mhurhangee/ep-ind-claims huggingface dataset:
A low alloy heat-resistant steel comprising, by mass: from 0.03% to 0.09% of C; from 0.10% to 0.30% of Si; from 0.15% to 0.60% of Mn; 0.020% or less of P; 0.0060% or less of S; from 0.01% to 0.50% of Ni; from 0.01% to 0.50% of Co; from 0.01% to 0.50% of Cu; from 2.0% to 3.0% of Cr; from 0.05% to 0.35% of Mo; from 1.0% to 2.2% of W; from 0.15% to 0.28% of V; from 0.01% to 0.11% of Nb; from 0.002% to 0.022% of Ti; from 0.001% to 0.006% of B; from 0.001% to 0.012% of N; 0.020% or less of Al; and 0.020% or less of O; and optionally at least one element selected from the group consisting of 0.20% or less of Ta; 0.0150% or less of Ca; 0.0150% or less of Mg; 0.050% or less of REM; and Sn in an amount satisfying the following Formula; % Sn ≤ 2 × % B + 0.010 % with a balance consisting of Fe and impurities, wherein a total amount of Ni, Co and Cu satisfies the following Formula, and an amount of W, analyzed as an electrolytic extraction residue, satisfies the following Formula: 0.03 ≤ % Ni + % Co + % Cu ≤ 0.80 − 10 × % B + 0.07 ≤ % W ER ≤ 10 × % B + 0.18 wherein in Formuale, and, [%Ni], [%Co], [%Cu], [%B] and [%Sn] represent amounts of Ni, Co, Cu, B and Sn, in % by mass, contained in the steel, respectively; and [%W] ER represents an amount of W, analyzed as the electrolytic extraction residue determined by the method defined in the description, in % by mass. from 0.03% to 0.09% of C; from 0.10% to 0.30% of Si; from 0.15% to 0.60% of Mn; 0.020% or less of P; 0.0060% or less of S; from 0.01% to 0.50% of Ni; from 0.01% to 0.50% of Co; from 0.01% to 0.50% of Cu; from 2.0% to 3.0% of Cr; from 0.05% to 0.35% of Mo; from 1.0% to 2.2% of W; from 0.15% to 0.28% of V; from 0.01% to 0.11% of Nb; from 0.002% to 0.022% of Ti; from 0.001% to 0.006% of B; from 0.001% to 0.012% of N; 0.020% or less of Al; and 0.020% or less of O; and optionally at least one element selected from the group consisting of 0.20% or less of Ta; 0.0150% or less of Ca; 0.0150% or less of Mg; 0.050% or less of REM; and Sn in an amount satisfying the following Formula; % Sn ≤ 2 × % B + 0.010 % with a balance consisting of Fe and impurities, wherein a total amount of Ni, Co and Cu satisfies the following Formula, and an amount of W, analyzed as an electrolytic extraction residue, satisfies the following Formula: 0.03 ≤ % Ni + % Co + % Cu ≤ 0.80 − 10 × % B + 0.07 ≤ % W ER ≤ 10 × % B + 0.18 wherein in Formuale, and, [%Ni], [%Co], [%Cu], [%B] and [%Sn] represent amounts of Ni, Co, Cu, B and Sn, in % by mass, contained in the steel, respectively; and [%W] ER represents an amount of W, analyzed as the electrolytic extraction residue determined by the method defined in the description, in % by mass.
