mhurhangee/ep-ind-claims huggingface dataset:
A structure for supporting a bioprosthetic heart valve comprising: a cylindrical anchoring structure defining a central longitudinal axis, the cylindrical anchoring structure comprising: an inflow ring including at least one sinusoidal-shaped wire having a plurality of peaks and troughs; an outflow ring including at least one sinusoidal-shaped wire having a plurality of peaks and troughs, and at least one flexible commissure post having a longitudinal axis, the flexible commissure post connecting the inflow ring and the outflow ring, wherein the flexible commissure post has a bending flexibility along a plane defined by a surface containing all straight lines connecting any point on the central longitudinal axis of the cylindrical anchoring structure and any point on the longitudinal axis of the flexible commissure post, wherein the at least one flexible commissure post includes a paddle portion operably connected to the outflow ring, the paddle portion including an axial slot extending along the longitudinal axis thereof. an inflow ring including at least one sinusoidal-shaped wire having a plurality of peaks and troughs; an outflow ring including at least one sinusoidal-shaped wire having a plurality of peaks and troughs, and at least one flexible commissure post having a longitudinal axis, the flexible commissure post connecting the inflow ring and the outflow ring,
A wing extension (100, 200, 304, 414, 418, 420, 422, 424, 426) fixedly attachable to a baseline wing of an aircraft, the wing extension comprising: a horizontal portion that, when attached to the aircraft, is substantially parallel to the baseline wing of the aircraft, the horizontal portion being configured to fixedly attach to an outboard portion of the baseline wing of the aircraft; and a controllable airflow modification device, CAMD, coupled to the horizontal portion of the wing extension (100, 200, 304, 414, 418, 420, 422, 424, 426) and configured to be controllable independently of a control surface of the baseline wing; characterized in that the CAMD (110, 318) is configured to alleviate a flutter condition on the baseline wing; and at least two sensors are located in the wing extension at different spanwise locations for detection of torques and/or onset of a flutter condition. a horizontal portion that, when attached to the aircraft, is substantially parallel to the baseline wing of the aircraft, the horizontal portion being configured to fixedly attach to an outboard portion of the baseline wing of the aircraft; and a controllable airflow modification device, CAMD, coupled to the horizontal portion of the wing extension (100, 200, 304, 414, 418, 420, 422, 424, 426) and configured to be controllable independently of a control surface of the baseline wing; characterized in that the CAMD (110, 318) is configured to alleviate a flutter condition on the baseline wing; and at least two sensors are located in the wing extension at different spanwise locations for detection of torques and/or onset of a flutter condition.
Vehicle seat having a seat part and having a backrest, the backrest having a foam part with a cavity for at least partially receiving an airbag device, wherein, in the region of the cavity, the foam part is lined at least partially with a reinforcement-layer arrangement, wherein, in the event of a deploying airbag of the airbag device, the reinforcement-layer arrangement guides the deploying airbag to a predetermined tearing point of the foam part, and the reinforcement-layer arrangement has a first reinforcement layer and a second reinforcement layer (34, 134, 234, 334), characterized in that the foam part has a first flange, a second flange and a web connecting the first flange to the second flange, which delimit the cavity, and an outer end region (32.1) of the first reinforcement layer and/or an outer end region (34.1, 134.1, 234.1, 334.1) of the second reinforcement layer (34, 134, 234, 334) are/is incorporated into the web by foaming.
A method for producing a thermosetting resin molded article, comprising: disposing a decorative film having a base film and a decorative layer on at least a design forming area in a surface of a shaping mold (1,2) so that the decorative layer is faced inwardly; and injecting a thermosetting resin composition into a cavity of the shaping mold and thermally curing the thermosetting resin composition, to obtain a thermosetting resin molded article having the decorative film formed on the surface of the cured material of the thermosetting resin composition; wherein the base film used is a film which has a tensile elongation at break of more than 500% and a tensile stress at 100% of 0.1 MPa to 2.5 MPa, at the thermal curing temperature for the thermosetting resin composition. disposing a decorative film having a base film and a decorative layer on at least a design forming area in a surface of a shaping mold (1,2) so that the decorative layer is faced inwardly; and injecting a thermosetting resin composition into a cavity of the shaping mold and thermally curing the thermosetting resin composition, to obtain a thermosetting resin molded article having the decorative film formed on the surface of the cured material of the thermosetting resin composition; wherein the base film used is a film which has a tensile elongation at break of more than 500% and a tensile stress at 100% of 0.1 MPa to 2.5 MPa, at the thermal curing temperature for the thermosetting resin composition.
