mhurhangee/ep-ind-claims huggingface dataset:
An air-borne apparatus for detecting icing conditions, the apparatus comprising: a laser system configured and operative to generate a light signal and direct the light signal into a cloud; a lens component configured and operative to collect echo signals (122,124) from a cloud caused by the light signal directed into the cloud by the laser system; and a beam splitter component configured and operative to redirect signals received and passing through the lens component into at least first and second paths; a supercooled large droplet detector (127,128) positioned to receive the redirected signals from the beam splitter, the supercooled large droplet detector including: a first signal detector component configured and operative to perform a first color measurement on the first redirected signal; and a second signal detector (133,135,136) component configured and operative to perform a second color measurement on the second redirected signal wherein the supercooled large droplet detector is configured and operative to use the first and second color measurements to determine liquid water content and droplet diameter distribution for the cloud in which the light signal was directed into by the laser system. a laser system configured and operative to generate a light signal and direct the light signal into a cloud; a lens component configured and operative to collect echo signals (122,124) from a cloud caused by the light signal directed into the cloud by the laser system; and a beam splitter component configured and operative to redirect signals received and passing through the lens component into at least first and second paths; a supercooled large droplet detector (127,128) positioned to receive the redirected signals from the beam splitter, the supercooled large droplet detector including: a first signal detector component configured and operative to perform a first color measurement on the first redirected signal; and a second signal detector (133,135,136) component configured and operative to perform a second color measurement on the second redirected signal wherein the supercooled large droplet detector is configured and operative to use the first and second color measurements to determine liquid water content and droplet diameter distribution for the cloud in which the light signal was directed into by the laser system. a first signal detector component configured and operative to perform a first color measurement on the first redirected signal; and a second signal detector (133,135,136) component configured and operative to perform a second color measurement on the second redirected signal wherein the supercooled large droplet detector is configured and operative to use the first and second color measurements to determine liquid water content and droplet diameter distribution for the cloud in which the light signal was directed into by the laser system.
A ventilation grid for ventilation of an enclosure, comprising an outer grid, having a plurality of horizontal outer ribs for preventing water or solid foreign objects to enter the interior of the enclosure, an inner grid adjacent to the outer grid in interior of the enclosure having a plurality of horizontal inner ribs for directing water that enters the interior of the outer grid, at least one of the horizontal outer ribs of the outer grid having a cross-section with two legs (6,7) connected to each other in a connection point and arranged to an angle with respect to each other, each of the legs (6,7) extending downwards from the connection point of the two sides, characterized in that the ventilation grid comprises a hinge for connecting the inner grid and the outer grid hinged to each other.
A woven fabric suitable for use in arc protection, the fabric having a first face and a second face, the fabric having a warp yarn dissimilar to a fill yarn, wherein either: a) a majority of the first face of the fabric is a first yarn that is the warp yarn in the fabric and a majority of the second face of the fabric is a second yarn that is the fill yarn in the fabric; or b) a majority of the first face of the fabric is a first yarn that is a fill yarn in the fabric and a majority of the second face of the fabric is a second yarn that is the warp yarn in the fabric; and wherein the second yarn forming the majority of the second face of the fabric comprises: i) 25 to 100 parts aramid fiber containing 0.5 to 20 weight percent discrete carbon particles, based on the amount of carbon particles in an individual fiber, the carbon particles being homogeneously dispersed in that fiber, and ii) 0 to 75 parts aramid fiber free of discrete carbon particles; based on the total amount of i) and ii) in the second yarn; and wherein the first yarn forming the majority of the first face of the fabric comprises aramid fiber being free of discrete carbon particles; the fabric having a total content of 0.5 to 3 weight percent discrete carbon particles. a) a majority of the first face of the fabric is a first yarn that is the warp yarn in the fabric and a majority of the second face of the fabric is a second yarn that is the fill yarn in the fabric; or b) a majority of the first face of the fabric is a first yarn that is a fill yarn in the fabric and a majority of the second face of the fabric is a second yarn that is the warp yarn in the fabric; and i) 25 to 100 parts aramid fiber containing 0.5 to 20 weight percent discrete carbon particles, based on the amount of carbon particles in an individual fiber, the carbon particles being homogeneously dispersed in that fiber, and ii) 0 to 75 parts aramid fiber free of discrete carbon particles; based on the total amount of i) and ii) in the second yarn; and
A lighting device comprising a surface-mountable elongated carrier for positioning relative to a surface, at least one light source, and an adjustable cover; wherein the elongated carrier comprises opposite to each other a first face on a first side and a second face on a second side, the at least one light source is located on the first and second face; and wherein the elongated carrier comprises a third face on a third side for facing the surface in mounted position; and wherein the adjustable cover is in connection with the carrier and is positioned on a fourth side of the carrier opposite to the third side, and wherein the adjustable cover is movable relative to the elongated carrier for controlling a light effect originating from the at least one light source, wherein the at least one light source comprises a LED light source, characterized in that the adjustable cover is moveable in translation with respect to the carrier in the direction perpendicular to the direction defined by the shortest distance between the third side and the fourth side, whereby said perpendicular direction is the direction defined by the shortest distance between the first side and the second side.
