mhurhangee/ep-ind-claims huggingface dataset:
A vehicle environment detection system that comprises at least one detection device (3, 4) and at least one processing unit, where the vehicle environment detection system is arranged to detect at least two feature points (12, 13) at an object outside a vehicle, where each feature point constitutes a retrievable point that has a fixed position (x 1, y 1; x 2, y 2) on said object, wherein said processing unit is arranged to: - determine the positions (x 1, y 1; x 2, y 2) and the resulting velocities (v r1, v r2) for each one of said feature points (12, 13) for multiple frames by means of a feature point tracker; and - determine a reference position (x 0, y 0), a corresponding reference velocity and reference angular velocity (ω), constituting a common motion state for the object, by means of the positions and resulting velocities for each one of the feature points; where the feature point tracker is constituted by a tracking algorithm based on a temporal filter applied to states for each feature point, in particular a Kalman filter, which is arranged to track the multiple feature points, characterized in that the vehicle environment detection system is arranged to calculate said common motion state by solving the linear equation system: v x 1 v y 1 v x 2 v y 2 ⋮ v xN v yN = − y 1 + y 0 1 0 x 1 − x 0 0 1 − y 2 + y 0 1 0 x 2 − x 0 0 1 ⋮ − y N + y 0 1 0 x N − x 0 0 1 ω v x 0 v y 0 where v x1... v xN are determined velocity x-components for each feature point (12, 13), v y1... v yN are determined velocity y-components for each feature point (12, 13), x 1... x N are x-coordinates for each feature point position, y 1... y N are y-coordinates for each feature point position, v x0 is a velocity x-component for the reference velocity vector (v r0), v y0 is a velocity y-component for the reference velocity vector (v r0), x 0 is a reference position x-coordinate and y 0 is a reference position y-coordinate, where all coordinates are determined relative a coordinate system having an x-axis and a y-axis. - determine the positions (x 1, y 1; x 2, y 2) and the resulting velocities (v r1, v r2) for each one of said feature points (12, 13) for multiple frames by means of a feature point tracker; and - determine a reference position (x 0, y 0), a corresponding reference velocity and reference angular velocity (ω), constituting a common motion state for the object, by means of the positions and resulting velocities for each one of the feature points;
A casing assembly, comprising: a rear casing comprising an outer surface and an inner surface opposite the outer surface, and the rear casing defining a mounting hole through the outer surface and the inner surface; and an assembly for reducing wearing of the outer surface of the rear casing, comprising a coupling member and a decorative member, the decorative member having a decorative effect to improve appearance of the rear casing, the coupling member being coupled to the rear casing passing through the mounting hole and defining a recess at a side of the coupling member opposite the inner surface, the decorative member being embedded in the recess and the decorative member protruding from the outer surface, characterized in that the coupling member protrudes from the outer surface and is exposed from the outer surface. a rear casing comprising an outer surface and an inner surface opposite the outer surface, and the rear casing defining a mounting hole through the outer surface and the inner surface; and an assembly for reducing wearing of the outer surface of the rear casing, comprising a coupling member and a decorative member, the decorative member having a decorative effect to improve appearance of the rear casing, the coupling member being coupled to the rear casing passing through the mounting hole and defining a recess at a side of the coupling member opposite the inner surface, the decorative member being embedded in the recess and the decorative member protruding from the outer surface, characterized in that the coupling member protrudes from the outer surface and is exposed from the outer surface.
