mhurhangee/ep-ind-claims huggingface dataset:
A wind farm comprising a plurality of wind turbines, each wind turbine comprising a generator, a nacelle, and a tower supporting the nacelle, wherein each of at least two of the wind turbines further comprises an electrolytic unit electrically coupled to the generator of said wind turbine for producing hydrogen and a hydrogen output for transporting the produced hydrogen out of the wind turbine, wherein each hydrogen output is connected to a manifold by means of a manifold input, wherein the manifold is arranged above sea level and comprises a first manifold output configured to be connected to a first hydrogen pipeline for transporting the hydrogen produced by the wind farm out of the wind farm, wherein the plurality of wind turbines is arranged in at least two wind turbine arrays comprising at least one manifold per wind turbine array, wherein the manifold of each wind turbine array is coupled to the manifold of at least another wind turbine array by means of a hydrogen connection. wherein each hydrogen output is connected to a manifold by means of a manifold input, wherein the manifold is arranged above sea level and comprises a first manifold output configured to be connected to a first hydrogen pipeline for transporting the hydrogen produced by the wind farm out of the wind farm, wherein the plurality of wind turbines is arranged in at least two wind turbine arrays comprising at least one manifold per wind turbine array, wherein the manifold of each wind turbine array is coupled to the manifold of at least another wind turbine array by means of a hydrogen connection.
A pressure sensitive adhesive sheet comprising a sheet-form substrate and a silicone pressure sensitive adhesive layer formed thereon, wherein the sheet-form substrate comprises at least one polyolefin-based resin film having a melting start temperature (Tm i) of 120°C or higher and a peak melting temperature (Tm P) of from 160°C to 180°C, measured by differential scanning calorimetry according to ASTM D3418 as described hereinbefore in the description, wherein the sheet-form substrate is selected from the group consisting of at least one polypropylene homopolymer resin film, at least one polypropylene block-copolymer resin film consisting of polypropylene units and other non-propylene olefin units, and a combination thereof, and wherein the silicone pressure sensitive adhesive layer is an addition-cured releasable silicone pressure sensitive adhesive layer which is obtained by heat-curing a silicone pressure sensitive adhesive composition comprising: (a) polydiorganosiloxane having an average of at least two alkenyl radicals per molecule, (b) organohydrogenpolysiloxane having an average of more than two silicon-bonded hydrogen atoms per molecule, (c) an optional organopolysiloxane resin, (d) a platinum-type catalyst, (e) an optional solvent, and (f) an optional inhibitor. (a) polydiorganosiloxane having an average of at least two alkenyl radicals per molecule, (b) organohydrogenpolysiloxane having an average of more than two silicon-bonded hydrogen atoms per molecule, (c) an optional organopolysiloxane resin, (d) a platinum-type catalyst, (e) an optional solvent, and (f) an optional inhibitor.
An exam room shielding made of an electrically conductive material, the exam room shielding being arranged for electromagnetically shielding a magnetic resonance imaging system, the exam room shielding comprising a ceiling, a floor, side walls interconnecting the ceiling and the floor, and a tubular shielding device, which is arranged to surround an examination tube of the magnetic resonance imaging system, wherein both longitudinal ends of the tubular shielding device are circumferentially connected to openings of the side walls, to provide an electrically conductive connection therebetween and the side walls of the shielding form the outline of a U-shaped room having two lateral flanks, wherein the longitudinal ends of the tubular shielding device interconnect said lateral flanks of the U-shaped room. both longitudinal ends of the tubular shielding device are circumferentially connected to openings of the side walls, to provide an electrically conductive connection therebetween and the side walls of the shielding form the outline of a U-shaped room having two lateral flanks, wherein the longitudinal ends of the tubular shielding device interconnect said lateral flanks of the U-shaped room.
An individually packaged wipe for the treatment of hyperhidrosis comprising 0.25 to 6% w/w of a glycopyrrolate compound comprising those having the following formula: wherein X - is a pharmaceutically acceptable counter ion salt; alcohol and water in a weight ratio of 40:60 to 60:40, and a buffering agent in an amount sufficient to maintain a pH of 3.5 to 6, wherein said wipe is contained within a pouch resistant to leakage. wherein X - is a pharmaceutically acceptable counter ion salt; alcohol and water in a weight ratio of 40:60 to 60:40, and a buffering agent in an amount sufficient to maintain a pH of 3.5 to 6, wherein said wipe is contained within a pouch resistant to leakage.
