mhurhangee/ep-ind-claims huggingface dataset:
Measuring instrument for the gravimetric determination of moisture content, with a housing and a weighing device arranged inside the housing, wherein the weighing device comprises a load receiver onto which a sample can be placed, wherein the housing comprises a stationary housing part and a movable housing part, wherein the movable housing part can occupy a measuring position and a servicing position, wherein in said measuring position, the stationary housing part and the movable housing part form an essentially enclosed testing compartment surrounding the load receiver, wherein a sample-heating means is arranged in the testing compartment to perform the function of heating a sample that is placed on the load receiver, wherein in said servicing position the stationary housing part and the movable housing part are spaced apart from each other in such a way that the sample-heating means is accessible for servicing, and wherein the sample-heating means is protected by means of a glass shield which in the measuring position is located between the sample-heating means and the load receiver, characterized in that the glass shield is arranged on the movable housing part and, when in the servicing position, can be taken out without using tools and the measuring instrument can be brought into a loading position, wherein in said loading position the stationary housing part and the movable housing part are spaced apart from each other in such a way that a sample can be put on the load receiver and that the movable housing part can be brought from the measuring position into the loading position by means of a position-changing device and the glass shield can be seated between an upper holder and a lower holder, and that at least one of the holders is removable without the use of tools.
A flame retarded polyamide composition consisting of: (a) at least one polyamide; (b) a hydroquinone diphenyl phosphate ester of the general formula: wherein R 1, R 2, R 3 and R 4 each independently is aryl, or arylalkyl each independently containing up to 30 carbon atoms, optionally interrupted with heteroatoms, X is a divalent hydroquinone group, containing up to 20 carbon atoms, and n has an average value of from 1.0 to 2.0; and, (c) at least one brominated flame retardant. (a) at least one polyamide; (b) a hydroquinone diphenyl phosphate ester of the general formula: wherein R 1, R 2, R 3 and R 4 each independently is aryl, or arylalkyl each independently containing up to 30 carbon atoms, optionally interrupted with heteroatoms, X is a divalent hydroquinone group, containing up to 20 carbon atoms, and n has an average value of from 1.0 to 2.0; and, (c) at least one brominated flame retardant.
A billet thermoforming system comprising: - a heating apparatus having one or more heating elements; - a conveyor; - a plurality of billet carriers attached to the conveyor; - a billet loader configured to load each of the plurality of billets in the plurality of billet carriers attached to the conveyor; - a rotary billet thermoformer comprising a plurality of form molds angularly positioned about an axis of rotation and a plurality of plungers and being configured to form each of the plurality of billets into a container while the plurality of billets are disposed within the plurality of billet carriers and while the rotary billet thermoformer continuously rotates after each of the plurality of billets is heated by the heating apparatus; and - a discharge system configured to sequentially evacuate individual formed containers from the rotary billet thermoformer; wherein - the conveyor is configured to continuously transport the plurality of billets horizontally in the plurality of billet carriers through the heating apparatus along a billet transport path and around the rotary billet thermoformer; and - each of the plurality of plungers is aligned with one of the plurality of form molds and each of the plurality of form molds is adapted to engage one of the plurality of billet carriers prior to forming the container with the billet in the billet carrier as the conveyor passes around the rotary billet thermoformer. - a heating apparatus having one or more heating elements; - a conveyor; - a plurality of billet carriers attached to the conveyor; - a billet loader configured to load each of the plurality of billets in the plurality of billet carriers attached to the conveyor; - a rotary billet thermoformer comprising a plurality of form molds angularly positioned about an axis of rotation and a plurality of plungers and being configured to form each of the plurality of billets into a container while the plurality of billets are disposed within the plurality of billet carriers and while the rotary billet thermoformer continuously rotates after each of the plurality of billets is heated by the heating apparatus; and - a discharge system configured to sequentially evacuate individual formed containers from the rotary billet thermoformer; wherein - the conveyor is configured to continuously transport the plurality of billets horizontally in the plurality of billet carriers through the heating apparatus along a billet transport path and around the rotary billet thermoformer; and - each of the plurality of plungers is aligned with one of the plurality of form molds and each of the plurality of form molds is adapted to engage one of the plurality of billet carriers prior to forming the container with the billet in the billet carrier as the conveyor passes around the rotary billet thermoformer.
A scoop for an aircraft turbine engine, this scoop comprising a body which is movable between at least two positions, including a first position in which it is configured to capture a part of a first air stream flowing in a first direction, and a second position in which it is configured to capture a part of a second air stream flowing in a second direction which is opposite to the first direction, characterized in that said body is mounted to move freely between said at least two positions so as to automatically adopt the first position when the first air stream flows, and to automatically adopt the second position when the second air stream flows.