A sintered foam structure formed from foam beads that are formed from a composition comprising: an ionomer comprising, in polymerized form, ethylene, an unsaturated acid comonomer, and, optionally, an acrylate comonomer, wherein the unsaturated acid comonomer is completely or partially neutralized with a neutralizing agent, and wherein the composition comprises from 25 wt.% to 100 wt.% of the ionomer. an ionomer comprising, in polymerized form, ethylene, an unsaturated acid comonomer, and, optionally, an acrylate comonomer, wherein the unsaturated acid comonomer is completely or partially neutralized with a neutralizing agent, and
A method of checking an amount of a hydrogen gas delivered to a vehicle at a hydrogen refueling station during a refueling process of the vehicle, the method comprising the steps of: (a) Filling a vehicle tank of the vehicle during the refueling process at the hydrogen refueling station, (b) Measuring the amount of hydrogen gas delivered to the vehicle tank during the refueling process by means of a gas meter of the hydrogen refueling station, (c) Establishing a communication link between the hydrogen refueling station and the vehicle or an external device connected to the vehicle, (d) Transmitting at least one meter information of the gas meter, which contains the amount of hydrogen gas measured by the gas meter, to the vehicle or the external device by means of the communication link, and (e) Determining the amount of hydrogen gas absorbed in the vehicle tank during the refueling process, - Determining a differential gas quantity between the measured gas quantity of hydrogen and the absorbed gas quantity of hydrogen, characterized in that the method further comprises the step: - Transmission of a message (330, 340) based on the determined differential gas quantity to the hydrogen refueling station by means of the communication link. (a) Filling a vehicle tank of the vehicle during the refueling process at the hydrogen refueling station, (b) Measuring the amount of hydrogen gas delivered to the vehicle tank during the refueling process by means of a gas meter of the hydrogen refueling station, (c) Establishing a communication link between the hydrogen refueling station and the vehicle or an external device connected to the vehicle, (d) Transmitting at least one meter information of the gas meter, which contains the amount of hydrogen gas measured by the gas meter, to the vehicle or the external device by means of the communication link, and (e) Determining the amount of hydrogen gas absorbed in the vehicle tank during the refueling process, - Determining a differential gas quantity between the measured gas quantity of hydrogen and the absorbed gas quantity of hydrogen, characterized in that the method further comprises the step: - Transmission of a message (330, 340) based on the determined differential gas quantity to the hydrogen refueling station by means of the communication link. - Determining a differential gas quantity between the measured gas quantity of hydrogen and the absorbed gas quantity of hydrogen, - Transmission of a message (330, 340) based on the determined differential gas quantity to the hydrogen refueling station by means of the communication link.
A method of treating a coated cutting tool using laser shock peening, the coated cutting tool consists of a substrate and a coating, wherein the substrate is of cemented carbide or cermet, preferably cemented carbide, and wherein the coating comprises a CVD layer and/or a PVD layer, wherein said method comprises a step of applying LSP to at least a portion of the cutting tool, wherein the LSP energy density is within 0.4 to 1.6 J/mm 2, preferably within 0.9 to 1.4 J/mm 2, more preferably within 1.1 to 1.3 J/mm 2.
Wiper blade with a wiper strip, a supporting element, which distributes a contact pressure onto the windscreen over the length of the wiper blade, an adapter for connection to a wiper arm, at least one end cap at one or both ends of the wiper blade, said end caps covering at least the supporting element, and nozzle elements for applying a cleaning fluid to the pane, and fluid lines (5, 10, 13) to the nozzle elements, which fluid lines are connectable to fluid feed lines of the wiper arm via the adapter, characterized in that a fluid feed line leads from the adapter to the at least one end cap, and a valve unit is connected to the fluid feed line in front of or in the end cap, and the nozzle elements are connected downstream of the valve unit, wherein end caps with a valve unit are arranged at both ends of the wiper blade.
A heat exchange fin, with a tube hole formed thereon for a heat exchange tube to be inserted into, and with a corrugated structure arranged near the tube hole, wherein, the corrugated structure comprises a wave section arranged along a flow direction of fluid medium, wherein the wave section is the total length of corrugation in the corrugated structure, where a distance between two adjacent wave crests or wave troughs of the wave section is one wavelength, and wherein, a bridge plate is further arranged at the wave crests and wave troughs of the wave section, respectively, where the bridge plate deflects relative to the wave crests and wave troughs by a preset distance, characterised in that a total length of the wave section is 1-1.5 times the wavelength. wherein, a bridge plate is further arranged at the wave crests and wave troughs of the wave section, respectively, where the bridge plate deflects relative to the wave crests and wave troughs by a preset distance, characterised in that a total length of the wave section is 1-1.5 times the wavelength.
