mhurhangee/ep-ind-claims huggingface dataset:
A method for advertising a service, the method comprising: in a local device, performing operations for: based on a condition of the local device, dynamically adjusting a time period between a broadcast of a service advertisement and an availability window during which the local device monitors for service requests; broadcasting, a service advertisement in a wireless network, the service advertisement including one or more service identifiers, IDs, identifying one or more services being advertised and an availability schedule of the local device; wherein the availability schedule comprises a specification of the availability window; reducing power to at least a portion of the local device for a time period after the service advertisement has been broadcast and before the availability window; restoring power to the at least the portion of the local device and monitoring for service requests in the wireless network during the availability window; and in response to receiving a service request from a remote device during the availability window, transmitting a service response to the remote device, the service response having detailed information associated with one or more services identified by one or more service IDs in the service request. in a local device, performing operations for: based on a condition of the local device, dynamically adjusting a time period between a broadcast of a service advertisement and an availability window during which the local device monitors for service requests; broadcasting, a service advertisement in a wireless network, the service advertisement including one or more service identifiers, IDs, identifying one or more services being advertised and an availability schedule of the local device; based on a condition of the local device, dynamically adjusting a time period between a broadcast of a service advertisement and an availability window during which the local device monitors for service requests; broadcasting, a service advertisement in a wireless network, the service advertisement including one or more service identifiers, IDs, identifying one or more services being advertised and an availability schedule of the local device; wherein the availability schedule comprises a specification of the availability window; reducing power to at least a portion of the local device for a time period after the service advertisement has been broadcast and before the availability window; restoring power to the at least the portion of the local device and monitoring for service requests in the wireless network during the availability window; and in response to receiving a service request from a remote device during the availability window, transmitting a service response to the remote device, the service response having detailed information associated with one or more services identified by one or more service IDs in the service request.
A turbine shroud for use in a gas turbine engine, the turbine shroud comprising a carrier comprising metallic materials and adapted to be coupled to a turbine case, a blade track comprising ceramic-matrix composite materials and coupled to the carrier, the blade track including a runner and extending at least a portion of the way around a central axis so that the blade track is adapted to block hot gasses from passing over a turbine wheel surrounded by the turbine shroud, characterized in a retainer coupled to the carrier and coupled to the blade track, and the carrier comprises at least one bulkhead (82, 86) that radially interconnects the carrier and the blade track, wherein the at least one bulkhead (82, 86) includes a divider (81, 85) extending radially inward from the carrier and a seal member (83, 87) positioned between the divider (81, 85) and the blade track, thereby a space between the carrier and the runner is divided into at least a first cooling-air cavity and a second cooling-air cavity, the at least one bulkhead (82, 86) formed to include a plurality of pressure-control holes (84, 88) sized to cause the first cooling-air cavity to have a first pressure and the second cooling-air cavity to have a second pressure, lower than the first pressure.
A surgical scaffold device, comprising a laminar scaffold complex, comprising: polymeric fibers having a mean diameter of from 100 nm to 8000 nm covalently linked to a hydrogel material, wherein: a) the polymeric fibers are dispersed throughout the hydrogel material, wherein the polymeric fibers have a reduced average fiber length sufficiently short to allow them to remain in suspension in aqueous solution and are produced by cryomilling electrospun fiber sheets; b) the scaffold complex comprises a plurality of pores present on or within a surface of the device, wherein the pores are present at a concentration of at least 50 pores per cm 2 and wherein at least 80% of the pores have an average pore diameter of at least 5 micrometers; c) the device is configured in a geometry suitable for implantation in an organ or tissue selected from skin, fascia, pleura, dura, pericardium, paratenon, periosteum, perineurium, blood vessel wall, and lymphatic wall; and d) the device is configured as a sheet having a first dimension and a second dimension independently at least five times as great in length as a third dimension. a) the polymeric fibers are dispersed throughout the hydrogel material, wherein the polymeric fibers have a reduced average fiber length sufficiently short to allow them to remain in suspension in aqueous solution and are produced by cryomilling electrospun fiber sheets; b) the scaffold complex comprises a plurality of pores present on or within a surface of the device, wherein the pores are present at a concentration of at least 50 pores per cm 2 and wherein at least 80% of the pores have an average pore diameter of at least 5 micrometers; c) the device is configured in a geometry suitable for implantation in an organ or tissue selected from skin, fascia, pleura, dura, pericardium, paratenon, periosteum, perineurium, blood vessel wall, and lymphatic wall; and d) the device is configured as a sheet having a first dimension and a second dimension independently at least five times as great in length as a third dimension.
