mhurhangee/ep-ind-claims huggingface dataset:
Rotary encoder comprising a first component group and a second component group, the component groups (1, 2) being arranged such that they can be rotated relative to each other about an axis and - the first component group comprising. a trigger sensor (1.1) - the second component group comprising. a first magnet (2.1, 2.4). a second magnet (2.2, 2.5) and. a third magnet (2.3, 2.6), characterized in that the first component group comprises a plurality of omnipolar sensitive magnetic sensors (1.3, 1.4) which are arranged offset in the circumferential direction with respect to the axis, the trigger sensor (1.1) comprises an impulse wire and a reset magnet (1.2), and the reset magnet (1.2) is oriented such that the latter has a directional component parallel to the longitudinal extent of the impulse wire, wherein the component groups (1, 2) are additionally configured such that, during a relative rotation of the two components (1, 2) by at least one full revolution the magnetic field of the first magnet (2.1, 2.4) and of the third magnet (2.3, 2.6) can be detected by the magnetic sensors (1.3, 1.4), wherein a trigger signal in the form of a voltage pulse from the impulse wire can be generated by the second magnet (2.2, 2.5) and the third magnet (2.3, 2.6), while a generation of the trigger signal from the impulse wire by the first magnet (2.1, 2.4) is stopped. - the first component group comprising. a trigger sensor (1.1). a trigger sensor (1.1) - the second component group comprising. a first magnet (2.1, 2.4). a second magnet (2.2, 2.5) and. a third magnet (2.3, 2.6),. a first magnet (2.1, 2.4). a second magnet (2.2, 2.5) and. a third magnet (2.3, 2.6),
Cover for closing a sealed chamber (2; 22) of a condensing boiler on which at least one exhaust conduit of the combustion fumes produced in said condensing boiler and at least one conduit for the entry of combustion air required for said combustion are intended to fit, said cover - acting as an upper wall of said sealed chamber (2; 22) - comprising setting means (3; 4) for said coupling of: - said at least one exhaust conduit of the combustion fumes, and - said at least one conduit for the entry of combustion air said setting means (3; 4) being integrated and integrally made with said cover characterised in that said setting means (3; 4) comprise: - first setting means for a fume exhaust and combustion air intake conduit of the "coaxial" type, said first setting means comprising, in turn, a coaxial collar integrally made with said cover and comprising a fume exhaust outlet within the annular air intake - second setting means for a combustion fume exhaust and combustion air intake system of a "split system", said second setting means, integrated and integrally made with said cover comprising: - a first coupling for a combustion fume exhaust conduit, said first coupling comprising said fume exhaust outlet of said coaxial collar, - at least a second coupling for a combustion air intake conduit, said second coupling comprising an opening adapted to accommodate the lower end of said combustion air intake conduit, said cover being suitable with both "coaxial system" and "split system" for the discharge of combustion fumes and for the intake of combustion air. - acting as an upper wall of said sealed chamber (2; 22) - comprising setting means (3; 4) for said coupling of: - said at least one exhaust conduit of the combustion fumes, and - said at least one conduit for the entry of combustion air said setting means (3; 4) being integrated and integrally made with said cover - first setting means for a fume exhaust and combustion air intake conduit of the "coaxial" type, said first setting means comprising, in turn, a coaxial collar integrally made with said cover and comprising a fume exhaust outlet within the annular air intake - second setting means for a combustion fume exhaust and combustion air intake system of a "split system", said second setting means, integrated and integrally made with said cover comprising: - a first coupling for a combustion fume exhaust conduit, said first coupling comprising said fume exhaust outlet of said coaxial collar, - at least a second coupling for a combustion air intake conduit, said second coupling comprising an opening adapted to accommodate the lower end of said combustion air intake conduit, - a first coupling for a combustion fume exhaust conduit, said first coupling comprising said fume exhaust outlet of said coaxial collar, - at least a second coupling for a combustion air intake conduit, said second coupling comprising an opening adapted to accommodate the lower end of said combustion air intake conduit,
A virtualisation platform comprising a plurality of integrated independent levels of security components (3a-3f) interconnected via communication channels, wherein each of said components (3a-3f): - is one of an application partition (3a-3c), an input-output partition or an external communication interface (3e-3f), and - has a specified function, wherein the virtualisation platform is built such as to fulfil the properties of strict segregation and non-interference between said functions, characterised in that said virtualization platform further comprises: - integrated interceptor modules (11a-11h) connected to said components (3a-3f) via said communication channels, each interceptor module being interposed in the communication channel connecting two components, and - integrated analysing means connected to said interceptor modules (11a-11h) and comprising control means and testing means, said control means being configured to put each interceptor module in an operational mode selected out of a set of predetermined operational modes including a testing mode, and said testing means being configured to locally test the components connected to the interceptor modules being put in the testing mode. - is one of an application partition (3a-3c), an input-output partition or an external communication interface (3e-3f), and - has a specified function, - integrated interceptor modules (11a-11h) connected to said components (3a-3f) via said communication channels, each interceptor module being interposed in the communication channel connecting two components, and - integrated analysing means connected to said interceptor modules (11a-11h) and comprising control means and testing means, said control means being configured to put each interceptor module in an operational mode selected out of a set of predetermined operational modes including a testing mode, and said testing means being configured to locally test the components connected to the interceptor modules being put in the testing mode.
