mhurhangee/ep-ind-claims huggingface dataset:
A vehicle brake hydraulic controller including: an antilock braking controlling module configured to perform an antilock braking control in which a brake hydraulic pressure applied to wheel brakes is reduced under the condition that a slip-related amount has reached a pressure reduction threshold value (Sr, Sf), the slip-related amount being calculated using a vehicle speed and a wheel speed; and a turning judging module configured to judge whether a vehicle is turning based on a steering angle, wherein when the antilock braking control is performed and in the case that the turning judging module judges that the vehicle is turning, the antilock braking controlling module performs a turning pressure reduction control so as to: change the pressure reduction threshold values (Sr, Sf) to be more easily reached by the slip-related amount than at the time of straight running; characterized in that the antilock braking controlling module further performs the turning pressure reduction control so as to change the pressure reduction amounts (Pr, Pf) to be larger than that at the time of straight running. an antilock braking controlling module configured to perform an antilock braking control in which a brake hydraulic pressure applied to wheel brakes is reduced under the condition that a slip-related amount has reached a pressure reduction threshold value (Sr, Sf), the slip-related amount being calculated using a vehicle speed and a wheel speed; and a turning judging module configured to judge whether a vehicle is turning based on a steering angle, wherein when the antilock braking control is performed and in the case that the turning judging module judges that the vehicle is turning, the antilock braking controlling module performs a turning pressure reduction control so as to: change the pressure reduction threshold values (Sr, Sf) to be more easily reached by the slip-related amount than at the time of straight running; characterized in that the antilock braking controlling module further performs the turning pressure reduction control so as to change the pressure reduction amounts (Pr, Pf) to be larger than that at the time of straight running. change the pressure reduction threshold values (Sr, Sf) to be more easily reached by the slip-related amount than at the time of straight running; characterized in that the antilock braking controlling module further performs the turning pressure reduction control so as to change the pressure reduction amounts (Pr, Pf) to be larger than that at the time of straight running.
Dispenser container consisting of an outer container and an inner container for receiving a fluid, the outer container and the inner container being formed of blow-moulded plastics materials that do not form an integral connection to one another, and a first plastics material of which the inner container is formed having a higher elasticity than a second plastics material of which the outer container is formed, such that the inner container can be deformed by a low pressure that is generated, the dispenser container comprising an outlet region, a middle region and a bottom region, and the outer container comprising at least one pressure compensation opening for pressure compensation in the region between the outer container and the inner container, characterised in that both the outer container and the inner container are formed in one piece without connection seams, the inner container comprising, on the outer face thereof, at least one projection that projects into the at least one pressure compensation opening before the first deformation of the inner container such that the pressure compensation opening is closed.
An organic electroluminescence device having at least an anode, a hole injection layer, a first hole transport layer, a second hole transport layer, a luminous layer, an electron transport layer, and a cathode in order of description, characterized in that wherein the second hole transport layer includes an arylamine compound represented by the following general formula, and the electron transport layer includes a pyrimidine derivative represented by the following general formula: wherein Ar 1 to Ar 4 each represent an unsubstituted aromatic hydrocarbon group, an unsubstituted aromatic heterocyclic group, or an unsubstituted condensed polycyclic aromatic group, wherein Ar 1 and Ar 2 are different groups and Ar 3 and Ar 4 are different groups; and n represents an integer of 2 or 3, wherein Ar 5 represents an aromatic hydrocarbon group; Ar 6 represents a phenyl group substituted with a condensed polycyclic aromatic group; Ar 7 represents a hydrogen atom; and A represents a monovalent group represented by the following structural formula: wherein Ar 8 represents an aromatic heterocyclic group; R 1 to R 4 each represent a hydrogen atom. Ar 1 to Ar 4 each represent an unsubstituted aromatic hydrocarbon group, an unsubstituted aromatic heterocyclic group, or an unsubstituted condensed polycyclic aromatic group, wherein Ar 1 and Ar 2 are different groups and Ar 3 and Ar 4 are different groups; and n represents an integer of 2 or 3, Ar 5 represents an aromatic hydrocarbon group; Ar 6 represents a phenyl group substituted with a condensed polycyclic aromatic group; Ar 7 represents a hydrogen atom; and A represents a monovalent group represented by the following structural formula: Ar 8 represents an aromatic heterocyclic group; R 1 to R 4 each represent a hydrogen atom.
