mhurhangee/patent-ind-claim-en huggingface dataset:
A flow sensor comprising: a first silicon block comprising: a top surface, a bottom surface, a passage extending from the top surface to the bottom surface and an opening in the top surface formed by the passage ; a sense resistor located on or in the top surface; and a refractory resistor located on or in the top surface and apart from the sense resistor ; and a second silicon block attached to the first silicon block to provide a channel to direct a gas flow across the top surface of the first silicon block ; characterized in that the sense resistor and the refractory resistor are circumferentially located around the opening in the top surface, wherein the channel and the passage define a flow path for gas or other fluid through the sensor between the channel and the passage. a first silicon block comprising: a top surface, a bottom surface, a passage extending from the top surface to the bottom surface and an opening in the top surface formed by the passage ; a sense resistor located on or in the top surface; and a refractory resistor located on or in the top surface and apart from the sense resistor ; and a top surface, a bottom surface, a passage extending from the top surface to the bottom surface and an opening in the top surface formed by the passage ; a sense resistor located on or in the top surface; and a refractory resistor located on or in the top surface and apart from the sense resistor ; and a second silicon block attached to the first silicon block to provide a channel to direct a gas flow across the top surface of the first silicon block ; characterized in that the sense resistor and the refractory resistor are circumferentially located around the opening in the top surface, wherein the channel and the passage define a flow path for gas or other fluid through the sensor between the channel and the passage.
Conveying apparatus for conveying a tire layer , wherein the conveying apparatus comprises a swivel conveyor with at least one endless belt or wire and a first pulley , a second pulley and a third pulley that define a minimal loop (L) for guiding said at least one endless belt or wire along a conveying run and a return run , wherein the first pulley defines at least a first part of the conveying run , wherein the second pulley defines at least a first part of the return run and wherein the third pulley is arranged between the first part of the conveying run and the first part of the return run , wherein the third pulley is swivable with respect to the first pulley and the second pulley about a swivel axis (X) that is located at a pivot position (Y) spaced apart from the third pulley towards the first pulley and the second pulley , wherein the third pulley is swivable about said swivel axis (X) between a first swivel position and a second swivel position to align the first part of the conveying run with a first conveying plane (H1) and a second conveying plane (H2), respectively, wherein the minimal loop (L) has a length, wherein the pivot position (Y) is chosen such that the length of the minimal loop (L) when the third pulley is in the first swivel position is the same within a tolerance of less than 1 percent with respect to the length of the minimal loop (L) when the third pulley is in the second swivel position.
A method in a network node configured to communicate with a wireless device, the network node comprising a time domain beamformer , the method comprising: filtering (S10) each signal output by the time domain beamformer by a band stop filter , the band stop filter including a stop band overlapping a pass band of the signal output by the time domain beamformer ; filtering (S12) each signal output by the time domain beamformer by a group delay filter in electrical parallel with the band stop filter , the group delay filter providing a group delay to the signal output by the time domain beamformer ; and subtracting (S14) an output of each band stop filter from an output of a corresponding group delay filter . filtering (S10) each signal output by the time domain beamformer by a band stop filter , the band stop filter including a stop band overlapping a pass band of the signal output by the time domain beamformer ; filtering (S12) each signal output by the time domain beamformer by a group delay filter in electrical parallel with the band stop filter , the group delay filter providing a group delay to the signal output by the time domain beamformer ; and subtracting (S14) an output of each band stop filter from an output of a corresponding group delay filter .
