mhurhangee/ep-ind-claims huggingface dataset:
A mounting apparatus (100, 200), comprising: a body portion (102, 202) configured to be at least partially positioned between a first airfoil and a second airfoil of a turbine system; an adjustable, first retention component (108, 208) formed on a first side (104, 204) of the body portion (102, 202), the adjustable, first retention component (108, 208) configured to contact a portion of a suction side of the first airfoil of the turbine system; and a second retention component (120, 220) formed on a second side (106, 206) of the body portion (102, 202), opposite the first side (104, 204), the second retention component (120, 220) configured to contact a portion of a pressure side of the second airfoil of the turbine system, characterized in that the adjustable, first retention component includes a first inflatable pouch positioned on the first side of the body portion, the first inflatable pouch configured to contact and substantially contour to the portion of the suction side of the first airfoil in an inflated state of the first inflatable pouch and to contact and be oriented substantially planar with the first side of the body portion in a deflated state of the first inflatable pouch, and in that the second retention component includes a curved portion formed integral with the second side of the body portion, the curved portion configured to contact the portion of the pressure side of the second airfoil of the turbine system in the inflated state and the deflated state of the first inflatable pouch. a body portion (102, 202) configured to be at least partially positioned between a first airfoil and a second airfoil of a turbine system; an adjustable, first retention component (108, 208) formed on a first side (104, 204) of the body portion (102, 202), the adjustable, first retention component (108, 208) configured to contact a portion of a suction side of the first airfoil of the turbine system; and a second retention component (120, 220) formed on a second side (106, 206) of the body portion (102, 202), opposite the first side (104, 204), the second retention component (120, 220) configured to contact a portion of a pressure side of the second airfoil of the turbine system, characterized in that the adjustable, first retention component includes a first inflatable pouch positioned on the first side of the body portion, the first inflatable pouch configured to contact and substantially contour to the portion of the suction side of the first airfoil in an inflated state of the first inflatable pouch and to contact and be oriented substantially planar with the first side of the body portion in a deflated state of the first inflatable pouch, and in that the second retention component includes a curved portion formed integral with the second side of the body portion, the curved portion configured to contact the portion of the pressure side of the second airfoil of the turbine system in the inflated state and the deflated state of the first inflatable pouch.
A superplastic-forming aluminum alloy plate comprising an aluminum alloy containing 2.0 to 6.0 mass% Mg, 0.5 to 1.8 mass% Mn, 0.40 mass% Cr or less and a balance of Al and unavoidable impurities, wherein the unavoidable impurities are restricted to have 0.20 mass% Fe or less, 0.20 mass% Si or less, 0.10 mass% Ti or less and at least one selected from 0.05 mass% Cu or less and 0.05 mass% Zn or less, the 0.2% proof stress is 340 MPa or more and the density of intermetallic compounds having an equivalent circle diameter of 5 to 15 μm at the RD-TD plane which extends along the center of the plate cross-section is 50 to 400 pieces/mm 2. wherein the unavoidable impurities are restricted to have 0.20 mass% Fe or less, 0.20 mass% Si or less, 0.10 mass% Ti or less and at least one selected from 0.05 mass% Cu or less and 0.05 mass% Zn or less, the 0.2% proof stress is 340 MPa or more and the density of intermetallic compounds having an equivalent circle diameter of 5 to 15 μm at the RD-TD plane which extends along the center of the plate cross-section is 50 to 400 pieces/mm 2.