A method of analyzing a pressure distribution profile (P(x,y,t)) of the spatial distribution of pressure over time of a subject lying on a pressure mat to derive a measure of pulse wave velocity of blood in the subject, wherein the method comprises: identifying beat locations in the subject where beat pressure signals are identified; obtaining pulse timing information from the beat locations; determining from the pressure distribution profile a subject posture and mapping the beat locations to anatomical body locations of the subject according to that posture; determining an arterial path length for the anatomical body locations; and estimating a pulse wave velocity from the pulse timing information and arterial path length. identifying beat locations in the subject where beat pressure signals are identified; obtaining pulse timing information from the beat locations; determining from the pressure distribution profile a subject posture and mapping the beat locations to anatomical body locations of the subject according to that posture; determining an arterial path length for the anatomical body locations; and estimating a pulse wave velocity from the pulse timing information and arterial path length.
A mobile terminal, comprising: a camera; a touch screen; and a controller configured to control the touch screen to output a preview screen of the camera when a video is recorded by the camera, wherein the controller is further configured to: pause the output of the preview screen and store a touch path of a touch and drag input as a handwriting memo which is contained in the recorded video, when the touch and drag input is received on the outputted preview screen. a camera; a touch screen; and a controller configured to control the touch screen to output a preview screen of the camera when a video is recorded by the camera, wherein the controller is further configured to: pause the output of the preview screen and store a touch path of a touch and drag input as a handwriting memo which is contained in the recorded video, when the touch and drag input is received on the outputted preview screen.
A cosmetic application tool, including: a shaft; and an applicator, in which electrostatic flocking is implemented on a surface of a spatula, the applicator being formed by an application portion in a flat plate shape and a root portion in a columnar shape attached to the shaft, wherein said flat application portion deforms gradually from said columnar shape of the root portion into said plate shape, wherein a projecting portion that projects outward beyond an outer diameter of said shaft is formed on said spatula between said root portion and said application portion, wherein a maximum projection portion having a greater width than said projecting portion is formed in said application portion, and characterized in that a part extending from said root portion to said maximum projecting portion is not subjected to flocking. a shaft; and an applicator, in which electrostatic flocking is implemented on a surface of a spatula, the applicator being formed by an application portion in a flat plate shape and a root portion in a columnar shape attached to the shaft, wherein said flat application portion deforms gradually from said columnar shape of the root portion into said plate shape, wherein a projecting portion that projects outward beyond an outer diameter of said shaft is formed on said spatula between said root portion and said application portion, wherein a maximum projection portion having a greater width than said projecting portion is formed in said application portion, and characterized in that a part extending from said root portion to said maximum projecting portion is not subjected to flocking.
A spunbond nonwoven fabric for use in filters, comprising a thermoplastic continuous filament and having a partially fused portion, wherein the nonwoven fabric has a stiffness as measured according to the description of 2 mN or more and 100 mN or less, a weight per unit area-CV value as measured according to the description of 5% or less, and a weight per unit area of 150 g/m 2 or more and 300 g/m 2 or less and wherein the spunbond nonwoven fabric is obtainable by a method comprising the following steps (a) to (c) to be sequentially performed: the step (a) of melt-extruding a thermoplastic polymer from a spinneret, and then towing and stretching the melt-extruded product using an air sucker to obtain thermoplastic continuous filaments; the step (b) of regulating alignment of fibers using a fiber spreading plate to deposit the obtained filaments on a moving net conveyor, thereby forming a fiber web; and the step (c) of subjecting the obtained fiber web to partial thermocompression bonding. the step (a) of melt-extruding a thermoplastic polymer from a spinneret, and then towing and stretching the melt-extruded product using an air sucker to obtain thermoplastic continuous filaments; the step (b) of regulating alignment of fibers using a fiber spreading plate to deposit the obtained filaments on a moving net conveyor, thereby forming a fiber web; and the step (c) of subjecting the obtained fiber web to partial thermocompression bonding.