A stratified scavenging engine comprising: a cylinder having a cylinder bore ; and a piston stored in the cylinder bore to be movable in a reciprocating manner, the cylinder having an intake port to intake leading air and a scavenging port to scavenge combustion gas, the intake port and the scavenging port being open to the cylinder bore , wherein the piston has a peripheral surface including a piston groove to guide leading air from the intake port to the scavenging port , and the piston groove has a recess near the intake port , wherein the piston groove has a bottom face , and the recess is formed on the bottom face near the intake port , wherein the piston groove has a first border and a second border as a pair on the bottom face with the peripheral surface of the piston , and the recess is formed in a predetermined range from the first border near the intake port as an origin, whereby the recess has a deepest part that is close to the first border , characterised in that the recess has an erected wall surface having a steep rising angle from the deepest part to the first border and an inclined face having a gently rising angle from the deepest part to the second border , whereby said steep and gently rising angles indicate the inclinations relative to the tangential direction of the deepest part , to generate a swirling flow (V) around the recess , when leading air returning from the scavenging port to the piston groove is guided along the inclined face to the erected wall surface , the piston has a peripheral surface including a piston groove to guide leading air from the intake port to the scavenging port , and the piston groove has a recess near the intake port , wherein the piston groove has a bottom face , and the recess is formed on the bottom face near the intake port , wherein the piston groove has a first border and a second border as a pair on the bottom face with the peripheral surface of the piston , and the recess is formed in a predetermined range from the first border near the intake port as an origin, whereby the recess has a deepest part that is close to the first border , characterised in that the recess has an erected wall surface having a steep rising angle from the deepest part to the first border and an inclined face having a gently rising angle from the deepest part to the second border , whereby said steep and gently rising angles indicate the inclinations relative to the tangential direction of the deepest part , to generate a swirling flow (V) around the recess , when leading air returning from the scavenging port to the piston groove is guided along the inclined face to the erected wall surface ,
A method for the production of a transparent conductive carbon film comprising the steps (i) coating of a solution of discotic precursors onto a substrate and (ii) heating the coated substrate under a protective gas to a temperature of from 400-2000°C, wherein the produced transparent carbon film has a transmittance in the range of 60-95%, for a carbon film having a thickness of 30 nm-4 nm at a wavelength of 700 nm and wherein the produced carbon film has a sheet resistance of at most 30 kohm/sq, and wherein the discotic precursors are selected from superphenalenes, hexabenzocoronenes (HBC), ovalenes, coronenes, perylenes, pyrenes, and their derivatives; pitches, heavy oils from coal or petroleum; or exfoliated graphite from chemical or physical exfoliation of any graphite or from graphite oxide. (i) coating of a solution of discotic precursors onto a substrate and (ii) heating the coated substrate under a protective gas to a temperature of from 400-2000°C, wherein the produced transparent carbon film has a transmittance in the range of 60-95%, for a carbon film having a thickness of 30 nm-4 nm at a wavelength of 700 nm and wherein the produced carbon film has a sheet resistance of at most 30 kohm/sq, and wherein the discotic precursors are selected from superphenalenes, hexabenzocoronenes (HBC), ovalenes, coronenes, perylenes, pyrenes, and their derivatives; pitches, heavy oils from coal or petroleum; or exfoliated graphite from chemical or physical exfoliation of any graphite or from graphite oxide.
Cooling system with icing protection for a coolant flowing in a cooling circuit of the cooling system , comprising: - a heat source which releases waste heat to the coolant in the cooling circuit and heats the coolant; - a first heat exchanger which is configured to extract heat energy from the coolant heated by the heat source , wherein the first heat exchanger uses a first fluid flow as a heat sink; - a second heat exchanger which is configured to extract heat energy from the coolant heated by the heat source , wherein the second heat exchanger uses a second fluid flow , which is different from the first fluid flow , as a heat sink; and - a conveying device which is configured to feed the coolant to the first heat exchanger and to the second heat exchanger , characterized by : - a valve which is configured to regulate a volume flow of the coolant which is fed to the second heat exchanger ; - at least one temperature sensor (121-125) which is configured to measure a temperature of the coolant downstream of the first heat exchanger and/or the second heat exchanger ; and - a control unit which is configured to control a conveying rate of the conveying device , and/or the volume flow regulated by the valve , in such a way that the temperature measured by the temperature sensor (121-125) does not fall below a threshold value corresponding to a predefined viscosity of the coolant. - a heat source which releases waste heat to the coolant in the cooling circuit and heats the coolant; - a first heat exchanger which is configured to extract heat energy from the coolant heated by the heat source , wherein the first heat exchanger uses a first fluid flow as a heat sink; - a second heat exchanger which is configured to extract heat energy from the coolant heated by the heat source , wherein the second heat exchanger uses a second fluid flow , which is different from the first fluid flow , as a heat sink; and - a conveying device which is configured to feed the coolant to the first heat exchanger and to the second heat exchanger , - a valve which is configured to regulate a volume flow of the coolant which is fed to the second heat exchanger ; - at least one temperature sensor (121-125) which is configured to measure a temperature of the coolant downstream of the first heat exchanger and/or the second heat exchanger ; and - a control unit which is configured to control a conveying rate of the conveying device , and/or the volume flow regulated by the valve , in such a way that the temperature measured by the temperature sensor (121-125) does not fall below a threshold value corresponding to a predefined viscosity of the coolant.