A method of reducing paper web adhesion on a press roll and improving release from roll surface in papermaking processes comprising applying to the roll surfaces a composition comprising at least one low molecular weight hydrophobic imidazoline having a molecular weight of 1,000 daltons or less.
A method for making patterns at the surface of a substrate by graphoepitaxy including the following steps: - a step of depositing a layer of resin at the surface of the substrate; - a step of making resin patterns at the surface of a substrate; - a step of hardening the resin patterns by creating a layer of amorphous carbon at the surface of the resin patterns; - a step of depositing a layer of random copolymer after the step of hardening the resin patterns; - a step of grafting the layer of random copolymer on the resin patterns, between the resin patterns and on the flanks of the resin patterns, by annealing; - a step of depositing a layer of a block copolymer in the spaces defined by the resin patterns after the step of hardening the patterns and grafting the layer of random copolymer. - a step of depositing a layer of resin at the surface of the substrate; - a step of making resin patterns at the surface of a substrate; - a step of hardening the resin patterns by creating a layer of amorphous carbon at the surface of the resin patterns; - a step of depositing a layer of random copolymer after the step of hardening the resin patterns; - a step of grafting the layer of random copolymer on the resin patterns, between the resin patterns and on the flanks of the resin patterns, by annealing; - a step of depositing a layer of a block copolymer in the spaces defined by the resin patterns after the step of hardening the patterns and grafting the layer of random copolymer.
A pump for sampling a gas to be analysed comprising: a pump housing member having a chamber with inner walls and an open end having a first area, said pump housing member comprises an enlarged surface surrounding said open end of said chamber; a second pump housing member; a membrane element (6, 32) with a second area; said membrane element has a first central section having a third area with same size as said first area of said open end of said chamber; wherein said membrane element (6, 32) is arranged on said pump housing member with said first central section positioned over said open end, forming a sealed chamber; and wherein a portion of said membrane element (6, 32) is slidably clamped between said enlarged surface and said second pump housing member in such way that the clamped portion is allowed to move radially and to stretch when a force is applied on said membrane. a pump housing member having a chamber with inner walls and an open end having a first area, said pump housing member comprises an enlarged surface surrounding said open end of said chamber; a second pump housing member; a membrane element (6, 32) with a second area; said membrane element has a first central section having a third area with same size as said first area of said open end of said chamber; wherein said membrane element (6, 32) is arranged on said pump housing member with said first central section positioned over said open end, forming a sealed chamber; and wherein a portion of said membrane element (6, 32) is slidably clamped between said enlarged surface and said second pump housing member in such way that the clamped portion is allowed to move radially and to stretch when a force is applied on said membrane.
A flight operable, modular aircraft having: a center section that includes right and left inboard ribs (493, 494), a forward horizontally curved composite spar member, and an aft horizontally curved composite spar member; a center section having an aircraft core with a central cavity that is (a) disposed along a centerline of the aircraft and (b) supported on only four sides by the right and left inboard ribs (493, 494) cooperating with the forward and aft horizontally curved composite spar members such that the central cavity is free from supporting structural members; an originally deployed right outer wing member having a right spar, and a right hardpoint that couples the right outer wing member to the forward and aft curved spars members (422, 424) of the center section during an operational life of the aircraft; an originally deployed left outer wing member having a left spar, and a left hardpoint that couples the left outer wing member to the forward and aft curved spars members (422, 424) of the center section during an operational life of the aircraft; a forward hardpoint adapted to couple an optional fuselage to the center section during the operational life of the aircraft; and the aircraft core comprises a right engine and a left engine to provide a propulsive force for the aircraft, wherein the engines (436, 438) are disposed so that they do not extend above or below the center section. a center section that includes right and left inboard ribs (493, 494), a forward horizontally curved composite spar member, and an aft horizontally curved composite spar member; a center section having an aircraft core with a central cavity that is (a) disposed along a centerline of the aircraft and (b) supported on only four sides by the right and left inboard ribs (493, 494) cooperating with the forward and aft horizontally curved composite spar members such that the central cavity is free from supporting structural members; an originally deployed right outer wing member having a right spar, and a right hardpoint that couples the right outer wing member to the forward and aft curved spars members (422, 424) of the center section during an operational life of the aircraft; an originally deployed left outer wing member having a left spar, and a left hardpoint that couples the left outer wing member to the forward and aft curved spars members (422, 424) of the center section during an operational life of the aircraft; a forward hardpoint adapted to couple an optional fuselage to the center section during the operational life of the aircraft; and the aircraft core comprises a right engine and a left engine to provide a propulsive force for the aircraft, wherein the engines (436, 438) are disposed so that they do not extend above or below the center section.
