mhurhangee/ep-ind-claims huggingface dataset:
A method for cutting a polarizing plate using a laser, characterised in that a beam shape of the laser is an elliptical shape and a major axis of the elliptical shape is parallel to a cutting direction, wherein the elliptical shape has a ratio of a major axis to a minor axis of 1: 0.8 to 1: 0.2, wherein the polarizing plate includes a polarizer composed of a polyvinyl alcohol-based resin impregnated with a dichroic dye or iodine and stretched, and has a multilayered structure in which an optical film (20, 30) stacked via an adhesive (15, 16) on at least one surface of the polarizer, a tackifier layer to be bonded to a liquid crystal cell, and a release film are stacked on one surface of the optical film (20, 30), and a protective film is stacked on the other surface thereof, wherein the optical film (20, 30) is selected from the group consisting of a polyolefin film, a polypropylene film, a polyurethane film, an ester-based film, a polyethylene film, a cyclo olefin-based film, an acrylic film, a polyvinyl alcohol-based film, and a cellulose-based film. wherein the elliptical shape has a ratio of a major axis to a minor axis of 1: 0.8 to 1: 0.2, wherein the polarizing plate includes a polarizer composed of a polyvinyl alcohol-based resin impregnated with a dichroic dye or iodine and stretched, and has a multilayered structure in which an optical film (20, 30) stacked via an adhesive (15, 16) on at least one surface of the polarizer, a tackifier layer to be bonded to a liquid crystal cell, and a release film are stacked on one surface of the optical film (20, 30), and a protective film is stacked on the other surface thereof, wherein the optical film (20, 30) is selected from the group consisting of a polyolefin film, a polypropylene film, a polyurethane film, an ester-based film, a polyethylene film, a cyclo olefin-based film, an acrylic film, a polyvinyl alcohol-based film, and a cellulose-based film.
A mechanically operated device, in particular milling device comprising a driving shaft rotatably carried in a housing of the device, the first end of said driving shaft extending from the housing comprising means for coupling a rotary actuator and the second end of said driving shaft extending from the housing carrying a disc-type tool, in particular a milling tool, which is fitted with an axial hole on a disc block held on the shaft and provided with annular clamping members, engages a thrust-bearing integrated in the shaft, and the disc block thereof being clampable by means of a clamping means in a force-fit manner against the inner surface of the hole of the tool, characterized by that the driving shaft includes a channel being open toward the second end and extending over part of its axial extension, in which is fitted a pressure piece in an axially displaceable manner, said pressure piece being coupled at its first end region showing toward the second end of the driving shaft to the clamping means and at its second end region to a bolt transversely penetrating the driving shaft in an axially oriented oblong hole thereof, said bolt extending radially over the driving shaft into a free space of the housing, wherein between the protruding regions of the bolt and a bearing disposed close to the second end of the driving shaft between driving shaft and housing, a spring assembly with an axially acting spring force is disposed or gripped, and between the protruding regions of the bolt and a bearing disposed close to the first end of the driving shaft between driving shaft and housing, an axially displaceable piston is disposed that is adjustable, by means of application of pressure via a pressure medium connection in the housing, in the direction toward the second end of the driving shaft against the spring force of the spring assembly.
An engine configured to be coupled to an aircraft, the engine comprising: an engine core; a duct having a substantially circular shape and surrounding the engine core; a forward frame coupled to the duct and a forward portion of the engine core; and a plurality of coupling struts coupling a rear portion of the engine core to the duct; characterized in that a front mounting mounts a forward end portion of the duct to a side of the aircraft, and a rear mounting mounts a rear end portion of the duct to the side of the aircraft; and further characterized in that all of the coupling struts extend in a vertical or substantially vertical direction such that each of the coupling struts forms an angle with a downward direction of gravity equal to or less than 30 degrees, when the engine core is at a rest position with zero pitch and zero roll, the plurality of coupling struts (i) inhibiting displacement of the rear portion of the engine core in a vertical direction when operating under maneuver-induced loads, and (ii) permitting displacement of the rear portion of the engine core in a horizontal direction when operating under thrust-induced loads. an engine core; a duct having a substantially circular shape and surrounding the engine core; a forward frame coupled to the duct and a forward portion of the engine core; and a plurality of coupling struts coupling a rear portion of the engine core to the duct; characterized in that a front mounting mounts a forward end portion of the duct to a side of the aircraft, and a rear mounting mounts a rear end portion of the duct to the side of the aircraft; and further characterized in that all of the coupling struts extend in a vertical or substantially vertical direction such that each of the coupling struts forms an angle with a downward direction of gravity equal to or less than 30 degrees, when the engine core is at a rest position with zero pitch and zero roll, the plurality of coupling struts (i) inhibiting displacement of the rear portion of the engine core in a vertical direction when operating under maneuver-induced loads, and (ii) permitting displacement of the rear portion of the engine core in a horizontal direction when operating under thrust-induced loads.
