mhurhangee/ep-ind-claims huggingface dataset:
A paint baking method comprising: - preparing a paint baking oven, with the oven comprising an oven body and a hot air supplier, the hot air supplier supplying hot air into the oven body; and - baking a wet coating film applied to a vehicle body while conveying the vehicle body, with the vehicle body: - having a main shell body to which a lid part is attached via a hinge, and - including a body exterior part and a coated surface of the main shell body and the lid part adjacent to the hinge, characterized in that - the wet coating film is formed by a thermoset paint, and - baking the wet coating film applied to the vehicle body includes: - first and at an upstream side of the oven body blowing the hot air only toward the coated surface in a state in which the lid part is fully opened with a first, larger angle, to locally bake a coating film applied to the coated surface adjacent to the hinge, and - then afterwards and at a downstream side of the oven body blowing the hot air to the whole vehicle body in a state in which the lid part is slightly opened with a second, smaller angle, to bake the coating film applied to the vehicle body. - preparing a paint baking oven, with the oven comprising an oven body and a hot air supplier, the hot air supplier supplying hot air into the oven body; and - baking a wet coating film applied to a vehicle body while conveying the vehicle body, with the vehicle body: - having a main shell body to which a lid part is attached via a hinge, and - including a body exterior part and a coated surface of the main shell body and the lid part adjacent to the hinge, characterized in that - having a main shell body to which a lid part is attached via a hinge, and - including a body exterior part and a coated surface of the main shell body and the lid part adjacent to the hinge, - the wet coating film is formed by a thermoset paint, and - baking the wet coating film applied to the vehicle body includes: - first and at an upstream side of the oven body blowing the hot air only toward the coated surface in a state in which the lid part is fully opened with a first, larger angle, to locally bake a coating film applied to the coated surface adjacent to the hinge, and - then afterwards and at a downstream side of the oven body blowing the hot air to the whole vehicle body in a state in which the lid part is slightly opened with a second, smaller angle, to bake the coating film applied to the vehicle body. - first and at an upstream side of the oven body blowing the hot air only toward the coated surface in a state in which the lid part is fully opened with a first, larger angle, to locally bake a coating film applied to the coated surface adjacent to the hinge, and - then afterwards and at a downstream side of the oven body blowing the hot air to the whole vehicle body in a state in which the lid part is slightly opened with a second, smaller angle, to bake the coating film applied to the vehicle body.
A non-dispersive infrared carbon dioxide gas sensor for measuring a concentration of carbon dioxide included in a gas, wherein the gas sensor comprises a White cell including first, second and third reflectors (120, 130, 140), the radius of curvature of the third reflector being the same as the radius of curvature of the first and second reflectors (120,130) and the length of the third reflector being the double of the length of the first reflector and the length of the second reflector being equal to the length of the first reflector, wherein the first and second reflectors (120, 130) are disposed to face the third reflector; a first protective window; a light source arranged at one side of the third reflector, the light source being arranged to emit light in direction of the first reflector and the first protective window being arranged in front of the light source; a first detector for measuring the concentration of carbon dioxide; a second detector as a reference detector for detecting infrared light having a central wavelength of 3.91 μm, the first detector and the second detector being arranged at the other side of the third reflector to receive light reflected by the second reflector; a Fresnel lens provided in front of the first detector; a second protective window; a hollow disk, the second protective window and the hollow disk being provided in front of the second detector; a first and a second heater (230, 240), the first heater being mounted in the vicinity of the third reflector and the second heater being mounted in the vicinity of the first and second reflectors (120,130); and first, second and third hydrophobic thin films (122,132,142), wherein the first thin film is deposited on the entire reflective surface of the first reflector, the second thin film is deposited on the entire reflective surface of the second reflector and the third thin film is deposited on the entire reflective surface of the third reflector and wherein the first, second and third hydrophobic thin films (122,132,142) comprise parylene-C and wherein the deposition thickness of the parylene-C is 0.5 μm.