A system, comprising: a turbine combustor comprising: a first fuel nozzle comprising an outer body; a resonator configured to damp oscillations; and a first air path extending through the resonator into the first fuel nozzle; characterized in that the resonator comprises a resonator chamber disposed between first and second plates (90, 92) extending around the first fuel nozzle, the resonator chamber being partially defined by the first and second plates (90, 92), a portion of the outer body of the first fuel nozzle extending from the first plate to the second plate and a portion of an inner wall, disposed inside a casing wall of the turbine combustor, said portion extending from the first plate to the second plate, the first plate comprising a first plurality of openings therein configured to receive cooling air from first air path, the second plate comprising a second plurality of openings therein and the portion of the outer body of the first fuel nozzle having at least a third plurality of openings therein configured to pass cooling air out of the resonator chamber and into a second air path. a turbine combustor comprising: a first fuel nozzle comprising an outer body; a resonator configured to damp oscillations; and a first air path extending through the resonator into the first fuel nozzle; characterized in that a first fuel nozzle comprising an outer body; a resonator configured to damp oscillations; and a first air path extending through the resonator into the first fuel nozzle; characterized in that the resonator comprises a resonator chamber disposed between first and second plates (90, 92) extending around the first fuel nozzle, the resonator chamber being partially defined by the first and second plates (90, 92), a portion of the outer body of the first fuel nozzle extending from the first plate to the second plate and a portion of an inner wall, disposed inside a casing wall of the turbine combustor, said portion extending from the first plate to the second plate, the first plate comprising a first plurality of openings therein configured to receive cooling air from first air path, the second plate comprising a second plurality of openings therein and the portion of the outer body of the first fuel nozzle having at least a third plurality of openings therein configured to pass cooling air out of the resonator chamber and into a second air path.
An integrated sealed secondary battery comprising: a plurality of cells arranged in a row respectively accommodating electricity-generating elements within rectangular tubular cases having a bottom, with their upper open ends being sealed; first cooling medium passages formed on both sides of the row of the cells wherein a cooling jacket member is joined to both sides and/or both ends of the row of the cells with respect to the direction of the arrangement of the cells; characterised by second cooling medium passages formed between the cases of the cells that communicate with the first cooling medium passages on both sides of the row of the cells; an integral cover for closing upper open ends of the cases of the cells; connecting elements disposed inside of the integral cover for electrically connecting adjacent cells; third cooling medium passages formed above the connecting elements that communicate with the first cooling medium passages; wherein projections are provided projecting on at least one of mutually facing opposite wall surfaces of the cases of the cells, and the second cooling medium passages are formed by abutting these projections on the opposite wall surfaces of the cases of the cells. a plurality of cells arranged in a row respectively accommodating electricity-generating elements within rectangular tubular cases having a bottom, with their upper open ends being sealed; first cooling medium passages formed on both sides of the row of the cells wherein a cooling jacket member is joined to both sides and/or both ends of the row of the cells with respect to the direction of the arrangement of the cells; characterised by second cooling medium passages formed between the cases of the cells that communicate with the first cooling medium passages on both sides of the row of the cells; an integral cover for closing upper open ends of the cases of the cells; connecting elements disposed inside of the integral cover for electrically connecting adjacent cells; third cooling medium passages formed above the connecting elements that communicate with the first cooling medium passages; wherein projections are provided projecting on at least one of mutually facing opposite wall surfaces of the cases of the cells, and the second cooling medium passages are formed by abutting these projections on the opposite wall surfaces of the cases of the cells.
