mhurhangee/patent-ind-claim-en huggingface dataset:
A rubber composition for treads, comprising: a diene rubber including styrene-butadiene rubber; zinc dithiophosphate; a carbon black having a BET value of 151 m 2 /g or more; silica; an inorganic filler which comprises at least one selected from the group consisting of a compound represented by the formula below, magnesium sulfate, and silicon carbide, and has a BET value of 5 to 120 m 2 /g and a linseed oil absorption of 30 to 80 mL/100 g; and sulfur, wherein, per 100 parts by mass of the diene rubber, there are 0.2 to 15 parts by mass of the zinc dithiophosphate, 5 to 130 parts by mass of the carbon black, 50 parts by mass or more of the silica, 1 to 70 parts by mass of the inorganic filler, and less than 2.5 parts by mass of zinc oxide, the formula being mM·xSiO y ·zH 2 O wherein M represents at least one metal selected from the group consisting of Al, Mg, Ti, Ca, and Zr, or an oxide or hydroxide of the metal; m represents an integer of 1 to 5; x represents an integer of 0 to 10; y represents an integer of 2 to 5; and z represents an integer of 0 to 10, and the BET value of the inorganic filler is determined by the BET method in accordance with ASTM D3037-81, the linseed oil absorption of the inorganic filler is determined in accordance with JIS-K5101-13, and the BET value of the carbon black is determined in accordance with JIS K 6217-2:2001. a diene rubber including styrene-butadiene rubber; zinc dithiophosphate; a carbon black having a BET value of 151 m 2 /g or more; silica; an inorganic filler which comprises at least one selected from the group consisting of a compound represented by the formula below, magnesium sulfate, and silicon carbide, and has a BET value of 5 to 120 m 2 /g and a linseed oil absorption of 30 to 80 mL/100 g; and sulfur, wherein, per 100 parts by mass of the diene rubber, there are 0.2 to 15 parts by mass of the zinc dithiophosphate, 5 to 130 parts by mass of the carbon black, 50 parts by mass or more of the silica, 1 to 70 parts by mass of the inorganic filler, and less than 2.5 parts by mass of zinc oxide, the formula being mM·xSiO y ·zH 2 O wherein M represents at least one metal selected from the group consisting of Al, Mg, Ti, Ca, and Zr, or an oxide or hydroxide of the metal; m represents an integer of 1 to 5; x represents an integer of 0 to 10; y represents an integer of 2 to 5; and z represents an integer of 0 to 10, and the BET value of the inorganic filler is determined by the BET method in accordance with ASTM D3037-81, the linseed oil absorption of the inorganic filler is determined in accordance with JIS-K5101-13, and the BET value of the carbon black is determined in accordance with JIS K 6217-2:2001.
- Method for the production of an extruded plate comprising the following steps: a) providing calcium carbonate (CaCO3) powder; b) providing polyvinyl chloride (PVC) powder; c) providing additives as stabilizers, consisting of at least Ca/Zn stabilizers, impact modifiers and internal and external waxes; wherein c1), the proportion of calcium carbonate (CaCO 3 ) powder is between 60 and 80 % by weight, the proportion of polyvinyl chloride (PVC) powder is between 20 and 40 % by weight and the proportion of additives is up to 5 % by weight; d) mixing the calcium carbonate (CaCO 3 ) powder with the polyvinyl chloride (PVC) powder and the additives; e) heating the mixture to a temperature of 100 to 140°C until the polyvinyl chloride (PVC) softens to a kneadable mass and the calcium carbonate (CaCO 3 ) at least partially binds to the polyvinyl (PVC); f) cooling the mass to a temperature of 40 to 50°C; g) conveying the mass to an extruder; h) melting and extruding of the mass by means of an extruder and moulding by means of a slot die to yield a plate; i) pressing the still-warm plate to a desired final thickness by means of at least two calender rolls. a) providing calcium carbonate (CaCO3) powder; b) providing polyvinyl chloride (PVC) powder; c) providing additives as stabilizers, consisting of at least Ca/Zn stabilizers, impact modifiers and internal and external waxes; wherein c1), the proportion of calcium carbonate (CaCO 3 ) powder is between 60 and 80 % by weight, the proportion of polyvinyl chloride (PVC) powder is between 20 and 40 % by weight and the proportion of additives is up to 5 % by weight; d) mixing the calcium carbonate (CaCO 3 ) powder with the polyvinyl chloride (PVC) powder and the additives; e) heating the mixture to a temperature of 100 to 140°C until the polyvinyl chloride (PVC) softens to a kneadable mass and the calcium carbonate (CaCO 3 ) at least partially binds to the polyvinyl (PVC); f) cooling the mass to a temperature of 40 to 50°C; g) conveying the mass to an extruder; h) melting and extruding of the mass by means of an extruder and moulding by means of a slot die to yield a plate; i) pressing the still-warm plate to a desired final thickness by means of at least two calender rolls.