A process of using a finishing system for surfaces of a wind turbine blade, the finishing system consisting of a gel coat, a putty; and a top coat; wherein the process comprises: applying a gel coat to a mold substrate; laying up and infusing a resin with woven fiber cloth to form a shell with an outer surface defining a wind turbine blade; applying a putty to outer uneven surfaces to form an even surface; sanding the cured putty surface to yield a smooth finished sanded surface; and applying a top coat to the blade surface.
A brazing sheet formed of an aluminum alloy comprising a core layer, a brazing filler layer provided on one side of the core layer and formed of an Al-Si based alloy, and a sacrificial layer provided on the other side of the core layer, the brazing sheet having a thickness of less than 200 μm, wherein the core layer consists of Cu: more than 1.5% by mass and 2.5% or less by mass and Mn: 0.5 to 2.0% by mass, and optionally: Si: 0.05 to 0.5% by mass, Mg: 0.05 to 0.5% by mass, and/or at least one selected from the group consisting of Cr: 0.01 to 0.30% by mass, Zr: 0.01 to 0.30% by mass and Ti: 0.05 to 0.30% by mass, with the balance being Al and inevitable impurities, the sacrificial layer consists of Zn: 2.0 to 7.0% by mass and Mg: more than 0.10% by mass and 3.0% or less by mass, and optionally: Si: 0.05 to 0.5% by mass, Mn: 0.1 to 2.0% by mass, Ti: 0.01 to 0.30% by mass, and/or at least one of Cr: 0.01 to 0.30% by mass and Zr: 0.01 to 0.30% by mass, with the balance being Al and inevitable impurities, each of the brazing filler layer and the sacrificial layer has a thickness of 15 to 50 μm, and a total of clad rates of the brazing filler layer and the sacrificial layer is equal to or less than 50%.
A natural leather trimming machine comprising: - an ironing device for stretching and removing creases and wrinkles of said natural leather; - cutting means arranged downstream of said ironing device, and configured to cut said natural leather along at least one cutting line; - a detection unit arranged in correspondence of the entrance of said natural leather into said cutting means, said detection unit being configured to detect the position of said natural leather, the conformation of at least one end edge thereof, and the position of any defects of said natural leather in proximity to said at least one end edge; - a plurality of conveyor belts (51, 52, 53) configured, respectively, to move said natural leather from said ironing device towards said detection unit, present and subsequently move said natural leather away to/from said cutting means; - a first command and control unit configured to determine the cutting coordinates of the natural leather on the basis of said position of said natural leather, of said shape of at least one end edge, and of said position of any defects, wherein said cutting coordinates define said at least one cutting line; said machine being characterised in that said cutting means comprise at least one laser source, and said conveyor belt of said plurality of belts (51, 52, 53) has a conveying surface made with a metal mesh to prevent the laser emitted by said at least one source rebounding on said natural leather; said machine also comprising a shielding container inside of which is positioned said at least one laser source. - an ironing device for stretching and removing creases and wrinkles of said natural leather; - cutting means arranged downstream of said ironing device, and configured to cut said natural leather along at least one cutting line; - a detection unit arranged in correspondence of the entrance of said natural leather into said cutting means, said detection unit being configured to detect the position of said natural leather, the conformation of at least one end edge thereof, and the position of any defects of said natural leather in proximity to said at least one end edge; - a plurality of conveyor belts (51, 52, 53) configured, respectively, to move said natural leather from said ironing device towards said detection unit, present and subsequently move said natural leather away to/from said cutting means; - a first command and control unit configured to determine the cutting coordinates of the natural leather on the basis of said position of said natural leather, of said shape of at least one end edge, and of said position of any defects, wherein said cutting coordinates define said at least one cutting line; said machine being characterised in that said cutting means comprise at least one laser source, and said conveyor belt of said plurality of belts (51, 52, 53) has a conveying surface made with a metal mesh to prevent the laser emitted by said at least one source rebounding on said natural leather; said machine also comprising a shielding container inside of which is positioned said at least one laser source.