A method for generating at least one MR image of an object in an MR system comprising a plurality of signal receiving coils, the method comprising: - applying a sequence of RF pulses in order to generate a plurality of MR signal echoes, - detecting the MR signal echoes with the plurality of signal receiving coils in a 3-dimensional k-space, wherein the 3-dimensional k-space is undersampled with a plurality of constant radii corkscrew trajectories (51,52,53,54), - reconstructing the at least one MR image using the undersampled 3-dimensional k-space based on a compressed sensing technology, characterized in that the plurality of constant radii corkscrew trajectories (51,52,53,54) have different radii (R1,R2,R3,R4) resulting in a non-homogeneous undersampled 3-dimensional k-space. - applying a sequence of RF pulses in order to generate a plurality of MR signal echoes, - detecting the MR signal echoes with the plurality of signal receiving coils in a 3-dimensional k-space, wherein the 3-dimensional k-space is undersampled with a plurality of constant radii corkscrew trajectories (51,52,53,54), - reconstructing the at least one MR image using the undersampled 3-dimensional k-space based on a compressed sensing technology, characterized in that the plurality of constant radii corkscrew trajectories (51,52,53,54) have different radii (R1,R2,R3,R4) resulting in a non-homogeneous undersampled 3-dimensional k-space.
An integrated system comprising: a desalination plant comprising a reverse osmosis array configured to produce an RO permeate blending stream and a nanofiltration array configured to produce an NF permeate blending stream; a blending system; a control unit; an injection system for one or more injection wells, wherein the one or more injection wells penetrate an oil-bearing layer of a reservoir; and a production facility configured to: separate fluids produced from one or more production wells that penetrate the oil-bearing layer of the reservoir and deliver a produced water stream to the blending system, wherein the blending system is configured to blend the RO permeate and the NF permeate blending streams with the PW stream to produce a blended low salinity water stream, wherein the control unit is configured to: dynamically alter operation of the blending system to adjust amounts of at least one of the RO permeate blending stream or the NF permeate blending stream to maintain a composition of the blended low salinity water stream within a predetermined operating envelope; and dynamically adjust amounts of at least one of the RO permeate discharged from the blending system via an RO permeate dump line or the NF permeate discharged from the blending system via a NF permeate dump line. a desalination plant comprising a reverse osmosis array configured to produce an RO permeate blending stream and a nanofiltration array configured to produce an NF permeate blending stream; a blending system; a control unit; an injection system for one or more injection wells, wherein the one or more injection wells penetrate an oil-bearing layer of a reservoir; and a production facility configured to: separate fluids produced from one or more production wells that penetrate the oil-bearing layer of the reservoir and deliver a produced water stream to the blending system, wherein the blending system is configured to blend the RO permeate and the NF permeate blending streams with the PW stream to produce a blended low salinity water stream, wherein the control unit is configured to: dynamically alter operation of the blending system to adjust amounts of at least one of the RO permeate blending stream or the NF permeate blending stream to maintain a composition of the blended low salinity water stream within a predetermined operating envelope; and dynamically adjust amounts of at least one of the RO permeate discharged from the blending system via an RO permeate dump line or the NF permeate discharged from the blending system via a NF permeate dump line. dynamically alter operation of the blending system to adjust amounts of at least one of the RO permeate blending stream or the NF permeate blending stream to maintain a composition of the blended low salinity water stream within a predetermined operating envelope; and dynamically adjust amounts of at least one of the RO permeate discharged from the blending system via an RO permeate dump line or the NF permeate discharged from the blending system via a NF permeate dump line.
A control system for retracting and extending a landing gear assembly in an aircraft, wherein the control system comprises a first processing module and a second processing module, each of the first and second processing modules (22, 24) being able to control retraction and extension of the landing gear assembly independently of the other thus providing redundancy, each of the processing modules (22, 24) is configured to perform a first sequence of steps for retracting the landing gear assembly and a second sequence of steps for extending the landing gear assembly, characterised in that: at least one of the first sequence of steps and the second sequence of steps includes a step of switching control from one of the first processing module and the second processing module (22, 24) to the other of the first processing module and the second processing module (22. 24), and wherein the step of switching control is performed (a) as part of the first sequence of steps for retracting the landing gear assembly, but only after the landing gear assembly has been retracted, or (b) as part of the second sequence of steps for extending the landing gear assembly. at least one of the first sequence of steps and the second sequence of steps includes a step of switching control from one of the first processing module and the second processing module (22, 24) to the other of the first processing module and the second processing module (22. 24), and wherein the step of switching control is performed (a) as part of the first sequence of steps for retracting the landing gear assembly, but only after the landing gear assembly has been retracted, or (b) as part of the second sequence of steps for extending the landing gear assembly. (a) as part of the first sequence of steps for retracting the landing gear assembly, but only after the landing gear assembly has been retracted, or (b) as part of the second sequence of steps for extending the landing gear assembly.