Method for automatically adjusting at least one smoke detector, wherein the at least one smoke detector to be adjusted is positioned in a channel applied with a flowing aerosol, wherein a smoke detector which is already adjusted and functions as a reference detector is disposed in the channel together with the at least one smoke detector to be adjusted, wherein the channel for receiving the at least one smoke detector to be adjusted and the reference detector has a housing in each case and wherein the housings included in the channel are connected to one another by means of pipe sections such that each output side of a housing is connected to an input side of a housing which follows along the channel wherein the at least one smoke detector to be adjusted is adjusted by means of data available from the reference detector. wherein the at least one smoke detector to be adjusted is positioned in a channel applied with a flowing aerosol, wherein a smoke detector which is already adjusted and functions as a reference detector is disposed in the channel together with the at least one smoke detector to be adjusted, wherein the channel for receiving the at least one smoke detector to be adjusted and the reference detector has a housing in each case and wherein the housings included in the channel are connected to one another by means of pipe sections such that each output side of a housing is connected to an input side of a housing which follows along the channel wherein the at least one smoke detector to be adjusted is adjusted by means of data available from the reference detector.
An optical transmitter comprising: a mapper that is adapted to generate an electric signal that indicates an amplitude and a phase of a modulated optical signal to be output from the optical transmitter using an in-phase component and a quadrature component from transmission data; a phase rotation circuit adapted to add a phase rotation to the electric signal; a driver (13a-13d) adapted to generate a driving signal from the electric signal to which the phase rotation is added; a light source adapted to generate continuous wave light; and a modulator (15x, 15y) adapted to modulate the continuous wave light according to the driving signal to generate the modulated optical signal, characterized in that the optical transmitter further includes: a detector adapted to detect a carrier frequency of the modulated optical signal; and a bias controller adapted to control a bias of the modulator according to a change in the carrier frequency of the modulated optical signal detected by the detector corresponding to the phase rotation that is added to the electric signal by the phase rotation circuit. a mapper that is adapted to generate an electric signal that indicates an amplitude and a phase of a modulated optical signal to be output from the optical transmitter using an in-phase component and a quadrature component from transmission data; a phase rotation circuit adapted to add a phase rotation to the electric signal; a driver (13a-13d) adapted to generate a driving signal from the electric signal to which the phase rotation is added; a light source adapted to generate continuous wave light; and a modulator (15x, 15y) adapted to modulate the continuous wave light according to the driving signal to generate the modulated optical signal, characterized in that the optical transmitter further includes: a detector adapted to detect a carrier frequency of the modulated optical signal; and a bias controller adapted to control a bias of the modulator according to a change in the carrier frequency of the modulated optical signal detected by the detector corresponding to the phase rotation that is added to the electric signal by the phase rotation circuit. a detector adapted to detect a carrier frequency of the modulated optical signal; and a bias controller adapted to control a bias of the modulator according to a change in the carrier frequency of the modulated optical signal detected by the detector corresponding to the phase rotation that is added to the electric signal by the phase rotation circuit.
A method of processing label paper which comprises the steps of: with a printer in which label paper is adapted to be fed to travel intermittently in a path of intermittent travel, printing the la bel paper with a print image and a cutting locus along the contour of a shape to be cut out; and thereafter while the printed label paper is being fed to travel continuously in a path of continuous travel, half-cutting the printed label paper along the printed cutting locus, with a laser beam irradiated so as to trace and scan the printed cutting locus, thereby forming a half-cutout of said shape in the label paper. with a printer in which label paper is adapted to be fed to travel intermittently in a path of intermittent travel, printing the la bel paper with a print image and a cutting locus along the contour of a shape to be cut out; and thereafter while the printed label paper is being fed to travel continuously in a path of continuous travel, half-cutting the printed label paper along the printed cutting locus, with a laser beam irradiated so as to trace and scan the printed cutting locus, thereby forming a half-cutout of said shape in the label paper.
