613) of the heat exchanger fin (100; 600), and whereby the first portion of the at least one heat exchanger fin (100; 600) stands upright on the mounting surface , wherein the channel system comprises an evaporator region, a condenser region and a vapor flow region, whereby the evaporator region is disposed in the first portion , the condenser region is disposed in the second portion (113; 613) and the vapor flow region is disposed in the first portion and the second portion (113; 613) and connects the evaporator region with the condenser region, wherein the evaporator region of the first portion has at least one evaporation channel , a first part of the vapor flow region is disposed in the first portion and has at least one connecting channel communicating with the at least one evaporation channel , a second part of the vapor flow region is disposed in the second portion (113; 613) and has at least one auxiliary channel (147a, 147b; 647a, 647b) communicating with at least one of the at least one connecting channel ; wherein the condenser region of the second portion (113; 613) has at least one condensation channel communicating with the at least one auxiliary channel (147a, 147b; 647a, 647b); and wherein the at least one evaporation channel extends along and near to an outer perimeter length of the first portion of the heat exchanger fin (100; 600) and along and near to the mounting surface of the base plate , characterized in that the first portion and the second portion (113; 613) are angled towards each other in an angle range of >0° to <180°.
A remote tracking device for issuing a tracking signal containing position related data representing the momentary position of the tracking device, to a user station , the remote tracking device comprising: a GNSS receiver and a GNSS antenna for receiving satellite positioning signals; a processor for converting the satellite positioning signals into position related data; and a UHF transmitter and a UHF antenna for transmitting the tracking signal, the UHF antenna comprising an inner conducting cylinder and an outer conducting cylinder spaced from and encircling the inner conducting cylinder; characterized in that the inner conducting cylinder is hollow, and in that one or more electronic components selected from the group consisting of the processor , the GNSS receiver , the UHF transmitter , a UHF receiver, a UHF radio modem, a power supply , a battery, a power converter, a switch, and a motor, is located inside the inner conducting cylinder . a GNSS receiver and a GNSS antenna for receiving satellite positioning signals; a processor for converting the satellite positioning signals into position related data; and a UHF transmitter and a UHF antenna for transmitting the tracking signal, the UHF antenna comprising an inner conducting cylinder and an outer conducting cylinder spaced from and encircling the inner conducting cylinder; characterized in that the inner conducting cylinder is hollow, and in that one or more electronic components selected from the group consisting of the processor , the GNSS receiver , the UHF transmitter , a UHF receiver, a UHF radio modem, a power supply , a battery, a power converter, a switch, and a motor, is located inside the inner conducting cylinder .
An inspection template comprising: a template body having a component side and an opposing inspection side ; and a plurality of inspection bosses (26-1) projecting from the opposing inspection side, each of the plurality of inspection bosses (26-1) having a first coupling (82-1) and a sensor aperture (30-1), each aperture (30-1) disposed axially through each respective boss (26-1) to the component side of the template ; and characterized in that the component side of the template has a shape substantially identical to a shape of a surface of an airfoil or fan blade for a gas turbine engine, or a precursor of an airfoil or fan blade for a gas turbine engine. a template body having a component side and an opposing inspection side ; and a plurality of inspection bosses (26-1) projecting from the opposing inspection side, each of the plurality of inspection bosses (26-1) having a first coupling (82-1) and a sensor aperture (30-1), each aperture (30-1) disposed axially through each respective boss (26-1) to the component side of the template ; and characterized in that the component side of the template has a shape substantially identical to a shape of a surface of an airfoil or fan blade for a gas turbine engine, or a precursor of an airfoil or fan blade for a gas turbine engine.
Method for measuring a wall thickness (b) in hollow valves with and without a hollow valve head , in which - a wall thickness (b 2 ) is determined in the region of a chamfer , which is a transition between a valve shaft and the valve head , by means of at least one ultrasonic sensor , wherein the ultrasonic sensor is positioned at a point of the chamfer at which an inner tangent in the cavity runs parallel to an outer tangent on the chamfer and wherein the ultrasonic sensor is oriented relative to the tangents such that the emitted ultrasound is introduced to the surface in a perpendicular manner. - a wall thickness (b 2 ) is determined in the region of a chamfer , which is a transition between a valve shaft and the valve head , by means of at least one ultrasonic sensor , wherein the ultrasonic sensor is positioned at a point of the chamfer at which an inner tangent in the cavity runs parallel to an outer tangent on the chamfer and wherein the ultrasonic sensor is oriented relative to the tangents such that the emitted ultrasound is introduced to the surface in a perpendicular manner.