A propulsion system for an aircraft, the propulsion system comprising: an electric power source; an electric propulsor assembly comprising an electric motor and a propulsor configured to generate thrust for the aircraft; and a power bus electrically connecting the electric power source to the electric propulsor assembly such that the electric power source powers the electric propulsor assembly, the power bus comprising an electric line; characterized in that the power bus further comprises a fluid cooling system, wherein the fluid cooling system extends along at least a portion of a length of the electric line, the fluid cooling system in thermal communication with the electric line for cooling the electric line during operation and further in thermal communication with the electric motor of the electric propulsor assembly for cooling the electric motor of the electric propulsor assembly. an electric power source; an electric propulsor assembly comprising an electric motor and a propulsor configured to generate thrust for the aircraft; and a power bus electrically connecting the electric power source to the electric propulsor assembly such that the electric power source powers the electric propulsor assembly, the power bus comprising an electric line; characterized in that the power bus further comprises a fluid cooling system, wherein the fluid cooling system extends along at least a portion of a length of the electric line, the fluid cooling system in thermal communication with the electric line for cooling the electric line during operation and further in thermal communication with the electric motor of the electric propulsor assembly for cooling the electric motor of the electric propulsor assembly.
A telescopic device comprising a first tubular element and an extension member (2"), said extension member (2") having a first diameter and being displaceably arranged in an axial direction within the first tubular element, wherein a coupling member (3") is provided movably on the extension member (2") and being positionable in at least - a first axial position wherein the extension member (2") is displaceable within the first tubular element, - a second axial position wherein the coupling member (3") engages between the extension member (2") and the interior of the first tubular element limiting displacement in at least one longitudinal direction, and characterized in that - a third axial position wherein the coupling member is fixated relative to the extension member by a receiving section of the extension member having a second diameter of less than said first diameter, wherein the coupling member (3") is a coupling ring having an inner surface facing the extension member (2") and an outer surface facing the first tubular element, wherein a radial extent of the coupling ring is variable from a first radial extent to a second radial extent in the second axial position and to a third radial extent in the third axial position, wherein the radial extent of the coupling ring is larger in the second radial extent than in the first or third radial extent, and wherein, in the third axial position, the outer surface of the coupling ring is not in contact with the inner surface of the first tubular element. - a first axial position wherein the extension member (2") is displaceable within the first tubular element, - a second axial position wherein the coupling member (3") engages between the extension member (2") and the interior of the first tubular element limiting displacement in at least one longitudinal direction, and characterized in that - a third axial position wherein the coupling member is fixated relative to the extension member by a receiving section of the extension member having a second diameter of less than said first diameter, - a third axial position wherein the coupling member is fixated relative to the extension member by a receiving section of the extension member having a second diameter of less than said first diameter,
A device for inputting an authentication code, comprising a processing unit, a display unit connected to the processing unit and a capture means which may be connected to the processing unit, the capture means comprising m distinct actuatable areas in a detectable way and identifiable by the processing unit, the processing unit being able to assign n characters, comprising at least the characters contained in authentication code, to n from among m areas of the capture means, and the processing unit being further able to display on the display means an illustration of the assignment of said n characters to n from among m areas of the capture means, said device being characterized in that the capture means is removable and provided by a user of the device during use, the capture means being able to indicate to the processing unit a mapping of its m areas.
A compound of the formula: wherein: X is selected from the group consisting of: and R 1 to R 9 are independently C, N, O or S; R 10 is independently selected from C 1-6 alkyl, halo, carboxylic acid, amino, hydroxy and C 1-6 alkoxy; Y is A, CH 2 -A or CH=A; A is selected from: Z is selected from the group consisting of: R 11 is independently selected from halo, alkyl, hydroxy, amino and substituted amino; R 12, R 14 and R 15 are independently C, CH, CH 2, O, N, NH or S; R 13 is C, CH, CH 2, N, NH, C-CF 3, CH-CF 3 or C=O; m is 0, 1, 2, 3, 4 or 5; and n is 0, 1, 2, 3 or 4, or a stereoisomer or pharmaceutically acceptable salt thereof. X is selected from the group consisting of: and R 1 to R 9 are independently C, N, O or S; R 10 is independently selected from C 1-6 alkyl, halo, carboxylic acid, amino, hydroxy and C 1-6 alkoxy; Y is A, CH 2 -A or CH=A; A is selected from: Z is selected from the group consisting of: R 11 is independently selected from halo, alkyl, hydroxy, amino and substituted amino; R 12, R 14 and R 15 are independently C, CH, CH 2, O, N, NH or S; R 13 is C, CH, CH 2, N, NH, C-CF 3, CH-CF 3 or C=O; m is 0, 1, 2, 3, 4 or 5; and n is 0, 1, 2, 3 or 4, or a stereoisomer or pharmaceutically acceptable salt thereof.
