mhurhangee/ep-ind-claims huggingface dataset:
Magnetic trigger device for pretensioned fishing line, which comprises: a rope storing element formed with a base body, a cylindrical end and a connecting surface, as well as a truncated cone shaped line guiding element formed with a fastening surface, a cylindrical surface and a connecting surface, and reels (7, 17) are connected to side surfaces (48, 49) of the base body of the rope storing element, wherein supporting lugs (4, 14) are connected to the reels (7, 17), while a knot-free clip is fixed to the base body at an upper end of the base body, characterized in that, a magnet is located at the centre of the circular connecting surface of the rope storing element, and a rotating clip for guiding the fishing line is fixed at the centre of the fastening surface of the line guiding element, while a counter magnet is located at the centre of the circular connecting surface of the line guiding element. a rope storing element formed with a base body, a cylindrical end and a connecting surface, as well as a truncated cone shaped line guiding element formed with a fastening surface, a cylindrical surface and a connecting surface, and reels (7, 17) are connected to side surfaces (48, 49) of the base body of the rope storing element, wherein supporting lugs (4, 14) are connected to the reels (7, 17), while a knot-free clip is fixed to the base body at an upper end of the base body, characterized in that, a magnet is located at the centre of the circular connecting surface of the rope storing element, and a rotating clip for guiding the fishing line is fixed at the centre of the fastening surface of the line guiding element, while a counter magnet is located at the centre of the circular connecting surface of the line guiding element.
A turbine bucket for a gas turbine comprising: a platform portion; an airfoil extending radially outward from the platform portion; a shank portion extending radially inward from the platform portion; an angel wing extending axially from a face of the shank portion; characterised by a plurality of voids disposed along a length of the angel wing, each of the plurality of voids extending radially through the angel wing and angled with respect to a longitudinal axis (R L) of the turbine bucket and to a direction of rotation of the turbine bucket; wherein the plurality of voids is shaped to impart a swirl to purge air as the purge air passes radially outward through the angel wing, and wherein each of the plurality of voids includes a convex face and a concave face. a platform portion; an airfoil extending radially outward from the platform portion; a shank portion extending radially inward from the platform portion; an angel wing extending axially from a face of the shank portion; characterised by a plurality of voids disposed along a length of the angel wing, each of the plurality of voids extending radially through the angel wing and angled with respect to a longitudinal axis (R L) of the turbine bucket and to a direction of rotation of the turbine bucket; wherein the plurality of voids is shaped to impart a swirl to purge air as the purge air passes radially outward through the angel wing, and wherein each of the plurality of voids includes a convex face and a concave face.
A gas analyzer comprising: - a measuring volume for through flow of a sample gas mixture, at least one gas component of which is to be analyzed for determining its concentration in said mixture, and having first and second transparent ends; - a radiation source for providing a beam of electromagnetic radiation having a wavelength range, said beam directed to pass said measuring volume through said first and second transparent ends thereof; - a heat sink for said radiation source; - at least one thermal detector having an active radiation detecting sensor element with at least one support structure and receiving the radiation exiting said measuring volume, said thermal detector having a reference sensor element within the same support structure and protected from said radiation, said thermal detector generating an output signal indicative of a property of said at least one gas component of said mixture in the measuring volume; - a thermal mass (11, 12) formed of a material having high thermal conductance; having a cavity; being at least in partial thermal contact with said support structure inside said cavity; and extending towards the radiation source; - a first thermal barrier between the heat sink and the thermal mass (11, 12); - a second thermal barrier surrounding the thermal mass (11, 12) and extending towards the heat sink; characterized by - a shield or outer surface layers formed of a material or materials having high thermal conductance; said shield or outer surface layers being at least in thermal contact with said heat sink, and covering said second thermal barrier. - a measuring volume for through flow of a sample gas mixture, at least one gas component of which is to be analyzed for determining its concentration in said mixture, and having first and second transparent ends; - a radiation source for providing a beam of electromagnetic radiation having a wavelength range, said beam directed to pass said measuring volume through said first and second transparent ends thereof; - a heat sink for said radiation source; - at least one thermal detector having an active radiation detecting sensor element with at least one support structure and receiving the radiation exiting said measuring volume, said thermal detector having a reference sensor element within the same support structure and protected from said radiation, said thermal detector generating an output signal indicative of a property of said at least one gas component of said mixture in the measuring volume; - a thermal mass (11, 12) formed of a material having high thermal conductance; having a cavity; being at least in partial thermal contact with said support structure inside said cavity; and extending towards the radiation source; - a first thermal barrier between the heat sink and the thermal mass (11, 12); - a second thermal barrier surrounding the thermal mass (11, 12) and extending towards the heat sink; characterized by - a shield or outer surface layers formed of a material or materials having high thermal conductance; said shield or outer surface layers being at least in thermal contact with said heat sink, and covering said second thermal barrier.