A gear drive comprising: a motor having a motor output shaft ; and a gearing operatively coupled to the motor; wherein the gearing includes: a face gear having a toothed ridge engaging the motor output shaft, and a central sun gear ; and planetary gears engaging the sun gear; and wherein the motor output shaft defines a motor output shaft axis about which the motor output shaft rotates; and wherein the motor shaft output axis intersects the sun gear, with the motor output shaft axis substantially perpendicular to a sun gear shaft axis of the sun gear; and wherein the motor output shaft axis also intersects a volume swept out by the planetary gears as the planetary gears rotate about the sun gear. a motor having a motor output shaft ; and a gearing operatively coupled to the motor; wherein the gearing includes: a face gear having a toothed ridge engaging the motor output shaft, and a central sun gear ; and planetary gears engaging the sun gear; and a face gear having a toothed ridge engaging the motor output shaft, and a central sun gear ; and planetary gears engaging the sun gear; and wherein the motor output shaft defines a motor output shaft axis about which the motor output shaft rotates; and wherein the motor shaft output axis intersects the sun gear, with the motor output shaft axis substantially perpendicular to a sun gear shaft axis of the sun gear; and wherein the motor output shaft axis also intersects a volume swept out by the planetary gears as the planetary gears rotate about the sun gear.
A communications method, comprising: determining , by a first terminal side device, a frequency domain resource of a first physical downlink shared channel, PDSCH, scheduled for the first terminal side device, wherein the first PDSCH corresponds to a first demodulation reference signal, DM-RS, on a first antenna port; and characterized in that , when the frequency domain resource comprises N consecutive resource blocks, and there is a second DM-RS on a second antenna port in each of L consecutive resource blocks in the N resource blocks, determining , by the first terminal side device, that precoding of the second DM-RS in each of the L resource blocks is the same, wherein the second antenna port and the first antenna port are different, wherein the second DM-RS and the first DM-RS are in a same code division multiplexing, CDM, group, the second DM-RS corresponds to a second PDSCH scheduled for a second terminal side device, N is an integer greater than 1, and L is less than or equal to N, and is an integer greater than 1. determining , by a first terminal side device, a frequency domain resource of a first physical downlink shared channel, PDSCH, scheduled for the first terminal side device, wherein the first PDSCH corresponds to a first demodulation reference signal, DM-RS, on a first antenna port; and characterized in that , when the frequency domain resource comprises N consecutive resource blocks, and there is a second DM-RS on a second antenna port in each of L consecutive resource blocks in the N resource blocks, determining , by the first terminal side device, that precoding of the second DM-RS in each of the L resource blocks is the same, wherein the second antenna port and the first antenna port are different, wherein the second DM-RS and the first DM-RS are in a same code division multiplexing, CDM, group, the second DM-RS corresponds to a second PDSCH scheduled for a second terminal side device, N is an integer greater than 1, and L is less than or equal to N, and is an integer greater than 1.
A method for comfortable and/or fuel-efficient forward travel of a motor vehicle , comprising the steps of: - regeneratively braking (s430) said motor vehicle following detection of deactivated depression of the gas pedal, characterized by the steps of: - basing the regenerative braking on a continuously determined future magnitude of the resistance to forward travel and - decreasing said regenerative braking (s430) with increasing resistance to forward travel; and - increasing said regenerative braking (s430) with decreasing resistance to forward travel. - regeneratively braking (s430) said motor vehicle following detection of deactivated depression of the gas pedal, - basing the regenerative braking on a continuously determined future magnitude of the resistance to forward travel and - decreasing said regenerative braking (s430) with increasing resistance to forward travel; and - increasing said regenerative braking (s430) with decreasing resistance to forward travel.