mhurhangee/ep-ind-claims huggingface dataset:
A light-receiving device comprising at least one pixel, the at least one pixel including: a first electrode; a second electrode; and a photoelectric conversion layer between the first electrode and the second electrode, the photoelectric conversion layer configured to convert incident infrared light into electric charge, the photoelectric conversion layer having a first section and a second section, the first section being closer to the first electrode than the second section, the second section being closer to the second electrode than the first section, at least one of the first section and the second section having a plurality of inclined surfaces that guide incident light toward a central axis of the photoelectric conversion layer, characterized by further comprising: a first-conductivity-type layer between the photoelectric conversion layer and the first electrode, and in contact with the photoelectric conversion layer along the first section of the photoelectric conversion layer; and a second-conductivity-type layer between the photoelectric conversion layer and the second electrode, and in contact with the photoelectric conversion layer along the second section of the photoelectric conversion layer, wherein the first-conductivity-type layer and the second-conductivity-type layer each include a material that has a refractive index smaller than a refractive index of a material included in the photoelectric conversion layer. a first electrode; a second electrode; and a photoelectric conversion layer between the first electrode and the second electrode, the photoelectric conversion layer configured to convert incident infrared light into electric charge, the photoelectric conversion layer having a first section and a second section, the first section being closer to the first electrode than the second section, the second section being closer to the second electrode than the first section, at least one of the first section and the second section having a plurality of inclined surfaces that guide incident light toward a central axis of the photoelectric conversion layer, characterized by further comprising: a first-conductivity-type layer between the photoelectric conversion layer and the first electrode, and in contact with the photoelectric conversion layer along the first section of the photoelectric conversion layer; and a second-conductivity-type layer between the photoelectric conversion layer and the second electrode, and in contact with the photoelectric conversion layer along the second section of the photoelectric conversion layer, a first-conductivity-type layer between the photoelectric conversion layer and the first electrode, and in contact with the photoelectric conversion layer along the first section of the photoelectric conversion layer; and a second-conductivity-type layer between the photoelectric conversion layer and the second electrode, and in contact with the photoelectric conversion layer along the second section of the photoelectric conversion layer,
A rectally insertable drug delivery device for localized drug delivery to the anal sphincter of a subject, comprising: a shell sized for rectal insertion and which contains an active pharmaceutical ingredient, said shell being impermeable to said active pharmaceutical ingredient, wherein a lower portion of said shell is configured with an aperture of a size which enables release of said active pharmaceutical ingredient from said shell through said aperture, said ingredient being suitable for treating the anal canal; wherein said shell is configured to be collapsible as said active pharmaceutical ingredient is released, wherein said active pharmaceutical ingredient forms a part of a pharmaceutical composition, said pharmaceutical composition further comprising a pharmaceutically acceptable carrier, which is a liquid at room temperature, wherein the lower portion of the shell comprises a wick having an upper end in contact with the carrier and a lower end which protrudes from the lower portion of the shell.
A sheath for use with a medical device, comprising: an inner liner defining a lumen extending longitudinally through the sheath; a coil having a series of windings with an outer surface and inner surface, the coil having a predetermined coil spacing between adjacent coil windings to define voids between adjacent windings, the coil fitted around at least a part of the inner liner; an intermediate layer disposed between the inner surface of the coil windings and a portion of the inner liner and adapted to bond to the inner surface of the coil and to the inner liner; and an outer layer positioned over and attached to the outer surface of the coil, the outer layer having a lower melt temperature than the inner liner, wherein the inner liner and the outer layer are adhered to the coil independent from one another so that in response to the bending of said sheath the inner liner and the outer layer are capable of moving coaxially independent relative to one another; the sheath further comprising a filler material disposed within at least a portion of said voids between adjacent windings of the coil, the filler material having a dimension sized to bridge said voids to inhibit portions of the outer layer from bonding to the inner liner, the filler material having a higher melt temperature than the outer layer. an inner liner defining a lumen extending longitudinally through the sheath; a coil having a series of windings with an outer surface and inner surface, the coil having a predetermined coil spacing between adjacent coil windings to define voids between adjacent windings, the coil fitted around at least a part of the inner liner; an intermediate layer disposed between the inner surface of the coil windings and a portion of the inner liner and adapted to bond to the inner surface of the coil and to the inner liner; and an outer layer positioned over and attached to the outer surface of the coil, the outer layer having a lower melt temperature than the inner liner, wherein the inner liner and the outer layer are adhered to the coil independent from one another so that in response to the bending of said sheath the inner liner and the outer layer are capable of moving coaxially independent relative to one another; the sheath further comprising a filler material disposed within at least a portion of said voids between adjacent windings of the coil, the filler material having a dimension sized to bridge said voids to inhibit portions of the outer layer from bonding to the inner liner, the filler material having a higher melt temperature than the outer layer.