A human monoclonal antibody or antigen binding fragment thereof capable of recognizing and binding to an epitope in the HA2 subunit of the influenza haemagglutinin protein, characterized in that said antibody or antigen-binding fragment has neutralizing activity against an influenza virus comprising HA of the H5 subtype and wherein said antibody or antigen-binding fragment has neutralizing activity against an influenza virus comprising HA of the H1 subtype, wherein the antibody or antigen-binding fragment comprises a heavy chain CDR1 region of SEQ ID NO:1, a heavy chain CDR2 region of SEQ ID NO:2, and a heavy chain CDR3 region of SEQ ID NO:3 and wherein the antibody or antigen-binding fragment thereof comprises a light chain CDR1 of SEQ ID NO: 4, a light chain CDR2 of SEQ ID NO: 5 and a light chain CDR3 of SEQ ID NO: 6; or a light chain CDR1 of SEQ ID NO: 7, a light chain CDR2 of SEQ ID NO: 8, and a light chain CDR3 of SEQ ID NO: 9; or a light chain CDR1 of SEQ ID NO: 10, a light chain CDR2 of SEQ ID NO: 11, and a light chain CDR3 of SEQ ID NO: 12; or a light chain CDR1 of SEQ ID NO: 13, a light chain CDR2 of SEQ ID NO: 14, and a light chain CDR3 of SEQ ID NO: 15; or a light chain CDR1 of SEQ ID NO: 33, a light chain CDR2 of SEQ ID NO: 34, and a light chain CDR3 of SEQ ID NO: 35; or a light chain CDR1 of SEQ ID NO: 36, a light chain CDR2 of SEQ ID NO: 37, and a light chain CDR3 of SEQ ID NO: 38.
A flow heater apparatus for heating liquid as it flows therethrough comprising: a liquid source; a conduit (4, 5) for conveying liquid from the liquid source towards an outlet, said conduit comprising sequentially at least a first zone and a second zone; heating means for heating liquid in said conduit; and control means for controlling the rate of flow of fluid through said conduit, said control means being in data communication with a first temperature sensor responsive to a temperature of the liquid in the conduit at a point between said first and second zones, a second temperature sensor responsive to a temperature of the liquid upstream of said first temperature sensor, characterized in that the flow heater apparatus comprises a third temperature sensor responsive to a temperature of the liquid downstream of said first temperature sensor.
Antenna equipment comprising: • an antenna comprising a feed point, • a board on which the antenna is disposed, wherein the board is a printed circuit board, • a first surface area of the board that is not covered by a metal layer, • a further surface area of the board in a corner of the board, wherein the further surface area is not covered by the metal layer and within the further surface area the antenna including the antenna feed point is disposed, • wherein a first edge of the board is a longer edge of the board among two edges of the board that are close to the antenna, wherein a first current maximum point at which a first current maximum is present is a point at an intersection on the first edge between the first edge and an edge of the further surface area when the antenna is operated at its operating wavelength λ, wherein a point that is on the first edge and whose distance to the first current maximum point on the first edge is λ/4, is a first point, wherein the first current maximum is a current maximum that is on the first edge and that is closest to the feed point of the antenna, and the first surface area that is not covered by the metal layer comprises the first point, and a maximum distance from an edge of the first surface area to the first edge of the board is λ/4. • an antenna comprising a feed point, • a board on which the antenna is disposed, wherein the board is a printed circuit board, • a first surface area of the board that is not covered by a metal layer, • a further surface area of the board in a corner of the board, wherein the further surface area is not covered by the metal layer and within the further surface area the antenna including the antenna feed point is disposed, • wherein a first edge of the board is a longer edge of the board among two edges of the board that are close to the antenna, wherein a first current maximum point at which a first current maximum is present is a point at an intersection on the first edge between the first edge and an edge of the further surface area when the antenna is operated at its operating wavelength λ, wherein a point that is on the first edge and whose distance to the first current maximum point on the first edge is λ/4, is a first point, wherein the first current maximum is a current maximum that is on the first edge and that is closest to the feed point of the antenna, and the first surface area that is not covered by the metal layer comprises the first point, and a maximum distance from an edge of the first surface area to the first edge of the board is λ/4.