A two-part epoxy adhesive comprising: a Part A comprising, based on the total weight of components a) and b): a) 99.5 to 99.99 weight percent of at least one curable epoxy resin; b) 0.01 to 0.5 weight percent of at least one pH indicator dye exhibiting an abrupt color change from colorless to a color in the pH range of 8.0-10.6; and a Part B comprising, based on the total weight of components c) - f): c) 89 to 97 weight percent of at least one aliphatic primary polyamine; d) 1 to 3 weight percent of at least one tris(2,4,6-dialkylaminoalkyl)phenol having from 13 to 24 carbon atoms; e) 1 to 3 weight percent of at least one aliphatic tertiary 1,3-bis(N,N-dialkylaminoalkyl)urea having from 6 to 24 carbon atoms; and f) 1 to 5 weight percent at least one of an alkali metal nitrate or an alkaline earth nitrate, wherein the ratio of the total combined weight of components a) and b) to the total combined weight of components c) - f) is in the range 1.0 to 1.5. a Part A comprising, based on the total weight of components a) and b): a) 99.5 to 99.99 weight percent of at least one curable epoxy resin; b) 0.01 to 0.5 weight percent of at least one pH indicator dye exhibiting an abrupt color change from colorless to a color in the pH range of 8.0-10.6; and a) 99.5 to 99.99 weight percent of at least one curable epoxy resin; b) 0.01 to 0.5 weight percent of at least one pH indicator dye exhibiting an abrupt color change from colorless to a color in the pH range of 8.0-10.6; and a Part B comprising, based on the total weight of components c) - f): c) 89 to 97 weight percent of at least one aliphatic primary polyamine; d) 1 to 3 weight percent of at least one tris(2,4,6-dialkylaminoalkyl)phenol having from 13 to 24 carbon atoms; e) 1 to 3 weight percent of at least one aliphatic tertiary 1,3-bis(N,N-dialkylaminoalkyl)urea having from 6 to 24 carbon atoms; and f) 1 to 5 weight percent at least one of an alkali metal nitrate or an alkaline earth nitrate, c) 89 to 97 weight percent of at least one aliphatic primary polyamine; d) 1 to 3 weight percent of at least one tris(2,4,6-dialkylaminoalkyl)phenol having from 13 to 24 carbon atoms; e) 1 to 3 weight percent of at least one aliphatic tertiary 1,3-bis(N,N-dialkylaminoalkyl)urea having from 6 to 24 carbon atoms; and f) 1 to 5 weight percent at least one of an alkali metal nitrate or an alkaline earth nitrate, wherein the ratio of the total combined weight of components a) and b) to the total combined weight of components c) - f) is in the range 1.0 to 1.5.
- A dishwasher comprising a body ; a tub wherein the processes of washing, rinsing and drying are performed; a drying duct that provides the drying of the items washed; a drying fan that provides the flow of the air in the drying duct ; a heat pump system that is disposed at the lower part of the tub and that provides the heating of the washing water; a casing that constitutes the lower section of the body and encloses the region wherein the heat pump system is integrated; a compressor , a condenser , an evaporator , at least one evaporator fan and an expansion element that constitute the heat pump system ; an air duct having at least one inlet port arranged at the front surface of the body and opening to the outer environment and an outlet port opening into the region enclosed by the casing at the lower section of the body , wherein the air duct enables the outer environment air received through the inlet port to be transferred into the body and into the region surrounded by the casing through the outlet port by means of the vacuum created in the body by the at least one evaporator fan , characterized by the at least one inlet port being arranged at the upper part of the front side of the body .