An oral care composition comprising: a) calcium silicate; b) composite particles; and c) a physiologically acceptable carrier. wherein the composite particle comprises a first component core comprising a metal compound having a refractive index in the range from 1.9 to 4.0, and a second component coating comprising a mixture of: 1) metal oxides and/or hydrated metal oxides; and 2) solid non-metal oxides and/or solid hydrated non-metal oxides; and wherein the metal oxide is alumina and the non-metal oxide is silica. a) calcium silicate; b) composite particles; and c) a physiologically acceptable carrier. wherein the composite particle comprises a first component core comprising a metal compound having a refractive index in the range from 1.9 to 4.0, and a second component coating comprising a mixture of: 1) metal oxides and/or hydrated metal oxides; and 2) solid non-metal oxides and/or solid hydrated non-metal oxides; and wherein the metal oxide is alumina and the non-metal oxide is silica. 1) metal oxides and/or hydrated metal oxides; and 2) solid non-metal oxides and/or solid hydrated non-metal oxides; and wherein the metal oxide is alumina and the non-metal oxide is silica.
A pharmaceutical tablet for oral administration comprising: - from 3 wt% to 18wt% of ulipristal acetate, wherein ulipristal acetate is present in the tablet in an amount ranging from 1 mg to 50 mg together with the following excipients: - from 60 wt% to 95 wt% of a diluent selected from the group consisting of monosaccharides, disaccharides, sugar alcohols, and hydrates thereof, cellulose, and microcrystalline cellulose. - from 0 wt% to 10wt% of a binder, - from 1 wt% to 10 wt% of croscarmellose sodium, and - from 0.5 wt% to 4 wt% of magnesium stearate wt% designating an amount by weight, as a percentage of the total weight of the composition. - from 3 wt% to 18wt% of ulipristal acetate, wherein ulipristal acetate is present in the tablet in an amount ranging from 1 mg to 50 mg together with the following excipients: - from 60 wt% to 95 wt% of a diluent selected from the group consisting of monosaccharides, disaccharides, sugar alcohols, and hydrates thereof, cellulose, and microcrystalline cellulose. - from 0 wt% to 10wt% of a binder, - from 1 wt% to 10 wt% of croscarmellose sodium, and - from 0.5 wt% to 4 wt% of magnesium stearate
Electrical connector, including: - a body, and - a barrel, - at least one electrically conductive sleeve extending around an axis and having a first end and a second end, the second end being opposite the first end, at least one slot being produced in the sleeve and extending from the first end in the direction of the second end, at least one lug extending transversely, notably radially, relative to the axis of the sleeve, characterized by the fact that it includes at least two sleeves, these two sleeves having different dimensions, in such a manner than one sleeve may be received in the interior of the other sleeve. - a body, and - a barrel, - at least one electrically conductive sleeve extending around an axis and having a first end and a second end, the second end being opposite the first end, at least one slot being produced in the sleeve and extending from the first end in the direction of the second end, at least one lug extending transversely, notably radially, relative to the axis of the sleeve,
A method for the microphysiological co-cultivation of organoid tissue in a bioreactor vessel with a semi-permeable membrane on the bottom, comprising the steps: (a) seeding cells of at least one first cell type onto the membrane, (b) cultivating these seeded cells to form at least one 2D cell layer supported on this membrane and (c) introducing into the bioreactor vessel on the supported 2D cell layer - an organoid containing cells of at least two further cell types which are arranged in a defined 3D structure relative to each other, and - a hydrogel with the proviso that the organoid in the bioreactor vessel is defined spaced apart from the supported 2D cell layer by the introduced hydrogel. (a) seeding cells of at least one first cell type onto the membrane, (b) cultivating these seeded cells to form at least one 2D cell layer supported on this membrane and (c) introducing into the bioreactor vessel on the supported 2D cell layer - an organoid containing cells of at least two further cell types which are arranged in a defined 3D structure relative to each other, and - a hydrogel with the proviso that the organoid in the bioreactor vessel is defined spaced apart from the supported 2D cell layer by the introduced hydrogel. - an organoid containing cells of at least two further cell types which are arranged in a defined 3D structure relative to each other, and - a hydrogel