Method for analyzing biological material, wherein the method includes the following steps: reading a measurement signal, a first reference signal, and a second reference signal, wherein the measurement signal represents acquired optofluidic data of the biological material, wherein the first reference signal having a sigmoid curve represents first optofluidic model data which correspond to a first property of the biological material, wherein the second reference signal having a linear curve represents second optofluidic model data which correspond to a second property of the biological material; ascertaining a noise (η) of the measurement signal, to generate noise data; applying the noise data to the first reference signal and to the second reference signal, to generate an adapted first reference signal and an adapted second reference signal; transforming the measurement signal, the adapted first reference signal, and the adapted second reference signal into a frequency distribution form to generate a measurement signal distribution, a first bimodal reference distribution, and a second unimodal reference distribution; and performing a cluster analysis using the measurement signal distribution, the first reference distribution, and the second reference distribution to establish as a function of a result of the cluster analysis whether the biological material has the first property or the second property. reading a measurement signal, a first reference signal, and a second reference signal, wherein the measurement signal represents acquired optofluidic data of the biological material, wherein the first reference signal having a sigmoid curve represents first optofluidic model data which correspond to a first property of the biological material, wherein the second reference signal having a linear curve represents second optofluidic model data which correspond to a second property of the biological material; ascertaining a noise (η) of the measurement signal, to generate noise data; applying the noise data to the first reference signal and to the second reference signal, to generate an adapted first reference signal and an adapted second reference signal; transforming the measurement signal, the adapted first reference signal, and the adapted second reference signal into a frequency distribution form to generate a measurement signal distribution, a first bimodal reference distribution, and a second unimodal reference distribution; and performing a cluster analysis using the measurement signal distribution, the first reference distribution, and the second reference distribution to establish as a function of a result of the cluster analysis whether the biological material has the first property or the second property.
A gas turbine engine blade, comprising: a blade core portion including a shroud tip portion; the shroud tip portion extending from the blade core portion; an airfoil portion formed exteriorly to the blade core portion; and wherein the blade core portion and the shroud tip portion are constructed as a first unitary structure and the airfoil portion is constructed as a second structure and wherein the blade core portion extends from a dovetail portion to an integration region, the integration region including an area between the blade core portion and the shroud tip portion, wherein the first unitary structure is formed of a single-piece monolithic material and the second structure is formed of a composite material having a plurality of fiber plies with a two dimensional orientation, wherein the single-piece monolithic material comprises a first composite material and wherein the second structure comprises a second composite material, wherein the first composite material includes a first plurality of fiber plies having a three dimensional orientation, and wherein the second composite material includes a second plurality of fiber plies having a two dimensional orientation, and wherein the gas turbine engine blade further includes a sealing knife portion extending from the shroud tip portion. a blade core portion including a shroud tip portion; the shroud tip portion extending from the blade core portion; an airfoil portion formed exteriorly to the blade core portion; and wherein the blade core portion and the shroud tip portion are constructed as a first unitary structure and the airfoil portion is constructed as a second structure and wherein the blade core portion extends from a dovetail portion to an integration region, the integration region including an area between the blade core portion and the shroud tip portion, wherein the first unitary structure is formed of a single-piece monolithic material and the second structure is formed of a composite material having a plurality of fiber plies with a two dimensional orientation, wherein the single-piece monolithic material comprises a first composite material and wherein the second structure comprises a second composite material, wherein the first composite material includes a first plurality of fiber plies having a three dimensional orientation, and wherein the second composite material includes a second plurality of fiber plies having a two dimensional orientation, and wherein the gas turbine engine blade further includes a sealing knife portion extending from the shroud tip portion.
Rotary equipment, comprising: a base part, configured by a plurality of split bodies (13, 18), having a working chamber; and a rotor, provided rotatably in the working chamber, on which a sliding surface is formed, characterized in that at least one of the plurality of the split bodies is made of an aluminum alloy, and on which an opposed sliding surface, formed of a ceramic film that contains α - alumina and zirconia having a hardness of approximately Hv 500 to 1100 and a surface roughness of approximately 2 to 8 micrometers, is formed, and wherein the opposed sliding surface faces the sliding surface of the rotor that slides against the opposed sliding surface. a base part, configured by a plurality of split bodies (13, 18), having a working chamber; and a rotor, provided rotatably in the working chamber, on which a sliding surface is formed, characterized in that at least one of the plurality of the split bodies is made of an aluminum alloy, and on which an opposed sliding surface, formed of a ceramic film that contains α - alumina and zirconia having a hardness of approximately Hv 500 to 1100 and a surface roughness of approximately 2 to 8 micrometers, is formed, and wherein the opposed sliding surface faces the sliding surface of the rotor that slides against the opposed sliding surface.
