mhurhangee/patent-ind-claim-en huggingface dataset:
A collimating lens for collimating an input beam and accordingly forming an output beam, consisting in: a first lens group , a second lens group and a third lens group disposed in an order from an input-beam side to an output-beam side, each of the first lens group and the third lens group having an aspherical surface (s1/s9); and a flat diffraction lens arranged in the third lens group and disposed nearest to the output beam, characterized in that the first lens group includes a negative-powered first lens with an aspherical concave surface (s1) on the input-beam side, a flat second lens and a positive-powered third lens in the order from the input-beam side to the output-beam side, the negative-powered first lens is in contact with the flat second lens, and the positive-powered third lens is in contact with the flat second lens; the second lens group includes a negative-powered fourth lens , a flat fifth lens and a positive-powered sixth lens in the order from the input-beam side to the output-beam side, the negative-powered fourth lens is in contact with the flat fifth lens, and the positive-powered sixth lens is in contact with the flat fifth lens; and the third lens group includes a positive-powered seventh lens with an aspherical convex surface (s9) on the input-beam side, a flat eighth lens and the flat diffraction lens in the order from the input-beam side to the output-beam side, the positive-powered seventh lens is in contact with the flat eighth lens, and the flat diffraction lens is in contact with the flat eighth lens. a first lens group , a second lens group and a third lens group disposed in an order from an input-beam side to an output-beam side, each of the first lens group and the third lens group having an aspherical surface (s1/s9); and a flat diffraction lens arranged in the third lens group and disposed nearest to the output beam, characterized in that the first lens group includes a negative-powered first lens with an aspherical concave surface (s1) on the input-beam side, a flat second lens and a positive-powered third lens in the order from the input-beam side to the output-beam side, the negative-powered first lens is in contact with the flat second lens, and the positive-powered third lens is in contact with the flat second lens; the second lens group includes a negative-powered fourth lens , a flat fifth lens and a positive-powered sixth lens in the order from the input-beam side to the output-beam side, the negative-powered fourth lens is in contact with the flat fifth lens, and the positive-powered sixth lens is in contact with the flat fifth lens; and the third lens group includes a positive-powered seventh lens with an aspherical convex surface (s9) on the input-beam side, a flat eighth lens and the flat diffraction lens in the order from the input-beam side to the output-beam side, the positive-powered seventh lens is in contact with the flat eighth lens, and the flat diffraction lens is in contact with the flat eighth lens.
An audio signal processing system , comprising: an input interface to receive a noisy audio signal including a mixture of a target audio signal and noise; an encoder to map each time-frequency bin of the noisy audio signal to one or more phase-related values from one or more phase quantization codebooks of phase-related values indicative of the phase of the target signal, and to calculate, for each time-frequency bin of the noisy audio signal , a magnitude ratio value indicative of a ratio of a magnitude of the target audio signal to a magnitude of the noisy audio signal ; a filter to cancel the noise from the noisy audio signal based on the one or more phase-related values and the magnitude ratio values to produce an enhanced audio signal; and an output interface to output the enhanced audio signal. an input interface to receive a noisy audio signal including a mixture of a target audio signal and noise; an encoder to map each time-frequency bin of the noisy audio signal to one or more phase-related values from one or more phase quantization codebooks of phase-related values indicative of the phase of the target signal, and to calculate, for each time-frequency bin of the noisy audio signal , a magnitude ratio value indicative of a ratio of a magnitude of the target audio signal to a magnitude of the noisy audio signal ; a filter to cancel the noise from the noisy audio signal based on the one or more phase-related values and the magnitude ratio values to produce an enhanced audio signal; and an output interface to output the enhanced audio signal.
A method of making a nuclear fuel structure, comprising: manufacturing a cathode plate by securing an upper blade to a lower blade portion with a connection structure , the upper blade including an electrically conductive material, the connection structure configured to provide electrical continuity between the lower blade portion and the upper blade when the connection structure secures the lower blade portion to the upper blade , the lower blade portion including uranium, zirconium, or a combination thereof, the connection structure is configured to be disconnected from the lower blade portion to detach the lower blade portion from the upper blade ; reducing a metal oxide in a cathode assembly including the cathode plate so as to deposit a metal of the metal oxide on the cathode plate of the cathode assembly; and processing the cathode plate with the metal deposited thereon to fabricate the nuclear fuel structure. manufacturing a cathode plate by securing an upper blade to a lower blade portion with a connection structure , the upper blade including an electrically conductive material, the connection structure configured to provide electrical continuity between the lower blade portion and the upper blade when the connection structure secures the lower blade portion to the upper blade , the lower blade portion including uranium, zirconium, or a combination thereof, the connection structure is configured to be disconnected from the lower blade portion to detach the lower blade portion from the upper blade ; reducing a metal oxide in a cathode assembly including the cathode plate so as to deposit a metal of the metal oxide on the cathode plate of the cathode assembly; and processing the cathode plate with the metal deposited thereon to fabricate the nuclear fuel structure.
