mhurhangee/patent-ind-claim-en huggingface dataset:
A vane assembly in a duct comprising: a plurality of vanes arranged circumferentially about an axis (A) defined by the duct , the duct being an airflow or gas path duct; wherein each of said plurality of vanes has a throat distance defining a shortest distance between the vane and an adjacent vane at a constant span; wherein a line drawn along the throat distance defines a throat angle relative to a circumferential line that is tangential to a trailing edge of each of said plurality of vanes ; characterized in that : the throat angle of each vane at its mid-span region of 45 to 55% span is greater than the throat angle at its tip region of 95% to 100% span and greater than the throat angle at its root region of 0% to 5% span wherein, as a result thereof, an airflow at an outer diameter and an airflow at an inner diameter of said vane assembly are elevated relative to an airflow at a mid span region of the vane assembly; and wherein the throat root angle has a low root throat angle at 0% span and increases at a constant rate as a percentage span increases from 0% span to 45% to 55% span , and decreases again at a constant rate as the percentage span increases from 45% to 55% span to 100% span . a plurality of vanes arranged circumferentially about an axis (A) defined by the duct , the duct being an airflow or gas path duct; wherein each of said plurality of vanes has a throat distance defining a shortest distance between the vane and an adjacent vane at a constant span; wherein a line drawn along the throat distance defines a throat angle relative to a circumferential line that is tangential to a trailing edge of each of said plurality of vanes ; characterized in that : the throat angle of each vane at its mid-span region of 45 to 55% span is greater than the throat angle at its tip region of 95% to 100% span and greater than the throat angle at its root region of 0% to 5% span wherein, as a result thereof, an airflow at an outer diameter and an airflow at an inner diameter of said vane assembly are elevated relative to an airflow at a mid span region of the vane assembly; and wherein the throat root angle has a low root throat angle at 0% span and increases at a constant rate as a percentage span increases from 0% span to 45% to 55% span , and decreases again at a constant rate as the percentage span increases from 45% to 55% span to 100% span . the throat angle of each vane at its mid-span region of 45 to 55% span is greater than the throat angle at its tip region of 95% to 100% span and greater than the throat angle at its root region of 0% to 5% span wherein, as a result thereof, an airflow at an outer diameter and an airflow at an inner diameter of said vane assembly are elevated relative to an airflow at a mid span region of the vane assembly; and wherein the throat root angle has a low root throat angle at 0% span and increases at a constant rate as a percentage span increases from 0% span to 45% to 55% span , and decreases again at a constant rate as the percentage span increases from 45% to 55% span to 100% span .
A hot stamped steel material, characterized in that , the hot stamped steel material comprises the following components by weight: 0.27 to 0.40% of C; 0.2 to 3.0% of Mn; 0.11 to 0.4% of V; 0 to 0.8% of Si; 0 to 0.5% of Al; 0 to 2% of Cr; 0 to 0.15% of Ti; 0 to 0.15 of Nb; 0 to 0.004% of B; the content of Mo, Ni, Cu in combination amounts a total of less than 2%; and inevitable impurity elements, wherein the balance consists of Fe, the hot stamped steel material having a yield strength of 1300 MPa to 1700 MPa, a tensile strength of 1800 to 2200 MPa, and an elongation of 6 to 9% without tempering. 0.27 to 0.40% of C; 0.2 to 3.0% of Mn; 0.11 to 0.4% of V; 0 to 0.8% of Si; 0 to 0.5% of Al; 0 to 2% of Cr; 0 to 0.15% of Ti; 0 to 0.15 of Nb; 0 to 0.004% of B; the content of Mo, Ni, Cu in combination amounts a total of less than 2%; and inevitable impurity elements, wherein the balance consists of Fe, the hot stamped steel material having a yield strength of 1300 MPa to 1700 MPa, a tensile strength of 1800 to 2200 MPa, and an elongation of 6 to 9% without tempering.