Synthetic leather comprising: a fibrous substrate, which fibrous substrate is a circular knitted fabric, wherein a mass per unit area of the fibrous substrate is 350 to 600 g/m 2 and a thickness of the fibrous substrate is 0.9 to 1.2 mm; and a polyurethane resin layer that is formed on the fibrous substrate, wherein an amount of dry application of the polyurethane resin layer is 120 to 320 g/m 2 , the synthetic leather having a grain pattern on a front surface, wherein a stiffness of the front surface of the synthetic leather is 65 to 95 mm and a stiffness of a rear surface of the synthetic leather is 55 to 85 mm, wherein the stiffness of the front surface and the stiffness of the rear surface are measured in accordance with JIS L1096 8.21.1A, "45° cantilever method", as described in the description. a fibrous substrate, which fibrous substrate is a circular knitted fabric, wherein a mass per unit area of the fibrous substrate is 350 to 600 g/m 2 and a thickness of the fibrous substrate is 0.9 to 1.2 mm; and a polyurethane resin layer that is formed on the fibrous substrate, wherein an amount of dry application of the polyurethane resin layer is 120 to 320 g/m 2 , the synthetic leather having a grain pattern on a front surface, wherein a stiffness of the front surface of the synthetic leather is 65 to 95 mm and a stiffness of a rear surface of the synthetic leather is 55 to 85 mm, wherein the stiffness of the front surface and the stiffness of the rear surface are measured in accordance with JIS L1096 8.21.1A, "45° cantilever method", as described in the description.
An electrical connector assembly , comprising: a first connector body defining a first terminal cavity therein; a male terminal projecting along a terminal axis to a tip and secured within the terminal cavity by a first primary lock feature ; and a terminal stabilizer defining an aperture , disposed within the connector body , and moveable within the connector body from a pre-staged position to a staged position , wherein a primary lock retaining feature in the form of a rib feature is integrated with the terminal stabilizer and extends parallel to the terminal axis from a first face of the terminal stabilizer defining the aperture , and wherein the rib feature is configured to engage the primary lock feature as the terminal stabilizer moves from the pre-staged position to the staged position ; a second connector body defining a second terminal cavity therein and configured to mate with the first connector body ; and a female terminal secured within the second terminal cavity by a second primary lock feature and configured to mate with the male terminal , wherein the terminal stabilizer defines a second primary lock retaining feature configured to engage the second primary lock feature as the terminal stabilizer moves from the pre-staged position to the staged position as the first connector body is mated with the second connector body , characterized in that , the terminal stabilizer defines a retraction feature configured to move the terminal stabilizer from the staged position to the pre-staged position as the first connector body is unmated from the second connector body . a first connector body defining a first terminal cavity therein; a male terminal projecting along a terminal axis to a tip and secured within the terminal cavity by a first primary lock feature ; and a terminal stabilizer defining an aperture , disposed within the connector body , and moveable within the connector body from a pre-staged position to a staged position , wherein a primary lock retaining feature in the form of a rib feature is integrated with the terminal stabilizer and extends parallel to the terminal axis from a first face of the terminal stabilizer defining the aperture , and wherein the rib feature is configured to engage the primary lock feature as the terminal stabilizer moves from the pre-staged position to the staged position ; a second connector body defining a second terminal cavity therein and configured to mate with the first connector body ; and a female terminal secured within the second terminal cavity by a second primary lock feature and configured to mate with the male terminal , wherein the terminal stabilizer defines a second primary lock retaining feature configured to engage the second primary lock feature as the terminal stabilizer moves from the pre-staged position to the staged position as the first connector body is mated with the second connector body , characterized in that , the terminal stabilizer defines a retraction feature configured to move the terminal stabilizer from the staged position to the pre-staged position as the first connector body is unmated from the second connector body .