An assembly for an aircraft, comprising: a geartrain including a first gear system and a second gear system; the first gear system including a first sun gear, a first ring gear, a plurality of first intermediate gears and a first carrier, the first ring gear rotatable about an axis (28, 40, 106), the plurality of first intermediate gears between and meshed with the first sun gear and the first ring gear, each of the plurality of first intermediate gears rotatably mounted to the first carrier, and the first carrier rotatable about the axis (28, 40, 106); the second gear system including a second sun gear, a second ring gear, a plurality of second intermediate gears and a second carrier, the plurality of second intermediate gears between and meshed with the second sun gear and the second ring gear, and each of the plurality of second intermediate gears rotatably mounted to the second carrier; a first propulsor rotor coupled to the first carrier; and a rotating structure coupled to the first ring gear and comprising a turbine rotor, the rotating structure configured to drive rotation of the first propulsor rotor through the geartrain, characterised in that the second ring gear is rotatable about the axis (28, 40, 106) and coupled to the first carrier. a geartrain including a first gear system and a second gear system; the first gear system including a first sun gear, a first ring gear, a plurality of first intermediate gears and a first carrier, the first ring gear rotatable about an axis (28, 40, 106), the plurality of first intermediate gears between and meshed with the first sun gear and the first ring gear, each of the plurality of first intermediate gears rotatably mounted to the first carrier, and the first carrier rotatable about the axis (28, 40, 106); the second gear system including a second sun gear, a second ring gear, a plurality of second intermediate gears and a second carrier, the plurality of second intermediate gears between and meshed with the second sun gear and the second ring gear, and each of the plurality of second intermediate gears rotatably mounted to the second carrier; a first propulsor rotor coupled to the first carrier; and a rotating structure coupled to the first ring gear and comprising a turbine rotor, the rotating structure configured to drive rotation of the first propulsor rotor through the geartrain, characterised in that the second ring gear is rotatable about the axis (28, 40, 106) and coupled to the first carrier.
Process for manufacturing an assembly capable of use in the production of a supporting structure, said assembly being constituted by parts (7, 8) made of a fibrous material forming an element that is at least partially hollow, elongated, with a longitudinal symmetry axis, delimiting an inner area and an outer area, wherein the process consists of producing localized densification of the fibrous material on the two end portions of the elongated hollow element, in order to exert, simultaneously or following this densification, outward tensile forces in opposite directions to each other along its longitudinal axis in order to create an axial prestressing force having a determined value, and to maintain the elongated hollow element in this prestressed conditions during the installation of the assembly in the structure, characterized in that the densification of the fibrous material is achieved according to a mechanical process capable of reducing or even removing the cell voids in the material, obtained by means of a radial compressive force exerted on each of the two end portions of the elongated hollow element, in a direction perpendicular to its longitudinal axis.