The compound {5-(4-bromo-phenyl)-6-[2-(5-bromo-pyrimidin-2-yloxy)-ethoxy]-pyrimidin-4-yl}-sulfamide: or a pharmaceutically acceptable salt thereof, for use in the treatment of chronic kidney disease of stages 1 to 4 as defined by the Kidney Disease Improving Global Outcomes (KDIGO) Guidelines, wherein said CKD is caused by essential hypertension wherein said compound is to be administered in combination with an Angiotensin Receptor Blocker which is valsartan, or a pharmaceutically acceptable salt thereof.
A control apparatus for an internal combustion engine, the apparatus comprising: a variable valve operating mechanism (44, 46) which is capable of changing at least a closing timing of an exhaust valve; fuel cut execution means which is configured so as to execute a fuel cut when a predetermined execution condition is established during an operation of the internal combustion engine; and valve timing control means which is configured so as to control at least the closing timing of the exhaust valve to obtain a fuel-cut-time valve timing when the fuel cut is executed, wherein the fuel-cut-time valve timing is set so that the exhaust valve is closed at an advance side relative to an exhaust top dead center and an intake valve is closed at a timing which is after the closing timing of the exhaust valve; and the control apparatus being characterized in that it further comprises accumulating amount determination means for determining whether or not an accumulating amount of a deposit that accumulates in an intake system is equal to or larger than a predetermined value; and wherein the valve timing control means is configured so as to increase the advance angle amount of the closing timing of the exhaust valve more when the accumulating amount of the deposit is determined to be equal to or larger than the predetermined value by the accumulating amount determination means than when the accumulating amount is determined to be smaller than the predetermined value. a variable valve operating mechanism (44, 46) which is capable of changing at least a closing timing of an exhaust valve; fuel cut execution means which is configured so as to execute a fuel cut when a predetermined execution condition is established during an operation of the internal combustion engine; and valve timing control means which is configured so as to control at least the closing timing of the exhaust valve to obtain a fuel-cut-time valve timing when the fuel cut is executed, wherein the fuel-cut-time valve timing is set so that the exhaust valve is closed at an advance side relative to an exhaust top dead center and an intake valve is closed at a timing which is after the closing timing of the exhaust valve; and the control apparatus being characterized in that it further comprises accumulating amount determination means for determining whether or not an accumulating amount of a deposit that accumulates in an intake system is equal to or larger than a predetermined value; and wherein the valve timing control means is configured so as to increase the advance angle amount of the closing timing of the exhaust valve more when the accumulating amount of the deposit is determined to be equal to or larger than the predetermined value by the accumulating amount determination means than when the accumulating amount is determined to be smaller than the predetermined value.
A beverage brewing process comprising the steps of: placing a desired amount of a solid beverage brewing material into a chamber; placing a desired amount of a liquid into said chamber; sealing said chamber from the surrounding atmosphere; creating a vacuum within said chamber by drawing a vacuum utilizing a vacuum source located outside of said chamber; allowing said brewing material and liquid to brew in said chamber for a desired period of time while said vacuum is applied, removed and reapplied in the range -5 to -20 inches of mercury (about 17 to 68kPa); removing said vacuum from said chamber, and separating said brewed liquid from said solid to create said beverage. placing a desired amount of a solid beverage brewing material into a chamber; placing a desired amount of a liquid into said chamber; sealing said chamber from the surrounding atmosphere; creating a vacuum within said chamber by drawing a vacuum utilizing a vacuum source located outside of said chamber; allowing said brewing material and liquid to brew in said chamber for a desired period of time while said vacuum is applied, removed and reapplied in the range -5 to -20 inches of mercury (about 17 to 68kPa); removing said vacuum from said chamber, and separating said brewed liquid from said solid to create said beverage.
A method for preparing a sorbate powder comprising dissolving sorbate salt in water to form a sorbate solution, adding a stabilizing carrier to the sorbate solution to form a carrier-sorbate solution, and spray drying the carrier-sorbate solution to form the sorbate powder.