Tile or slab comprising a fired ceramic material, wherein the fired ceramic material has a length of at least 1.2 m and a width of at least 0.6 m, and has a chemical composition comprising a combination of oxides according to: SiO 2 54.0-64.0 wt% Al 2 O 3 17.5-23.0 wt% CaO 2.7-6.8 wt% MgO 1.0-5.5 wt% ZrO 2 2.0-6.6 wt% based on the total weight of the fired ceramic material.
An ion pump comprising: a casing; a first electrode inside the casing; a plurality of cylindrical magnets fixed to the casing, which are located in a row at intervals in the central axis direction of the casing; a second electrode arranged between the first electrode and the plurality of cylindrical magnets, which has a different polarity from that of the first electrode; and a connection part for connecting the casing with another device, characterized by that the plurality of cylindrical magnets are configured so that adjacent surfaces of adjacent cylindrical magnets have the same polarity. a casing; a first electrode inside the casing; a plurality of cylindrical magnets fixed to the casing, which are located in a row at intervals in the central axis direction of the casing; a second electrode arranged between the first electrode and the plurality of cylindrical magnets, which has a different polarity from that of the first electrode; and a connection part for connecting the casing with another device, characterized by that the plurality of cylindrical magnets are configured so that adjacent surfaces of adjacent cylindrical magnets have the same polarity.
A multilayer coating film sequentially comprising, on a substrate, a colored coating film, an effect coating film, and a clear coating film, wherein the effect coating film is obtained from an effect pigment dispersion containing water in an amount of 70 to 99 parts by mass, a surface modifier in an amount of 0.1 to 10 parts by solids mass, a flake-effect pigment in an amount of 0.05 to 3.0 parts by solids mass and a viscosity modifier in an amount of 0.1 to 26 parts by solids mass, based on 100 parts by mass of the total amount of water, the surface modifier, the flake-effect pigment, and the viscosity modifier; the surface modifier is one or a combination of 2 or more of a silicone-based surface modifier, an acrylic-based surface modifier, a vinyl-based surface modifier, and a fluorine-based surface modifier; the multilayer coating film has: a lightness L*110 within a range of 60 to 90, the lightness L*110 being based on a spectral reflectance of light illuminated at an angle of 45 degrees with respect to the coating surface and received at an angle of 110 degrees with respect to the specularly reflected light; a 60-degree specular gloss within a range of 105 to 180; a graininess HG within a range of 10 to 40; and a flip-flop value within a range of 1.0 to 1.8. wherein the effect coating film is obtained from an effect pigment dispersion containing water in an amount of 70 to 99 parts by mass, a surface modifier in an amount of 0.1 to 10 parts by solids mass, a flake-effect pigment in an amount of 0.05 to 3.0 parts by solids mass and a viscosity modifier in an amount of 0.1 to 26 parts by solids mass, based on 100 parts by mass of the total amount of water, the surface modifier, the flake-effect pigment, and the viscosity modifier; the surface modifier is one or a combination of 2 or more of a silicone-based surface modifier, an acrylic-based surface modifier, a vinyl-based surface modifier, and a fluorine-based surface modifier; the multilayer coating film has: a lightness L*110 within a range of 60 to 90, the lightness L*110 being based on a spectral reflectance of light illuminated at an angle of 45 degrees with respect to the coating surface and received at an angle of 110 degrees with respect to the specularly reflected light; a 60-degree specular gloss within a range of 105 to 180; a graininess HG within a range of 10 to 40; and a flip-flop value within a range of 1.0 to 1.8. a lightness L*110 within a range of 60 to 90, the lightness L*110 being based on a spectral reflectance of light illuminated at an angle of 45 degrees with respect to the coating surface and received at an angle of 110 degrees with respect to the specularly reflected light; a 60-degree specular gloss within a range of 105 to 180; a graininess HG within a range of 10 to 40; and a flip-flop value within a range of 1.0 to 1.8.