Method for separating excess material (WS) from an additively manufactured component (BT), wherein a) spatially resolved structure data (CAD) of the component (BT) are received, b) the structure data (CAD) are used to divide a cavity (H) in the component (BT) into grid cells (GZ) by way of a virtual spatial grid (G), with a spatial alignment of the grid (G) relative to the component (BT) being specified by an alignment specification (RA), c) a discrete pattern (R) of spatial orientations of the component (BT) is ascertained on the basis of the alignment specification (RA), d) the grid cells (GZ) of the cavity (H) are filled with a virtual material (VWP) in a simulation, e) the structure data (CAD) are used to simulate an emptying procedure of the virtual material (VWP) from the component (BT) for spatial orientations restricted to the discrete pattern (R), with a temporal sequence of orientations (AP ,..., AP(N)) that are restricted to the discrete pattern (R) being ascertained, and f) the component (BT) is successively rotated into the orientations (AP ,..., AP(N)) of the temporal sequence on the basis of the simulated emptying procedure. a) spatially resolved structure data (CAD) of the component (BT) are received, b) the structure data (CAD) are used to divide a cavity (H) in the component (BT) into grid cells (GZ) by way of a virtual spatial grid (G), with a spatial alignment of the grid (G) relative to the component (BT) being specified by an alignment specification (RA), c) a discrete pattern (R) of spatial orientations of the component (BT) is ascertained on the basis of the alignment specification (RA), d) the grid cells (GZ) of the cavity (H) are filled with a virtual material (VWP) in a simulation, e) the structure data (CAD) are used to simulate an emptying procedure of the virtual material (VWP) from the component (BT) for spatial orientations restricted to the discrete pattern (R), with a temporal sequence of orientations (AP ,..., AP(N)) that are restricted to the discrete pattern (R) being ascertained, and f) the component (BT) is successively rotated into the orientations (AP ,..., AP(N)) of the temporal sequence on the basis of the simulated emptying procedure.
Valve unit for a valve of an inflatable bladder for a sports ball, the valve unit comprising: a. a cavity containing a viscous, non-solid material, the cavity being adapted to be repeatedly penetrated by a gas injector , b. wherein the viscous, non-solid material is adapted to seal the valve unit against gas leakage when the gas injector is not penetrating the cavity , characterized in that c. the viscous, non-solid material exhibits a viscosity at a temperature of 25°C in the range of 0,005 m 2 /s to 0,1 m 2 /s (5,000 cSt to 100,000 cSt). a. a cavity containing a viscous, non-solid material, the cavity being adapted to be repeatedly penetrated by a gas injector , b. wherein the viscous, non-solid material is adapted to seal the valve unit against gas leakage when the gas injector is not penetrating the cavity , c. the viscous, non-solid material exhibits a viscosity at a temperature of 25°C in the range of 0,005 m 2 /s to 0,1 m 2 /s (5,000 cSt to 100,000 cSt).
Method for generating energy, in particular for mobile applications, wherein - hydrogen (H2) is produced by at least partial dehydrogenation of a hydrogenated liquid organic hydrogen carrier (LOHC) in a chemical reactor , - electricity (I) and water (H2O) are generated in at least one fuel cell from hydrogen (H2) produced by the reactor and from oxygen (O2), - heat for the chemical reactor is generated in a heating device from hydrogen (H2) produced by the reactor , - the hydrogen (H2) produced by the chemical reactor is first conducted through the at least one fuel cell and then supplied to the heating device , characterised in that - a volumetric flow of hydrogen (H2) produced by the reactor that is supplied to the at least one fuel cell , or - in order to control and/or regulate the supply of hydrogen (H2) produced by the reactor to the at least one fuel cell , a pressure of the hydrogen (H2) after the latter has been conducted through the at least one fuel cell or a temperature of the at least one fuel cell is controlled and/or regulated as a function of an electrical power output to be generated by the at least one fuel cell and a volumetric flow of hydrogen produced by the reactor that is required for the heating device . - hydrogen (H2) is produced by at least partial dehydrogenation of a hydrogenated liquid organic hydrogen carrier (LOHC) in a chemical reactor , - electricity (I) and water (H2O) are generated in at least one fuel cell from hydrogen (H2) produced by the reactor and from oxygen (O2), - heat for the chemical reactor is generated in a heating device from hydrogen (H2) produced by the reactor , - the hydrogen (H2) produced by the chemical reactor is first conducted through the at least one fuel cell and then supplied to the heating device , characterised in that - a volumetric flow of hydrogen (H2) produced by the reactor that is supplied to the at least one fuel cell , or - in order to control and/or regulate the supply of hydrogen (H2) produced by the reactor to the at least one fuel cell , a pressure of the hydrogen (H2) after the latter has been conducted through the at least one fuel cell or a temperature of the at least one fuel cell