A system for use in cryoablation procedures, comprising a first device (14; 16), a second device comprising, an elongate body having a lumen dimensioned to receive the first device (14; 16) therethrough, the elongate body including a distal region, and a balloon positioned about the distal region and defining an interior in communication with the lumen, wherein the balloon is expandable outwardly from an outer surface of the elongate body, and a first pressure sensor positioned on the distal region of the first device (14; 16) extending distally of the second device when received in the lumen and characterized by a second pressure sensor positioned on the distal region of the second device distally of the balloon. a first device (14; 16), a second device comprising, an elongate body having a lumen dimensioned to receive the first device (14; 16) therethrough, the elongate body including a distal region, and a balloon positioned about the distal region and defining an interior in communication with the lumen, wherein the balloon is expandable outwardly from an outer surface of the elongate body, and an elongate body having a lumen dimensioned to receive the first device (14; 16) therethrough, the elongate body including a distal region, and a balloon positioned about the distal region and defining an interior in communication with the lumen, wherein the balloon is expandable outwardly from an outer surface of the elongate body, and a first pressure sensor positioned on the distal region of the first device (14; 16) extending distally of the second device when received in the lumen and characterized by a second pressure sensor positioned on the distal region of the second device distally of the balloon.
An aftertreatment assembly, comprising: a decomposition chamber having a reductant opening to receive reductant from a reductant source, the decomposition chamber including an inlet upstream of the reductant opening; a catalyst downstream of the decomposition chamber; and an exhaust flow directing device at the inlet and positioned upstream of the reductant opening, the exhaust flow directing device defining: a first exhaust flow path through the exhaust flow directing device and a second exhaust flow path between an outer wall of the exhaust flow directing device and the inlet, characterized in that the exhaust flow directing device comprises a slot (258; 358a) extending from a first end of the exhaust flow directing device, at which exhaust flow is received, to a second end of the exhaust flow directing device, which is located opposite the first end, the slot (258; 358a) being oriented toward a side of the decomposition chamber in which the reductant opening is located. a decomposition chamber having a reductant opening to receive reductant from a reductant source, the decomposition chamber including an inlet upstream of the reductant opening; a catalyst downstream of the decomposition chamber; and an exhaust flow directing device at the inlet and positioned upstream of the reductant opening, the exhaust flow directing device defining: a first exhaust flow path through the exhaust flow directing device and a second exhaust flow path between an outer wall of the exhaust flow directing device and the inlet, characterized in that the exhaust flow directing device comprises a slot (258; 358a) extending from a first end of the exhaust flow directing device, at which exhaust flow is received, to a second end of the exhaust flow directing device, which is located opposite the first end, the slot (258; 358a) being oriented toward a side of the decomposition chamber in which the reductant opening is located.
A method for determining the presence or absence of a fetal aneuploidy using fetal DNA from a maternal sample, wherein the maternal sample comprises differentially methylated maternal and fetal DNA, comprising a) digesting the maternal DNA in a maternal sample using one or more methylation sensitive restriction enzymes thereby enriching the fetal DNA; b) determining the amount of fetal DNA from a target chromosome in a multiplex single reaction, by determining the amount of fetal DNA at multiple loci selected from the differentially methylated nucleic acids as provided in SEQ ID NOs: 210, 176, 179, 180, 184, 188, 189, 190, 191, 193, 195, 198, 199, 200, 201, 202, 205, 207, 208, 209, 211, 212, 213, 214, 225, 226, 231, 232, 233, 235, 241, 257, 258, 259, and 261; c) determining the amount of fetal DNA from a reference chromosome in a multiplex single reaction, by determining the amount of fetal DNA at multiple loci of the reference genome; and d) comparing the amount of fetal DNA from step b) to step c), wherein a statistically significant difference between the amount of target and reference fetal DNA is indicative of the presence of a fetal aneuploidy. a) digesting the maternal DNA in a maternal sample using one or more methylation sensitive restriction enzymes thereby enriching the fetal DNA; b) determining the amount of fetal DNA from a target chromosome in a multiplex single reaction, by determining the amount of fetal DNA at multiple loci selected from the differentially methylated nucleic acids as provided in SEQ ID NOs: 210, 176, 179, 180, 184, 188, 189, 190, 191, 193, 195, 198, 199, 200, 201, 202, 205, 207, 208, 209, 211, 212, 213, 214, 225, 226, 231, 232, 233, 235, 241, 257, 258, 259, and 261; c) determining the amount of fetal DNA from a reference chromosome in a multiplex single reaction, by determining the amount of fetal DNA at multiple loci of the reference genome; and d) comparing the amount of fetal DNA from step b) to step c),