Modular platform for receiving vehicle components, comprising fastening means for fastening the platform on or to a vehicle, characterized in that at least two of the fastening means are designed as quick-locking devices, that the quick-locking device comprises a hook and a pawl and the hook comprises a U-shaped inner area, that the hook of the quick-locking device is shaped in such a way that it can receive a cylindrical body, for example a retaining bolt, in the inner area, that the quick-locking device comprises a clamping element which can transfer the pawl at least partially into the inner area of the hook by means of a force, and that the quick-locking device is arranged in such a way that, when the modular platform is mounted by means of the fastening means, the force of the pawl can be overcome by means of the gravitational force of the platform when the cylindrical bodies are moved into the inner area of the quick-locking device, and thus the pawl can be moved out of the inner area of the hook. comprising fastening means for fastening the platform on or to a vehicle, characterized in that at least two of the fastening means are designed as quick-locking devices, that the quick-locking device comprises a hook and a pawl and the hook comprises a U-shaped inner area, that the hook of the quick-locking device is shaped in such a way that it can receive a cylindrical body, for example a retaining bolt, in the inner area, that the quick-locking device comprises a clamping element which can transfer the pawl at least partially into the inner area of the hook by means of a force, and that the quick-locking device is arranged in such a way that, when the modular platform is mounted by means of the fastening means, the force of the pawl can be overcome by means of the gravitational force of the platform when the cylindrical bodies are moved into the inner area of the quick-locking device, and thus the pawl can be moved out of the inner area of the hook.
Electronically commutated electric motor with a stator, a rotor rotatably mounted relative to said stator, and at least one sensor for scanning a magnetic field that co-rotates with said rotor, where said stator comprises a stator winding and a magnetically soft stator core, where said rotor comprises several permanent magnets arranged distributed in the circumferential direction of said rotor as well as a first magnetically soft rotor core for said permanent magnets, and where said permanent magnets, together with said first magnetically soft rotor core, generate a rotor magnetic field which, for operating said electric motor, interacts with the stator magnetic field of said stator generated by said stator winding and said stator core, wherein said rotor further comprises a second magnetically soft rotor core which adjoins said first magnetically soft rotor core in the axial direction of said rotor, where a non-magnetic separator element is arranged in the axial direction between said first magnetically soft rotor core and said second magnetically soft rotor core, where said permanent magnets extend in the axial direction over said first magnetically soft rotor core, said non-magnetic separator element and said second magnetically soft rotor core, and where the magnetic field scanned by said sensor is a control magnetic field generated by said permanent magnets together with said second magnetically soft rotor core, characterized in that the thickness of the non-magnetic separator element measured in the axial direction is at least 10% of the outer diameter of the rotor, wherein said at least one sensor for scanning the control magnetic field is a Hall sensor, and wherein said Hall sensor is arranged on a side of a printed circuit board facing said second magnetically soft rotor core in the axial direction.
A gas turbine engine, comprising: a power turbine mechanically coupled with a load; and one or more processors configured to: determine a first fuel flow demand ( Ẇ f 1) based at least in part on a power demand rate ( dP dt) associated with the load; determine a second fuel flow demand ( Ẇ f 2) based at least in part on a power turbine speed error ( N p Error) associated with the power turbine and a power turbine speed error rate ( dNpError dt) derived from the power turbine speed error ( N p Error); determine a third fuel flow demand ( Ẇ f 3) based at least in part on the power turbine speed error ( N p Error); determine a composite fuel flow demand ( Ẇ f) based at least in part on the first fuel flow demand ( Ẇ f 1), the second fuel flow demand ( Ẇ f 2), and the third fuel flow demand ( Ẇ f 3); and control a fuel flow to the gas turbine engine based at least in part on the composite fuel flow demand ( Ẇ f). a power turbine mechanically coupled with a load; and one or more processors configured to: determine a first fuel flow demand ( Ẇ f 1) based at least in part on a power demand rate ( dP dt) associated with the load; determine a second fuel flow demand ( Ẇ f 2) based at least in part on a power turbine speed error ( N p Error) associated with the power turbine and a power turbine speed error rate ( dNpError dt) derived from the power turbine speed error ( N p Error); determine a third fuel flow demand ( Ẇ f 3) based at least in part on the power turbine speed error ( N p Error); determine a composite fuel flow demand ( Ẇ f) based at least in part on the first fuel flow demand ( Ẇ f 1), the second fuel flow demand ( Ẇ f 2), and the third fuel flow demand ( Ẇ f 3); and control a fuel flow to the gas turbine engine based at least in part on the composite fuel flow demand ( Ẇ f). determine a first fuel flow demand ( Ẇ f 1) based at least in part on a power demand rate ( dP dt) associated with the load; determine a second fuel flow demand ( Ẇ f 2) based at least in part on a power turbine speed error ( N p Error) associated with the power turbine and a power turbine speed error rate ( dNpError dt) derived from the power turbine speed error ( N p Error); determine a third fuel flow demand ( Ẇ f 3) based at least in part on the power turbine speed error ( N p Error); determine a composite fuel flow demand ( Ẇ f) based at least in part on the first fuel flow demand ( Ẇ f 1), the second fuel flow demand ( Ẇ f 2), and the third fuel flow demand ( Ẇ f 3); and control a fuel flow to the gas turbine engine based at least in part on the composite fuel flow demand ( Ẇ f).