A fluid product dispenser comprising: - a fluid product reservoir (R) provided with a neck (C) that is externally threaded and that internally defines an opening that communicates with the inside of the reservoir, the neck (C) forming at least one helical screw thread (T) and an annular upper edge (C1), - a dispensing head (D) mounted on the neck (C) of the reservoir (R), the head (D) comprising a dispensing member (P), such as a pump or a valve, a push-button (B) for actuating the dispensing member (P) and a fixing member (R6; R7) engaging both with the threaded neck (C) of the reservoir (R) and the dispensing member (P), the fixing member (R6; R7) comprising a skirt (61; 71) forming several bosses (62; 62'; 62") that are distributed over its inner periphery, at least some of these bosses (62; 62'; 62") coming into pressing contact with the screw thread (T) of the neck (C) so as to deform against the screw thread (T), characterised in that each boss (62; 62'; 62") comprises two substantially triangular lateral flanks (620; 620'; 620") and two opposite inclined ramps (621, 622; 621', 622'; 621", 622") which meet at an apex (623; 623'; 623") which points radially inwards. - a fluid product reservoir (R) provided with a neck (C) that is externally threaded and that internally defines an opening that communicates with the inside of the reservoir, the neck (C) forming at least one helical screw thread (T) and an annular upper edge (C1), - a dispensing head (D) mounted on the neck (C) of the reservoir (R), the head (D) comprising a dispensing member (P), such as a pump or a valve, a push-button (B) for actuating the dispensing member (P) and a fixing member (R6; R7) engaging both with the threaded neck (C) of the reservoir (R) and the dispensing member (P), the fixing member (R6; R7) comprising a skirt (61; 71) forming several bosses (62; 62'; 62") that are distributed over its inner periphery, at least some of these bosses (62; 62'; 62") coming into pressing contact with the screw thread (T) of the neck (C) so as to deform against the screw thread (T),
A method for evaluating adhesive strength among coal particles of different coal brands using interfacial tension determined on the basis of the surface tension of each kind of coal brand as an index, wherein the surface tension of each kind of coal brand is measured in cooled coal after heating the coal in an inert atmosphere to a temperature in which coal particles begin softening and cooling the heated coal at a cooling rate of 10°C/sec or more, and wherein the value of interfacial tension is calculated from the measured values of surface tension and the blending ratios of the two kinds of heat treated coals and wherein the adhesive strength is evaluated based on a value of interfacial tension between two kinds of heat treated coals obtained by heat treating the two kinds of coals, and wherein the adhesive strength among coal particles is evaluated as poor when the value of interfacial tension is more than a prescribed threshold. wherein the surface tension of each kind of coal brand is measured in cooled coal after heating the coal in an inert atmosphere to a temperature in which coal particles begin softening and cooling the heated coal at a cooling rate of 10°C/sec or more, and wherein the value of interfacial tension is calculated from the measured values of surface tension and the blending ratios of the two kinds of heat treated coals and wherein the adhesive strength is evaluated based on a value of interfacial tension between two kinds of heat treated coals obtained by heat treating the two kinds of coals, and wherein the adhesive strength among coal particles is evaluated as poor when the value of interfacial tension is more than a prescribed threshold.
A method for controlling a steering assist system of a vehicle ; the steering assist system comprising a fluid pump connected to a steering system of the vehicle , wherein the fluid pump is arranged to supply a flow of fluid for generating a steering assist force to a wheel of the vehicle during operation, the method comprising: - obtaining (S1) a signal indicative of a road characteristics of a road segment operable by the vehicle ; - determining (S2) a required wheel angle for operating the vehicle during the road segment; - determining (S3) a desired steering assist force to be applied to the wheel based on the required wheel angle; characterized by - controlling (S4) the flow of fluid supplied by the fluid pump based on the steering assist force when operating the vehicle at the road segment, wherein the flow of fluid supplied by the fluid pump is controlled proportionally to the desired steering assist force. - obtaining (S1) a signal indicative of a road characteristics of a road segment operable by the vehicle ; - determining (S2) a required wheel angle for operating the vehicle during the road segment; - determining (S3) a desired steering assist force to be applied to the wheel based on the required wheel angle; characterized by - controlling (S4) the flow of fluid supplied by the fluid pump based on the steering assist force when operating the vehicle at the road segment, wherein the flow of fluid supplied by the fluid pump is controlled proportionally to the desired steering assist force.
A mobile computing device comprising: a first port configured with a first pinout to support a first data format; a data source configured to provide data in a second data format different from the first data format; a first multiplexer configured to selectively transmit data from said data source towards said first port , wherein said first port is reconfigurable with a second pinout to support the second data format; characterised by a second multiplexer configured to selectively transmit data from another data source configured to provide data in the first data format and an output from said first multiplexer that includes data in the second data format from the data source configured to provide data in the second format, the data selectively transmitted to said first port . a first port configured with a first pinout to support a first data format; a data source configured to provide data in a second data format different from the first data format; a first multiplexer configured to selectively transmit data from said data source towards said first port , wherein said first port is reconfigurable with a second pinout to support the second data format; characterised by a second multiplexer configured to selectively transmit data from another data source configured to provide data in the first data format and an output from said first multiplexer that includes data in the second data format from the data source configured to provide data in the second format, the data selectively transmitted to said first port .