A screw for a plasticating apparatus, the screw comprising: a longitudinal axis, the screw being rotatably supportable in a barrel for rotation about the longitudinal axis, the screw having a core and at least one helical flight extending along a length of the screw, the helical flight having a radially outermost flight surface, the helical flight extending in a first threaded direction and defining a first helical path having a first helix angle less than ninety degrees; the helical flight defining a helical channel; and a longitudinal portion of the screw having a plurality of advancing grooves with each advancing groove having at least one closedend, the plurality of advancing grooves being arranged in a noncontinuous helix cut in the screw core in the helical channel of the screw, the plurality of advancing grooves forming a forward helical pathway in the helical channel for conveying material through the helical channel along the at least one helical flight, the advancing grooves being parallel to and having the same first helix angle as the helical flight; the longitudinal portion further having at least one undercut surface located radially inwardly from the radially outermost flight surface, characterized in that the at least one undercut surface has a depth that varies at least one of: in a longitudinal direction parallel to the plurality of advancing grooves; and in a direction traverse to the longitudinal direction. a longitudinal axis, the screw being rotatably supportable in a barrel for rotation about the longitudinal axis, the screw having a core and at least one helical flight extending along a length of the screw, the helical flight having a radially outermost flight surface, the helical flight extending in a first threaded direction and defining a first helical path having a first helix angle less than ninety degrees; the helical flight defining a helical channel; and a longitudinal portion of the screw having a plurality of advancing grooves with each advancing groove having at least one closedend, the plurality of advancing grooves being arranged in a noncontinuous helix cut in the screw core in the helical channel of the screw, the plurality of advancing grooves forming a forward helical pathway in the helical channel for conveying material through the helical channel along the at least one helical flight, the advancing grooves being parallel to and having the same first helix angle as the helical flight; the longitudinal portion further having at least one undercut surface located radially inwardly from the radially outermost flight surface, characterized in that the at least one undercut surface has a depth that varies at least one of: in a longitudinal direction parallel to the plurality of advancing grooves; and in a direction traverse to the longitudinal direction. in a longitudinal direction parallel to the plurality of advancing grooves; and in a direction traverse to the longitudinal direction.
A sequence of polymeric shell appliances (1010, 1020, 1030) for, when in position in the mouth, moving a tooth (1001, 1002) of a patient from a first position and orientation to a second position and orientation, each member of the sequence of appliances comprising: one or more teeth receiving cavities to couple the tooth to one or more other teeth with one or more other tooth receiving cavities, a first polymeric interproximal engagement structure (1014, 1024, 1034) positioned in an interproximal space between adjacent tooth receiving cavities, the structure extending from a lingual side to engage with and apply a force to the tooth from the interproximal space and move the tooth from the first position and orientation to the second position and orientation when the appliance is worn; and a second polymeric interproximal engagement structure (1014, 1024, 1034) positioned in the interproximal space between adjacent tooth receiving cavities, the structure extending from a buccal side to engage with and apply a force to the tooth from the interproximal space and move the tooth from the first position and orientation to the second position and orientation when the appliance is worn, wherein each of the interproximal engagement structures comprises a width extending between adjacent teeth receiving cavities defining the interproximal space, and wherein the width successively increases among the sequence of appliances in order to increase successively a distance between the adjacent teeth. one or more teeth receiving cavities to couple the tooth to one or more other teeth with one or more other tooth receiving cavities, a first polymeric interproximal engagement structure (1014, 1024, 1034) positioned in an interproximal space between adjacent tooth receiving cavities, the structure extending from a lingual side to engage with and apply a force to the tooth from the interproximal space and move the tooth from the first position and orientation to the second position and orientation when the appliance is worn; and a second polymeric interproximal engagement structure (1014, 1024, 1034) positioned in the interproximal space between adjacent tooth receiving cavities, the structure extending from a buccal side to engage with and apply a force to the tooth from the interproximal space and move the tooth from the first position and orientation to the second position and orientation when the appliance is worn, wherein each of the interproximal engagement structures comprises a width extending between adjacent teeth receiving cavities defining the interproximal space, and wherein the width successively increases among the sequence of appliances in order to increase successively a distance between the adjacent teeth.
A method of making a package of bulked continuous filament yarn wound on a tube core having an axis comprising: (a) rotating said tube upon its axis; (b) winding said yarn on said tube using at least one non-adjacent wind ratio until said package diameter is from about 130 mm to about 180 mm; and then (c) precision winding said yarn on said tube using at least one wind ratio that is adjacent to an integral ribbon or adjacent to a non-integral ribbon. (a) rotating said tube upon its axis; (b) winding said yarn on said tube using at least one non-adjacent wind ratio until said package diameter is from about 130 mm to about 180 mm; and then (c) precision winding said yarn on said tube using at least one wind ratio that is adjacent to an integral ribbon or adjacent to a non-integral ribbon.