A connecting rod, in particular for a turbomachine, comprising an intermediate body of generally elongated shape and connected at its longitudinal ends to connecting heads comprising orifices whose axes are for example substantially parallel, said heads being assembled or integrally formed with at least one part of said body and at least one of them comprising, about the axis of its orifice, an alveolar annular part forming a vibratory filter and having a flexural and/or compressive deformation capacity greater than that of the rest of the connecting rod and in particular that of said body, characterized in that said annular part comprises a lattice-shaped structure.
Method for the early detection of the risk of growing roll oscillations in the case of a watercraft in relation to a roll resonance, in which the movement state in relation to the roll resonance is detected, in which, during seaway, at least the heave motion and the roll motion are detected and related to one another, wherein the roll angle ( Φ) or the time profile thereof during a predetermined part of the heave motion is detected, characterized in that this is used to determine the roll power (P Φ), the roll energy or the time profile of the roll power or the roll energy and this is used as a measure for impending growth of the roll oscillation.
A paint composition comprising a binder component and a rheology control agent, the binder component comprising an alkoxysilyl-containing acrylic resin and the rheology control agent comprising a reaction product of a polyisocyanate compound, a primary monoamine having a number average molecular weight of 300 or less, and a polyether amine having a number average molecular weight of more than 300 but less than 6000, whereby the number average molecular weight is determined according to the disclosure in the description.
A method in a wireless device for reporting channel state information, CSI, for a CSI process, the CSI process corresponding to a reference signal resource and an associated interference measurement resource, IMR, wherein the IMR is a set of resource elements in which one or more signals assumed to be interfering with a desired signal are received, the method characterized in: - obtaining an interference power adjustment value; - estimating interference and noise based on the IMR, and on the interference power adjustment value, by measuring interference on the IMR corresponding to the CSI process, and applying the power adjustment value to the measured interference; - determining channel state information based on an estimated effective channel measured based on the reference signal resource, and on the estimated interference and noise; and - transmitting the channel state information to a network node. - obtaining an interference power adjustment value; - estimating interference and noise based on the IMR, and on the interference power adjustment value, by measuring interference on the IMR corresponding to the CSI process, and applying the power adjustment value to the measured interference; - determining channel state information based on an estimated effective channel measured based on the reference signal resource, and on the estimated interference and noise; and - transmitting the channel state information to a network node.
High-frequency module, comprising: - a semi-conductor part that is designed to generate and/or process electrical high-frequency signals (s HF, rHF), with ∘ a contact surface by means of which the electrical high-frequency signals (s HF, r HF) can be coupled or uncoupled, - a dielectric coupling element for coupling the high-frequency signals (s HF) as radar signals (S HF) into - a dielectric waveguide and/or for coupling radar signals (R HF) from the waveguide into the semi-conductor part as electrical high-frequency signals (r HF), wherein the coupling element and the waveguide form - a plug-in contact; characterized in that the dielectric coupling element is in contact with the semi-conductor module by means of the contact surface. - a semi-conductor part that is designed to generate and/or process electrical high-frequency signals (s HF, rHF), with ∘ a contact surface by means of which the electrical high-frequency signals (s HF, r HF) can be coupled or uncoupled, ∘ a contact surface by means of which the electrical high-frequency signals (s HF, r HF) can be coupled or uncoupled, - a dielectric coupling element for coupling the high-frequency signals (s HF) as radar signals (S HF) into - a dielectric waveguide and/or for coupling radar signals (R HF) from the waveguide into the semi-conductor part as electrical high-frequency signals (r HF), wherein the coupling element and the waveguide form - a plug-in contact;
A method of controlling beam transmission from a radio access node, comprising: identifying a number of user equipments, UEs, associated with a same beam set; grouping the identified UEs into one or more groups according to a criterion of the UEs being associated with a same active/monitored set of beams; assigning a same discontinuous reception, DRX, phase to the UEs in each group; and coordinating transmission from the beam set to UEs in the one or more groups based on the assigned DRX phase. identifying a number of user equipments, UEs, associated with a same beam set; grouping the identified UEs into one or more groups according to a criterion of the UEs being associated with a same active/monitored set of beams; assigning a same discontinuous reception, DRX, phase to the UEs in each group; and coordinating transmission from the beam set to UEs in the one or more groups based on the assigned DRX phase.