A reusable container comprising: a set rack composed of a base plate for positioning and retaining an object to be packaged and a reinforcing frame; an inner packaging cover having a rectangular parallelepiped shape for covering the set rack; and an outer packaging case having a rectangular parallelepiped shape for housing the inner packaging cover; wherein the reusable container has the object to be packaged positioned and secured on the base plate, and further comprises rails disposed between the inner packaging cover and the outer packaging case for guiding and pulling out the inner packaging cover; wherein the base plate of the set rack for positioning and retaining the object to be packaged has a rectangular shape, and the reinforcing frame is a reinforcing frame arranged to correspond to each side of a rectangular parallelepiped shape, one side of which is composed of the rectangular shape of the base plate; and wherein the inner packaging cover of the rectangular parallelepiped shape is composed of a single continuous synthetic resin sheet, having a pair of left and right box-shaped cover portions connectedly disposed to open and close via folding lines from a center area of upright plates (23, 24) folded up from a bottom panel, and wherein multiple buffer materials are bonded to and arranged on an upper surface of the bottom panel and an inner surface of the cover portions. a set rack composed of a base plate for positioning and retaining an object to be packaged and a reinforcing frame; an inner packaging cover having a rectangular parallelepiped shape for covering the set rack; and an outer packaging case having a rectangular parallelepiped shape for housing the inner packaging cover; wherein the reusable container has the object to be packaged positioned and secured on the base plate, and further comprises rails disposed between the inner packaging cover and the outer packaging case for guiding and pulling out the inner packaging cover; wherein the base plate of the set rack for positioning and retaining the object to be packaged has a rectangular shape, and the reinforcing frame is a reinforcing frame arranged to correspond to each side of a rectangular parallelepiped shape, one side of which is composed of the rectangular shape of the base plate; and wherein the inner packaging cover of the rectangular parallelepiped shape is composed of a single continuous synthetic resin sheet, having a pair of left and right box-shaped cover portions connectedly disposed to open and close via folding lines from a center area of upright plates (23, 24) folded up from a bottom panel, and wherein multiple buffer materials are bonded to and arranged on an upper surface of the bottom panel and an inner surface of the cover portions.
A monomeric Fc-containing polypeptide comprising an IgG CH2 and an IgG CH3 domain, wherein the CH3 domain comprises N-linked glycosylation sites in the CH3-CH3 dimerization interface, wherein the engineered N-linked glycosylation sites are selected from the group consisting of a) S364N and Y407N-X-K409T; b) S364N-X-T366S and Y407N-X-K409T; c) S364N and Y407N-X-K409S; and d) S364N-X-T366S and Y407N-X-K409S, wherein X is any amino acid except Pro, and wherein the numbering of the residues is based on the EU numbering scheme of Kabat.
A cover tape for electronic component packaging, comprising a heat sealant layer on a base layer, wherein said heat sealant layer contains: one or more resins selected from a group consisting of polyethylene, polypropylene, ethylene-vinyl acetate copolymer, ethylene-(meth)acrylic acid copolymer, ethylene-methyl (meth)acrylate copolymer, ethylene-methyl acrylate copolymer, ethylene-ethyl acrylate copolymer, and ethylene-butyl acrylate copolymer, and a polyether-polyolefin block copolymer; and the heat sealant layer further contains styrene methyl (meth)acrylate copolymers. one or more resins selected from a group consisting of polyethylene, polypropylene, ethylene-vinyl acetate copolymer, ethylene-(meth)acrylic acid copolymer, ethylene-methyl (meth)acrylate copolymer, ethylene-methyl acrylate copolymer, ethylene-ethyl acrylate copolymer, and ethylene-butyl acrylate copolymer, and a polyether-polyolefin block copolymer; and
A method for processing flexographic plates, comprising the steps of - providing a flexographic plate including a relief layer composed of a top part, a middle part and a bottom part forming subsequent layers in the plate, the relief layer containing a photosensitive material, the plate further including, on the relief layer, a carbon layer that is impenetrable for UV light, - locally ablating the carbon layer by exposure to radiation for forming a pattern in the carbon layer that is penetrable for UV light, and - polymerizing at least the top part of the relief layer under the carbon pattern layer by exposure to radiation, wherein a radiation source is used for generating a radiation beam forming a spot on the carbon layer both locally ablating the carbon layer and exposing at least the top part of the relief layer directly below said removed carbon to said radiation beam spot for polymerizing said top part layer, - backwardly exposing the relief layer to radiation for forming the bottom part of the relief layer as a floor layer. - providing a flexographic plate including a relief layer composed of a top part, a middle part and a bottom part forming subsequent layers in the plate, the relief layer containing a photosensitive material, the plate further including, on the relief layer, a carbon layer that is impenetrable for UV light, - locally ablating the carbon layer by exposure to radiation for forming a pattern in the carbon layer that is penetrable for UV light, and - polymerizing at least the top part of the relief layer under the carbon pattern layer by exposure to radiation, wherein a radiation source is used for generating a radiation beam forming a spot on the carbon layer both locally ablating the carbon layer and exposing at least the top part of the relief layer directly below said removed carbon to said radiation beam spot for polymerizing said top part layer, - backwardly exposing the relief layer to radiation for forming the bottom part of the relief layer as a floor layer.
