mhurhangee/patent-ind-claim-en huggingface dataset:
A process for cleaning raw product gas produced by gasifying a carbonaceous material, the process comprising: a) contacting the raw product gas with a flow of char or char-supported catalyst to reform organic contaminants in the raw product gas and to remove particulates, wherein the raw product gas flows in a direction perpendicular to the flow of the catalyst; and b) cooling the resulting product gas from step a) via heat exchange with a heat exchange medium in the presence of char or a solid adsorbent medium to condense remaining organic contaminants and inorganic contaminants on the char or solid adsorbent medium and to filter out fine particulates. a) contacting the raw product gas with a flow of char or char-supported catalyst to reform organic contaminants in the raw product gas and to remove particulates, wherein the raw product gas flows in a direction perpendicular to the flow of the catalyst; and b) cooling the resulting product gas from step a) via heat exchange with a heat exchange medium in the presence of char or a solid adsorbent medium to condense remaining organic contaminants and inorganic contaminants on the char or solid adsorbent medium and to filter out fine particulates.
A spectral sensor for near-infrared spectroscopy, which is used for distinguishing and/or recognizing objects and/or materials, wherein the spectral sensor comprises a computing device, a photosensor and a light source or a plurality of light sources for illuminating the object and/or material to be measured, wherein the spectral sensor is configured to operate in a learning mode , wherein the spectral sensor is configured to perform one or more measurements of intensity values of a first spectrum of wavelengths in the learning mode , wherein the spectral sensor is configured to determine the wavelengths of a second spectrum itself, wherein the second spectrum is fully included in the first spectrum but comprises fewer wavelengths than the first spectrum, wherein the spectral sensor is configured to select the wavelengths of the second spectrum with the aid of a machine learning method, characterized in that the spectral sensor is configured to operate in an operating mode and to carry out at least one measurement of intensity values of the second spectrum of wavelengths in the operating mode , with the spectral sensor being configured to collect only intensity values for wavelengths of the second spectrum in the operating mode , with the computing device enabling the learning mode and the operating mode. wherein the spectral sensor is configured to determine the wavelengths of a second spectrum itself, wherein the second spectrum is fully included in the first spectrum but comprises fewer wavelengths than the first spectrum, wherein the spectral sensor is configured to select the wavelengths of the second spectrum with the aid of a machine learning method, characterized in that the spectral sensor is configured to operate in an operating mode and to carry out at least one measurement of intensity values of the second spectrum of wavelengths in the operating mode , with the spectral sensor being configured to collect only intensity values for wavelengths of the second spectrum in the operating mode , with the computing device enabling the learning mode and the operating mode.
A method for manufacturing a spark plug , the spark plug comprising: a metal shell ; a rod-shaped ground electrode having a base end portion joined to the metal shell and a distal end portion located opposite the base end portion , the distal end portion including a tip weld surface and a distal end face ; and a tip welded to the tip weld surface of the distal end portion of the ground electrode , the method comprising: a welding step of welding the tip to the tip weld surface of the ground electrode ; and after the welding step, an image processing step of taking an image of the distal end face of the ground electrode and the tip with the use of reflected light and performing image processing on the taken image; characterised by a treatment step, after the welding step and before the image processing step, of performing polishing treatment or grinding treatment on at least a part of an edge region of the distal end face of the ground electrode . a welding step of welding the tip to the tip weld surface of the ground electrode ; and after the welding step, an image processing step of taking an image of the distal end face of the ground electrode and the tip with the use of reflected light and performing image processing on the taken image; characterised by a treatment step, after the welding step and before the image processing step, of performing polishing treatment or grinding treatment on at least a part of an edge region of the distal end face of the ground electrode .
A method of preparing a lysolecithin composition, the method comprising the steps of: (a) providing a lecithin mixture including a lecithin, water, and ethanol, wherein the lecithin contains phospholipids at least 60%, preferably at least 70% and more preferably at least 80%, by weight of the lecithin, and ethanol is present at 6 to 40%, preferably 10 to 15% by weight of the lecithin mixture; (b) adding phospholipase A1 or A2 to the lecithin mixture; and (c) allowing an enzymatic reaction to occur so that at least 70%, preferably at least 80% and more preferably at least 90%, of the phospholipids are converted to lysophospholipids to obtain the lysolecithin composition. (a) providing a lecithin mixture including a lecithin, water, and ethanol, wherein the lecithin contains phospholipids at least 60%, preferably at least 70% and more preferably at least 80%, by weight of the lecithin, and ethanol is present at 6 to 40%, preferably 10 to 15% by weight of the lecithin mixture; (b) adding phospholipase A1 or A2 to the lecithin mixture; and (c) allowing an enzymatic reaction to occur so that at least 70%, preferably at least 80% and more preferably at least 90%, of the phospholipids are converted to lysophospholipids to obtain the lysolecithin composition.