An unmanned aerial vehicle comprising: a frame elongated along a frame axis (A F ), the frame comprising a leading side and an aft side , the frame further comprising a left end portion and a right end portion ; a first forward rotor assembly connected to the left end portion of the frame ; a second forward rotor assembly connected to the right end portion of the frame , the first forward rotor assembly and the second forward rotor assembly being positioned on the leading side of the frame ; a first aft rotor assembly connected to the left end portion of the frame ; a second aft rotor assembly connected to the right end portion of the frame , the first aft rotor assembly and the second aft rotor assembly being positioned on the aft side of the frame ; a first aft boom connecting the first aft rotor assembly to the left end portion of the frame ; a second aft boom connecting the second aft rotor assembly to the right end portion of the frame ; a compartment connected to the frame , the compartment comprising a leading side ; a curved leading-edge fairing disposed on the frame , wherein a portion of the curved leading-edge fairing extends to cover the leading side of the compartment , and wherein the curved leading-edge fairing reduces drag during flight in a forward direction to enable a substantially level flight profile; a pair of outboard rotor assemblies disposed on a pair of outboard booms ; and a pair of forward boom fairings disposed on the pair of outboard booms . a frame elongated along a frame axis (A F ), the frame comprising a leading side and an aft side , the frame further comprising a left end portion and a right end portion ; a first forward rotor assembly connected to the left end portion of the frame ; a second forward rotor assembly connected to the right end portion of the frame , the first forward rotor assembly and the second forward rotor assembly being positioned on the leading side of the frame ; a first aft rotor assembly connected to the left end portion of the frame ; a second aft rotor assembly connected to the right end portion of the frame , the first aft rotor assembly and the second aft rotor assembly being positioned on the aft side of the frame ; a first aft boom connecting the first aft rotor assembly to the left end portion of the frame ; a second aft boom connecting the second aft rotor assembly to the right end portion of the frame ; a compartment connected to the frame , the compartment comprising a leading side ; a curved leading-edge fairing disposed on the frame , wherein a portion of the curved leading-edge fairing extends to cover the leading side of the compartment , and wherein the curved leading-edge fairing reduces drag during flight in a forward direction to enable a substantially level flight profile; a pair of outboard rotor assemblies disposed on a pair of outboard booms ; and a pair of forward boom fairings disposed on the pair of outboard booms .
A system for facilitating display of cardiac information based on sensed electrical signals, the system comprising: a processing unit configured to: receive a set of electrical signals; receive an indication of a measurement location corresponding to each electrical signal of the set of electrical signals; generate an activation waveform corresponding to the set of electrical signals, wherein the activation waveform comprises a plurality of activation waveform values based on each electrical signal of the set of electrical signals, each activation waveform value representing a probability that a deviation of the electrical signal from a baseline value represents an activation of tissue at the corresponding measurement location; generate, based on the activation waveform, a representation of a cardiac electrical signal feature; and facilitate presentation, on a display device , of a cardiac map and the representation of the cardiac electrical signal feature, wherein the cardiac map is an activation map and the cardiac electrical signal feature is a representation of a time duration since an activation was detected at a measurement location of the cardiac map. receive a set of electrical signals; receive an indication of a measurement location corresponding to each electrical signal of the set of electrical signals; generate an activation waveform corresponding to the set of electrical signals, wherein the activation waveform comprises a plurality of activation waveform values based on each electrical signal of the set of electrical signals, each activation waveform value representing a probability that a deviation of the electrical signal from a baseline value represents an activation of tissue at the corresponding measurement location; generate, based on the activation waveform, a representation of a cardiac electrical signal feature; and facilitate presentation, on a display device , of a cardiac map and the representation of the cardiac electrical signal feature, wherein the cardiac map is an activation map and the cardiac electrical signal feature is a representation of a time duration since an activation was detected at a measurement location of the cardiac map.