mhurhangee/patent-ind-claim-en huggingface dataset:
A method of controlling powdery mildew, the method comprising applying nanobubble water to a plant, wherein the nanobubble water contains bubbles in an amount of from 1 × 10 8 to 1 × 10 10 bubbles/mL generated by a pressurized dissolution method, and wherein bubbles contained in the nanobubble water include oxygen where, the containing oxygen means to contain oxygen at a higher concentration than the oxygen concentration in the air. wherein the nanobubble water contains bubbles in an amount of from 1 × 10 8 to 1 × 10 10 bubbles/mL generated by a pressurized dissolution method, and wherein bubbles contained in the nanobubble water include oxygen where, the containing oxygen means to contain oxygen at a higher concentration than the oxygen concentration in the air.
A bumper beam (B) comprising a main cross member and a cross member part fixedly attached to said main cross member , wherein said cross member part forms in itself or together with one or more portions of the main cross member a closed chamber (C) in a cross section of the bumper beam, arranged at an upper side or at a lower side of said main cross member , characterized in that said closed chamber (C) abuts and extends over only a portion of said upper side or said lower side of said main cross member as seen in the cross direction of said main cross member and over essentially the entire length and in a longitudinal direction of said main cross member , that said main cross member together with said cross member part form a closed main chamber (M), and that said closed chamber (C) and said closed main chamber (M) are arranged abutting on each other.
A noise reduction air duct device for an autonomous cleaning device, the autonomous cleaning device comprising a body and a motor mounted on the body , the noise reduction air duct device being configured to be mounted on the body and the noise reduction air duct device comprising: an upper housing ; a lower housing ; and a support noise reduction structure , wherein the support noise reduction structure is made of an elastic material, the lower housing and the upper housing enclose to form an air duct , the air duct comprises an air inlet at a position corresponding to the motor , and the air duct comprises an air outlet at a side of the air duct away from the air inlet ; and the support noise reduction structure comprises a first end fixed on the lower housing , and a second end abutting against a lower surface of the upper housing , characterized in that along an airflow direction in the air duct , the air duct is divided into a first air duct and a second air duct downstream of the first air duct ; and a plurality of support noise reduction structures are mounted in the first air duct , the second air duct is provided with an airflow buffer and an exhaust port , a first end of the airflow buffer is connected to the first air duct , a second end of the airflow buffer is connected to a first end of the exhaust port , and a second end of the exhaust port is located at a position of the air outlet . an upper housing ; a lower housing ; and a support noise reduction structure , wherein the support noise reduction structure is made of an elastic material, the lower housing and the upper housing enclose to form an air duct , the air duct comprises an air inlet at a position corresponding to the motor , and the air duct comprises an air outlet at a side of the air duct away from the air inlet ; and the support noise reduction structure comprises a first end fixed on the lower housing , and a second end abutting against a lower surface of the upper housing , characterized in that along an airflow direction in the air duct , the air duct is divided into a first air duct and a second air duct downstream of the first air duct ; and a plurality of support noise reduction structures are mounted in the first air duct , the second air duct is provided with an airflow buffer and an exhaust port , a first end of the airflow buffer is connected to the first air duct , a second end of the airflow buffer is connected to a first end of the exhaust port , and a second end of the exhaust port is located at a position of the air outlet .
A routing control method, wherein a network device has a first routing entry and a second routing entry, an address prefix of the first routing entry is a first address prefix, an address prefix of the second routing entry is a second address prefix, a network segment to which the second address prefix belongs is a subset of a network segment to which the first address prefix belongs, a mask value in the second address prefix is greater than a mask value in the first address prefix, and the method comprises: a) obtaining , by a control module of the network device, a route suppression request; b) determining , by the control module , the second routing entry; and c) setting , by the control module , a state of the second routing entry to a non-delivery state, wherein the non-delivery state is used to indicate that the second routing entry does not need to be delivered to a forwarding table; and d) before setting the state of the second routing entry to the non-delivery state, determining that the first routing entry is in a delivery state in an active state; and e) delivering the first routing entry to the forwarding table after setting the state of the second routing entry to the non-delivery state. a) obtaining , by a control module of the network device, a route suppression request; b) determining , by the control module , the second routing entry; and c) setting , by the control module , a state of the second routing entry to a non-delivery state, wherein the non-delivery state is used to indicate that the second routing entry does not need to be delivered to a forwarding table; and d) before setting the state of the second routing entry to the non-delivery state, determining that the first routing entry is in a delivery state in an active state; and e) delivering the first routing entry to the forwarding table after setting the state of the second routing entry to the non-delivery state.