A propeller fan comprising: a hub formed into a cylindrical shape; and a plurality of blades (20a to 20c) extending outward from a side of the hub, at least two of the blades (20a to 20c) having different circumferential pitches, at least two of the blades (20a to 20c) having different masses so that a center of gravity of the propeller fan is positioned near or on a rotational center axis of the propeller fan, projections of the blades (20a to 20c) on a plane orthogonal to the rotational center axis of the propeller fan having a common shape, leading edge portions (41a to 41c) of the blades (20a to 20c) having a common shape, wherein the circumferential pitch of each blade (20a to 20c) is an angle formed between a front end plane (35a to 35c) of the blade (20a to 20c) and a front end plane (35b to 35a) of another one of the blades (20b to 20a) located behind the blade (20a to 20c) in the rotation direction of the propeller fan and the front end plane (35a to 35c) is a plane including the rotational center axis of the propeller fan and being in contact with the leading edge (23a to 23c) of the blade (20a to 20c), characterized in that regions of the blades (20a to 20c) closer to trailing edges (24a to 24c) than to the leading edge portions (41a to 41c) partly or entirely have different thicknesses, allowing the blades (20a to 20c) to have different masses. a hub formed into a cylindrical shape; and a plurality of blades (20a to 20c) extending outward from a side of the hub, at least two of the blades (20a to 20c) having different circumferential pitches, at least two of the blades (20a to 20c) having different masses so that a center of gravity of the propeller fan is positioned near or on a rotational center axis of the propeller fan, projections of the blades (20a to 20c) on a plane orthogonal to the rotational center axis of the propeller fan having a common shape, leading edge portions (41a to 41c) of the blades (20a to 20c) having a common shape, wherein the circumferential pitch of each blade (20a to 20c) is an angle formed between a front end plane (35a to 35c) of the blade (20a to 20c) and a front end plane (35b to 35a) of another one of the blades (20b to 20a) located behind the blade (20a to 20c) in the rotation direction of the propeller fan and the front end plane (35a to 35c) is a plane including the rotational center axis of the propeller fan and being in contact with the leading edge (23a to 23c) of the blade (20a to 20c), characterized in that regions of the blades (20a to 20c) closer to trailing edges (24a to 24c) than to the leading edge portions (41a to 41c) partly or entirely have different thicknesses, allowing the blades (20a to 20c) to have different masses.
A motor control method for controlling a rotation speed of a motor that is driven according to a speed command, wherein an integration of a speed deviation is started when the speed deviation obtained by subtracting a detection speed of a motor rotation from a speed command is equal to or larger than a threshold value, and a sign of a product of acceleration obtained by subtracting a last detection speed from a detection speed this time that are detected in a predetermined cycle and a torque command obtained by proportionally integrating the speed deviation is negative; and it is determined that the motor is in an abnormal-rotation state when the integration value of the speed deviation exceeds a predetermined value.
A method for detecting pathogens, comprising: receiving a test sample comprising environmental air dust captured from airflow within an exhaust plenum of an individually ventilated cage rack by air filtering collection media, wherein a surface of the collection media is oriented at an acute angle within the range from 15° to 25° with respect to a direction of airflow within the exhaust plenum during capture of the test sample; isolating a plurality of nucleic acids from the test sample, wherein the plurality of nucleic acids is representative of one or more pathogens; amplifying at least one of the plurality of nucleic acids; and analyzing the amplified nucleic acids to identify the presence or absence of a pathogen attached to the test sample. receiving a test sample comprising environmental air dust captured from airflow within an exhaust plenum of an individually ventilated cage rack by air filtering collection media, wherein a surface of the collection media is oriented at an acute angle within the range from 15° to 25° with respect to a direction of airflow within the exhaust plenum during capture of the test sample; isolating a plurality of nucleic acids from the test sample, wherein the plurality of nucleic acids is representative of one or more pathogens; amplifying at least one of the plurality of nucleic acids; and analyzing the amplified nucleic acids to identify the presence or absence of a pathogen attached to the test sample.