A method of detecting type I ice crystals using an onboard weather radar system of an aircraft, wherein type I ice crystals are found at altitudes between 9,000 and 40,000 feet, and/or when the ambient temperature is between -5 °C to -55 °C, and wherein type II ice crystals are found with and are associated with liquid water droplets in a convective cloud weather , the method comprising: at a processor , identifying radar returns having a return level signal strength less than a radar reflectivity display threshold which defines a minimum level of reflectivity signal strength returns that are displayed by the onboard weather radar system; determining if, for a region of airspace, at least one of a weather condition or a flight condition associated with the type I ice crystals exists in the region of airspace concurrently with the identified radar returns for the region of airspace having the return level signal strength less than the radar reflectivity display threshold level; and identifying the region of airspace as potentially having type I ice crystals when the at least one of the weather condition or the flight condition exists in the region of airspace concurrently with the identified radar returns for the region of airspace having the return level signal strength less than the the radar reflectivity display threshold level. at a processor , identifying radar returns having a return level signal strength less than a radar reflectivity display threshold which defines a minimum level of reflectivity signal strength returns that are displayed by the onboard weather radar system; determining if, for a region of airspace, at least one of a weather condition or a flight condition associated with the type I ice crystals exists in the region of airspace concurrently with the identified radar returns for the region of airspace having the return level signal strength less than the radar reflectivity display threshold level; and identifying the region of airspace as potentially having type I ice crystals when the at least one of the weather condition or the flight condition exists in the region of airspace concurrently with the identified radar returns for the region of airspace having the return level signal strength less than the the radar reflectivity display threshold level.
A power conversion device comprising: a power semiconductor (PM); a cooling fin configured to cool the power semiconductor; a first case disposed on the cooling fin, and including an opening (A) corresponding to a shape of the power semiconductor through which the power semiconductor is mounted on the cooling fin; and a second case configured to cover the power semiconductor mounted on the cooling fin, and comprising openings through which lead terminals of the power semiconductor pass; characterized in that the second case includes a projection that covers an opening (C) for gel injection provided in the power semiconductor between the lead terminals. a power semiconductor (PM); a cooling fin configured to cool the power semiconductor; a first case disposed on the cooling fin, and including an opening (A) corresponding to a shape of the power semiconductor through which the power semiconductor is mounted on the cooling fin; and a second case configured to cover the power semiconductor mounted on the cooling fin, and comprising openings through which lead terminals of the power semiconductor pass; characterized in that the second case includes a projection that covers an opening (C) for gel injection provided in the power semiconductor between the lead terminals.
A stent assembly, comprising: a. a stent jacket , comprising an expansible mesh structure, having a retracted state and a deployed state, and further wherein in the deployed state, the expansible mesh structure defines apertures and the mesh structure has a coverage area of less than 25%, wherein the expansible mesh structure is formed of fibers of a diameter between about 5 micrometers and about 25 micrometers, the diameter having a property of forming a substantially stable layer of endothelial cells, covering the fibers, thus reducing platelet aggregation, wherein in the deployed state the expansible mesh structure defines apertures having aperture diameters greater than 20 micrometers; and b. an expansible stent , operatively associated with the stent jacket , the stent jacket being located on the exterior of the expansible stent ; wherein the stent jacket is attached to the expansible stent using a sliding connection . a. a stent jacket , comprising an expansible mesh structure, having a retracted state and a deployed state, and further wherein in the deployed state, the expansible mesh structure defines apertures and the mesh structure has a coverage area of less than 25%, wherein the expansible mesh structure is formed of fibers of a diameter between about 5 micrometers and about 25 micrometers, the diameter having a property of forming a substantially stable layer of endothelial cells, covering the fibers, thus reducing platelet aggregation, wherein in the deployed state the expansible mesh structure defines apertures having aperture diameters greater than 20 micrometers; and b. an expansible stent , operatively associated with the stent jacket , the stent jacket being located on the exterior of the expansible stent ;