A method for calibrating sensors in drilling equipment provided with a movable carrier, a frame, a boom assembly mounted to turn about a turning axis vertical to the frame, an angle sensor for measuring a turning angle of the boom assembly in relation to the frame, and gravity-based inclination sensors mounted to the boom assembly and rotating with the assembly about the turning axis for measuring inclination in the direction of two co-ordinate axes that are perpendicular to each other, the method comprising: moving the drilling apparatus on a surface beneath it to a position where it stays in place steadily, without tilting, when the boom assembly is turned about the turning axis; turning the boom assembly about the turning axis to a plural number of different turning angle positions in relation to the frame; measuring the value of the turning angle and the inclination values provided by the inclination sensors for each turning angle position; and determining on the basis of the measured turning angle value and the inclination values provided by the inclination sensors deviations of the values provided by the inclination sensors from the actual inclination angle. moving the drilling apparatus on a surface beneath it to a position where it stays in place steadily, without tilting, when the boom assembly is turned about the turning axis; turning the boom assembly about the turning axis to a plural number of different turning angle positions in relation to the frame; measuring the value of the turning angle and the inclination values provided by the inclination sensors for each turning angle position; and determining on the basis of the measured turning angle value and the inclination values provided by the inclination sensors deviations of the values provided by the inclination sensors from the actual inclination angle.
An axial bearing for a percussion rock drilling machine, the axial bearing comprising at least: a frame; at least a first piston and a second piston arranged in a space formed in the frame, both comprising at least one pressure surface facing into the same direction; at least one pressure duct for leading pressure fluid to said pressure surfaces for axial movement of the pistons (20, 21) to the same direction; and between the pistons (20, 21), axial contact surfaces (60, 43a) facing towards each other, and located in the same pressure space, wherein behind the second piston is provided a first pressure space that is in contact with a first pressure duct for feeding pressure fluid to the axial bearing; and wherein a rear end of the second piston is provided with a pressure surface located in the first pressure space; characterized in that a second pressure space is located on the front side of the second piston and acts as a damper between the first piston and the second piston; the axial contact surfaces are a first contact surface of the first piston and a second contact surface of the second piston, said axial contact surfaces being located in the second pressure space in front of the first pressure space; the first contact surface of the first piston serving also as a pressure surface in the second pressure space; the pressure fluid fed to the axial bearing is arranged to flow from the first pressure space to the second pressure space; whereby the same pressure fluid fed to the axial bearing is arranged to act on said axial contact surfaces (60, 43a) and on said pressure surfaces (43b, 60). a frame; at least a first piston and a second piston arranged in a space formed in the frame, both comprising at least one pressure surface facing into the same direction; at least one pressure duct for leading pressure fluid to said pressure surfaces for axial movement of the pistons (20, 21) to the same direction; and between the pistons (20, 21), axial contact surfaces (60, 43a) facing towards each other, and located in the same pressure space, wherein behind the second piston is provided a first pressure space that is in contact with a first pressure duct for feeding pressure fluid to the axial bearing; and wherein a rear end of the second piston is provided with a pressure surface located in the first pressure space; characterized in that a second pressure space is located on the front side of the second piston and acts as a damper between the first piston and the second piston; the axial contact surfaces are a first contact surface of the first piston and a second contact surface of the second piston, said axial contact surfaces being located in the second pressure space in front of the first pressure space; the first contact surface of the first piston serving also as a pressure surface in the second pressure space; the pressure fluid fed to the axial bearing is arranged to flow from the first pressure space to the second pressure space; whereby the same pressure fluid fed to the axial bearing is arranged to act on said axial contact surfaces (60, 43a) and on said pressure surfaces (43b, 60).
A method of electroplating bismuth metal comprising: a) providing a substrate; b) providing a bismuth electroplating bath consisting of one or more sources of bismuth ions; one or more acids; and 0.5 g/L to 12 g/L of one or more polyoxyethylene aryl ethers having the following formula: wherein R 1 is phenyl and R 2 and R 3 are the same and are chosen from methyl, ethyl or propyl, n is an integer from 1-10, and, optionally an antifoam agent, and, optionally an antimicrobial, and water; c) contacting the substrate with the bismuth electroplating bath; d) applying a current density from 0.5 ASD to 25 ASD to the bismuth electroplating bath and substrate; and e) electroplating bismuth on the substrate. a) providing a substrate; b) providing a bismuth electroplating bath consisting of one or more sources of bismuth ions; one or more acids; and 0.5 g/L to 12 g/L of one or more polyoxyethylene aryl ethers having the following formula: wherein R 1 is phenyl and R 2 and R 3 are the same and are chosen from methyl, ethyl or propyl, n is an integer from 1-10, and, optionally an antifoam agent, and, optionally an antimicrobial, and water; c) contacting the substrate with the bismuth electroplating bath; d) applying a current density from 0.5 ASD to 25 ASD to the bismuth electroplating bath and substrate; and e) electroplating bismuth on the substrate.