A cushion including: a pillow portion, an elongate trunk portion and a scarf; the pillow portion having a front side and a rear side, and defining a support surface on the front side which is useable for supporting the head of a user of the cushion; the trunk portion extending away from the pillow portion and having a terminal end which is distal to the pillow portion, wherein the scarf is attached to the pillow portion and/or the trunk portion at a first end portion of the scarf and is engageable, in use, with the trunk portion at a portion of the scarf that is spaced from the first end portion, and characterized in that the pillow portion projects from the trunk portion transversely to the elongation of the trunk portion from two opposite sides of the trunk portion. a pillow portion, an elongate trunk portion and a scarf; the pillow portion having a front side and a rear side, and defining a support surface on the front side which is useable for supporting the head of a user of the cushion; the trunk portion extending away from the pillow portion and having a terminal end which is distal to the pillow portion, wherein the scarf is attached to the pillow portion and/or the trunk portion at a first end portion of the scarf and is engageable, in use, with the trunk portion at a portion of the scarf that is spaced from the first end portion, and characterized in that the pillow portion projects from the trunk portion transversely to the elongation of the trunk portion from two opposite sides of the trunk portion.
Turbofan engine for a civil supersonic aircraft, which turbofan engine has: - an engine inlet which is provided and configured to slow down the incoming air during supersonic flight to speeds below the speed of sound, - a multiple-stage fan which is arranged behind the engine inlet, - a core engine which comprises a compressor, a combustion chamber and a turbine (91, 92), - a primary flow duct which leads through the core engine, - a secondary flow duct which leads past the core engine, - an adjustable convergent-divergent thrust nozzle which configures a nozzle throat area and a nozzle outlet area, at least the nozzle throat area being adjustable, - the thrust nozzle having a front, upstream non-adjustable region and a rear, downstream adjustable region (42, 43), and - a thrust reverser which has thrust reverser doors (151, 160) and is integrated into the adjustable convergent-divergent thrust nozzle, characterized in that the thrust reverser including the thrust reverser doors (151, 160) which deflect the gas stream in the case of a thrust reversal is integrated into the front, non-adjustable region of the thrust nozzle. - an engine inlet which is provided and configured to slow down the incoming air during supersonic flight to speeds below the speed of sound, - a multiple-stage fan which is arranged behind the engine inlet, - a core engine which comprises a compressor, a combustion chamber and a turbine (91, 92), - a primary flow duct which leads through the core engine, - a secondary flow duct which leads past the core engine, - an adjustable convergent-divergent thrust nozzle which configures a nozzle throat area and a nozzle outlet area, at least the nozzle throat area being adjustable, - the thrust nozzle having a front, upstream non-adjustable region and a rear, downstream adjustable region (42, 43), and - a thrust reverser which has thrust reverser doors (151, 160) and is integrated into the adjustable convergent-divergent thrust nozzle,
A low alloy steel with a high yield strength and excellent sulphide stress cracking behaviour, characterized in that it contains, by weight: C: 0.2% to 0.5% Si: 0.1% to 0.5% Mn: 0.1% to 1% P: 0.03% or less S: 0.005% or less Cr: 0.3% to 1.5% Mo: 0.3% to 1% Al: 0.01% to 0.1% V: 0.1% to 0.5% Nb: 0.01% to 0.05% Ti: 0 to 0.01% W: 0.3% to 1% N: 0.01% or less, the remainder of the chemical composition of said steel being constituted by Fe and impurities or residuals resulting from or necessary to steel production and casting processes.