A lifting element connection device (1; 1') for connecting a lifting element suspended from a cable to a sling element, characterised in that the lifting element connection device (1; 1') comprises: a top surface having at least one angled portion for guiding the lifting element towards a receiving area of the lifting element connection device (1; 1') and a lifting element receiving portion configured for holding the sling element; wherein the lifting element receiving portion is further configured for receiving the lifting element from the receiving area and providing a connection between the lifting element and the sling element when the lifting element is positioned in the lifting element receiving portion, and wherein the lifting element connection device (1; 1') comprises a groove in the top surface, the groove extending from the receiving area to a periphery of the top surface for allowing the cable to move through at least a portion of the top surface. a top surface having at least one angled portion for guiding the lifting element towards a receiving area of the lifting element connection device (1; 1') and a lifting element receiving portion configured for holding the sling element; wherein the lifting element receiving portion is further configured for receiving the lifting element from the receiving area and providing a connection between the lifting element and the sling element when the lifting element is positioned in the lifting element receiving portion, and wherein the lifting element connection device (1; 1') comprises a groove in the top surface, the groove extending from the receiving area to a periphery of the top surface for allowing the cable to move through at least a portion of the top surface.
An intercooled cooling air system (100;200;300) for a gas turbine engine, the intercooled cooling system comprising: a first duct wall configured to isolate a main bypass stream from a secondary bypass stream of the gas turbine engine; a second duct wall configured to isolate the secondary bypass stream from a third bypass stream of the gas turbine engine, wherein the third bypass stream is defined between the second duct wall and a casing of the gas turbine engine; a plurality of cooling stages (110,115;210,215;310,315) in fluid communication with an air stream of the secondary bypass stream utilized by the plurality of cooling stages for cooling, wherein a first cooling stage (110;210;310) of the plurality of cooling stages is fluidly coupled to a bleed port of a compressor of the gas turbine engine to receive bleed air and cool the bleed air with the air stream to produce a cool bleed air; and a pump fluidly coupled to the first cooling stage (110;210;310) to receive the cool bleed air and increase a pressure of the cool bleed air to produce a pressurized cool bleed air, wherein a second cooling stage (115;215;315) of the plurality of cooling stages is fluidly coupled to the pump to receive the pressurized cool bleed air and cool the pressurized cool bleed air to produce an intercooled cooling air, wherein the second cooling stage (115;215;315) provides the intercooled cooling air to a port located downstream of a combustor section of the gas turbine engine and located at or near an intake of a turbine section of the gas turbine engine. a first duct wall configured to isolate a main bypass stream from a secondary bypass stream of the gas turbine engine; a second duct wall configured to isolate the secondary bypass stream from a third bypass stream of the gas turbine engine, wherein the third bypass stream is defined between the second duct wall and a casing of the gas turbine engine; a plurality of cooling stages (110,115;210,215;310,315) in fluid communication with an air stream of the secondary bypass stream utilized by the plurality of cooling stages for cooling, wherein a first cooling stage (110;210;310) of the plurality of cooling stages is fluidly coupled to a bleed port of a compressor of the gas turbine engine to receive bleed air and cool the bleed air with the air stream to produce a cool bleed air; and a pump fluidly coupled to the first cooling stage (110;210;310) to receive the cool bleed air and increase a pressure of the cool bleed air to produce a pressurized cool bleed air, wherein a second cooling stage (115;215;315) of the plurality of cooling stages is fluidly coupled to the pump to receive the pressurized cool bleed air and cool the pressurized cool bleed air to produce an intercooled cooling air, wherein the second cooling stage (115;215;315) provides the intercooled cooling air to a port located downstream of a combustor section of the gas turbine engine and located at or near an intake of a turbine section of the gas turbine engine.