A cooking appliance, comprising: a cabinet including a cooking chamber and a rear space separated from cooking chamber by a partition surface ; a convection fan installed inside of the cooking chamber ; a fan motor installed outside of the cooking chamber and configured to rotate the convection fan ; a cooling fan installed outside of the cooking chamber for cooling the fan motor , the cooling fan configured to be rotated by the fan motor ; an exhaust duct connecting an inside of the cooking chamber to an outside of the cabinet ; and a duct connecting the outside of the cooking chamber and the exhaust duct , wherein an opening of the duct is disposed outside of the cooking chamber and opened toward the cooling fan ; characterized by : a broil burner inside the cooking chamber ; a mixing tube connected to the broil burner for supplying a mixture of air and gases to the broil burner , the mixing tube forming a flow path that passes through the partition surface and connects the broil burner and the duct ; and a blocking member for blocking a path of airflow from the opening to the cooling fan , the blocking member including a first blocking unit between the opening and the cooling fan . a cabinet including a cooking chamber and a rear space separated from cooking chamber by a partition surface ; a convection fan installed inside of the cooking chamber ; a fan motor installed outside of the cooking chamber and configured to rotate the convection fan ; a cooling fan installed outside of the cooking chamber for cooling the fan motor , the cooling fan configured to be rotated by the fan motor ; an exhaust duct connecting an inside of the cooking chamber to an outside of the cabinet ; and a duct connecting the outside of the cooking chamber and the exhaust duct , wherein an opening of the duct is disposed outside of the cooking chamber and opened toward the cooling fan ; characterized by : a broil burner inside the cooking chamber ; a mixing tube connected to the broil burner for supplying a mixture of air and gases to the broil burner , the mixing tube forming a flow path that passes through the partition surface and connects the broil burner and the duct ; and a blocking member for blocking a path of airflow from the opening to the cooling fan , the blocking member including a first blocking unit between the opening and the cooling fan . a broil burner inside the cooking chamber ; a mixing tube connected to the broil burner for supplying a mixture of air and gases to the broil burner , the mixing tube forming a flow path that passes through the partition surface and connects the broil burner and the duct ; and a blocking member for blocking a path of airflow from the opening to the cooling fan , the blocking member including a first blocking unit between the opening and the cooling fan .
A track vehicle having a steering system comprising: a mechanical connection to a hydro-mechanical steering unit ; a steering pump displacement control unit that controls output to a right track and a left track of the track vehicle from an input from the hydro-mechanical steering unit ,wherein the hydro-mechanical steering unit is hydraulically connected to the steering pump displacement control unit ; a steering pump mechanically connected to the steering pump displacement control unit ; and a steering motor hydraulically connected to the steering pump for varying output to the left and right tracks of the vehicle; characterised in that the steering system further comprises an electronic connection from at least one steering input sensor to a transmission control module and from the transmission control module to at least one electro-hydraulic control valve ; and the steering pump displacement control unit controls output to said right and left tracks of the track vehicle from simultaneous inputs from the hydro-mechanical steering unit and the at least one electro-hydraulic control valve , wherein both the hydro-mechanical steering unit and the at least one electro-hydraulic control valve are hydraulically connected to the steering pump displacement control unit . a mechanical connection to a hydro-mechanical steering unit ; a steering pump displacement control unit that controls output to a right track and a left track of the track vehicle from an input from the hydro-mechanical steering unit ,wherein the hydro-mechanical steering unit is hydraulically connected to the steering pump displacement control unit ; a steering pump mechanically connected to the steering pump displacement control unit ; and a steering motor hydraulically connected to the steering pump for varying output to the left and right tracks of the vehicle; characterised in that the steering system further comprises an electronic connection from at least one steering input sensor to a transmission control module and from the transmission control module to at least one electro-hydraulic control valve ; and the steering pump displacement control unit controls output to said right and left tracks of the track vehicle from simultaneous inputs from the hydro-mechanical steering unit and the at least one electro-hydraulic control valve , wherein both the hydro-mechanical steering unit and the at least one electro-hydraulic control valve are hydraulically connected to the steering pump displacement control unit .
Glass structural element, having a plastic-coated glass panel and at least one assembly element attached to the plastic-coated glass panel, the glass panel being coated over its full area with a silicone-based elastomer, and the coating at the same time producing an adhesive bond to a section of the assembly element that lies on the glass panel.