A compound of Formula or a pharmaceutically acceptable salt thereof, or hydrate thereof, (wherein, X 1 represents CH 2 or O, k represents 1, 2, or 3, R 3 represents H or C 1-6 alkyl, X 2 represents CH or N, L 1 represents C 1-6 alkylene, R 1 represents H or C 1-6 alkyl, X 3 represents CH or N, L 2 represents C 1-6 alkylene, R 5 represents H or C 1-6 alkyl, R 6 represents H, C 1-6 alkyl, C 1-6 alkyl substituted with one to two of -OR 0, -C - C 1-6 alkyl, -S m - C 1-6 alkyl, - C 1-6 alkylene-N(C 1-6 alkyl) 2, -R 00 -heterocycle, -R 00 -phenyl, or -R 00 -C 3-10 cycloalkyl, wherein the heterocycle, phenyl and C 3-10 cycloalkyl may be substituted with one to two C 1-6 alkyl or C -C 1-6 alkyl, and -R 00 may be substituted with one -OR 0, R 00 represents a bond or C 1-6 alkylene, R 0 represents H or C 1-6 alkyl, m represents 0, 1, or 2, L 3 represents C 1-6 alkylene, n represents 0 or 1, R 4 represents H, C 1-6 alkyl, -C 1-6 alkylene-COO-R 0, -C 1-6 alkylene-OR 0, -C 1-6 alkylene-NHR 0, -C 1-6 alkylene-N(C 1-6 alkyl) 2, or C 3-10 cycloalkyl, L 4 represents a bond, O, or -NR 0 -, Y represents -R 00 -monocyclic heterocycle-R 00 -, -R 00 -phenyl-R 00 -, -C 1-6 alkylene-NR 0 - C 1-6 alkylene-, C 1-6 alkylene-O-C 1-6 alkylene-, or C 1-6 alkylene which may be substituted with a hydroxyl group, and, R 2 represents H or C 1-6 alkyl); wherein the heterocycle is a 3 to 15 membered mono- to tricyclic heterocycle containing 1 to 4 hetero atoms selected from O, S and N. X 1 represents CH 2 or O, k represents 1, 2, or 3, R 3 represents H or C 1-6 alkyl, X 2 represents CH or N, L 1 represents C 1-6 alkylene, R 1 represents H or C 1-6 alkyl, X 3 represents CH or N, L 2 represents C 1-6 alkylene, R 5 represents H or C 1-6 alkyl, R 6 represents H, C 1-6 alkyl, C 1-6 alkyl substituted with one to two of -OR 0, -C - C 1-6 alkyl, -S m - C 1-6 alkyl, - C 1-6 alkylene-N(C 1-6 alkyl) 2, -R 00 -heterocycle, -R 00 -phenyl, or -R 00 -C 3-10 cycloalkyl, wherein the heterocycle, phenyl and C 3-10 cycloalkyl may be substituted with one to two C 1-6 alkyl or C -C 1-6 alkyl, and -R 00 may be substituted with one -OR 0, R 00 represents a bond or C 1-6 alkylene, R 0 represents H or C 1-6 alkyl, m represents 0, 1, or 2, L 3 represents C 1-6 alkylene, n represents 0 or 1, R 4 represents H, C 1-6 alkyl, -C 1-6 alkylene-COO-R 0, -C 1-6 alkylene-OR 0, -C 1-6 alkylene-NHR 0, -C 1-6 alkylene-N(C 1-6 alkyl) 2, or C 3-10 cycloalkyl, L 4 represents a bond, O, or -NR 0 -, Y represents -R 00 -monocyclic heterocycle-R 00 -, -R 00 -phenyl-R 00 -, -C 1-6 alkylene-NR 0 - C 1-6 alkylene-, C 1-6 alkylene-O-C 1-6 alkylene-, or C 1-6 alkylene which may be substituted with a hydroxyl group, and, R 2 represents H or C 1-6 alkyl); wherein the heterocycle is a 3 to 15 membered mono- to tricyclic heterocycle containing 1 to 4 hetero atoms selected from O, S and N.
A process group comprising a first and a second process unit which are designed as reactors, wherein a front, a middle and a rear heat accumulator are provided which are connected in series and which are designed as layered heat accumulators in such a way that a temperature distribution can be generated in them which form a temperature wave, wherein, via line connections, of a conduit arrangement for heat-transporting fluid, this fluid can flow longitudinally through the arrangement of alternately the heat accumulators to and the process units,, wherein the conduit arrangement can be switched in such a way that the fluid flows through the combined process group cyclically alternately from the conduit connection to the conduit connection and from the conduit connection to the conduit connection.
A jewelry system comprising a clasp, the clasp comprising two arms (13, 14) and a sleeve slidable to a position covering at least portions of both arms in order to urge the clasp from an un-locked state towards a locked state, each arm has an end and the ends of the arms are more distant from each other in the un-locked state than in the locked state, wherein one of the arms adjacent its end is configured to attach to a chain of the jewelry system, and wherein the attachment is permanent, for example by welding, and at least portions of both arms are adapted to bear against an inner surface of the sleeve in the locked state of the clasp, and characterized in that the sleeve at least in the un-locked state of the clasp is slidable over the chain.