A method of preparing a molded product of a network of polymer coated filaments, the method comprising the steps of: providing a plastic foil having a first face and a second face; laying a plurality of sisal filaments on either the first face or the second face of the foil to form an interconnected network of filaments, the filaments measuring on average 90 cm in length and having a diameter of 25 μm, the filaments being laid on the foil with an average density of 350 filaments/m 2 ; rolling flat the plurality of filaments on the foil such that the filaments are entangled within the interconnected network in a configuration which allows air circulation between at least two or more of the filaments; separating the foil from the network of filaments as the network of filaments is fed into a container holding an emulsion of polymer molecules comprising latex rubber in an aqueous medium; coating the network of filaments with an emulsion of polymer molecules in an aqueous medium to form a coated network; drying the coated network by allowing air circulation between the interconnected network of filaments to form a network of polymer coated filaments; and shaping the network of polymer coated filaments to form the molded product. providing a plastic foil having a first face and a second face; laying a plurality of sisal filaments on either the first face or the second face of the foil to form an interconnected network of filaments, the filaments measuring on average 90 cm in length and having a diameter of 25 μm, the filaments being laid on the foil with an average density of 350 filaments/m 2 ; rolling flat the plurality of filaments on the foil such that the filaments are entangled within the interconnected network in a configuration which allows air circulation between at least two or more of the filaments; separating the foil from the network of filaments as the network of filaments is fed into a container holding an emulsion of polymer molecules comprising latex rubber in an aqueous medium; coating the network of filaments with an emulsion of polymer molecules in an aqueous medium to form a coated network; drying the coated network by allowing air circulation between the interconnected network of filaments to form a network of polymer coated filaments; and shaping the network of polymer coated filaments to form the molded product.
A printing system , comprising: a print engine ; a print engine controller operatively connected to the print engine to print, on a single substrate web : graphics for multiple different layouts of corrugated boxes to be lined with the web , and machine readable images (44A-44D; 50A-50F) representing corrugator control information for making the multiple different layouts of boxes, characterized in that the corrugator control information includes registration marks depicting positional information to be used for dynamically adjusting a position of a corrugated board and/or cutting and creasing dies for each of the different layouts . a print engine ; a print engine controller operatively connected to the print engine to print, on a single substrate web : graphics for multiple different layouts of corrugated boxes to be lined with the web , and machine readable images (44A-44D; 50A-50F) representing corrugator control information for making the multiple different layouts of boxes, characterized in that the corrugator control information includes registration marks depicting positional information to be used for dynamically adjusting a position of a corrugated board and/or cutting and creasing dies for each of the different layouts .
An aircraft with a fuselage and at least one emergency exit system , the at least one emergency exit system comprising: a jettisonable component that is: - accommodated and locked in an associated frame structure of the aircraft in normal operation mode, and - releasable from the associated frame structure for being jettisoned from the aircraft in an emergency mode; and an emergency evacuation assistance device that is adapted to assist in an emergency evacuation of the aircraft via the associated frame structure in the emergency mode; characterized in that the jettisonable component is at least provided with an inner operating device and an outer operating device , the inner and outer operating devices (6a; 6b) being arranged on opposed sides of the jettisonable component and is operable from inside and outside of the aircraft for being released from the associated frame structure , wherein the emergency evacuation assistance device is attached to the jettisonable component such that the emergency evacuation assistance device is deployed by means of the jettisonable component when the jettisonable component is jettisoned from the aircraft in the emergency mode; and wherein the emergency evacuation assistance device is stored in the associated frame structure of the aircraft in the normal operation mode, and deployed from the associated frame structure by means of the jettisonable component when the jettisonable component is jettisoned from the aircraft in the emergency mode. a jettisonable component that is: - accommodated and locked in an associated frame structure of the aircraft in normal operation mode, and - releasable from the associated frame structure for being jettisoned from the aircraft in an emergency mode; and - accommodated and locked in an associated frame structure of the aircraft in normal operation mode, and - releasable from the associated frame structure for being jettisoned from the aircraft in an emergency mode; and an emergency evacuation assistance device that is adapted to assist in an emergency evacuation of the aircraft via the associated frame structure in the emergency mode; characterized in that the jettisonable component is at least provided with an inner operating device and an outer operating device , the inner and outer operating devices (6a; 6b) being arranged on opposed sides of the jettisonable component and is operable from inside and outside of the aircraft for being released from the associated frame structure , wherein the emergency evacuation assistance device is attached to the jettisonable component such that the emergency evacuation assistance device is deployed by means of the jettisonable component when the jettisonable component is jettisoned from the aircraft in the emergency mode; and wherein the emergency evacuation assistance device is stored in the associated frame structure of the aircraft in the normal operation mode, and deployed from the associated frame structure by means of the jettisonable component when the jettisonable component is jettisoned from the aircraft in the emergency mode.
