mhurhangee/patent-ind-claim-en huggingface dataset:
A communication network for communicating between a plurality of modules associated with an aircraft, the communication network comprising: a plurality of communication gateways (200,300...600), each communication gateway being connectable to at least one other of the communication gateways; a plurality of modules (A,B...E), wherein each module is a monitoring unit operable to obtain data for a component of the aircraft, wherein each module is connected with or associated with one of the plurality of communication gateways; wherein each of the communication gateways has a dynamic module naming list providing a route table indicating at least one route from the communication gateway to those of the modules registered in the network, to enable the communication gateway to direct a message to an appropriate recipient module of the plurality of modules on a route having the least number of communication gateways to pass through to reach the recipient module's local communication gateway; wherein the dynamic module naming list of each of the communication gateways (200,300...600) is updated as to available modules in the network wherein when a module (A,B...E) is added to the network, it is arranged to register with a communication gateway of the plurality of communication gateways such that the dynamic module naming list for that gateway is updated, and the registration of the added module to that gateway is arranged to be sent to all communication gateways directly connected to that gateway and cascaded to all of the communication gateways in the network for their dynamic module naming lists to be updated; and when a module (A,B...E) is shutdown, it is arranged to de-register with a communication gateway of the plurality of communication gateways such that the dynamic module naming list for that gateway is updated, and the de-registration of the shut-down module to that gateway is arranged to be sent to all communication gateways directly connected to that gateway and cascaded to all of the communication gateways in the network for their dynamic module naming lists to be updated. a plurality of communication gateways (200,300...600), each communication gateway being connectable to at least one other of the communication gateways; a plurality of modules (A,B...E), wherein each module is a monitoring unit operable to obtain data for a component of the aircraft, wherein each module is connected with or associated with one of the plurality of communication gateways; wherein each of the communication gateways has a dynamic module naming list providing a route table indicating at least one route from the communication gateway to those of the modules registered in the network, to enable the communication gateway to direct a message to an appropriate recipient module of the plurality of modules on a route having the least number of communication gateways to pass through to reach the recipient module's local communication gateway; wherein the dynamic module naming list of each of the communication gateways (200,300...600) is updated as to available modules in the network wherein
A method comprising: receiving probe data from a plurality of probes within a region, wherein the probe data comprises at least one of heading information and location information for each probe data point; matching the probe data to a link segment to generate map-matched probe data; calculating a difference between the at least one of heading information and location information of the map-matched probe data points and of the link segment; determining a statistical mean of the difference between the at least one of heading information and location information of the map-matched probe data points and the link segment; determining an error of the statistical mean of the difference between the at least one of heading information and location information of the map-matched probe data points and the link segment; the method being characterised in that it further comprises the step of flagging the link segment for manual review in response to the statistical mean of the difference between the at least one of heading information and location information of the map-matched probe data points and the link segment being greater than the error of the statistical mean multiplied by a biasing factor, wherein the biasing factor controls the trade-off between false positives and false negatives. receiving probe data from a plurality of probes within a region, wherein the probe data comprises at least one of heading information and location information for each probe data point; matching the probe data to a link segment to generate map-matched probe data; calculating a difference between the at least one of heading information and location information of the map-matched probe data points and of the link segment; determining a statistical mean of the difference between the at least one of heading information and location information of the map-matched probe data points and the link segment; determining an error of the statistical mean of the difference between the at least one of heading information and location information of the map-matched probe data points and the link segment; the method being characterised in that it further comprises the step of flagging the link segment for manual review in response to the statistical mean of the difference between the at least one of heading information and location information of the map-matched probe data points and the link segment being greater than the error of the statistical mean multiplied by a biasing factor, wherein the biasing factor controls the trade-off between false positives and false negatives.
A textile comprising fiber elements each comprising a core yarn (302; 304; 803) which is helically wrapped by a twisted or coiled polymer fiber actuator (301; 303; 804, 805); wherein the polymer fiber actuator comprises a fiber having a degree of twist in which the product of (a) the degree of twist per unit length multiplied by (b) the average diameter of the fiber is at least 50°; and wherein the polymer fiber actuator is operable to reversibly change either the porosity of at least one single layer of the textile, the textile coloration, or combinations thereof, in response to a change in temperature or moisture absorption, wherein either the overall textile width or length changes by less than 5%. wherein the polymer fiber actuator comprises a fiber having a degree of twist in which the product of (a) the degree of twist per unit length multiplied by (b) the average diameter of the fiber is at least 50°; and wherein the polymer fiber actuator is operable to reversibly change either the porosity of at least one single layer of the textile, the textile coloration, or combinations thereof, in response to a change in temperature or moisture absorption, wherein either the overall textile width or length changes by less than 5%.