A method for separating up-going and down-going wave fields (U, D) in seismic data related to a subsurface of a body of water, or to a subsurface of a body of rock, the method comprising: receiving seismic data (P o, Z o) recorded in the time-space domain with seismic recorders distributed on a first datum, wherein the first datum is non-flat; establishing a mathematical relation expressing transformed seismic data (P, Z) as a function of the up-going and down-going wave fields (U, D) on a second planar datum; and solving with an inversion procedure, run on a processor, the mathematical relation to obtain the up-going and down-going wave fields (U, D) for the second datum expressed as a function of transformed seismic data (P, Z), wherein the second datum is different from the first datum. receiving seismic data (P o, Z o) recorded in the time-space domain with seismic recorders distributed on a first datum, wherein the first datum is non-flat; establishing a mathematical relation expressing transformed seismic data (P, Z) as a function of the up-going and down-going wave fields (U, D) on a second planar datum; and solving with an inversion procedure, run on a processor, the mathematical relation to obtain the up-going and down-going wave fields (U, D) for the second datum expressed as a function of transformed seismic data (P, Z), wherein the second datum is different from the first datum.
A photosensitive resin composition suitable for forming a solid-state imaging device, the composition comprising: a resin; an oxime photopolymerization initiator; a UV-absorbing agent; and a monomer containing one or more hydrogen bonding groups; wherein the monomer is contained in the composition in an amount of 30 mass% or more based on the total solid content of the composition; and wherein the oxime photopolymerization initiator is selected from the following compounds: a resin; an oxime photopolymerization initiator; a UV-absorbing agent; and a monomer containing one or more hydrogen bonding groups; wherein the monomer is contained in the composition in an amount of 30 mass% or more based on the total solid content of the composition; and wherein the oxime photopolymerization initiator is selected from the following compounds:
Method for operating a combined cycle power plant with a gas turbine installation, wherein the gas turbine installation comprises at least one compressor for compressing combustion air, at least one combustion chamber (13, 17) for burning a supplied fuel (14, 15, 18, 19) using the compressed combustion air, and at least one turbine (16, 20) through which flow the hot gases from the at least one combustion chamber (13, 17); wherein both a first carbon-based fuel (14, 18) in the form of natural gas, and a second fuel (15, 19) in the form of a hydrogen-rich fuel or pure hydrogen, are used as a fuel; wherein the first and second fuels (14, 18 or 15, 19) are mixed together and burned together in the at least one combustion chamber (13, 17); wherein the combined cycle power plant comprises a separate water/steam circuit with a waste heat steam generator, a steam turbine, a condenser, a feed water tank and a feed water pump, and the exhaust gases from the gas turbine installation flow through the waste heat steam generator; wherein a gas is obtained from a carbon-containing additive product in a gasification unit, from which gas a hydrogen-rich syngas is produced after cooling and COS hydrolysis in a cooling and hydrolysis unit, separation of acidic gases in an MDEA washing unit, and separation of metal carbonyl in a metal carbonyl removal unit; wherein the hydrogen is extracted from part of the syngas in a membrane separating unit, supplied as a crude hydrogen to a PSA cleaning unit and there refined into pure hydrogen, and a residual gas occurring from membrane separation and PSA cleaning is processed in the combined cycle power plant; wherein the hydrogen-rich syngas or the pure hydrogen is supplied to the gas turbine installation as a second fuel (15, 19); and wherein the combustion chamber or chambers (13, 17) is/are equipped with premix burners and in the flow direction, firstly the first fuel (14, 18) and further downstream the second fuel (15, 19) are injected; wherein the premix burner comprises a premix device in the form of a double cone and a subsequent mixing pipe, and the first fuel (14, 18) is injected in the premix device and the second fuel (15, 19) in the mixing pipe; and wherein air from the outside flows into the premix device between the conical shells, into which the first fuel (14, 18) is injected perpendicularly to the cone casing via several nozzle openings.