An enthalpy exchanger for an earth-to-air heat exchanger, said exchanger comprising: - an air duct including a side wall provided with openings; - a waterproof-breathable membrane disposed on an outer surface of the side wall of the air duct or on an inner surface of this side wall; and characterised in that the exchanger further includes: - a porous outer layer, permeable to water vapour and designed to trap a volume of buffer air, said porous outer layer covering the assembly formed by the side wall of the air duct and the waterproof-breathable membrane. - an air duct including a side wall provided with openings; - a waterproof-breathable membrane disposed on an outer surface of the side wall of the air duct or on an inner surface of this side wall; and - a porous outer layer, permeable to water vapour and designed to trap a volume of buffer air, said porous outer layer covering the assembly formed by the side wall of the air duct and the waterproof-breathable membrane.
Arrangement for inductive energy transmission to an electrical load, wherein a secondary winding is inductively coupled to a primary conductor, wherein to form a resonant circuit an arrangement of capacitors (C_res2, C_res3, C_res4) is connected to the secondary winding, characterised in that the capacitors (C_res2, C_res3, C_res4) are respectively connectable or respectively disconnectable with a controllable semiconductor switch (AC-S2, AC-S3, AC-S4) connected in parallel with respectively one capacitor (C_res2, C_res3, C-_res4), in particular therefore can be made active or inactive for the resonant circuit, in particular for tuning the resonant frequency of the resonant circuit to a target frequency, in particular to a frequency of the current applied to the primary conductor, wherein the arrangement of capacitors (C_res2, C_res3, C_res4) is configured as a series connection of the capacitors (C_res2, C_res3, C_res4), wherein the capacitors (C_res2, C_res3, C_res4) are short-circuitable with the respectively controllable semiconductor switch (AC-S2, AC-S3, AC-S4) connected in parallel, in particular wherein a boost converter arrangement with rectifier arrangement is supplied from the resonant circuit, the output voltage of which arrangement supplies a load.
A method of making glass containers, the method including the steps of: preparing a black-strikable glass composition that is used to produce cobalt blue glass, which, upon heat treatment and striking, develops a visually black color, the black-strikable glass composition having a base glass portion and a latent colorant portion, the base glass portion including 60-75 wt. % SiO 2, 7-15 wt. % Na 2 O, 6-12 wt. % CaO, 0.1-3.0 wt. % Al 2 O 3, 0.0-2.0 wt. % MgO, 0.0-2.0 wt. % K 2 O, 0.01-0.25 wt. % SO 3, 0.01-0.25 wt. % Fe 2 O 3, and 0.01-0.15 wt. % CoO and the latent colorant portion including 0.0875-0.35 wt. % cuprous oxide (Cu 2 O), 0.06-0.5 wt. % stannous oxide (SnO), 0.006-0.05 wt. % bismuth oxide (Bi 2 O 3), and 0.02-0.10 wt. % carbon; and forming a plurality of glass containers from the black-strikable glass composition, wherein the plurality of glass containers can be struck black to produce a plurality of black glass containers that transmit infrared light in the near-infrared region of the electromagnetic spectrum so as to be inspectable using an infrared light source. preparing a black-strikable glass composition that is used to produce cobalt blue glass, which, upon heat treatment and striking, develops a visually black color, the black-strikable glass composition having a base glass portion and a latent colorant portion, the base glass portion including 60-75 wt. % SiO 2, 7-15 wt. % Na 2 O, 6-12 wt. % CaO, 0.1-3.0 wt. % Al 2 O 3, 0.0-2.0 wt. % MgO, 0.0-2.0 wt. % K 2 O, 0.01-0.25 wt. % SO 3, 0.01-0.25 wt. % Fe 2 O 3, and 0.01-0.15 wt. % CoO and the latent colorant portion including 0.0875-0.35 wt. % cuprous oxide (Cu 2 O), 0.06-0.5 wt. % stannous oxide (SnO), 0.006-0.05 wt. % bismuth oxide (Bi 2 O 3), and 0.02-0.10 wt. % carbon; and forming a plurality of glass containers from the black-strikable glass composition, wherein the plurality of glass containers can be struck black to produce a plurality of black glass containers that transmit infrared light in the near-infrared region of the electromagnetic spectrum so as to be inspectable using an infrared light source.