A system comprising: a processing unit ; and a storage device including program code that when executed by the processing unit causes the system to: determine (S405) a first batch size for processing an audio signal; collect (S410) a first batch comprising a first number of raw acoustic feature frames of the audio signal, the first number equal to the first batch size; input (S415) the first batch to a speech recognition network; determine (S425) a second batch size based on a word hypothesis output (S420) by the speech recognition network, the second batch size greater than the first batch size; collect (S435) a second batch comprising a second number of acoustic feature frames of the audio signal, the second number equal to the second batch size; and input (S445) the second batch to the speech recognition network. a processing unit ; and a storage device including program code that when executed by the processing unit causes the system to: determine (S405) a first batch size for processing an audio signal; collect (S410) a first batch comprising a first number of raw acoustic feature frames of the audio signal, the first number equal to the first batch size; input (S415) the first batch to a speech recognition network; determine (S425) a second batch size based on a word hypothesis output (S420) by the speech recognition network, the second batch size greater than the first batch size; collect (S435) a second batch comprising a second number of acoustic feature frames of the audio signal, the second number equal to the second batch size; and input (S445) the second batch to the speech recognition network. determine (S405) a first batch size for processing an audio signal; collect (S410) a first batch comprising a first number of raw acoustic feature frames of the audio signal, the first number equal to the first batch size; input (S415) the first batch to a speech recognition network; determine (S425) a second batch size based on a word hypothesis output (S420) by the speech recognition network, the second batch size greater than the first batch size; collect (S435) a second batch comprising a second number of acoustic feature frames of the audio signal, the second number equal to the second batch size; and input (S445) the second batch to the speech recognition network.
A radome for an aircraft , the radome comprising: a shell , the shell forming an outer surface of an enclosure when mounted on an aircraft , the enclosure being sized and shaped to house a first radio antenna configured to transmit and receive in a first frequency, wherein the shell includes a first portion that has mechanical properties that are different from the mechanical properties of the remaining portions of the shell and a second portion forming a transmission/reception window for the first radio antenna , the second portion having a reduced radio signal attenuation property of the first radio frequency when compared to the first portion , characterized in that the enclosure is sized and shaped to house a second radio antenna configured to transmit and receive in a second frequency, and the shell includes a third portion forming a transmission/reception window for the second radio antenna , the third portion having a reduced radio signal attenuation property of the second radio frequency when compared to the first portion and to the second portion , the first radio frequency and the second radio frequency being different radio frequencies. a shell , the shell forming an outer surface of an enclosure when mounted on an aircraft , the enclosure being sized and shaped to house a first radio antenna configured to transmit and receive in a first frequency, wherein the shell includes a first portion that has mechanical properties that are different from the mechanical properties of the remaining portions of the shell and a second portion forming a transmission/reception window for the first radio antenna , the second portion having a reduced radio signal attenuation property of the first radio frequency when compared to the first portion , characterized in that the enclosure is sized and shaped to house a second radio antenna configured to transmit and receive in a second frequency, and the shell includes a third portion forming a transmission/reception window for the second radio antenna , the third portion having a reduced radio signal attenuation property of the second radio frequency when compared to the first portion and to the second portion , the first radio frequency and the second radio frequency being different radio frequencies.