A method for providing reduced flaps takeoff or landing advice in an aircraft, the method comprising: receiving , via at least one processor, takeoff or landing performance data including weather data and runway conditions data for a plurality of runways at a destination aerodrome; calculating , via the at least one processor, values of takeoff or landing performance parameters for a plurality of flap configurations for each of the plurality of runways; presenting , via the at least one processor and a user interface, at least one of the values of takeoff or landing performance parameters; and providing, via the at least one processor and the user interface, an alert regarding noise restrictions for the destination aerodrome, wherein the step of providing the alert comprises determining a predicted time at which the aircraft will be landing at the destination aerodrome and providing the alert at a time determined using the determined predicted time at which the aircraft will be landing at the destination aerodrome. receiving , via at least one processor, takeoff or landing performance data including weather data and runway conditions data for a plurality of runways at a destination aerodrome; calculating , via the at least one processor, values of takeoff or landing performance parameters for a plurality of flap configurations for each of the plurality of runways; presenting , via the at least one processor and a user interface, at least one of the values of takeoff or landing performance parameters; and providing, via the at least one processor and the user interface, an alert regarding noise restrictions for the destination aerodrome, wherein the step of providing the alert comprises determining a predicted time at which the aircraft will be landing at the destination aerodrome and providing the alert at a time determined using the determined predicted time at which the aircraft will be landing at the destination aerodrome.
A surface treatment method performed in a surface treatment apparatus that includes a treatment vessel , a single-fluid spray nozzle and a circulation device , the surface treatment method comprising the steps of: supplying mist of a non-chromate conversion treatment liquid (PL) with an average droplet diameter of 70 μm or less from the single-fluid spray nozzle to a treatment space of the treatment vessel in which a metal component (S) is disposed; collecting, by the circulation device , the non-chromate conversion treatment liquid (PL) from the treatment space ; and supplying, by the circulation device , the non-chromate conversion treatment liquid (PL) collected from the treatment space to the spray nozzle , and wherein the mist of the non-chromate conversion treatment liquid (PL) is supplied from the spray nozzle in such a manner that the treatment space is filled with the mist of the non-chromate conversion treatment liquid (PL), characterized in that an amount of non-chromate conversion treatment liquid (PL) that is held and circulates in a treatment liquid circulation system is 10 L or less per cubic meter m 3 of the treatment space , the treatment liquid circulation system including the spray nozzle , the treatment vessel and the circulation device , and an amount of non-chromate conversion treatment liquid (PL) to be supplied from the spray nozzle to the treatment space is 10 L/min or less per cubic meter m 3 of the treatment space . supplying mist of a non-chromate conversion treatment liquid (PL) with an average droplet diameter of 70 μm or less from the single-fluid spray nozzle to a treatment space of the treatment vessel in which a metal component (S) is disposed; collecting, by the circulation device , the non-chromate conversion treatment liquid (PL) from the treatment space ; and supplying, by the circulation device , the non-chromate conversion treatment liquid (PL) collected from the treatment space to the spray nozzle , and wherein the mist of the non-chromate conversion treatment liquid (PL) is supplied from the spray nozzle in such a manner that the treatment space is filled with the mist of the non-chromate conversion treatment liquid (PL), characterized in that an amount of non-chromate conversion treatment liquid (PL) that is held and circulates in a treatment liquid circulation system is 10 L or less per cubic meter m 3 of the treatment space , the treatment liquid circulation system including the spray nozzle , the treatment vessel and the circulation device , and an amount of non-chromate conversion treatment liquid (PL) to be supplied from the spray nozzle to the treatment space is 10 L/min or less per cubic meter m 3 of the treatment space .