A compressor, comprising: an electric motor, including: a stator; and a rotor configured to rotate with respect to the stator, wherein the stator has a length L s and the rotor has a length L r, and wherein the length L r of the rotor is less than the length L s of the stator; at least one impeller configured to be driven by the electric motor via a shaft; at least one bearing configured to facilitate rotation of the shaft; and at least one balance piston configured to balance aerodynamic forces on the shaft, the aerodynamic forces generally aligned with an axis of the compressor. an electric motor, including: a stator; and a rotor configured to rotate with respect to the stator, wherein the stator has a length L s and the rotor has a length L r, and wherein the length L r of the rotor is less than the length L s of the stator; a stator; and a rotor configured to rotate with respect to the stator, wherein the stator has a length L s and the rotor has a length L r, and wherein the length L r of the rotor is less than the length L s of the stator; at least one impeller configured to be driven by the electric motor via a shaft; at least one bearing configured to facilitate rotation of the shaft; and at least one balance piston configured to balance aerodynamic forces on the shaft, the aerodynamic forces generally aligned with an axis of the compressor.
Switching device, in particular load interrupter, for medium-voltage switchgear assemblies, having a quenching contact system for quenching an arc in the event of a switch-off process of the switching device and having a main contact system, which is connected in series with the quenching contact system, for forming a dielectric isolating distance in an open state of the main contact system and when the arc is quenched, wherein the main contact system has a first fixed contact and a second fixed contact, which fixed contacts are diametrically opposite one another, and also a moving contact which can be rotated by means of a rotation support, which is arranged centrally between the first fixed contact and the second fixed contact, and has the quenching contact system integrated in it, characterized in that the moving contact of the main contact system is designed such that it can be rotated through 360°.
An electrosurgical system for the application of treatment energy to a patient and suitable for use in bipolar electrosurgery, the system comprising: an electrosurgical generator (12, 12') configured to generate and output a treatment energy along with a measurement signal; an electrosurgical control unit (20, 20', 1800) configured to direct the output of treatment energy and a measurement signal; and an electrosurgical tool removably connected to one of the electrosurgical generator (12, 12') and the electrosurgical control unit (20, 20', 1800) and arranged to contact tissue and apply the treatment energy and the measurement signal to the tissue, the electrosurgical control unit (20, 20', 1800) measuring permittivity and conductivity of the tissue through the application of the measurement signal; characterized in that the electrosurgical control unit (20, 20', 1800) is configured to determine an end point to disrupt the application of the treatment energy based on the product of the measured permittivity and conductivity of the tissue. an electrosurgical generator (12, 12') configured to generate and output a treatment energy along with a measurement signal; an electrosurgical control unit (20, 20', 1800) configured to direct the output of treatment energy and a measurement signal; and an electrosurgical tool removably connected to one of the electrosurgical generator (12, 12') and the electrosurgical control unit (20, 20', 1800) and arranged to contact tissue and apply the treatment energy and the measurement signal to the tissue, the electrosurgical control unit (20, 20', 1800) measuring permittivity and conductivity of the tissue through the application of the measurement signal; characterized in that the electrosurgical control unit (20, 20', 1800) is configured to determine an end point to disrupt the application of the treatment energy based on the product of the measured permittivity and conductivity of the tissue.
Method for manufacturing two or more thin-walled structures (1,11,13,17,18), whereby the ratio of the horizontal length to the horizontal thickness of each of said thin-walled structures (1,11,13,17,18) is larger than 10, whereby these thin-walled structures (1,11,13,17,18) are built together and in layers by applying successive powder layers extending substantially horizontally and by moving an energy beam over each of these powder layers according to a predetermined pattern so as to make said powder melt entirely or partly and subsequently make it solidify or sinter, such that successive layers of said thin-walled structures (1,11,13,17,18) are formed which extend according to a horizontal cross section of these structures, whereby said thin-walled structures (1,11,13,17,18) are connected to each other over at least a part of their surface, without building a support structure round the thin walled-structures, such that these thin-walled structures (1,11,13,17,18) form a rigid unit, whereby after said unit has been built in layers with said thin-walled structures (1,11,13,17,18), at least the thin-walled structures (1,11,13,17,18) are annealed in order to at least partly eliminate any stresses present, and whereby said thin-walled structures (1,11,13,17,18) are separated from each other, characterized in that said thin-walled structures (1,11,13,17,18) are oriented in relation to each other such that any stresses being built up in the thin-walled structures (1,11,13,17,18) during their manufacture will at least partly neutralize each other.