A breathing apparatus for providing a respiratory gas to a crewmember in a cabin of an aircraft, said breathing apparatus comprising: - - an air inlet for admission of ambient air in said breathing apparatus, - - an additional gas inlet for admission of additional gas in said breathing apparatus, - - mixing means for mixing the ambient air with the additional gas, - - an outlet nozzle for feeding said crew member with the respiratory gas comprising said ambient air and/or additional gas, and wherein said breathing apparatus further comprises neutralizing means (70, 141) for neutralizing the admission of said additional gas below a predefined cabin altitude (Z 1), the neutralizing means comprising: • an air circuit (52, 62) for feeding said mixing means with ambient air, • a sealing element (70, 141) movable between a first position wherein the pressure loss of the air circuit (52, 62) is minimal and a second position wherein the pressure loss of said air circuit (52, 62) is increased, said sealing element (70, 141) being in its first position when the cabin altitude is below the predefined cabin altitude (Z 1), and said sealing element (70, 141) being in its second position when the cabin altitude is above said predefined altitude (Z 1), characterized in that the neutralizing means further comprises non return means to maintain the sealing element in its second position. - - an air inlet for admission of ambient air in said breathing apparatus, - - an additional gas inlet for admission of additional gas in said breathing apparatus, - - mixing means for mixing the ambient air with the additional gas, - - an outlet nozzle for feeding said crew member with the respiratory gas comprising said ambient air and/or additional gas, and • an air circuit (52, 62) for feeding said mixing means with ambient air, • a sealing element (70, 141) movable between a first position wherein the pressure loss of the air circuit (52, 62) is minimal and a second position wherein the pressure loss of said air circuit (52, 62) is increased, said sealing element (70, 141) being in its first position when the cabin altitude is below the predefined cabin altitude (Z 1), and said sealing element (70, 141) being in its second position when the cabin altitude is above said predefined altitude (Z 1),
A spark plug (5; 5'), comprising: a connector (10; 100); a center electrode connected to the connector (5; 5'); an insulator (15; 115) surrounding the center electrode; a shell (20; 120) surrounding a lower part of the insulator (15; 115), the shell (20; 120) being provided with a tool engaging portion (25; 125), a seal face (30; 130) configured to contact a corresponding seal of a cylinder head of an internal combustion engine, a cylinder engaging threaded portion (40; 140) having a thread diameter configured to screw the spark plug (5; 5') in a threaded bore of the cylinder head, and an intermediate portion (35; 135) extending between the shoulder (30; 130) and the cylinder engaging threaded portion (40; 140), wherein the intermediate portion (35; 135) has a length (L 1) and a constant outer diameter (d 1) over substantially the entire length (L 1), wherein the outer diameter (d 1) is equal to or smaller than the external diameter of the cylinder engaging threaded portion (40; 140) and at least one ground electrode disposed at an end of the cylinder engaging threaded portion (40, 140), characterized in that: 0.20 <= L 1 /D <= 0.80 and L 1 is the length and D is the thread diameter. a connector (10; 100); a center electrode connected to the connector (5; 5'); an insulator (15; 115) surrounding the center electrode; a shell (20; 120) surrounding a lower part of the insulator (15; 115), the shell (20; 120) being provided with a tool engaging portion (25; 125), a seal face (30; 130) configured to contact a corresponding seal of a cylinder head of an internal combustion engine, a cylinder engaging threaded portion (40; 140) having a thread diameter configured to screw the spark plug (5; 5') in a threaded bore of the cylinder head, and an intermediate portion (35; 135) extending between the shoulder (30; 130) and the cylinder engaging threaded portion (40; 140), wherein the intermediate portion (35; 135) has a length (L 1) and a constant outer diameter (d 1) over substantially the entire length (L 1), wherein the outer diameter (d 1) is equal to or smaller than the external diameter of the cylinder engaging threaded portion (40; 140) and at least one ground electrode disposed at an end of the cylinder engaging threaded portion (40, 140), characterized in that: 0.20 <= L 1 /D <= 0.80 and L 1 is the length and D is the thread diameter. 0.20 <= L 1 /D <= 0.80 and L 1 is the length and D is the thread diameter.