Axial turbomachine having a rotor blade cascade which is formed by rotor blades in each case with a front edge and a freestanding blade tip which lies radially on the outside, and an annular chamber wall which encases the rotor blade cascade and has an annular chamber inner side, by way of which the annular chamber wall is arranged directly adjacently with respect to the blade tips with the configuration of a radial gap between the envelope of the blade tips and the annular chamber inner side, the gap size of the radial gap being constant, and the radial gap having a homogeneous and undulating course which does not change abruptly along the main throughflow direction of the axial turbomachine, each rotor blade having, at its blade tip, a first radial elevation with a first curvature section and a second curvature section, the annular chamber wall having, on the annular chamber inner side, a circumferential first radial depression with a first and a second curvature section (19, 21) within an axial section of the annular chamber inner side, which axial section lies opposite the blade tip, which circumferential first radial depression is arranged at a constant radial spacing along the main throughflow direction of the axial turbomachine from the envelope of the blade tips which correspond to the annular chamber inner side, characterized in that the courses of the annular chamber inner side, the rotor blade tip and the radial gap, which courses are configured in the manner of a double wave, have in each case at least four curvature sections which are delimited by way of inflection points, the blade tip having, along a profile chord of the rotor blade, and the annular chamber wall having, along the main throughflow direction of the axial turbomachine, in each case at least • one third curvature section which adjoins the second curvature section, and • one fourth curvature section which adjoins the third curvature section, • the first curvature section being delimited from the second curvature section by way of a first inflection point, • the second curvature section being delimited from the third curvature section by way of a second inflection point, and • the third curvature section being delimited from the fourth curvature section by way of a third inflection point, the curvatures of adjacent curvature sections (19, 21, 23, 25) having different algebraic signs, the curvature sections (19, 21, 23, 25) being formed in such a way that the course of the radial gap runs substantially free of edges and steps along the main throughflow direction of the axial turbomachine. • one third curvature section which adjoins the second curvature section, and • one fourth curvature section which adjoins the third curvature section, • the first curvature section being delimited from the second curvature section by way of a first inflection point, • the second curvature section being delimited from the third curvature section by way of a second inflection point, and • the third curvature section being delimited from the fourth curvature section by way of a third inflection point,
A method for manufacturing face protection masks, comprising: - forming an array of mask bodies advancing in a machine direction, - forming a first and a second array (108', 108") of ear loops, wherein each ear loop includes a respective portion of U-bent elastic thread, - attaching successive pairs of ear loops to respective mask bodies, wherein said step of forming a first and a second array (108', 108") of ear loops, comprises: - feeding two continuous elastic threads in respective longitudinal directions, said method being characterised in that it further comprises: - retaining terminal portions of each of said continuous elastic threads by respective arrays of holding sectors (90, 92) carried by a mobile structure, wherein said holding sectors (90, 92) are arranged in groups of sectors which hold respective elastic thread portions, wherein each of said groups of sectors comprises a fixed sector and two movable sectors arranged laterally on opposite sides of the fixed sector, - cutting successive elastic thread portions between each pair of groups of sectors adjacent to each other so that each group of sectors holds a respective discrete elastic thread portion, - bending each of said discrete elastic thread portions into a U-shape by rotating said movable sectors of each of said groups of sectors with respect to the respective fixed sector, so as to form a succession of discrete U-bent elastic thread portions. - forming an array of mask bodies advancing in a machine direction, - forming a first and a second array (108', 108") of ear loops, wherein each ear loop includes a respective portion of U-bent elastic thread, - attaching successive pairs of ear loops to respective mask bodies, - feeding two continuous elastic threads in respective longitudinal directions, - retaining terminal portions of each of said continuous elastic threads by respective arrays of holding sectors (90, 92) carried by a mobile structure, wherein said holding sectors (90, 92) are arranged in groups of sectors which hold respective elastic thread portions, wherein each of said groups of sectors comprises a fixed sector and two movable sectors arranged laterally on opposite sides of the fixed sector, - cutting successive elastic thread portions between each pair of groups of sectors adjacent to each other so that each group of sectors holds a respective discrete elastic thread portion, - bending each of said discrete elastic thread portions into a U-shape by rotating said movable sectors of each of said groups of sectors with respect to the respective fixed sector, so as to form a succession of discrete U-bent elastic thread portions.