A third harmonic generator comprising: a first beam combiner (25, 85) configured to combine a first fundamental optical beam with a second harmonic optical beam; a third harmonic crystal (28, 88) coupled to the first beam combiner (25, 85), configured to generate a third harmonic optical beam from the first fundamental optical beam and the second harmonic optical beam, wherein upon generation of the third harmonic optical beam, a residual fundamental optical beam exits the third harmonic crystal (28, 88); a first beam splitter (27, 87) coupled to the third harmonic crystal (28, 88), configured to separate the residual fundamental optical beam and the third harmonic optical beam; and a second harmonic crystal (26, 86) coupled to the first beam splitter (27, 87), configured to generate the second harmonic optical beam from the residual fundamental optical beam, and for coupling the second harmonic optical beam to the first beam combiner (25, 85), characterised in that the third harmonic crystal (28, 88) and the second harmonic crystal (26, 86) are arranged such that the first fundamental optical beam enters the third harmonic generator through the first beam combiner (25,85) and propagates in sequence first through the third harmonic crystal (28, 88) and then through the second harmonic crystal (26, 86), via the first beam splitter (27, 87), to generate the third harmonic optical beam from the first fundamental optical beam and the second harmonic optical beam, as combined by the first beam combiner (25, 85). a first beam combiner (25, 85) configured to combine a first fundamental optical beam with a second harmonic optical beam; a third harmonic crystal (28, 88) coupled to the first beam combiner (25, 85), configured to generate a third harmonic optical beam from the first fundamental optical beam and the second harmonic optical beam, wherein upon generation of the third harmonic optical beam, a residual fundamental optical beam exits the third harmonic crystal (28, 88); a first beam splitter (27, 87) coupled to the third harmonic crystal (28, 88), configured to separate the residual fundamental optical beam and the third harmonic optical beam; and a second harmonic crystal (26, 86) coupled to the first beam splitter (27, 87), configured to generate the second harmonic optical beam from the residual fundamental optical beam, and for coupling the second harmonic optical beam to the first beam combiner (25, 85), characterised in that the third harmonic crystal (28, 88) and the second harmonic crystal (26, 86) are arranged such that the first fundamental optical beam enters the third harmonic generator through the first beam combiner (25,85) and propagates in sequence first through the third harmonic crystal (28, 88) and then through the second harmonic crystal (26, 86), via the first beam splitter (27, 87), to generate the third harmonic optical beam from the first fundamental optical beam and the second harmonic optical beam, as combined by the first beam combiner (25, 85).
A composite airfoil for a gas turbine engine comprising: first pressure and suction side layers (84, 88) constructed from a composite material and forming a cavity; characterized in that the first pressure and suction side (84, 88) layers terminate in ends (96, 98) near a trailing edge; and in that the airfoil further comprises a bridge wrapped about the ends (96, 98). first pressure and suction side layers (84, 88) constructed from a composite material and forming a cavity; characterized in that the first pressure and suction side (84, 88) layers terminate in ends (96, 98) near a trailing edge; and in that the airfoil further comprises a bridge wrapped about the ends (96, 98).