A bore cutting tool comprising a tool substrate; and a tool coating on a surface of the tool substrate, wherein the bore cutting tool comprises a plurality of pits in the surface of the tool substrate, characterized in that the tool coating follows the contour of each of the plurality of pits. a tool substrate; and a tool coating on a surface of the tool substrate, wherein the bore cutting tool comprises a plurality of pits in the surface of the tool substrate,
A method of identifying photoreceptor cells in a population of human cells, comprising the steps of: a) determining whether or not cells in the population express CD29 or CD49 on the cell surface; b) determining whether or not cells in the population express CD73 on the cell surface; and c) identifying a cell as a photoreceptor cell if it is CD29 or CD49 negative and CD73 positive. a) determining whether or not cells in the population express CD29 or CD49 on the cell surface; b) determining whether or not cells in the population express CD73 on the cell surface; and c) identifying a cell as a photoreceptor cell if it is CD29 or CD49 negative and CD73 positive.
A block type organopolysiloxane represented by the following average composition formula, wherein each R 1 independently represents a monovalent hydrocarbon group having 1 to 12 carbons; R 2 represents any of a hydrogen atom, a monovalent hydrocarbon group having 1 to 15 carbons, and a monovalent acyl group having 2 to 7 carbons; R 3 represents a hydrogen atom or a monovalent hydrocarbon group having 1 to 4 carbons; X represents a divalent hydrocarbon group having 2 to 15 carbons; "n" represents an integer of 1 or more; "m" represents an integer of 1 or more; "s" represents an integer of 1 to 100; "t" represents an integer of 0 to 50; "z" represents an integer of 0 to 50; and each R 4 independently represents a hydrogen atom, a hydroxyl group, an alkoxy group, or an organic group represented by the following general formula, wherein R 2 represents any of a hydrogen atom, a monovalent hydrocarbon group having 1 to 15 carbons, and a monovalent acyl group having 2 to 7 carbons; R 3 represents a hydrogen atom or a monovalent hydrocarbon group having 1 to 4 carbons; X represents a divalent hydrocarbon group having 2 to 15 carbons; "s" represents an integer of 0 to 100; "t" represents an integer of 0 to 50; "z" represents an integer of 0 to 50; Y represents a hydrogen atom, or a monovalent hydrocarbon group having 2 to 15 carbons having a carbon-carbon double bond.
An unmanned aerial vehicle, comprising: a fuselage; wings, which are symmetrically arranged on two sides of the fuselage along the central axis of the fuselage; linear reinforcements, the linear reinforcements parallel to the central axis of the fuselage are arranged on two sides of the fuselage; a landing gear, connected to the fuselage; two vertical fins, one vertical fin is arranged at the end of each linear reinforcement of the unmanned aerial vehicle; a water collection and emission equipment, comprising a sealed cabin connected to the fuselage; the water collection and emission equipment further comprises buoyancy units (311, 312, 313) connected to the fuselage; the water collection and emission equipment further comprises a water pump arranged in the sealed cabin; the water collection and emission equipment further comprises a water collection and emission pipe connected with the water pump; a side wall of the sealed cabin in its length direction comprises at least one concave part, which is used for slowing down the swaying of the water. a fuselage; wings, which are symmetrically arranged on two sides of the fuselage along the central axis of the fuselage; linear reinforcements, the linear reinforcements parallel to the central axis of the fuselage are arranged on two sides of the fuselage; a landing gear, connected to the fuselage; two vertical fins, one vertical fin is arranged at the end of each linear reinforcement of the unmanned aerial vehicle; a water collection and emission equipment, comprising a sealed cabin connected to the fuselage; the water collection and emission equipment further comprises buoyancy units (311, 312, 313) connected to the fuselage; the water collection and emission equipment further comprises a water pump arranged in the sealed cabin; the water collection and emission equipment further comprises a water collection and emission pipe connected with the water pump; a side wall of the sealed cabin in its length direction comprises at least one concave part, which is used for slowing down the swaying of the water.