A method for controlling movement of an unmanned aerial vehicle, UAV , having one or more propulsion units, the method comprising: receiving , at one or more processors, one or more altitude restrictions for the UAV ; receiving , at the one or more processors, map information for an area; modifying , with aid of the one or more processors, the one or more altitude restrictions based on the map information so as to produce one or more modified altitude restrictions; and outputting , from the one or more processors, control signals to the one or more propulsion units to cause the UAV to comply with the one or more modified altitude restrictions while moving over the area, characterized in that : the modifying step is performed during operation of the UAV . receiving , at one or more processors, one or more altitude restrictions for the UAV ; receiving , at the one or more processors, map information for an area; modifying , with aid of the one or more processors, the one or more altitude restrictions based on the map information so as to produce one or more modified altitude restrictions; and outputting , from the one or more processors, control signals to the one or more propulsion units to cause the UAV to comply with the one or more modified altitude restrictions while moving over the area, characterized in that : the modifying step is performed during operation of the UAV .
Method for starting the casting operation of a multi-strand continuous casting machine , in particular for casting long products from steel, comprising the steps of: - mounting a multi-plug drive according to Claim 10 on a tundish , wherein the tundish is in a setting-up area , preferably on a casting platform, of the continuous casting machine and the multi-plug drive can open and close a number of plugs independently of one another; - attaching plugs to the multi-plug drive ; - placing the tundish onto a tundish car , wherein the tundish car is in a parking position on the casting platform of the continuous casting machine ; - establishing electrical connections between a control of the continuous casting machine and the multi-plug drive ; - heating the tundish ; - displacing the tundish car into a casting position; - filling the tundish ; - opening at least one outlet channel from the tundish by moving a plug of the multi-plug drive , whereby the casting operation of the continuous casting machine is started. - mounting a multi-plug drive according to Claim 10 on a tundish , wherein the tundish is in a setting-up area , preferably on a casting platform, of the continuous casting machine and the multi-plug drive can open and close a number of plugs independently of one another; - attaching plugs to the multi-plug drive ; - placing the tundish onto a tundish car , wherein the tundish car is in a parking position on the casting platform of the continuous casting machine ; - establishing electrical connections between a control of the continuous casting machine and the multi-plug drive ; - heating the tundish ; - displacing the tundish car into a casting position; - filling the tundish ; - opening at least one outlet channel from the tundish by moving a plug of the multi-plug drive , whereby the casting operation of the continuous casting machine is started.
A cooling structure for a rotary electric machine , the cooling structure comprising: a first supply pipe that is disposed vertically above a rotary electric machine and that has a discharge hole through which oil is discharged toward the rotary electric machine ; a second supply pipe that is disposed in parallel with the first supply pipe vertically above the rotary electric machine and that has a discharge hole through which the oil is discharged toward the rotary electric machine ; a first, mechanical oil, pump configured to deliver the oil to the first supply pipe ; a second, electric oil, pump configured to deliver the oil to the second supply pipe ; an electric motor configured to drive the second, electric oil, pump ; and a control device configured to control the electric motor to control driving of the second, electric oil, pump ; wherein the cooling structure is configured such that a direction of the oil flowing through the first supply pipe and a direction of the oil flowing through the second supply pipe are opposite to each other; and wherein the control device is further configured to control driving of the second, electric oil, pump to increase the flow rate and pressure of the oil flowing through the second supply pipe responsive to an increase in flow rate and pressure of the oil pumped by the first, mechanical oil, pump through the first supply pipe . a first supply pipe that is disposed vertically above a rotary electric machine and that has a discharge hole through which oil is discharged toward the rotary electric machine ; a second supply pipe that is disposed in parallel with the first supply pipe vertically above the rotary electric machine and that has a discharge hole through which the oil is discharged toward the rotary electric machine ; a first, mechanical oil, pump configured to deliver the oil to the first supply pipe ; a second, electric oil, pump configured to deliver the oil to the second supply pipe ; an electric motor configured to drive the second, electric oil, pump ; and a control device configured to control the electric motor to control driving of the second, electric oil, pump ; wherein the cooling structure is configured such that a direction of the oil flowing through the first supply pipe and a direction of the oil flowing through the second supply pipe are opposite to each other; and wherein the control device is further configured to control driving of the second, electric oil, pump to increase the flow rate and pressure of the oil flowing through the second supply pipe responsive to an increase in flow rate and pressure of the oil pumped by the first, mechanical oil, pump through the first supply pipe .