A gas turbine engine comprising: a nose cone ; and a fan for delivering air into a bypass duct as bypass flow (B), and into a core engine, to be delivered to a compressor, said nose cone including a vent to receive air and deliver said air across a heat exchanger , said heat exchanger receiving a fluid to be cooled, and the air from the vents being delivered to an outlet downstream of the heat exchanger , such that a majority of the air being delivered to said outlet becomes part of the bypass flow (B), wherein a stationary vane is included, and said nose cone communicates air downstream of the heat exchanger into an interior of the stationary vane to be delivered to said outlet ; characterised in that there are a plurality of said outlets , and said vane has a radial span and at least a majority of said outlets are positioned in an outer 50 percent of said span. a nose cone ; and a fan for delivering air into a bypass duct as bypass flow (B), and into a core engine, to be delivered to a compressor, said nose cone including a vent to receive air and deliver said air across a heat exchanger , said heat exchanger receiving a fluid to be cooled, and the air from the vents being delivered to an outlet downstream of the heat exchanger , such that a majority of the air being delivered to said outlet becomes part of the bypass flow (B), wherein a stationary vane is included, and said nose cone communicates air downstream of the heat exchanger into an interior of the stationary vane to be delivered to said outlet ; characterised in that there are a plurality of said outlets , and said vane has a radial span and at least a majority of said outlets are positioned in an outer 50 percent of said span.
A composition, comprising: 45 to 85 weight percent of a polycarbonate comprising 35 to 75 weight percent of a copolyestercarbonate comprising ester units of the formula wherein, independently in each ester unit, R 1 is an unsubstituted or substituted divalent C 6 -C 30 aromatic group; and T is an unsubstituted or substituted C 4 -C 18 aliphatic divalent group; and carbonate units of the formula wherein, independently in each carbonate unit, R 2 is a radical of the formula wherein each of A 1 and A 2 is independently a monocyclic divalent aryl radical and Y 1 is a bridging radical having one or two atoms that separate A 1 from A 2 ; and 10 to 30 weight percent of a polycarbonate-polydiorganosiloxane block copolymer; 10 to 30 weight percent of poly(butylene terephthalate); 5 to 20 weight percent reinforcing filler having an aspect ratio of at least 5:1; and 0 to 1 weight percent of particulate filler having an aspect ratio less than 5:1; wherein all weight percents are based on the total weight of the composition. 45 to 85 weight percent of a polycarbonate comprising 35 to 75 weight percent of a copolyestercarbonate comprising ester units of the formula wherein, independently in each ester unit, R 1 is an unsubstituted or substituted divalent C 6 -C 30 aromatic group; and T is an unsubstituted or substituted C 4 -C 18 aliphatic divalent group; and carbonate units of the formula wherein, independently in each carbonate unit, R 2 is a radical of the formula wherein each of A 1 and A 2 is independently a monocyclic divalent aryl radical and Y 1 is a bridging radical having one or two atoms that separate A 1 from A 2 ; and 10 to 30 weight percent of a polycarbonate-polydiorganosiloxane block copolymer; 35 to 75 weight percent of a copolyestercarbonate comprising ester units of the formula wherein, independently in each ester unit, R 1 is an unsubstituted or substituted divalent C 6 -C 30 aromatic group; and T is an unsubstituted or substituted C 4 -C 18 aliphatic divalent group; and carbonate units of the formula wherein, independently in each carbonate unit, R 2 is a radical of the formula wherein each of A 1 and A 2 is independently a monocyclic divalent aryl radical and Y 1 is a bridging radical having one or two atoms that separate A 1 from A 2 ; and 10 to 30 weight percent of a polycarbonate-polydiorganosiloxane block copolymer; 10 to 30 weight percent of poly(butylene terephthalate); 5 to 20 weight percent reinforcing filler having an aspect ratio of at least 5:1; and 0 to 1 weight percent of particulate filler having an aspect ratio less than 5:1; wherein all weight percents are based on the total weight of the composition.
A real-time engine management system comprising: a controller system configured to control demand on a first component of an engine , the controller system is configured to: access a first set of prognostic data about the first component , wherein the first set of prognostic data includes a remaining lifespan approximation of the first component operating at a present operating condition; identify a temporal length of an engine procedure operating at the present operating condition; alter a maximum current limit constant associated with the first component to increase the remaining lifespan approximation of the first component beyond the temporal length; implement the maximum current limit constant associated with the first component so that the first component does not fault during engine operation; characterized in that the controller system is further configured to alter a minimum current limit constant associated with the first component to increase the remaining lifespan approximation of the first component beyond the temporal length. access a first set of prognostic data about the first component , wherein the first set of prognostic data includes a remaining lifespan approximation of the first component operating at a present operating condition; identify a temporal length of an engine procedure operating at the present operating condition; alter a maximum current limit constant associated with the first component to increase the remaining lifespan approximation of the first component beyond the temporal length; implement the maximum current limit constant associated with the first component so that the first component does not fault during engine operation; characterized in that the controller system is further configured to alter a minimum current limit constant associated with the first component to increase the remaining lifespan approximation of the first component beyond the temporal length.