A ceramic tile comprising: a substrate; and a surface coating comprising a base formula comprising a glaze; characterized in that the surface coating comprises solid particles comprising alumina-zirconium-silicate and wherein the solid particles make up from 1% to 25% of the weight of the surface coating and wherein between the 40% and 95% by weight of the solid particles are alumina-zirconium silicate. a substrate; and a surface coating comprising a base formula comprising a glaze; characterized in that the surface coating comprises solid particles comprising alumina-zirconium-silicate and wherein the solid particles make up from 1% to 25% of the weight of the surface coating and wherein between the 40% and 95% by weight of the solid particles are alumina-zirconium silicate.
A display method of a multimedia apparatus (100; 300), the display method comprising: acquiring exercise information of a user which includes an exercise speed (S810); transmitting the exercise information to a server (S820); in response to transmitting the exercise information, receiving from the server a transport stream comprising video data in which a screen is changed at a rate; and displaying the video data by processing the transport stream (S860), wherein, if the exercise speed is in a preset range of a recommended exercise criterion which is determined based on physical information of the user, the rate is in proportion to the exercise speed, wherein, if the exercise speed is outside the preset range of the recommended exercise criterion, the rate corresponds to the recommended exercise criterion, and wherein the displaying comprises, if the exercise speed is outside the preset range of the recommended exercise criterion, displaying a guidance message for the recommended exercise criterion. acquiring exercise information of a user which includes an exercise speed (S810); transmitting the exercise information to a server (S820); in response to transmitting the exercise information, receiving from the server a transport stream comprising video data in which a screen is changed at a rate; and displaying the video data by processing the transport stream (S860), wherein, if the exercise speed is in a preset range of a recommended exercise criterion which is determined based on physical information of the user, the rate is in proportion to the exercise speed, wherein, if the exercise speed is outside the preset range of the recommended exercise criterion, the rate corresponds to the recommended exercise criterion, and wherein the displaying comprises, if the exercise speed is outside the preset range of the recommended exercise criterion, displaying a guidance message for the recommended exercise criterion.
Power distributor having a housing and a mounting plate , which is arranged within the housing, for mounting electrical functional components , wherein the mounting plate comprises a front side for arranging the electrical functional components and a rear side facing a housing rear wall and located opposite the front side , wherein the mounting plate comprises, starting from the front side , a plurality of contacting recesses extending in the direction of the rear side , wherein electrical contacting elements for making contact with electrical functional components are arranged in the region of the contacting recesses , wherein individual contacting elements are electrically conductively connected to one another by means of electrical connecting conductors , wherein the connecting conductors are arranged between the rear side of the mounting plate and the housing rear wall and wherein the connecting conductors are respectively a wire or a cable and the contacting elements are respectively an end section of a connecting conductor , wherein the end section is guided through the associated contacting recess from the rear side of the mounting plate and protrudes from the front side of the mounting plate , characterised in that a plurality of end sections of a plurality of connecting conductors which are arranged next to one another are connected to one another by a dimensionally stable connecting device and can be displaced together by displacing the connecting device .
A gas turbine engine comprising: a front center body case structure defining a core flow path for a core airflow; a geared architecture at least partially supported by said front center body case structure ; an inner shaft that drives a fan through said geared architecture ; an outer shaft ; a low pressure compressor along an axis (A), said low pressure compressor including a plurality of stages; a first bearing system (138-2) which at least partially supports said inner shaft along said axis (A), said first bearing system (138-2) mounted to said front center body case structure ; a coupling shaft mounted to said inner shaft and said geared architecture , said coupling shaft at least partially supported by said first bearing system (138-2); a second bearing system (138-3) which at least partially supports said outer shaft along said axis (A); and a low pressure compressor hub mounted to said inner shaft , wherein said low pressure compressor hub extends to said low pressure compressor between said first bearing system (138-2) and said second bearing system (138-3), said low pressure compressor hub including a frustoconical web which extends between said first bearing system (138-2) and said second bearing system (138-3), characterised in that said low pressure compressor hub further includes a tubular hub mounted to said inner shaft adjacent said first bearing system (138-2), said frustoconical web extending in a forwardly direction from the tubular hub axially between the first bearing system (138-2) and the second bearing system (138-3). a front center body case structure defining a core flow path for a core airflow; a geared architecture at least partially supported by said front center body case structure ; an inner shaft that drives a fan through said geared architecture ; an outer shaft ; a low pressure compressor along an axis (A), said low pressure compressor including a plurality of stages; a first bearing system (138-2) which at least partially supports said inner shaft along said axis (A), said first bearing system (138-2) mounted to said front center body case structure ; a coupling shaft mounted to said inner shaft and said geared architecture , said coupling shaft at least partially supported by said first bearing system (138-2); a second bearing system (138-3) which at least partially supports said outer shaft along said axis (A); and a low pressure compressor hub mounted to said inner shaft , wherein said low pressure compressor hub extends to said low pressure compressor between said first bearing system (138-2) and said second bearing system (138-3), said low pressure compressor hub including a frustoconical web which extends between said first bearing system (138-2) and said second bearing system (138-3), characterised in that said low pressure compressor hub further includes a tubular hub mounted to said inner shaft adjacent said first bearing system (138-2), said frustoconical web extending in a forwardly direction from the tubular hub axially between the first bearing system (138-2) and the second bearing system (138-3).