A device having an array provided with microprotrusions, comprising: an array provided with microprotrusions, having a base and tapered microprotrusions each disposed on the base, each microprotrusion comprising a tip, a bottom and a surface, and tapering down toward the tip from the bottom connected to the base; and a holding member for placing the array provided with microprotrusions against the skin, wherein denoting the distance from the tip to the bottom on an arbitrary side of each of the microprotrusions as a and denoting the length of a second line segment obtained by projecting a first line segment representing the distance onto the base as b, the ratio a/b satisfies 1.0 < (a/b) ≤ 7.5, the height of the microprotrusions is 50 to 300 μm, and the tip is flat and the area of the tip is 20 to 600 μm 2, wherein the microprotrusions are made of polylactic acid, and wherein an active ingredient is coated at least on a portion on the surfaces of the microprotrusions and/or on the base, said active ingredient being a low-molecular weight sodium hyaluronate with a molecular weight of 50,000 to 110,000. an array provided with microprotrusions, having a base and tapered microprotrusions each disposed on the base, each microprotrusion comprising a tip, a bottom and a surface, and tapering down toward the tip from the bottom connected to the base; and a holding member for placing the array provided with microprotrusions against the skin, wherein denoting the distance from the tip to the bottom on an arbitrary side of each of the microprotrusions as a and denoting the length of a second line segment obtained by projecting a first line segment representing the distance onto the base as b, the ratio a/b satisfies 1.0 < (a/b) ≤ 7.5, the height of the microprotrusions is 50 to 300 μm, and the tip is flat and the area of the tip is 20 to 600 μm 2, wherein the microprotrusions are made of polylactic acid, and wherein an active ingredient is coated at least on a portion on the surfaces of the microprotrusions and/or on the base, said active ingredient being a low-molecular weight sodium hyaluronate with a molecular weight of 50,000 to 110,000.
A method to generate terahertz radiation in a nonlinear optical medium, wherein a pump beam is pre-tilted by subjecting the pump beam to pulse-front-tilting, the thus obtained tilted-pulse-front pump beam is coupled into the nonlinear optical medium and THz radiation is generated in the optical medium by nonlinear optical processes, in particular by optical rectification, by means of the pump beam, wherein pulse-front-tilt of the pump beam required to satisfy the velocity matching condition of v p;gr cos( γ) = v THz; ph is induced as a sum of a plurality of pulse-front-tilts, each pulse-front-tilt is induced separately as a partial pulse-front-tilt of the pump beam in subsequent steps, here v p;gr is the group velocity of the pump beam, v THz;ph is the phase velocity of the THz pulse, and γ is the angle formed between the pulse front and the phase front of said pump beam, wherein the last step of pulse-front-tilting of said pump beam is performed by coupling the pump beam into the nonlinear optical medium through a stair-step structure, wherein the nonlinear optical medium comprises an entry surface and an exit surface bounding the nonlinear optical medium in the pump beam's propagation direction, and wherein said stair-step structure is formed in the entry surface, characterized in that the entry surface and the exit surface form a non-zero angle (Γ) with one another.