A composition comprising: a. one or more agents that reduce the level of an ikaros family member transcription factor in a cell, wherein the one or more agents are selected from the group consisting of pomalidomide and lenalidomide; and b. one or more agents that inhibit TGFβ signaling, wherein the one or more agents that inhibit TGFβ signaling comprise a TGFβ receptor inhibitor, and wherein said TGFβ receptor inhibitor is selected from the group consisting of ALK5 inhibitor II, LY364947, DMH1, and A83-01. a. one or more agents that reduce the level of an ikaros family member transcription factor in a cell, wherein the one or more agents are selected from the group consisting of pomalidomide and lenalidomide; and b. one or more agents that inhibit TGFβ signaling, wherein the one or more agents that inhibit TGFβ signaling comprise a TGFβ receptor inhibitor, and wherein said TGFβ receptor inhibitor is selected from the group consisting of ALK5 inhibitor II, LY364947, DMH1, and A83-01.
An image forming method using at least four color toners of yellow, magenta, cyan and black, and comprising a fixation step of fixing a toner image on a recording medium using a fixing unit, wherein the total of a dust emission amount from each of the four color toners is less than 16 mg/h, and when, of the yellow toner, the magenta toner and the cyan toner, just before the fixation step, a dust emission amount from the toner to be the outermost layer on the recording medium is represented by A (mg/h), a dust emission amount from the toner to be the interlayer on the recording medium is represented by B (mg/h), a dust emission amount from the toner to be the lowermost layer on the recording medium is represented by C (mg/h), A/C is from 1.5 to 23.7, and A, B and C each satisfy the relationship of 0.9 ≤ A < 14.2, 0.6 ≤ B < 14.2 and 0.6 ≤ C < 14.2; wherein the toner to be the outermost layer on the recording medium just before the fixation step contains a hydrocarbon wax, and the toner to be the lowermost layer on the recording medium just before the fixation step contains a microcrystalline wax or an ester wax; wherein the dust emission amount is measured according to the description.
Shut-off device for a motor vehicle front-end air inlet, comprising: ■ a support frame, ■ at least one flap pivoting about a horizontal pivot axis between a shut-off position and an open position, said at least one flap being installed within the support frame, the support frame comprising means of connection with said at least one flap at a connection region, ■ at least one control element governing the positioning of the flap(s), the support frame comprising pre-cut-out portions in the vicinity of at least one connection means, characterized in that the support frame comprises a least one means (61, 62) for retaining the elements capable of detaching by breaking at the pre-cut-out portions. ■ a support frame, ■ at least one flap pivoting about a horizontal pivot axis between a shut-off position and an open position, said at least one flap being installed within the support frame, the support frame comprising means of connection with said at least one flap at a connection region, ■ at least one control element governing the positioning of the flap(s),
An absorbent article comprising a liquid-permeable topsheet, a liquid-impermeable backsheet and an absorbent core sandwiched between said topsheet and said backsheet, said article being arranged along a longitudinal axis and a transversal axis extending in a perpendicular direction in relation to the longitudinal axis and said article comprising a front portion, a back portion and a crotch portion, wherein said absorbent core is formed with a sealing arrangement (9, 10, 15, 16) comprising two channel sealings (9, 10) extending along said longitudinal axis in said crotch portion and defining a first effective channel sealing width and a second effective channel sealing width, respectively; characterized in that the sealing arrangement (9, 10, 15, 16) furthermore comprises two side seams (15, 16) extending along two side edges (25, 26) of said core, said side seams (15,16) defining a third and fourth effective width (w3, w4), respectively, along said crotch portion and defining a fifth and sixth effective width (w5, w6), respectively, along said front portion and back portion; said effective widths (w1, w2, w3, w4, w5, w6) being defined as the extension of said sealing arrangement (9, 10, 14, 15) in the transverse direction of the article, along any cross-section of the crotch portion, wherein the sum of said first to sixth effective widths (w1, w2, w3, w4, w5, w6) in the transversal direction is constant along said core (5, wherein the sealing arrangement (9, 10, 15, 16) is constituted by a welding pattern, in particular produced by means of ultrasonic welding. a liquid-permeable topsheet, a liquid-impermeable backsheet and an absorbent core sandwiched between said topsheet and said backsheet, said article being arranged along a longitudinal axis and a transversal axis extending in a perpendicular direction in relation to the longitudinal axis and said article comprising a front portion, a back portion and a crotch portion, wherein said absorbent core is formed with a sealing arrangement (9, 10, 15, 16) comprising two channel sealings (9, 10) extending along said longitudinal axis in said crotch portion and defining a first effective channel sealing width and a second effective channel sealing width, respectively; characterized in that the sealing arrangement (9, 10, 15, 16) furthermore comprises two side seams (15, 16) extending along two side edges (25, 26) of said core, said side seams (15,16) defining a third and fourth effective width (w3, w4), respectively, along said crotch portion and defining a fifth and sixth effective width (w5, w6), respectively, along said front portion and back portion; said effective widths (w1, w2, w3, w4, w5, w6) being defined as the extension of said sealing arrangement (9, 10, 14, 15) in the transverse direction of the article, along any cross-section of the crotch portion, wherein the sum of said first to sixth effective widths (w1, w2, w3, w4, w5, w6) in the transversal direction is constant along said core (5, wherein the sealing arrangement (9, 10, 15, 16) is constituted by a welding pattern, in particular produced by means of ultrasonic welding.