Pad holder for a brake pad mount of a rail vehicle, having a pressing-on plate with a guide channel , which extends in the longitudinal direction of the pad holder and in which a brake pad can be located displaceably and positively perpendicular to the normal of the pressing-on plate , a locking bar pivotably mounted at the pressing-on plate for locking the brake pad in the longitudinal direction of the pad holder , which locking bar projects into the guide channel in a locking position fixing the brake pad in a functional position and can be removed from the guide channel in a release position, two brake lever mounting points for the pivotable mounting of a brake lever , a suspension bracket mounting point for the pivotable mounting of a suspension bracket , characterised in that the pressing-on plate has a plurality of window-like recesses , wherein at least two of the recesses are separated from each other by a transverse strut . a pressing-on plate with a guide channel , which extends in the longitudinal direction of the pad holder and in which a brake pad can be located displaceably and positively perpendicular to the normal of the pressing-on plate , a locking bar pivotably mounted at the pressing-on plate for locking the brake pad in the longitudinal direction of the pad holder , which locking bar projects into the guide channel in a locking position fixing the brake pad in a functional position and can be removed from the guide channel in a release position, two brake lever mounting points for the pivotable mounting of a brake lever , a suspension bracket mounting point for the pivotable mounting of a suspension bracket , characterised in that the pressing-on plate has a plurality of window-like recesses , wherein at least two of the recesses are separated from each other by a transverse strut .
A tire comprising a rubber composition in the form of a sheet disposed between the sidewall of the tire and its carcass, wherein the rubber composition comprises 100 parts by weight of a base rubber, 20 to 60 parts by weight of carbon black, and 2 to 5 parts by weight of an amine-based anti-aging agent and 1 to 3 parts by weight of a quinoline-based anti-aging agent; the base rubber is a combination of a natural rubber or a modified natural rubber and a synthetic rubber which are mixed in a weight ratio of 1:9 to 9:1, the amine-based anti-aging agent is any one selected from the group consisting of N-phenyl-N'-(1,3-dimethyl)-p-phenylenediamine, N-(1,3-dimethylbutyl)-N'-phenyl-p-phenylenediamine, N-phenyl-N'-isopropyl-p-phenylenediamine, N,N'-diphenyl-p-phenylenediamine, N,N'-diaryl-p-phenylenediamine, N-phenyl-N'-cyclohexyl-p-phenylenediamine, N-phenyl-N'-octyl-p-phenylenediamine and a combination thereof, and the sidewall does not comprise an amine-based anti-aging agent.
Axial impeller having a hub and a blading , for a fan or blower, in which the geometry of the blades is determined by a progression of a blade inlet angle (β f1 ) and of a blade outlet angle (β f2 ) of blade sections from a blade root at the hub to a blade tip opposite the blade root , that is to say as a function of the hub ratio, characterized in that the blade inlet angle (β f1 ) is left-curved as a function of the hub ratio, and the blade outlet angle (β f2 ) is right-curved as a function of the hub ratio, wherein the progression of the blade inlet angle (β f1 ), as a function of the hub ratio, is as per the following table: Hub ratio Blade inlet angle [°] 1.00 29.2 0.92 26.3 0.85 23.7 0.79 21.2 0.74 19.0 0.69 17.1 0.65 15.4 0.62 14.1 0.58 13.1 0.56 12.5 0.53 12.3 0.51 12.7 0.49 13.6 or that the progression of the blade inlet angle (β f1 ), as a function of the hub ratio, deviates from the above table values by at most +/- 1°, and wherein the progression of the blade outlet angle (β f2 ), as a function of the hub ratio, is as per the following table: Hub ratio Blade outlet angle [°] 1.00 68.8 0.92 67.5 0.85 66.0 0.79 64.2 0.74 62.0 0.69 59.4 0.65 56.6 0.62 53.3 0.58 49.6 0.56 45.3 0.53 40.1 0.51 34.1 0.49 27.0 or that the progression of the blade outlet angle (β f2 ), as a function of the hub ratio, deviates from the above table values by at most +/- 2°. in that the blade inlet angle (β f1 ) is left-curved as a function of the hub ratio, and the blade outlet angle (β f2 ) is right-curved as a function of the hub ratio, wherein the progression of the blade inlet angle (β f1 ), as a function of the hub ratio, is as per the following table: Hub ratio Blade inlet angle [°] 1.00 29.2 0.92 26.3 0.85 23.7 0.79 21.2 0.74 19.0 0.69 17.1 0.65 15.4 0.62 14.1 0.58 13.1 0.56 12.5 0.53 12.3 0.51 12.7 0.49 13.6 or that the progression of the blade inlet angle (β f1 ), as a function of the hub ratio, deviates from the above table values by at most +/- 1°, and wherein the progression of the blade outlet angle (β f2 ), as a function of the hub ratio, is as per the following table: Hub ratio Blade outlet angle [°] 1.00 68.8 0.92 67.5 0.85 66.0 0.79 64.2 0.74 62.0 0.69 59.4 0.65 56.6 0.62 53.3 0.58 49.6 0.56 45.3 0.53 40.1 0.51 34.1 0.49 27.0 or that the progression of the blade outlet angle (β f2 ), as a function of the hub ratio, deviates from the above table values by at most +/- 2°.