A system for powering a datacenter campus, characterised in that the datacenter campus is a datacenter that is distributed among a plurality of datacenter buildings, each datacenter building housing a plurality of server racks on one or more floors of the datacenter building, the system comprising: a first main direct current, DC, superconductor cable configured to receive direct current DC electrical power from a first alternating current, AC, power grid through a first AC-DC converter, wherein the first main DC superconductor cable has a first end connected to the first AC-DC converter; a second main DC superconductor cable configured to receive DC electrical power from a second AC power grid through a second AC-DC converter, wherein the second main DC superconductor cable has a first end connected to the second AC-DC converter; a DC-DC hub, which is positioned outside the plurality of datacenter buildings of the datacenter campus and is connected to a second end of the first superconductor cable and to a second end of the second main superconductor cable; and a plurality of secondary DC superconductor cables, wherein each secondary DC superconductor cable includes a first end electrically connected to the DC-DC hub and a second end electrically connected to server racks housed in a respective datacenter building of the plurality of datacenter buildings of the datacenter campus. a first main direct current, DC, superconductor cable configured to receive direct current DC electrical power from a first alternating current, AC, power grid through a first AC-DC converter, wherein the first main DC superconductor cable has a first end connected to the first AC-DC converter; a second main DC superconductor cable configured to receive DC electrical power from a second AC power grid through a second AC-DC converter, wherein the second main DC superconductor cable has a first end connected to the second AC-DC converter; a DC-DC hub, which is positioned outside the plurality of datacenter buildings of the datacenter campus and is connected to a second end of the first superconductor cable and to a second end of the second main superconductor cable; and a plurality of secondary DC superconductor cables, wherein each secondary DC superconductor cable includes a first end electrically connected to the DC-DC hub and a second end electrically connected to server racks housed in a respective datacenter building of the plurality of datacenter buildings of the datacenter campus.
A shaped polymer article comprising: a blow molded hollow member including an interior surface and an exterior surface and having a wall thickness between the interior surface and the exterior surface, the hollow member being made from a fiber reinforced polymeric composition comprising on a weight percent basis: a) a linear polyphenylene sulfide having a melt viscosity of from 20 Pa.s to 500 Pa.s; as determined in accordance with the ASTM Test No. 1238-70 at 316°C and at 1200 sec -1 b) a branched polyphenylene sulfide, the weight ratio of the branched polyphenylene sulfide to the linear polyphenylene sulfide being from 1:5 to 1:60, the linear polyphenylene sulfide and the branched polyphenylene sulfide being present in the composition in an amount of at least 35% by weight; c) reinforcing fibers present in the composition in an amount from 10% to 50% by weight; and d) a compatibilizer; and e) a polytetrafluoroethylene present in an amount from 0.01% to 3% by weight; wherein the composition has a melt viscosity of at least 3500 poise measured at 316oC and at 400 s -1, has a low shear rate storage modulus of at least 1500 Pa measured at 310°C and at 0.1 rad/s, and has an engineering stress of at least 350 kPa at a percent strain of 100%. a blow molded hollow member including an interior surface and an exterior surface and having a wall thickness between the interior surface and the exterior surface, the hollow member being made from a fiber reinforced polymeric composition comprising on a weight percent basis: a) a linear polyphenylene sulfide having a melt viscosity of from 20 Pa.s to 500 Pa.s; as determined in accordance with the ASTM Test No. 1238-70 at 316°C and at 1200 sec -1 b) a branched polyphenylene sulfide, the weight ratio of the branched polyphenylene sulfide to the linear polyphenylene sulfide being from 1:5 to 1:60, the linear polyphenylene sulfide and the branched polyphenylene sulfide being present in the composition in an amount of at least 35% by weight; c) reinforcing fibers present in the composition in an amount from 10% to 50% by weight; and d) a compatibilizer; and e) a polytetrafluoroethylene present in an amount from 0.01% to 3% by weight; a) a linear polyphenylene sulfide having a melt viscosity of from 20 Pa.s to 500 Pa.s; as determined in accordance with the ASTM Test No. 1238-70 at 316°C and at 1200 sec -1 b) a branched polyphenylene sulfide, the weight ratio of the branched polyphenylene sulfide to the linear polyphenylene sulfide being from 1:5 to 1:60, the linear polyphenylene sulfide and the branched polyphenylene sulfide being present in the composition in an amount of at least 35% by weight; c) reinforcing fibers present in the composition in an amount from 10% to 50% by weight; and d) a compatibilizer; and e) a polytetrafluoroethylene present in an amount from 0.01% to 3% by weight; wherein the composition has a melt viscosity of at least 3500 poise measured at 316oC and at 400 s -1, has a low shear rate storage modulus of at least 1500 Pa measured at 310°C and at 0.1 rad/s, and has an engineering stress of at least 350 kPa at a percent strain of 100%.
Electrode, comprising at least one oscillation generator and a carrier substrate with a carrier side and an electrochemically active side with an electrochemically active layer, wherein the electrochemically active layer, by means of a connector pad from the carrier side via electrically conductive connections is connected to a first voltage source or wherein the electrochemically active layer is connected directly to the first voltage source via laterally protruding contacts, characterised in that the at least one oscillation generator is applied to the carrier substrate on the carrier side or is embedded in the surface of the carrier substrate, in that the oscillation generator is electrically contacted with the first voltage source or a further voltage source and in that the carrier substrate is partially or completely composed of a ceramic material and/or at least one valve metal or comprises a ceramic material and/or at least one valve metal.