A combination printing and cutting apparatus comprising: a printer , a carriage assembly , a cutter assembly comprised of a cutter carrier and a cutter cartridge , a drive element , a cartridge release actuator , a pressure adjusting element , and a pressure hub , characterized in that the cutter cartridge comprises a cut depth adjuster, a rotatable eccentric pinion shaft , a cutter wheel , a detent component , and a bearer roller , wherein the eccentric pinion shaft is held in an indexed position by means of the detent component that is actuated by the pressure adjusting element , and wherein a cut depth is adjusted by means of the rotatable eccentric pinion shaft shared by both the bearer roller and the cutter wheel . a printer , a carriage assembly , a cutter assembly comprised of a cutter carrier and a cutter cartridge , a drive element , a cartridge release actuator , a pressure adjusting element , and a pressure hub , characterized in that the cutter cartridge comprises a cut depth adjuster, a rotatable eccentric pinion shaft , a cutter wheel , a detent component , and a bearer roller , wherein the eccentric pinion shaft is held in an indexed position by means of the detent component that is actuated by the pressure adjusting element , and wherein a cut depth is adjusted by means of the rotatable eccentric pinion shaft shared by both the bearer roller and the cutter wheel . characterized in that the cutter cartridge comprises a cut depth adjuster, a rotatable eccentric pinion shaft , a cutter wheel , a detent component , and a bearer roller , wherein the eccentric pinion shaft is held in an indexed position by means of the detent component that is actuated by the pressure adjusting element , and wherein a cut depth is adjusted by means of the rotatable eccentric pinion shaft shared by both the bearer roller and the cutter wheel .
A slat assembly for a wing of an aircraft , the slat assembly comprising a slat and at least one connection assembly for movably connecting the slat to a main wing for an aircraft , the connection assembly comprising an elongate slat track that extends along a track longitudinal axis between a front end and a rear end and has an intermediate portion between the front and rear ends , wherein the front end of the slat track is configured to be mounted to the slat , wherein the rear end and/or the intermediate portion of the slat track are configured to be mounted to the main wing by a roller or slide bearing such that the slat track is movable along the track longitudinal axis , wherein the connection assembly comprises a drive unit configured for driving the slat track for movement along the track longitudinal axis , wherein the drive unit comprises a rotary actuator configured to be mounted to the main wing and having at least one drive arm rotatably driven about a rotation axis and drivingly engaging the slat track , characterized in that : one of the drive arm and the slat track comprises at least one groove and the other one of the drive arm and the slat track comprises at least one spigot drivingly engaging the groove. a slat and at least one connection assembly for movably connecting the slat to a main wing for an aircraft , the connection assembly comprising an elongate slat track that extends along a track longitudinal axis between a front end and a rear end and has an intermediate portion between the front and rear ends , wherein the front end of the slat track is configured to be mounted to the slat , wherein the rear end and/or the intermediate portion of the slat track are configured to be mounted to the main wing by a roller or slide bearing such that the slat track is movable along the track longitudinal axis , wherein the connection assembly comprises a drive unit configured for driving the slat track for movement along the track longitudinal axis , wherein the drive unit comprises a rotary actuator configured to be mounted to the main wing and having at least one drive arm rotatably driven about a rotation axis and drivingly engaging the slat track , characterized in that : one of the drive arm and the slat track comprises at least one groove and the other one of the drive arm and the slat track comprises at least one spigot drivingly engaging the groove.
A compound to produce an inner liner layer; said compound comprising a polymer base with a cross-linking unsaturated chain comprising at least 50 phr of a halobutyl rubber, a reinforcing filler and a vulcanization system; said compound being characterized in that it comprises an oxygen-proofing chemical in granular form made up of a mineral filler bonded with fatty acids comprising a chain of carbon atoms ranging in number from 6 to 24 and having at least one unsaturation; said oxygen-proofing chemical being produced by causing the fatty acids and the mineral filler to react with a molar ratio that is equal to or greater than 5:2; said oxygen-proofing chemical in granular form having dimensions ranging from 5nm to 50μm.
A display device for a vehicle having - at least one display , - a control device , which is coupled with the display and by means of which graphic data can be generated for display on the display , and - a first sensor (9-2), with which the energy consumption at least of the drive motor of the vehicle can be detected and can be stored by means of a memory (5-1), characterized in that - depending on the stored data for the energy consumption the remaining range, the distance to the next gas station and the distance from the destination of the destination guide device can be displayed by means of the control device on a single distance scale . - at least one display , - a control device , which is coupled with the display and by means of which graphic data can be generated for display on the display , and - a first sensor (9-2), with which the energy consumption at least of the drive motor of the vehicle can be detected and can be stored by means of a memory (5-1), characterized in that - depending on the stored data for the energy consumption the remaining range, the distance to the next gas station and the distance from the destination of the destination guide device can be displayed by means of the control device on a single distance scale .
An structuring premix comprising: a) a non-polymeric, crystalline, hydroxyl-containing structuring agent; and b) a linear alkyl sulphate surfactant. a) a non-polymeric, crystalline, hydroxyl-containing structuring agent; and b) a linear alkyl sulphate surfactant.