An insulating spacer configured to be used in a battery pack including unit cells stacked on each other and electrically connected by a bus bar along a stacking direction of the unit cells, and each of the unit cells having a cell body including a power-generating element formed in a flat shape and an electrode tab extending out from the cell body with a distal end portion of the electrode tab being bent along a thickness direction of the cell body, the insulating spacer being configured to be provided between each of the unit cells, and the insulating spacer comprising: an abutting portion arranged and configured to abut the distal end portion of the electrode tab from a direction intersecting the stacking direction of the unit cells; a side surface arranged to face the distal end portion of the electrode tab in the direction intersecting the stacking direction of the unit cells; and a recessed portion formed in the side surface, the recessed portion arranged to be recessed in the direction intersecting the stacking direction of the unit cells so as to be separated from the distal end portion of the electrode tab; characterized in that the insulating spacer further comprises a communicating portion that includes a gap between the side surface and the electrode tab and communicates an inside of the recessed portion with an outside of the recessed portion when the abutting portion is abutted against the distal end portion of the electrode tab. an abutting portion arranged and configured to abut the distal end portion of the electrode tab from a direction intersecting the stacking direction of the unit cells; a side surface arranged to face the distal end portion of the electrode tab in the direction intersecting the stacking direction of the unit cells; and a recessed portion formed in the side surface, the recessed portion arranged to be recessed in the direction intersecting the stacking direction of the unit cells so as to be separated from the distal end portion of the electrode tab; characterized in that the insulating spacer further comprises a communicating portion that includes a gap between the side surface and the electrode tab and communicates an inside of the recessed portion with an outside of the recessed portion when the abutting portion is abutted against the distal end portion of the electrode tab.
A wearable antenna , for wirelessly receiving sensor data generated by an implantable sensor device implanted in a uterus, the wearable antenna having a downwardly extending portion for location at the front of the wearer's body, characterized in that the wearable antenna is configured to, in use, extend around the waist of the wearer's body in a continuous loop.
A heat exchanger comprising: a plurality of integrally formed contiguous unit cells defining a three-dimensional lattice of repeating unit cells, the plurality of integrally formed contiguous unit cells comprising: a plurality of pathway cells having a solid domain comprising: an interior pathway-cell surface contiguously defining a first furcated fluid domain for a first fluid to flow across the plurality of pathway cells ; and an exterior pathway-cell surface contiguously defining a second furcated fluid domain for a second fluid to flow across the plurality of pathway cells ; and a plurality of baffle cells integrally formed among the plurality of pathway cells , the plurality of baffle cells having a solid domain comprising: one or more first furcated-pathway blinds together providing one or more first furcated-pathway baffles , each of the first furcated-pathway baffles contiguously defining a first boundary to the first furcated fluid domain ; and/or one or more second furcated-pathway blinds together providing a one or more second furcated-pathway baffles , each of the second furcated-pathway baffles contiguously defining a second boundary to the second furcated fluid domain . an interior pathway-cell surface contiguously defining a first furcated fluid domain for a first fluid to flow across the plurality of pathway cells ; and an exterior pathway-cell surface contiguously defining a second furcated fluid domain for a second fluid to flow across the plurality of pathway cells ; and a plurality of baffle cells integrally formed among the plurality of pathway cells , the plurality of baffle cells having a solid domain comprising: one or more first furcated-pathway blinds together providing one or more first furcated-pathway baffles , each of the first furcated-pathway baffles contiguously defining a first boundary to the first furcated fluid domain ; and/or one or more second furcated-pathway blinds together providing a one or more second furcated-pathway baffles , each of the second furcated-pathway baffles contiguously defining a second boundary to the second furcated fluid domain . one or more first furcated-pathway blinds together providing one or more first furcated-pathway baffles , each of the first furcated-pathway baffles contiguously defining a first boundary to the first furcated fluid domain ; and/or one or more second furcated-pathway blinds together providing a one or more second furcated-pathway baffles , each of the second furcated-pathway baffles contiguously defining a second boundary to the second furcated fluid domain .