A system for storing and producing air-free hypochlorous acid (HOCI), the system comprising: a container from which air has been purged, the container comprising a first compartment, comprising a mixture of sodium hypochlorite (NaOCI) and water, a separate second compartment comprising a mixture of an organic acid and water, and a separate third compartment for receiving contents of the first and second compartments, wherein each of the first, second, and third compartments comprises a wall forming an exterior of the container; a first one-way valve that permits fluid flow in a direction from the first compartment towards the third compartment; and a second one-way valve that permits fluid flow in a direction from the second compartment towards the third compartment; wherein the first and second one-way valves permit flow from the first and second compartments into the third compartment in response to an increase in pressure within the first and second compartments and the first and second compartments comprise walls of a flexible material configured to allow an increase in internal pressure of the first and second compartments in response to a force directly administered to respective walls of the first and second compartments forming the exterior of the container. a container from which air has been purged, the container comprising a first compartment, comprising a mixture of sodium hypochlorite (NaOCI) and water, a separate second compartment comprising a mixture of an organic acid and water, and a separate third compartment for receiving contents of the first and second compartments, wherein each of the first, second, and third compartments comprises a wall forming an exterior of the container; a first one-way valve that permits fluid flow in a direction from the first compartment towards the third compartment; and a second one-way valve that permits fluid flow in a direction from the second compartment towards the third compartment; wherein the first and second one-way valves permit flow from the first and second compartments into the third compartment in response to an increase in pressure within the first and second compartments and the first and second compartments comprise walls of a flexible material configured to allow an increase in internal pressure of the first and second compartments in response to a force directly administered to respective walls of the first and second compartments forming the exterior of the container.
A method for reconstructing a hyperspectral image, the method comprising: obtaining a dispersion model for dispersion created by a prism included in a camera, the camera including no coded aperture; aligning an input dispersed captured image obtained through the prism to obtain edge information without dispersion; wherein the captured image is an image captured without passing through a coded aperture; estimating spectral information based on the obtained edge information and the dispersion model; and reconstructing a hyperspectral image corresponding to a captured image based on the dispersion model and the estimated spectral information; characterized in that the obtaining of the edge information comprises: computing a difference between unnormalized gradient values of adjacent spectral channels in the captured image; performing spatial alignment between spectral channels; projecting an aligned spectral image onto RGB channels via a response function of the camera; and obtaining the edge information using an edge detector. obtaining a dispersion model for dispersion created by a prism included in a camera, the camera including no coded aperture; aligning an input dispersed captured image obtained through the prism to obtain edge information without dispersion; wherein the captured image is an image captured without passing through a coded aperture; estimating spectral information based on the obtained edge information and the dispersion model; and reconstructing a hyperspectral image corresponding to a captured image based on the dispersion model and the estimated spectral information; characterized in that the obtaining of the edge information comprises: computing a difference between unnormalized gradient values of adjacent spectral channels in the captured image; performing spatial alignment between spectral channels; projecting an aligned spectral image onto RGB channels via a response function of the camera; and obtaining the edge information using an edge detector. computing a difference between unnormalized gradient values of adjacent spectral channels in the captured image; performing spatial alignment between spectral channels; projecting an aligned spectral image onto RGB channels via a response function of the camera; and obtaining the edge information using an edge detector.
A barrel for a barrel joint for parts of furniture and furnishing items comprising a hollow cylindrical body containing a blocking element , said cylindrical body providing, on its side surface, at least one hole for receiving a pin of the barrel joint, and being provided with an internal threading in which said blocking element is screwed in the form of a grub screw , characterized in that said hollow cylindrical body provides at least one further hole on its side surface, for the passage of a tip of a tool suitable for acting on a peripheral toothing of the grub screw .