Hose for transferring of fluids, said fluid being compressed air for the brake circuits of heavy goods vehicles, and in which the inner layer is in contact with said fluid, said hose comprising in succession from the outside inwards: - a layer consisting of a composition, noted C, comprising, by weight, the total being 100%: 70 to 95%, advantageously 75 to 90%, of at least one polyamide A1, said polyamide A1 being chosen between PA-6.10, PA-6.14, PA-6.18 and PA-10.10, - 5 to 20%, advantageously 10 to 15%, of a plasticizer; - 0 to 5% of an impact modifier; and - 0 to 5% of a polyamide A2 - a coextrusion tie; and - a layer of another polyamide. - a layer consisting of a composition, noted C, comprising, by weight, the total being 100%: 70 to 95%, advantageously 75 to 90%, of at least one polyamide A1, said polyamide A1 being chosen between PA-6.10, PA-6.14, PA-6.18 and PA-10.10, - 5 to 20%, advantageously 10 to 15%, of a plasticizer; - 0 to 5% of an impact modifier; and - 0 to 5% of a polyamide A2 - 5 to 20%, advantageously 10 to 15%, of a plasticizer; - 0 to 5% of an impact modifier; and - 0 to 5% of a polyamide A2 - a coextrusion tie; and - a layer of another polyamide.
A footwear sole moulding assembly comprising: - a premanufactured primary sole part configured for forming part of an article of footwear, said premanufactured primary sole part being an outsole and having a foot facing surface, and a ground facing surface, wherein the premanufactured primary sole part comprises a plurality of through-going holes, wherein the plurality of through-going holes extends in a vertical direction from the foot facing surface to the ground facing surface; wherein the foot facing surface is configured to receive an injected sole material for attaching the premanufactured primary sole part to a ground facing surface of an upper; and - a primary mould part comprising a plurality of protrusions configured to mate with the plurality of through-going holes of the premanufactured primary sole part. - a premanufactured primary sole part configured for forming part of an article of footwear, said premanufactured primary sole part being an outsole and having a foot facing surface, and a ground facing surface, wherein the premanufactured primary sole part comprises a plurality of through-going holes, wherein the plurality of through-going holes extends in a vertical direction from the foot facing surface to the ground facing surface; wherein the foot facing surface is configured to receive an injected sole material for attaching the premanufactured primary sole part to a ground facing surface of an upper; and - a primary mould part comprising a plurality of protrusions configured to mate with the plurality of through-going holes of the premanufactured primary sole part.
A method of operating a rotorcraft, the method comprising: receiving a measured yaw rate from a yaw rate sensor or a measured lateral acceleration from a lateral acceleration sensor of the rotorcraft; regulating a yaw rate or a lateral acceleration of the rotorcraft based on a filtered measured yaw rate or a filtered measured lateral acceleration by providing an actuator signal to a tail rotor of the rotorcraft, the actuator signal controlling the pitch of the blades; characterized by filtering the measured yaw rate or the measured lateral acceleration using an aeroservoelastic filter and a lateral shuffle filter to form the filtered measured yaw rate or filtered measured lateral acceleration, wherein the lateral shuffle filter comprises a bandpass characteristic or a notch characteristic, and the filtering of the lateral shuffle filter is configured to reduce lateral vibrations caused by airflow in a tail section of the rotorcraft and the filtering of the aeroservoelastic filter is configured to prevent excitation of structural modes, and whereby the frequency of the passband or stopband of the lateral shuffle filter is configured to be at a different frequency from the frequencies of the structural modes targeted by the aeroservoelastic filter. receiving a measured yaw rate from a yaw rate sensor or a measured lateral acceleration from a lateral acceleration sensor of the rotorcraft; regulating a yaw rate or a lateral acceleration of the rotorcraft based on a filtered measured yaw rate or a filtered measured lateral acceleration by providing an actuator signal to a tail rotor of the rotorcraft, the actuator signal controlling the pitch of the blades; characterized by filtering the measured yaw rate or the measured lateral acceleration using an aeroservoelastic filter and a lateral shuffle filter to form the filtered measured yaw rate or filtered measured lateral acceleration, wherein the lateral shuffle filter comprises a bandpass characteristic or a notch characteristic, and the filtering of the lateral shuffle filter is configured to reduce lateral vibrations caused by airflow in a tail section of the rotorcraft and the filtering of the aeroservoelastic filter is configured to prevent excitation of structural modes, and whereby the frequency of the passband or stopband of the lateral shuffle filter is configured to be at a different frequency from the frequencies of the structural modes targeted by the aeroservoelastic filter.