Tanning or retanning compound characterized by comprising an inclusion compound based on a cyclodextrin and at least one synthetic tanning agent
A power generation system for ships needing a maximum power for a bow thruster during entry and departure, comprising: a plurality of generators that supply power to an interior of a ship; a secondary battery that stores power output from the plurality of generators and supplies the stored power to the interior of the ship; a control device that, during normal sailing of the ship, causes a first generator among the plurality of generators and the secondary battery to supply power to the interior of the ship, and causes the secondary battery to charge so as to enable output power equivalent to that of the first generator during entry and departure, and a shaft generator provided in a rotary shaft of propulsion equipment of the ship, wherein the propulsion equipment is a main engine of the ship, and the rotary shaft transmits power of the main engine to a propeller . a plurality of generators that supply power to an interior of a ship; a secondary battery that stores power output from the plurality of generators and supplies the stored power to the interior of the ship; a control device that, during normal sailing of the ship, causes a first generator among the plurality of generators and the secondary battery to supply power to the interior of the ship, and causes the secondary battery to charge so as to enable output power equivalent to that of the first generator during entry and departure, and a shaft generator provided in a rotary shaft of propulsion equipment of the ship, wherein the propulsion equipment is a main engine of the ship, and the rotary shaft transmits power of the main engine to a propeller .
Method for masking surfaces to be matted, having the following steps: providing a workpiece having a surface to be matted; masking at least one region , not to be matted, of the surface with a first layer (S1) of a first coating material which is a water-based coating, masking the same region , not to be matted, with a second layer (S2) of a second coating material which is a solvent-based coating, wherein the first coating material is designed such that the first layer (S1) can be easily detached from the surface , wherein the second coating material is selected and applied such that high resistance of the second layer (S2) to a jet of abrasive material is achieved, said resistance being higher than the resistance of the first layer , wherein in at least one masking application a high second layer thickness (D2) of the second layer (S2) is achieved which is higher than a first layer thickness (D1) of the first layer . providing a workpiece having a surface to be matted; masking at least one region , not to be matted, of the surface with a first layer (S1) of a first coating material which is a water-based coating, masking the same region , not to be matted, with a second layer (S2) of a second coating material which is a solvent-based coating, wherein the first coating material is designed such that the first layer (S1) can be easily detached from the surface , wherein the second coating material is selected and applied such that high resistance of the second layer (S2) to a jet of abrasive material is achieved, said resistance being higher than the resistance of the first layer , wherein in at least one masking application a high second layer thickness (D2) of the second layer (S2) is achieved which is higher than a first layer thickness (D1) of the first layer .
An anti-canine PD-1 antibody that specifically binds to a canine PD-1 consisting of the amino acid sequence set forth in SEQ ID NO: 1, the anti-canine PD-1 antibody comprising: a heavy chain variable region comprising a CDR1 consisting of the amino acid sequence set forth in SEQ ID NO: 11, a CDR2 consisting of the amino acid sequence set forth in SEQ ID NO: 12, and a CDR 3 consisting of the amino acid sequence set forth in SEQ ID NO: 13; and a light chain variable region comprising a CDR1 consisting of the amino acid sequence set forth in SEQ ID NO: 14, a CDR2 consisting of the amino acid sequence set forth in SEQ ID NO: 15, and a CDR 3 consisting of the amino acid sequence set forth in SEQ ID NO: 16. a heavy chain variable region comprising a CDR1 consisting of the amino acid sequence set forth in SEQ ID NO: 11, a CDR2 consisting of the amino acid sequence set forth in SEQ ID NO: 12, and a CDR 3 consisting of the amino acid sequence set forth in SEQ ID NO: 13; and a light chain variable region comprising a CDR1 consisting of the amino acid sequence set forth in SEQ ID NO: 14, a CDR2 consisting of the amino acid sequence set forth in SEQ ID NO: 15, and a CDR 3 consisting of the amino acid sequence set forth in SEQ ID NO: 16.
A laminated magnetic core comprising: a plurality of magnetic layers ; and a plurality of interlamination layers disposed between the magnetic layers in an alternating fashion; a low deposition potential metal film deposited by pre-electrodeposition on each interlamination layer , wherein the low deposition potential metal film has a film thickness much smaller than a lamination thickness, wherein the interlamination layers comprise a partially conducting material having a conductivity greater than or equal to 10 -4 S/cm and less than or equal to 10 5 S/cm a plurality of magnetic layers ; and a plurality of interlamination layers disposed between the magnetic layers in an alternating fashion; a low deposition potential metal film deposited by pre-electrodeposition on each interlamination layer , wherein the low deposition potential metal film has a film thickness much smaller than a lamination thickness, wherein the interlamination layers comprise a partially conducting material having a conductivity greater than or equal to 10 -4 S/cm and less than or equal to 10 5 S/cm