A quantum dot device, comprising an anode and a cathode facing each other, a quantum dot layer disposed between the anode and the cathode, and an electron transport layer disposed between the cathode and the quantum dot layer, and characterized in that the quantum dot layer comprises an emissive quantum dot configured to emit light in at least one part of a wavelength region in a visible region and a non-emissive quantum dot configured to not emit light in the visible region, and a difference between an absolute value of a lowest unoccupied molecular orbital energy level of the non-emissive quantum dot and an absolute value of a lowest unoccupied molecular orbital energy level of the electron transport layer is greater than or equal to 0.5 electron volts, and wherein the absolute value of the lowest unoccupied molecular orbital energy level of the non-emissive quantum dot is less than the absolute value of the lowest unoccupied molecular orbital energy level of the electron transport layer 2. such that the non-emissive quantum dot acts as an energy barrier to electrons moving from the electron transport layer to the quantum dot layer. an anode and a cathode facing each other, a quantum dot layer disposed between the anode and the cathode, and an electron transport layer disposed between the cathode and the quantum dot layer, and characterized in that the quantum dot layer comprises an emissive quantum dot configured to emit light in at least one part of a wavelength region in a visible region and a non-emissive quantum dot configured to not emit light in the visible region, and a difference between an absolute value of a lowest unoccupied molecular orbital energy level of the non-emissive quantum dot and an absolute value of a lowest unoccupied molecular orbital energy level of the electron transport layer is greater than or equal to 0.5 electron volts, and wherein the absolute value of the lowest unoccupied molecular orbital energy level of the non-emissive quantum dot is less than the absolute value of the lowest unoccupied molecular orbital energy level of the electron transport layer 2. such that the non-emissive quantum dot acts as an energy barrier to electrons moving from the electron transport layer to the quantum dot layer.
A method of manufacturing an optical fibre preform comprising: - producing a core rod having a core rod diameter; - inserting the core rod into a glass fluorine-doped intermediate cladding tube so as to form a core assembly having a length, the intermediate cladding tube having an inner diameter and an outer diameter, wherein the inner diameter is larger than the core rod diameter, the radial difference between the inner diameter and the core rod diameter defining an annular gap; - applying a negative pressure inside the annular gap; - forming a core preform by heating the core assembly to collapse the intermediate cladding tube around the core rod while maintaining the negative pressure, wherein heating comprises moving a heater outside the intermediate cladding tube and along an axial direction of the same at a traverse speed of from 20 mm/min to 40 mm/min, and - forming an overcladding region surrounding the core preform so as to form an optical fibre preform, characterised in that the intermediate cladding tube has a radial thickness of from 1 mm to 10 mm, and the method further comprises, between inserting the core rod into the intermediate cladding tube and heating, arranging the core assembly in such a way that it extends vertically and heating comprises moving at least upwardly the heater from an initial position at the lower end of the core assembly to traverse the length of the same. - producing a core rod having a core rod diameter; - inserting the core rod into a glass fluorine-doped intermediate cladding tube so as to form a core assembly having a length, the intermediate cladding tube having an inner diameter and an outer diameter, wherein the inner diameter is larger than the core rod diameter, the radial difference between the inner diameter and the core rod diameter defining an annular gap; - applying a negative pressure inside the annular gap; - forming a core preform by heating the core assembly to collapse the intermediate cladding tube around the core rod while maintaining the negative pressure, wherein heating comprises moving a heater outside the intermediate cladding tube and along an axial direction of the same at a traverse speed of from 20 mm/min to 40 mm/min, and - forming an overcladding region surrounding the core preform so as to form an optical fibre preform,
Coupling hook for a lower link of an agricultural tractor, wherein the coupling hook has a hook body with at least one receptacle for a coupling body, and at least one receiving chamber, in which at least one safety catch is held, which safety catch can be pivoted between a locking blocking position engaging over the coupling body and a release position which is pulled back into the receiving chamber to an extent such that the coupling body can be removed from the receptacle, wherein the coupling body, as it presses into the receptacle, can adjust the safety catch into an activation position such that the safety catch is subsequently automatically transferred into the blocking position, that the safety catch is operatively connected to at least one cam of at least one adjustable blocking lever, said cam retaining the safety catch in the blocking position thereof, and therefore said safety catch withstands a force originating from the coupled coupling body and acting on the safety catch, and can be transferred into the release position firstly by a force directed towards the receptacle and secondly by adjustment of the blocking lever, characterized in that the safety catch can be displaced to a limited extent in the direction of the receptacle, the safety catch, in the activation position adjusted with respect to the receptacle, being pressable into the release position.