An industrial automation controller, comprising: a receiver component that receives a request for structured data retained within the industrial controller; and a location component that locates metadata associated with the structured data, wherein the metadata describes a structure of the requested structured data. a receiver component that receives a request for structured data retained within the industrial controller; and a location component that locates metadata associated with the structured data, wherein the metadata describes a structure of the requested structured data.
An aerosol-generating article comprising an aerosol-forming substrate and a susceptor (1,4) for heating the aerosol-forming substrate, characterised in that the susceptor (1,4) comprises a first susceptor material (2,5) and a second susceptor material (3,6), the first susceptor material being disposed in intimate physical contact with the second susceptor material, and the second susceptor material having a Curie temperature that is lower than 500 °C.
Device for the mechanical cleaning of wire rods for the production of drawn metallic wires, comprising a pair of elements supported by a shaft; each element comprising a truncated-conical body and a flat disk that covers the truncated-conical body, defining an internal annular space that contains steel wool; the flat disk being provided with openings shaped like a slot; the two elements being disposed one in front of the other along a plane of symmetry, wherein a space is provided between the two flat disks; said space being suitable for receiving said wire rod; wherein, during the operation, by means of a rapid rotation of the shaft, said steel wool expands under the effect of a centrifugal force in radial direction, thus creating an axial thrust component on said steel wool towards said flat disks in such a way that said steel wool escapes partially and elastically from the openings of the flat disks, so that the steel wool brushes against the surface of the wire rod that is in transit in the space between the two elements, thus producing a cleaning action on the surface of the wire rod in contact with the steel wool by means of high-speed rubbing. the flat disk being provided with openings shaped like a slot; the two elements being disposed one in front of the other along a plane of symmetry, wherein a space is provided between the two flat disks; said space being suitable for receiving said wire rod; wherein, during the operation, by means of a rapid rotation of the shaft, said steel wool expands under the effect of a centrifugal force in radial direction, thus creating an axial thrust component on said steel wool towards said flat disks in such a way that said steel wool escapes partially and elastically from the openings of the flat disks, so that the steel wool brushes against the surface of the wire rod that is in transit in the space between the two elements, thus producing a cleaning action on the surface of the wire rod in contact with the steel wool by means of high-speed rubbing.
A high-strength steel sheet having excellent room-temperature formability and warm formability, the steel sheet having a composition consisting of, by mass percent (the same applies to the following for the chemical components), C: 0.02 to 0.3%, Si: 1.0 to 3.0%, Mn: 1.8 to 3.0%, P: 0.1% or less (including 0%), S: 0.01% or less (including 0%), Al: 0.001 to 0.1%, N: 0.01 to 0.03%, and optionally: Cr: 0.01 to 3.0%, Mo: 0.01 to 1.0%, Cu: 0.01 to 2.0%, Ni: 0.01 to 2.0%, B: 0.00001 to 0.01%, Ca: 0.0005 to 0.01%, Mg: 0.0005 to 0.01%, and REM: 0.0001 to 0.01% of one or at least two elements, and the remainder consisting of iron and impurities, and having a microstructure containing phases of, by area ratio to the entire microstructure (the same applies to the following for the microstructures), bainitic ferrite: 50 to 85%, retained austenite: 3% or more, martensite and the retained austenite in total: 10 to 45%, and ferrite: 5 to 40%, wherein C concentration (CγR) in the retained austenite is 0.3 to 1.2 mass percent, and part or all of N in the composition exists as dissolved N, and the amount of the dissolved N is 30 to 100 ppm. C: 0.02 to 0.3%, Si: 1.0 to 3.0%, Mn: 1.8 to 3.0%, P: 0.1% or less (including 0%), S: 0.01% or less (including 0%), Al: 0.001 to 0.1%, N: 0.01 to 0.03%, and Cr: 0.01 to 3.0%, Mo: 0.01 to 1.0%, Cu: 0.01 to 2.0%, Ni: 0.01 to 2.0%, B: 0.00001 to 0.01%, Ca: 0.0005 to 0.01%, Mg: 0.0005 to 0.01%, and REM: 0.0001 to 0.01% of one or at least two elements, and