A heat exchanger comprising: an inner tube forming an inner flow path and having an inlet and an outlet; an outer tube radially surrounding at least portion of the inner tube and spaced radially outwardly therefrom to form an annular space; and a thermally conductive spiral element wound around the inner tube and disposed in the space, wherein the spiral element forms, in conjunction with the inner tube and the outer tube, a helical flow path through the space, the helical flow path in fluid communication with an inlet and an outlet of the outer tube, and wherein the outer tube is thermally isolated from the spiral element 170), the heat exchanger being characterized in that the spiral element is a spring held tightly against the outer diameter of the inner tube by its inherent resiliency. an inner tube forming an inner flow path and having an inlet and an outlet; an outer tube radially surrounding at least portion of the inner tube and spaced radially outwardly therefrom to form an annular space; and a thermally conductive spiral element wound around the inner tube and disposed in the space, wherein the spiral element forms, in conjunction with the inner tube and the outer tube, a helical flow path through the space, the helical flow path in fluid communication with an inlet and an outlet of the outer tube, and wherein the outer tube is thermally isolated from the spiral element 170), the heat exchanger being characterized in that the spiral element is a spring held tightly against the outer diameter of the inner tube by its inherent resiliency.
A gear centering device for use in connection with shifting gears of a bicycle transmission system, the gear centering device comprising: a derailleur attach component comprising a first attach point configured to be connected to a moveable derailleur; a main body comprising a second attach point configured to be connected to a fixed portion of a bicycle; and a rotary gear climb in mechanical communication with a first threaded component, wherein rotation of the rotary gear climb imparts rotational motion to the first threaded component, and wherein the rotary gear climb comprises a plurality of peaks and valleys that limit the lateral displacement of a second threaded component to discrete distances, characterized by the second threaded component being a female lead screw having a tube-like structure with female threading extending along the entirety of its interior, the pair of first and second threaded components being configured to translate rotational motion received at the first threaded component into a lateral displacement of the second threaded component, wherein lateral displacement of the second threaded component further translates to lateral movement of the first attach point relative to the second attach point. a derailleur attach component comprising a first attach point configured to be connected to a moveable derailleur; a main body comprising a second attach point configured to be connected to a fixed portion of a bicycle; and a rotary gear climb in mechanical communication with a first threaded component, wherein rotation of the rotary gear climb imparts rotational motion to the first threaded component, and wherein the rotary gear climb comprises a plurality of peaks and valleys that limit the lateral displacement of a second threaded component to discrete distances, characterized by the second threaded component being a female lead screw having a tube-like structure with female threading extending along the entirety of its interior, the pair of first and second threaded components being configured to translate rotational motion received at the first threaded component into a lateral displacement of the second threaded component, wherein lateral displacement of the second threaded component further translates to lateral movement of the first attach point relative to the second attach point.
A wind turbine comprising: - a rotor comprising one or more rotor blades and a hub, the hub being attached to a nacelle; - a yaw system for rotating the nacelle; - a first detector for detecting a component of wind velocity along a line of sight, wherein the line of sight does not pass through the area swept out by the rotor blades during rotation, the detector being mounted on the nacelle such that it rotates under the action of the yaw system; - a control system coupled to the detector and arranged to compare the detected component of wind velocity with a wind velocity value and to control the yaw system in response to the comparison. - a rotor comprising one or more rotor blades and a hub, the hub being attached to a nacelle; - a yaw system for rotating the nacelle; - a first detector for detecting a component of wind velocity along a line of sight, wherein the line of sight does not pass through the area swept out by the rotor blades during rotation, the detector being mounted on the nacelle such that it rotates under the action of the yaw system; - a control system coupled to the detector and arranged to compare the detected component of wind velocity with a wind velocity value and to control the yaw system in response to the comparison.