A large-scale manipulator having an extendable folding boom that has a turntable, which is rotatable about a vertical axis, and a plurality of boom segments (14, 16, 18), wherein the boom segments (14, 16, 18) are pivotable to a limited extent at folding joints (20, 22, 24) about respectively horizontal folding axes with respect to an adjacent boom segment (14, 16, 18) or the turntable, by means of a respective drive unit, wherein at least one contactlessly operating rotation angle sensor (38, 38') for sensing the folding angle between two adjacent boom segments (14, 16, 18) or between a boom segment and the adjacent turntable, characterized by a pivot bolt that is arranged at the folding joint (20, 22, 24), wherein one element of the rotation angle sensor (38, 38') is arranged at the pivot bolt on one abutting face of the pivot bolt and that one element of the rotation angle sensor (38, 38') is arranged on a holding element that is connected with a boom segments (14, 16, 18).
A resin composition comprising an epoxy resin represented by following general formula; and a cyanate compound, wherein R each independently represents an alkyl group having 1 to 3 carbon atoms, or a hydrogen atom.
Device for taking out and analysing a representative sample from a polymerisation reactor, said device comprising: one or more sample conduits connected to said reactor and arranged to take a sample out of said reactor, one or more sample flash tanks connected to said conduits and arranged to separate solid particles from evaporated gas, and one or more sample receivers connected to said sample flash tanks and arranged to purify said solid particles, whereby each conduit is further provided with a first sample valve and a second sample valve, each conduit comprising means for periodically sequentially opening and closing said valves (4,5) and arranged to take a specific volume of a sample from said reactor, and a flushing valve downstream the first valve and upstream the second valve arranged to automatically flush the conduit with a diluent to the reactor, wherein an automatic flushing mechanism is activated after taking a sample from the reactor and wherein during automatic flushing, the first valve remains open together with the flashing valve in order to provide continuous flushing to the reactor. one or more sample conduits connected to said reactor and arranged to take a sample out of said reactor, one or more sample flash tanks connected to said conduits and arranged to separate solid particles from evaporated gas, and one or more sample receivers connected to said sample flash tanks and arranged to purify said solid particles, whereby each conduit is further provided with a first sample valve and a second sample valve, each conduit comprising means for periodically sequentially opening and closing said valves (4,5) and arranged to take a specific volume of a sample from said reactor, and a flushing valve downstream the first valve and upstream the second valve arranged to automatically flush the conduit with a diluent to the reactor, wherein an automatic flushing mechanism is activated after taking a sample from the reactor and wherein during automatic flushing, the first valve remains open together with the flashing valve in order to provide continuous flushing to the reactor. a first sample valve and a second sample valve, each conduit comprising means for periodically sequentially opening and closing said valves (4,5) and arranged to take a specific volume of a sample from said reactor, and a flushing valve downstream the first valve and upstream the second valve arranged to automatically flush the conduit with a diluent to the reactor, wherein an automatic flushing mechanism is activated after taking a sample from the reactor and wherein during automatic flushing, the first valve remains open together with the flashing valve in order to provide continuous flushing to the reactor.
Porous soil granules suitable for the reversible storage of water and comprising at least one open-pore foam from the group consisting of foamed clay based on natural clay minerals, characterized in that the foamed clay comprises organically modified, aminated clay minerals from the group consisting of the sheet silicates and framework silicates.
A method for preparation of organofluoro compounds by reacting fluorine salt with sulfonate in the presence of alcohol selected from the group consisting isopropanol, isobutanol, isoamyl alcohol, and 3-pentanol; t-butanol, t-amyl alcohol, 2,3-dimethyl-2-butanol, 2-(trifluoromethyl)-2-propanol, 3-methyl-3-pentanol, 3-ethyl-3-pentanol, 2-methyl-2-pentanol, 2,3-dimethyl-3-pentanol, 2,4-dimethyl-2-pentanol, 2-methyl-2-hexanol, 2-cyclopropyl-2-propanol, 2-cyclopropyl-2-butanol, 2-cyclopropyl-3-methyl-2-butanol, 1-methylcyclopentanol, 1-ethylcyclopentanol, 1-propylcyclopentanol, 1-methylcyclohexanol, 1-ethylcyclohexanol and 1-methylcycloheptanol; and wherein the organofluoro compound is selected from: [ 18 F]fluorodeoxyglucose of Chemistry Formula 2 [ 18 F]fluoromisonidazole of Chemistry Formula 3 [ 18 F]fluoroestradiol of Chemistry Formula 4 [ 18 F]fluoropropylcarbomethoxytropane of Chemistry Formula 5 [ 18 F]fluoroDDNP of Chemistry Formula 6 [ 18 F]fluorothymidine of Chemistry Formula 7 [ 18 F]fluorocholine of Chemistry Formula 8 [ 18 F]fluoroethylcholine of Chemistry Formula 9 or [ 18 F]fluoropropylcholine of Chemistry Formula 10 [ 18 F]fluorodeoxyglucose of Chemistry Formula 2 [ 18 F]fluoromisonidazole of Chemistry Formula 3 [ 18 F]fluoroestradiol of Chemistry Formula 4 [ 18 F]fluoropropylcarbomethoxytropane of Chemistry Formula 5 [ 18 F]fluoroDDNP of Chemistry Formula 6 [ 18 F]fluorothymidine of Chemistry Formula 7 [ 18 F]fluorocholine of Chemistry Formula 8 [ 18 F]fluoroethylcholine of Chemistry Formula 9 or [ 18 F]fluoropropylcholine of Chemistry Formula 10