A composition comprising: a silk polypeptide wherein at least a portion of the silk polypeptide has a coiled coil structure, wherein the silk polypeptide comprises at least 5 copies of the heptad sequence abcdefg, and wherein at least 25% of the amino acids at position a in the heptad repeats are alanine; and a chelate comprising a chelating agent and a metal ion; wherein the chelate is bound to at least one amino acid in the core of the coiled coil; and wherein the chelating agent is not a polypeptide. a silk polypeptide wherein at least a portion of the silk polypeptide has a coiled coil structure, wherein the silk polypeptide comprises at least 5 copies of the heptad sequence abcdefg, and wherein at least 25% of the amino acids at position a in the heptad repeats are alanine; and a chelate comprising a chelating agent and a metal ion; wherein the chelate is bound to at least one amino acid in the core of the coiled coil; and wherein the chelating agent is not a polypeptide.
Dryer for drying coated fiber webs, wherein the dryer comprises three air compartments configured to provide drying air blows towards passing fiber web (W), wherein two of the air compartments are substantially rectangular chambers and located next to each other with two longitudinal back sides towards each other, wherein said third air compartment is a turning air compartment located with a straight surface towards ends of the two rectangular air compartments and having a substantially curved outer, advantageously semi-circular, outer surface, wherein the dryer is configured to form a first longitudinal drying run for the fiber web (W) in a first vertical portion , a curved drying run for the fiber web (W) in a turning portion and a second longitudinal drying run for the fiber web (W) in a second vertical portion , wherein the dryer further comprises along the vertical portions at a distance from the air compartments at least one blow device configured to provide support air blows to support the run of the passing fiber web (W), characterized in that the rectangular air compartments comprise an inlet channel and two outlet channels and that the inlet channel is located in between the outlet channels in length direction of the rectangular air compartment . wherein two of the air compartments are substantially rectangular chambers and located next to each other with two longitudinal back sides towards each other, wherein said third air compartment is a turning air compartment located with a straight surface towards ends of the two rectangular air compartments and having a substantially curved outer, advantageously semi-circular, outer surface, wherein the dryer is configured to form a first longitudinal drying run for the fiber web (W) in a first vertical portion , a curved drying run for the fiber web (W) in a turning portion and a second longitudinal drying run for the fiber web (W) in a second vertical portion , wherein the dryer further comprises along the vertical portions at a distance from the air compartments at least one blow device configured to provide support air blows to support the run of the passing fiber web (W), characterized in that the rectangular air compartments comprise an inlet channel and two outlet channels and that the inlet channel is located in between the outlet channels in length direction of the rectangular air compartment .
A three-dimensional imaging method, comprising the following steps: S1) determining, on a scanning object, a scanning range covering a portion comprising a scanning target for a three-dimensional scanning; S2) on a basis of the scanning range of the scanning object, extracting an existing initial three-dimensional structure of the scanning target from a database; S3) scanning the portion comprising the scanning target within the given scanning range from various angles to form a series of two-dimensional images with different spatial location and orientation information; S4) according to image information related to the scanning target or a local portion of the scanning target within the series of two-dimensional images, adjusting the initial three-dimensional structure of the scanning target or the local portion of the scanning target; S5) repeating steps S3) and S4) until the whole initial three-dimensional structure of the scanning target has been scanned over and is adjusted, based on the obtained two-dimensional images, and an overall three-dimensional structure image of the target is formed S6) continuously displaying the initial three-dimensional structure of the scanning target and the adjusted three-dimensional structure image during the two-dimensional scanning imaging process on a display device ; S7) displaying the final three-dimensional structure image of the scanning target after the adjustments. S1) determining, on a scanning object, a scanning range covering a portion comprising a scanning target for a three-dimensional scanning; S2) on a basis of the scanning range of the scanning object, extracting an existing initial three-dimensional structure of the scanning target from a database; S3) scanning the portion comprising the scanning target within the given scanning range from various angles to form a series of two-dimensional images with different spatial location and orientation information; S4) according to image information related to the scanning target or a local portion of the scanning target within the series of two-dimensional images, adjusting the initial three-dimensional structure of the scanning target or the local portion of the scanning target; S5) repeating steps S3) and S4) until the whole initial three-dimensional structure of the scanning target has been scanned over and is adjusted, based on the obtained two-dimensional images, and an overall three-dimensional structure image of the target is formed S6) continuously displaying the initial three-dimensional structure of the scanning target and the adjusted three-dimensional structure image during the two-dimensional scanning imaging process on a display device ; S7) displaying the final three-dimensional structure image of the scanning target after the adjustments.