A filtering device for liquids, comprising - a first chamber having an inlet opening configured to receive liquid to be filtered, said first chamber is defined at least in part by a pair of walls configured to rotate around an axis of rotation (A), whereby the axis of rotation (A) joins centres of the walls and is arranged perpendicular to both walls ; - a second chamber having an outlet opening configured to drain the filtered liquid, said second chamber having a perimeter wall placed at a filtering area and circumferentially facing said walls of said first chamber , the perimeter wall comprising a grid for the passage of the filtered liquid; - the filtering area is placed between the first and the second chamber and configured to receive a filtering belt , the axis of rotation (A) being oriented perpendicular to an advancement direction (B) of the filtering belt , said walls each having a respective edge configured to be pressed tightly against said filtering belt to drag said filtering belt ; - suction means active downstream of the outlet opening , the second chamber being defined at least partially by an inner tank arranged under the first chamber , the perimeter wall being fluid-tightly connected to the inner tank characterised in that said grid extends over a surface equal to or less than 50% of the perimeter wall . - a first chamber having an inlet opening configured to receive liquid to be filtered, said first chamber is defined at least in part by a pair of walls configured to rotate around an axis of rotation (A), whereby the axis of rotation (A) joins centres of the walls and is arranged perpendicular to both walls ; - a second chamber having an outlet opening configured to drain the filtered liquid, said second chamber having a perimeter wall placed at a filtering area and circumferentially facing said walls of said first chamber , the perimeter wall comprising a grid for the passage of the filtered liquid; - the filtering area is placed between the first and the second chamber and configured to receive a filtering belt , the axis of rotation (A) being oriented perpendicular to an advancement direction (B) of the filtering belt , said walls each having a respective edge configured to be pressed tightly against said filtering belt to drag said filtering belt ; - suction means active downstream of the outlet opening , the second chamber being defined at least partially by an inner tank arranged under the first chamber , the perimeter wall being fluid-tightly connected to the inner tank
A cryogenic machining system comprising: a cryogenic fluid source ; a flow regulator downstream of the cryogenic fluid source ; a machining control unit ; at least one sensor downstream of the flow regulator , the at least one sensor configured to assess cryogenic fluid and transmit first data to the machining control unit ; a cutting tool downstream of the at least one sensor , wherein the cutting tool is configured to work on a surface of a work piece ; and an infrared sensor configured to assess the cutting tool at the surface of the work piece and communicate second data to the machine control unit ; wherein the machining control unit is configured to control the flow regulator in response to the first and second data and to control action and placement of the cutting tool . a cryogenic fluid source ; a flow regulator downstream of the cryogenic fluid source ; a machining control unit ; at least one sensor downstream of the flow regulator , the at least one sensor configured to assess cryogenic fluid and transmit first data to the machining control unit ; a cutting tool downstream of the at least one sensor , wherein the cutting tool is configured to work on a surface of a work piece ; and an infrared sensor configured to assess the cutting tool at the surface of the work piece and communicate second data to the machine control unit ; wherein the machining control unit is configured to control the flow regulator in response to the first and second data and to control action and placement of the cutting tool .
Ventilation device having at least one fan and cooling ribs, which fan is driven by a fan motor , and in which device at least the fan motor is supported on at least one bearing element , and the bearing element has a guide structure by which cooling air, moved with the aid of the fan , is positively guided over the cooling ribs of the heat sink of the fan motor , wherein the bearing element is made of silicone, and wherein the bearing element implements the guide structure for the cooling air in such a way that the cooling air is guided in a manner adapted to the structure of the heat sink , and the bearing element can be slipped over the heat sink and radially peripherally encloses the heat sink .
An implantable delivery device for delivery of a bioactive agent to a subject, the device comprising: a bioactive agent within or on the implantable delivery device; a wall having a surface; a plurality of nanostructures extending from the surface of the wall, and a plurality of microstructures extending from the surface of the wall; wherein the nanostructures have a cross-sectional dimension smaller than the microstructures; and wherein the plurality of nanostructures and plurality of microstructures are arranged in a fractal dimension of greater than 1. a bioactive agent within or on the implantable delivery device; a wall having a surface; a plurality of nanostructures extending from the surface of the wall, and a plurality of microstructures extending from the surface of the wall; wherein the nanostructures have a cross-sectional dimension smaller than the microstructures; and wherein the plurality of nanostructures and plurality of microstructures are arranged in a fractal dimension of greater than 1.