A method of manufacturing a razor head component comprising: a) providing a strip of material elongated along a first direction, the strip having first and second edges (47, 46) parallel with said first direction, having a first portion comprising said first edge, a second portion comprising said second edge, and an intermediate portion intermediate said first and second portions, b) bending the intermediate portion of a part of said strip about a bending axis parallel to the first direction, c) fixing a razor blade onto the second portion of said part, and further comprising moving the strip along a process path, and repeating at least steps b) and c) for different parts of said strip. a) providing a strip of material elongated along a first direction, the strip having first and second edges (47, 46) parallel with said first direction, having a first portion comprising said first edge, a second portion comprising said second edge, and an intermediate portion intermediate said first and second portions, b) bending the intermediate portion of a part of said strip about a bending axis parallel to the first direction, c) fixing a razor blade onto the second portion of said part, and further comprising moving the strip along a process path, and repeating at least steps b) and c) for different parts of said strip.
A three-flute drill comprising: three chip discharge flutes axially disposed to open in a tip portion; and three cutting edges each formed at an intersecting portion between an inner wall surface of each of the chip discharge flutes facing in a drill rotation direction during hole drilling and a tip flank formed on the tip portion, the cutting edge having a concavely-curved cutting edge portion in a concavely-curved shape formed on an inner circumferential side and a convexly-curved cutting edge portion in a convexly-curved shape formed on an outer circumferential side, wherein an axially perpendicular cross-sectional view orthogonal to an axial center O has a first convex curve corresponding to the convexly-curved cutting edge portion and a first concave curve corresponding to the concavely-curved cutting edge portion intersecting with each other at an intersection A, wherein, in the axially perpendicular cross-sectional view, an inner wall surface of the chip discharge flute facing opposite to the drill rotation direction during hole drilling is made up of a second concave curve formed on the inner circumferential side and a second convex curve formed continuously from the second concave curve on the outer circumferential side, and wherein the second convex curve reaches a heel, and characterised in that the three-flute drill has the first convex curve with a curvature radius of R1, the first concave curve with a curvature radius of R2, the second concave curve with a curvature radius of R3, and the second convex curve with a curvature radius of R4 in the axially perpendicular cross-sectional view, the curvature radii R1 to R4 being within ranges of the following equations to, respectively, in terms of the drill cutting diameter D: R 1: 0.02 D to 0.4 D R 2: 0.10 D to 0.45 D R 3: 0.10 D to 0.45 D and R 4: 0.3 D to 1.2 D
A glove, inner glove, sock, knee sock or bra with ballistic protection, wherein the glove, the inner glove, the sock, the knee sock or the bra has at least one knitted fabric, wherein at least one first zone of the knitted fabric is formed from a yarn which inhibits the penetration of fragments and the glove, the inner glove, the sock, the knee sock or the bra which has a plurality of differently protected zones (1,3), characterized in that at least two different zones (1,3) of the glove, the inner glove, the sock, the knee sock or the bra are connected seamlessly to one another.
A method, comprising: analysing first and second images to determine an overlapping capture region for a first image portion and a second image portion, wherein analyzing comprises comparing the first and second images to determine content that is present in both of the images, the first image being captured by a first image sensor portion of an apparatus and the second image being captured by a second image sensor portion of the apparatus; retrieving from a memory any one of multiple different positions on the first and second images, each of the multiple different positions being associated with different environmental characteristics and/or different operational modes, the retrieved position being indicative of an expected overlapping capture region for the first image sensor portion and the second image sensor portion, and being a position at which the analysis of the first and second images is initiated; and stitching the first and second images together using the overlapping capture region. analysing first and second images to determine an overlapping capture region for a first image portion and a second image portion, wherein analyzing comprises comparing the first and second images to determine content that is present in both of the images, the first image being captured by a first image sensor portion of an apparatus and the second image being captured by a second image sensor portion of the apparatus; retrieving from a memory any one of multiple different positions on the first and second images, each of the multiple different positions being associated with different environmental characteristics and/or different operational modes, the retrieved position being indicative of an expected overlapping capture region for the first image sensor portion and the second image sensor portion, and being a position at which the analysis of the first and second images is initiated; and stitching the first and second images together using the overlapping capture region.