A liquid pharmaceutical composition comprising: - 45 to 55 mg/ml adalimumab; - 5 to 14 mM histidine (or histidine buffer system); - 190 to 210 mM trehalose; - 40 to 60 mM sodium chloride; - water (for injection); - wherein the composition: o has a pH between 6.3 and 6.5; ∘ is free of arginine or comprises arginine in a concentration of at most 0.001 mM; o Is free of amino acids other than histidine or comprises one or more amino acids other than histidine in a (collective) concentration of at most 0.001 mM; o is free of surfactants or comprises one or more surfactants in a (collective) concentration of at most 0.0001 mM; and/or o is free of phosphate buffering agents or comprises a phosphate buffer system in a concentration of at most 0.001 mM. - 45 to 55 mg/ml adalimumab; - 5 to 14 mM histidine (or histidine buffer system); - 190 to 210 mM trehalose; - 40 to 60 mM sodium chloride; - water (for injection); - wherein the composition: o has a pH between 6.3 and 6.5; ∘ is free of arginine or comprises arginine in a concentration of at most 0.001 mM; o Is free of amino acids other than histidine or comprises one or more amino acids other than histidine in a (collective) concentration of at most 0.001 mM; o is free of surfactants or comprises one or more surfactants in a (collective) concentration of at most 0.0001 mM; and/or o is free of phosphate buffering agents or comprises a phosphate buffer system in a concentration of at most 0.001 mM. o has a pH between 6.3 and 6.5; ∘ is free of arginine or comprises arginine in a concentration of at most 0.001 mM; o Is free of amino acids other than histidine or comprises one or more amino acids other than histidine in a (collective) concentration of at most 0.001 mM; o is free of surfactants or comprises one or more surfactants in a (collective) concentration of at most 0.0001 mM; and/or o is free of phosphate buffering agents or comprises a phosphate buffer system in a concentration of at most 0.001 mM.
A mechanism of a lipstick tube, comprising a cup, an innerbody, a spiral and an A-shell, wherein an axial key slot structure and a circumferential clasp clamping groove structure are provided between the spiral and the A-shell; wherein the clasp clamping groove structure comprises a first clasp provided on an outer wall of the spiral, and a first clamping groove located on an inner wall of the A-shell and matched with the first clasp; wherein a second clamping groove next to the first clasp is provided on the outer wall of the spiral; a second clasp matched with the second clamping groove is provided on the inner wall of the A-shell; and the second clasp is next to the first clamping groove; characterized in that a junction between the first clasp and the second clamping groove and a junction between the first clamping groove and the second clasp are matched to be a vertical step structure. wherein a second clamping groove next to the first clasp is provided on the outer wall of the spiral; a second clasp matched with the second clamping groove is provided on the inner wall of the A-shell; and the second clasp is next to the first clamping groove; characterized in that a junction between the first clasp and the second clamping groove and a junction between the first clamping groove and the second clasp are matched to be a vertical step structure.
An article of footwear having an upper and a sole structure secured to the upper, at least a portion of the upper comprising: a plurality of lace-receiving elements; a base layer extending from the lace-receiving elements to the sole structure, the base layer having at least one surface; a plurality of first strands having a substantially vertical orientation and extending from an area proximal to the lace-receiving elements to an area proximal to the sole structure, the first strands laying substantially parallel to the surface of the base layer in a region between the lace-receiving elements and the sole structure, and the first strands having a first tensile strength; and a plurality of second strands having, a rearwardly-angled orientation and extending from the area proximal to the lace-receiving elements to the area proximal to the sole structure, the second strands laying substantially parallel to the surface of the base layer in the region between the lace-receiving elements and the sole structure, and the second strands having a second tensile strength that is at least fifty percent greater than the first tensile strength. a plurality of lace-receiving elements; a base layer extending from the lace-receiving elements to the sole structure, the base layer having at least one surface; a plurality of first strands having a substantially vertical orientation and extending from an area proximal to the lace-receiving elements to an area proximal to the sole structure, the first strands laying substantially parallel to the surface of the base layer in a region between the lace-receiving elements and the sole structure, and the first strands having a first tensile strength; and a plurality of second strands having, a rearwardly-angled orientation and extending from the area proximal to the lace-receiving elements to the area proximal to the sole structure, the second strands laying substantially parallel to the surface of the base layer in the region between the lace-receiving elements and the sole structure, and the second strands having a second tensile strength that is at least fifty percent greater than the first tensile strength.