A posterior dynamic spinal stabilization system comprising: a) a rod having a first end and a second end, b) a mobile anchor having i) a shank (13; 403) and ii) a rod-receiving portion mated to the first end of the rod, wherein the rod-receiving portion can translate along the rod and pivot about the shank, c) a fixed anchor having i) a shank and ii) a rod-receiving portion locked to the second end of the rod, d) a first motion limiting stop positioned on the rod at a location superior to the mobile anchor, and e) a second motion limiting stop positioned on the rod at a location inferior to the mobile anchor, characterised in that at least one of the first and second motion limiting stops is provided by a secondary component which is attachable to the rod to create the stop, so that the stop can be positioned on the rod at a desired distance from the mobile anchor to produce a limited amount of translation of the mobile anchor along the rod. a) a rod having a first end and a second end, b) a mobile anchor having i) a shank (13; 403) and ii) a rod-receiving portion mated to the first end of the rod, wherein the rod-receiving portion can translate along the rod and pivot about the shank, c) a fixed anchor having i) a shank and ii) a rod-receiving portion locked to the second end of the rod, d) a first motion limiting stop positioned on the rod at a location superior to the mobile anchor, and e) a second motion limiting stop positioned on the rod at a location inferior to the mobile anchor,
A method of manufacturing a timber composite, the method comprising the steps of: cutting one or more timber pieces to form a plurality of timber layers applying adhesive to said plurality of timber layers; wherein said adhesive is a thermosetting adhesive; arranging the plurality of timber layers in a stack; applying pressure to the timber layers; and heating the timber layers; characterized in that the adhesive penetrates into the one or more timber layers and cures to form the timber composite, wherein the timber layers are arranged in the stack in their original order and orientation in the timber piece from which they are cut. cutting one or more timber pieces to form a plurality of timber layers applying adhesive to said plurality of timber layers; wherein said adhesive is a thermosetting adhesive; arranging the plurality of timber layers in a stack; applying pressure to the timber layers; and heating the timber layers;
A method of forming an absorbent article, the absorbent article comprising: a stretchable substrate layer; and a shaped absorbent core including a combination of superabsorbent particles and adhesive fibers formed by deposition onto, and adhesively attached to, the substrate layer; the absorbent core comprising about 40-99% by weight superabsorbent particles and about 1-60% by weight meltblown adhesive fibers, the absorbent core having a front end, a rear end, and two lateral sides wherein the lateral sides are uncut, and have a fuzzy or serrated configuration of laterally extending peaks and valleys; the absorbent core further comprising a central region and two end regions, wherein at least one of the end regions is wider than the central region, wherein the method comprises forming and shaping the absorbent core in-line during assembly of the absorbent article, and wherein the absorbent core is shaped by controlling the application of the adhesive meltblown fibers to the substrate layer using a plurality of individually programmable meltblowing nozzles. a stretchable substrate layer; and a shaped absorbent core including a combination of superabsorbent particles and adhesive fibers formed by deposition onto, and adhesively attached to, the substrate layer; the absorbent core comprising about 40-99% by weight superabsorbent particles and about 1-60% by weight meltblown adhesive fibers, the absorbent core having a front end, a rear end, and two lateral sides wherein the lateral sides are uncut, and have a fuzzy or serrated configuration of laterally extending peaks and valleys; the absorbent core further comprising a central region and two end regions, wherein at least one of the end regions is wider than the central region, wherein the method comprises forming and shaping the absorbent core in-line during assembly of the absorbent article, and wherein the absorbent core is shaped by controlling the application of the adhesive meltblown fibers to the substrate layer using a plurality of individually programmable meltblowing nozzles.
A non-thrombogenic medical device having a surface which comprises a coating layer, said coating layer being a biocompatible composition comprising a functionalized cationic polymer outer layer whereby a heparin moiety is covalently end point attached through its reducing end to the cationic polymer outer layer by means of a link comprising a 1,2,3-triazole.
A compound of formula including any stereochemically isomeric form thereof, wherein R 1 is hydroxyC 1-6 alkyl or C 2-6 alkenyl; provided that the R 1 substituent is placed in position 6 or 7 of the indole moiety; R 2 is hydrogen or C 1-4 alkyl; Z is a radical selected from R 3 is hydrogen or hydroxyC 1-4 alkyl; R 4 is hydroxy or C 1-4 alkyloxy; R 5 is hydrogen or C 1-4 alkyl; or R 4 and R 5 are taken together to form oxo; a pharmaceutically acceptable salt thereof or a solvate thereof. R 1 is hydroxyC 1-6 alkyl or C 2-6 alkenyl; provided that the R 1 substituent is placed in position 6 or 7 of the indole moiety; R 2 is hydrogen or C 1-4 alkyl; Z is a radical selected from R 3 is hydrogen or hydroxyC 1-4 alkyl; R 4 is hydroxy or C 1-4 alkyloxy; R 5 is hydrogen or C 1-4 alkyl; or R 4 and R 5 are taken together to form oxo; R 3 is hydrogen or hydroxyC 1-4 alkyl; R 4 is hydroxy or C 1-4 alkyloxy; R 5 is hydrogen or C 1-4 alkyl; or R 4 and R 5 are taken together to form oxo;