An RFID device comprising: a case including a rotation mechanism (21313, 2132); an antenna disposed in the case; and a cylindrical power receiving coil disposed in the case away from the antenna and extending in an axial direction of the rotation mechanism (21313, 2132), and connected to a power receiver configured to charge a battery; wherein the case includes a third housing having a shaft portion as the rotation mechanism and a first housing having a tubular shape disposed coaxially with the shaft portion, the antenna and the cylindrical power receiving coil being disposed in the first housing. a case including a rotation mechanism (21313, 2132); an antenna disposed in the case; and a cylindrical power receiving coil disposed in the case away from the antenna and extending in an axial direction of the rotation mechanism (21313, 2132), and connected to a power receiver configured to charge a battery; wherein the case includes a third housing having a shaft portion as the rotation mechanism and a first housing having a tubular shape disposed coaxially with the shaft portion, the antenna and the cylindrical power receiving coil being disposed in the first housing.
Substrate for generating surface plasmons (SPs) and surface plasmon polaritons (SPPs) by means of an excitation radiation of a determined wavelength, comprising a carrier layer which is transparent to the excitation radiation and which has a surface structure on a surface of the carrier layer, and a metal coating of gold or silver on the surface structure, the coating being reflective for the excitation radiation and suitable for propagating SPPs excited by the excitation radiation, characterized in that - the surface structure comprises a plurality of spaced apart prolate recesses of identical size, each recess having a length in a longitudinal direction selected from a range between 100 nm to 2500 nm, a width in a transverse direction directed orthogonal to the longitudinal direction, and a depth, - the recesses are arranged in rows and columns of a two-dimensional array, wherein longitudinal directions of the prolate recesses are parallel to one another and a direction of the rows, and the columns run at an angle α to the rows, - the array has a first periodicity (P H) of the surface structure in the direction of the rows and a second periodicity (P V) of the surface structure orthogonal to the direction of the rows, and - the length of the recess is an integer multiple of the wavelength of a surface plasmon polariton brought about by an excitation radiation of a determined wavelength so that standing Bloch waves (BSPPs) are generated in the recesses. - the surface structure comprises a plurality of spaced apart prolate recesses of identical size, each recess having a length in a longitudinal direction selected from a range between 100 nm to 2500 nm, a width in a transverse direction directed orthogonal to the longitudinal direction, and a depth, - the recesses are arranged in rows and columns of a two-dimensional array, wherein longitudinal directions of the prolate recesses are parallel to one another and a direction of the rows, and the columns run at an angle α to the rows, - the array has a first periodicity (P H) of the surface structure in the direction of the rows and a second periodicity (P V) of the surface structure orthogonal to the direction of the rows, and - the length of the recess is an integer multiple of the wavelength of a surface plasmon polariton brought about by an excitation radiation of a determined wavelength so that standing Bloch waves (BSPPs) are generated in the recesses.
A method for wireless communications by a user equipment, UE, comprising: determining a quasi-co-location, QCL, relationship of an aperiodic channel state information, CSI, reference signal, CSI-RS, to a physical channel to use for processing the aperiodic CSI-RS; and processing the aperiodic CSI-RS according to the determined QCL relationship; characterized by, wherein if an offset between a downlink control channel, received by the UE, conveying a downlink control information, DCI, scheduling the aperiodic CSI-RS and the aperiodic CSI-RS is not yet determined or is less than a threshold, then further determining to use a previous explicit QCL relationship indicated in an earlier grant of time and frequency resources of another transmission. determining a quasi-co-location, QCL, relationship of an aperiodic channel state information, CSI, reference signal, CSI-RS, to a physical channel to use for processing the aperiodic CSI-RS; and processing the aperiodic CSI-RS according to the determined QCL relationship; characterized by, wherein if an offset between a downlink control channel, received by the UE, conveying a downlink control information, DCI, scheduling the aperiodic CSI-RS and the aperiodic CSI-RS is not yet determined or is less than a threshold, then further determining to use a previous explicit QCL relationship indicated in an earlier grant of time and frequency resources of another transmission.