A system for an atmospheric suit, the system comprising: a controller within the atmospheric suit; and a first network configured as a first hub and spoke network arranged within the atmospheric suit, wherein the controller is the hub of the first network, each spoke of the first network represents first wiring that leads to one of a plurality of ports accessible from outside the atmospheric suit; a battery; characterized by a second network configured as a second hub and spoke network arranged within the atmospheric suit, wherein the battery is the hub of the second network, each spoke of the second network represents second wiring that leads to one of the plurality of ports accessible from outside the atmospheric suit. a controller within the atmospheric suit; and a first network configured as a first hub and spoke network arranged within the atmospheric suit, wherein the controller is the hub of the first network, each spoke of the first network represents first wiring that leads to one of a plurality of ports accessible from outside the atmospheric suit; a battery; characterized by a second network configured as a second hub and spoke network arranged within the atmospheric suit, wherein the battery is the hub of the second network, each spoke of the second network represents second wiring that leads to one of the plurality of ports accessible from outside the atmospheric suit.
A method for joining aligned discrete optical elements, wherein surface regions to be joined at the optical element are provided with at least one thin metal layer and are subsequently wetted with a liquid solder in a contact-free, metered manner; wherein the flux-free molten solder is applied to the surface regions to be joined via a nozzle using a pressurized gas flow, said solder being evenly distributed over surface regions to be joined with the aid of the energy of the gas pressure of the employed gas flow and being applied in a liquid, metered manner with a solder volume of 0.005 mm 3 to 1.5 mm 3 per area mm 2.
A pressure-sensitive adhesive resin composition comprising 100 parts by mass of an acrylic copolymer, 0.5 to 20 parts by mass of a crosslinking agent, and 0.1 to 5 parts by mass of a photopolymerization initiator, wherein the acrylic copolymer is a graft copolymer having a weight average molecular weight of 5.0 × 10 4 to 5.0 × 10 5, contains as a trunk component of the graft copolymer a repeating unit derived from a (meth)acrylate, contains as a branch component of the graft copolymer a repeating unit derived from a macromonomer having a number average molecular weight of 5.0 × 10 2 or more and less than 6.0 × 10 3, and contains the repeating unit derived from the macromonomer in the acrylic copolymer in a proportion in a range of 0.1 to 3 mol%.
A fastening of rotor blades to the rotor hub of wind power plants by means of transverse studs and tie rods (5, 6) in the region of the blade root, wherein the transverse studs are arranged such that they pass through the blade root shell wall and the transverse studs can be connected to a flange of the hub by means of the tie rods (5, 6) that are in the form of reduced-shaft bolts, characterized in that each transverse stud can be connected to the flange of the rotor hub by means of two tie rods (5, 6), wherein each tie rod (5, 6) is arranged in a separate tie rod bore (7, 8) in the blade root shell wall.
A wind velocity measurement method performed by an unmanned aerial vehicle, UAV, comprising: determining current wind resistance interference of the UAV by means of system identification based on flight data and attribute data of the UAV, wherein the flight data comprises an attitude angle, a flight velocity, an acceleration and a flight altitude of the UAV, and the attribute data comprises a mass of the UAV, an inherent wind resistance coefficient and a nonlinear function used to calculate a windward area, wherein the windward area is calculated by using the nonlinear function related to a current attitude angle of the UAV; and calculating a wind velocity of a flight environment of the UAV according to the wind resistance interference and the inherent wind resistance of the UAV. determining current wind resistance interference of the UAV by means of system identification based on flight data and attribute data of the UAV, wherein the flight data comprises an attitude angle, a flight velocity, an acceleration and a flight altitude of the UAV, and the attribute data comprises a mass of the UAV, an inherent wind resistance coefficient and a nonlinear function used to calculate a windward area, wherein the windward area is calculated by using the nonlinear function related to a current attitude angle of the UAV; and calculating a wind velocity of a flight environment of the UAV according to the wind resistance interference and the inherent wind resistance of the UAV.