A semiconductor package comprising: a redistribution substrate having first and second surfaces (130A,B) disposed opposite to each other, and including an insulation member, a plurality of redistribution layers (121, 122) disposed on different levels in the insulation member, and a redistribution via connecting the redistribution layers disposed on neighboring levels and having a shape narrowing from the second surface toward the first surface in a first direction; a plurality of under bump metallurgy layers, each of the plurality of UBM layers including a UBM pad disposed on the first surface of the redistribution substrate, and a UBM via connected to a redistribution layer adjacent to the first surface among the plurality of redistribution layers and connected to the UBM pad, and having a shape narrowing in a second direction opposite to the first direction, wherein each of the plurality of UBM layers has a thickness greater than a thickness of the redistribution layer adjacent to the first surface; and at least one semiconductor chip disposed on the second surface of the redistribution substrate, and having a plurality of contact pads electrically connected to a redistribution layer adjacent to the second surface among the plurality of redistribution layers. a redistribution substrate having first and second surfaces (130A,B) disposed opposite to each other, and including an insulation member, a plurality of redistribution layers (121, 122) disposed on different levels in the insulation member, and a redistribution via connecting the redistribution layers disposed on neighboring levels and having a shape narrowing from the second surface toward the first surface in a first direction; a plurality of under bump metallurgy layers, each of the plurality of UBM layers including a UBM pad disposed on the first surface of the redistribution substrate, and a UBM via connected to a redistribution layer adjacent to the first surface among the plurality of redistribution layers and connected to the UBM pad, and having a shape narrowing in a second direction opposite to the first direction, wherein each of the plurality of UBM layers has a thickness greater than a thickness of the redistribution layer adjacent to the first surface; and at least one semiconductor chip disposed on the second surface of the redistribution substrate, and having a plurality of contact pads electrically connected to a redistribution layer adjacent to the second surface among the plurality of redistribution layers.
A peptide comprising the amino acid sequence of SEQ ID NO: 2, with the proviso that the peptides with the amino acid sequences of SEQ ID NOs: 23 and 25 of WO/2013/025972 A1 are excluded.
A planet carrier for a speed reduction gear of a turbomachine, this planet carrier having a main axis X and comprising: - a cage carrier comprising an annular row of axial fingers about the axis X, which carry first connecting elements, and - a cage comprising an internal cavity configured to contain a central sun gear of axis X of rotation and an annular row of planet gears disposed about the axis X and meshed with said sun gear and with a ring gear for surrounding the cage, the cage comprising at its periphery housings and second connecting elements which are mounted in said housings and which cooperate with the first connecting elements to form connections between the cage carrier and the cage, which allow at least one degree of freedom, the cage comprising two shells (220a, 220b) which are axially fixed to each other and separated from each other by a plane, said housings being formed respectively in said shells (220a, 220b), each of said housings comprising a first orifice formed in a first of the shells and a second orifice formed in a second of the shells, the first and second orifices (280a, 280b) being aligned, characterised in that the shells (220a, 220b) comprise radial tabs in axial support against each other or axially spaced from each other and in which said first and second orifices (280a, 280b) are formed respectively. - a cage carrier comprising an annular row of axial fingers about the axis X, which carry first connecting elements, and - a cage comprising an internal cavity configured to contain a central sun gear of axis X of rotation and an annular row of planet gears disposed about the axis X and meshed with said sun gear and with a ring gear for surrounding the cage, the cage comprising at its periphery housings and second connecting elements which are mounted in said housings and which cooperate with the first connecting elements to form connections between the cage carrier and the cage, which allow at least one degree of freedom, the cage comprising two shells (220a, 220b) which are axially fixed to each other and separated from each other by a plane, said housings being formed respectively in said shells (220a, 220b), each of said housings comprising a first orifice formed in a first of the shells and a second orifice formed in a second of the shells, the first and second orifices (280a, 280b) being aligned, characterised in that the shells (220a, 220b) comprise radial tabs in axial support against each other or axially spaced from each other and in which said first and second orifices (280a, 280b) are formed respectively.