A lithium ion secondary battery comprising a negative electrode, a positive electrode and a separator interposed between the negative electrode and the positive electrode, wherein the negative electrode comprises a negative electrode active material comprising Si and/or Sn, or an oxide thereof; and wherein the separator comprises composite particles (A); the composite particles (A) comprise a core portion comprising lithium composite metal oxide particles and a shell portion comprising a carbonaceous material with which the core surface is coated at least partially; the composite particles (A) cause lithium deintercalation at 0.1 V to 2.5 V (vs. Li + /Li); wherein the separator comprises, as lithium composite metal oxide particles, any one selected from the group consisting of lithium phosphate (Li 3 PO 4 ), lithium titanium phosphate (Li x Ti y (PO 4 ) 3 , 0 < x < 2, 0 < y < 3), lithium aluminum titanium phosphate (Li x Al y Ti z (PO4) 3 , 0 < x < 2, 0 < y < 1, 0 < z < 3), (LiAlTiP) x O y -based glass (0 < x < 4, 0 < y < 13), lithium lanthanum titanate (Li x La y TiO 3 , 0 < x < 2, 0 < y < 3), lithium germanium thiophosphate (LixGe y P z S w , 0 < x < 4, 0 < y < 1, 0 < z < 1, 0 < w < 5), lithium nitride (Li x N y , 0 < x < 4, 0 < y < 2), SiS 2 (Li x Si y S z , 0 < x < 3, 0 < y < 2, 0 < z < 4)-based glass and P 2 S 5 (Li x P y S z , 0 < x < 3, 0 < y < 3, 0 < z < 7)-based glass, or a combination of two or more of them; the battery has a positive electrode potential of 3 V or more (vs. Li + /Li); and the battery has a driving voltage of 2.5 V to 4.5 V. wherein the negative electrode comprises a negative electrode active material comprising Si and/or Sn, or an oxide thereof; and wherein the separator comprises composite particles (A); the composite particles (A) comprise a core portion comprising lithium composite metal oxide particles and a shell portion comprising a carbonaceous material with which the core surface is coated at least partially; the composite particles (A) cause lithium deintercalation at 0.1 V to 2.5 V (vs. Li + /Li); wherein the separator comprises, as lithium composite metal oxide particles, any one selected from the group consisting of lithium phosphate (Li 3 PO 4 ), lithium titanium phosphate (Li x Ti y (PO 4 ) 3 , 0 < x < 2, 0 < y < 3), lithium aluminum titanium phosphate (Li x Al y Ti z (PO4) 3 , 0 < x < 2, 0 < y < 1, 0 < z < 3), (LiAlTiP) x O y -based glass (0 < x < 4, 0 < y < 13), lithium lanthanum titanate (Li x La y TiO 3 , 0 < x < 2, 0 < y < 3), lithium germanium thiophosphate (LixGe y P z S w , 0 < x < 4, 0 < y < 1, 0 < z < 1, 0 < w < 5), lithium nitride (Li x N y , 0 < x < 4, 0 < y < 2), SiS 2 (Li x Si y S z , 0 < x < 3, 0 < y < 2, 0 < z < 4)-based glass and P 2 S 5 (Li x P y S z , 0 < x < 3, 0 < y < 3, 0 < z < 7)-based glass, or a combination of two or more of them; the battery has a positive electrode potential of 3 V or more (vs. Li + /Li); and the battery has a driving voltage of 2.5 V to 4.5 V.