A preform configured to form a container by stretch blow molding, the preform comprising: a finish portion at a first end of the preform, the finish portion is a container finish of the container; a tip portion at a second end of the preform opposite to the first end, the tip portion configured to form a container base and a container heel of the container; and an outer surface of the tip portion including a flat surface, a first radius (R 1) on a first side of the flat surface, a second radius (R 2) between the first radius (R 1) and the flat surface, a third radius (R 3) extending from the flat surface on a second side of the flat surface, and a fourth radius (R 4) extending from the third radius (R 3) towards the second end of the preform through which a longitudinal axis of the preform extends, characterized in that the second radius (R 2) is greater than the first radius (R 1),and the fourth radius (R 4) is greater than the third radius (R 3), and an inner surface of the preform includes a fifth radius (R 5) that extends entirely across the inner surface. a finish portion at a first end of the preform, the finish portion is a container finish of the container; a tip portion at a second end of the preform opposite to the first end, the tip portion configured to form a container base and a container heel of the container; and an outer surface of the tip portion including a flat surface, a first radius (R 1) on a first side of the flat surface, a second radius (R 2) between the first radius (R 1) and the flat surface, a third radius (R 3) extending from the flat surface on a second side of the flat surface, and a fourth radius (R 4) extending from the third radius (R 3) towards the second end of the preform through which a longitudinal axis of the preform extends, characterized in that the second radius (R 2) is greater than the first radius (R 1),and the fourth radius (R 4) is greater than the third radius (R 3), and an inner surface of the preform includes a fifth radius (R 5) that extends entirely across the inner surface.
A method for automatically welding studs on a surface of a beam at pre-marked welding sites located on the surface of the beam, the beam having a longitudinal axis, the method being characterized by the steps of: instructing a carriage (15, 1350, 2022) to move parallel to the longitudinal axis (51, 1419, 2002) of the beam (50,1302, 2001), the carriage having at least one imager (90, 1570, 2282a) and at least one welding assembly attached thereto, the imager being operably configured to automatically capture a plurality of images of the surface (70, 1304, 2005) of the beam as the carriage is moving; instructing the at least one imager to capture the plurality of images of the surface of the beam and communicate image data regarding the plurality of images to a computer (155, 1595), the computer being in data communication with the at least one imager and the at least one welding assembly (135, 1300, 2170), the computer operably identifying at least one pre-marked welding site (600, 1317, 2007) that is located on the surface of the beam in one or more of the plurality of images and operably determining the location of the at least one pre-marked welding site relative to the location of the carriage and relative to the location of the at least one welding assembly with respect to said three coordinates; and instructing the at least one welding assembly to place and weld a stud (270, 2006) to the surface of the beam at the at least one pre-marked welding site. instructing a carriage (15, 1350, 2022) to move parallel to the longitudinal axis (51, 1419, 2002) of the beam (50,1302, 2001), the carriage having at least one imager (90, 1570, 2282a) and at least one welding assembly attached thereto, the imager being operably configured to automatically capture a plurality of images of the surface (70, 1304, 2005) of the beam as the carriage is moving; instructing the at least one imager to capture the plurality of images of the surface of the beam and communicate image data regarding the plurality of images to a computer (155, 1595), the computer being in data communication with the at least one imager and the at least one welding assembly (135, 1300, 2170), the computer operably identifying at least one pre-marked welding site (600, 1317, 2007) that is located on the surface of the beam in one or more of the plurality of images and operably determining the location of the at least one pre-marked welding site relative to the location of the carriage and relative to the location of the at least one welding assembly with respect to said three coordinates; and instructing the at least one welding assembly to place and weld a stud (270, 2006) to the surface of the beam at the at least one pre-marked welding site.