Method for start-up triggering in an Ethernet-based in-vehicle network that realizes time aware traffic shaping, wherein the network comprises at least one device (1; 8) configured for sending TAS-based frames (F1, F2, F3, F4, F8_1, F8_2), at least one bridge (2, 3, 4, 5) configured for transmitting TAS-based frames (F1, F2, F3, F4; F8_1, F8_2), and a trigger node (30; 60), and wherein the at least one device and the at least one bridge (2, 3, 4, 5) use a guard band for determining, when a TAS-based frame (F1, F2, F3, F4) has to be sent or transmitted, characterized in that the method comprises the steps of - transmitting a trigger message from the trigger node (30; 60) to the device, wherein the trigger message defines the time at which the device has to start sending its first scheduled frame; - adjusting the guard band of the device with respect to the transmitted time; - transmitting a trigger message from the trigger node (30; 60) to at least one bridge (2, 3, 4, 5) in the network, wherein the trigger message defines the time (t22, t23, t24, t25; t22_1; t23_1) at which the bridge (2, 3, 4, 5) will receive the first scheduled frame from the device; and - adjusting the guard band of the at least one bridge (2, 3, 4, 5) with respect to the transmitted time (t22, t23, t24, t25; t22_1; t23_1). - transmitting a trigger message from the trigger node (30; 60) to the device, wherein the trigger message defines the time at which the device has to start sending its first scheduled frame; - adjusting the guard band of the device with respect to the transmitted time; - transmitting a trigger message from the trigger node (30; 60) to at least one bridge (2, 3, 4, 5) in the network, wherein the trigger message defines the time (t22, t23, t24, t25; t22_1; t23_1) at which the bridge (2, 3, 4, 5) will receive the first scheduled frame from the device; and - adjusting the guard band of the at least one bridge (2, 3, 4, 5) with respect to the transmitted time (t22, t23, t24, t25; t22_1; t23_1).
A method for detecting cancer in a tissue specimen, comprising: preparing a cell lysate from the tissue specimen or a cell lysate from a region suspected to be cancer isolated from the tissue specimen; and evaluating a taxis behavior of a nematode for the cell lysate, wherein the taxis behavior means attraction behavior or avoidance behavior of the nematode to the cell lysate, wherein if the nematode exhibits an attraction behavior to the cell lysate, then it is indicated that the tissue specimen or the region suspected to be cancer which the cell lysate is derived from has cancer or a possibility of having cancer. preparing a cell lysate from the tissue specimen or a cell lysate from a region suspected to be cancer isolated from the tissue specimen; and evaluating a taxis behavior of a nematode for the cell lysate, wherein the taxis behavior means attraction behavior or avoidance behavior of the nematode to the cell lysate, wherein if the nematode exhibits an attraction behavior to the cell lysate, then it is indicated that the tissue specimen or the region suspected to be cancer which the cell lysate is derived from has cancer or a possibility of having cancer.
A method for treating an asbestos containing material with a mineralizing agent for the purpose of converting the asbestos into an essentially asbestos-free mineral that contains non-detectable concentrations of asbestos when analyzed using transmission electron microscopy, X-ray diffraction, and optical microscopy techniques, wherein the method is characterised in that it comprises: shredding the ACM into shredded ACM in a shredder to increase the surface area and to increase the rate of absorption of the mineralizing agent and discharging the shredded ACM by propulsion from the shredder to distribute the ACM as it exits the shredder for reception of the mineralizing agent; heating the mineralizing agent to, and maintaining the mineralizing agent at, a temperature in the range of 322 Kelvin (120 degrees Fahrenheit) and 344 Kelvin (160 degrees Fahrenheit); and applying the heated mineralizing agent in spray form to the shredded ACM after it exits the shredder, by using an apparatus to evenly distribute the mineralizing agent over the shredded ACM. shredding the ACM into shredded ACM in a shredder to increase the surface area and to increase the rate of absorption of the mineralizing agent and discharging the shredded ACM by propulsion from the shredder to distribute the ACM as it exits the shredder for reception of the mineralizing agent; heating the mineralizing agent to, and maintaining the mineralizing agent at, a temperature in the range of 322 Kelvin (120 degrees Fahrenheit) and 344 Kelvin (160 degrees Fahrenheit); and applying the heated mineralizing agent in spray form to the shredded ACM after it exits the shredder, by using an apparatus to evenly distribute the mineralizing agent over the shredded ACM.
Plasma spray apparatus for coating substrates, comprising at least a working chamber including at least a plasma torch and at least a substrate support for the substrate to be coated, in which an inert gas or a mixture of inert gases is contained at a pressure which is close to, or higher than, the normal pressure, and at least a gas circuit, in communication with said working chamber, comprising recirculating means of the inert gases contained in said working chamber, said recirculating means comprising a closed loop, including a first heat exchanger for cooling down the gases, communicating with said working chamber, and a recirculating blower, arranged upstream of said first heat exchanger, suitable for extracting the inert gases from said working chamber and supplying a first fraction of the cooled inert gases back into a first portion of said working chamber, characterized in that said recirculating means include at least a path, communicating with said closed loop and including a second heat exchanger for further cooling down the gases, and at least a compressor, arranged upstream of said second heat exchanger, suitable for supplying a second fraction of the cooled inert gases into a second portion of said working chamber, and pointed towards the substrate by means of properly placed conduits (31a,31b).