mhurhangee/ep-ind-claims huggingface dataset:
A method for operating an elevator system, wherein the elevator system comprises an elevator car (10; 10A-10C) movable between landings, such as in response to an elevator call registered by an elevator control unit, wherein the elevator car (10; 10A-10C) is configured to include a nominal capacity limit in a nominal operating mode, and a special capacity limit lower than the nominal capacity limit in a special operating mode, wherein the special capacity limit is related to a total weight of passengers inside the elevator car (10; 10A-10C), the method comprising: - determining the special operating mode of the elevator system, the special operating mode being different from the nominal operating mode at least with respect to a characteristic of use of the elevator car (10; 10A-10C), and - operating, in the special operating mode, the elevator system so as to reduce a number of passengers entering the elevator car (10; 10A-10C) from the landing compared to the nominal operating mode based on the characteristic by issuing an alert if the special capacity limit is exceeded inside the elevator car based on a measurement by a load weighing device arranged to determine the total weight. - determining the special operating mode of the elevator system, the special operating mode being different from the nominal operating mode at least with respect to a characteristic of use of the elevator car (10; 10A-10C), and - operating, in the special operating mode, the elevator system so as to reduce a number of passengers entering the elevator car (10; 10A-10C) from the landing compared to the nominal operating mode based on the characteristic by issuing an alert if the special capacity limit is exceeded inside the elevator car based on a measurement by a load weighing device arranged to determine the total weight.
A laser system comprising: a master oscillator for providing a laser beam; an amplifier adapted to amplify said laser beam; an aberrator and characterised by the aberrator being disposed between said master oscillator and said amplifier to pre-aberrate said laser beam to prevent the formation of caustic intensity patterns within said amplifier. a master oscillator for providing a laser beam; an amplifier adapted to amplify said laser beam; an aberrator and characterised by the aberrator being disposed between said master oscillator and said amplifier to pre-aberrate said laser beam to prevent the formation of caustic intensity patterns within said amplifier.
A method of manufacturing a product, comprising: extruding a parison (224, 24); positioning the parison (224, 24) in a mold (226, 26, 320, 326) having mold halves (226A, 24A, 26A, 326A); collapsing upper and lower portions of the parison (224, 24) to define a sealed interior of the parison (224, 24); partially closing the mold (226, 26, 320, 326) to leave gaps between the mold halves (226A, 24A, 26A, 326A); introducing pressurized gas into the sealed interior of the parison (224, 24) to inflate the parison (224, 24); forming the inflated parison against the mold halves (226A, 24A, 26A, 326A) in the partially closed mold (226, 26, 320, 326) to initially form the product, cutting the initially formed product into halves, the method being characterized in cutting the initially formed product into halves along the gaps between the mold halves (226A, 24A, 26A, 326A); and applying a film (352, 353) against at least one of the parison halves (224A, 226A, 24A, 324A, 524A) or the mold halves (226A, 24A, 26A, 326A).
An electronic device comprising: a display (160, 260) comprising a sensing panel configured to sense a handwriting input; at least one processor operatively connected to the display; and memory storing instructions which, when executed by the at least one processor, cause the electronic device to: acquire the handwriting input sensed by the sensing panel and displayed on the display (160, 260), the handwriting input comprising a first handwriting input corresponding to a first line and a second handwriting input corresponding to a second line, based on whether at least one of the first handwriting input or the second handwriting input satisfies at least one specified condition, determine to merge the second line into the first line or maintain the second line, based on a result of the determining convert the handwriting input into text by merging the second line into the first line or maintaining the second line, and control the display (160, 260) to display the converted handwriting input, characterised in that the specified condition includes a condition of a width of a region occupied by the first handwriting input in an input field being equal to or greater than a specified ratio of a width of the input field. a display (160, 260) comprising a sensing panel configured to sense a handwriting input; at least one processor operatively connected to the display; and memory storing instructions which, when executed by the at least one processor, cause the electronic device to: acquire the handwriting input sensed by the sensing panel and displayed on the display (160, 260), the handwriting input comprising a first handwriting input corresponding to a first line and a second handwriting input corresponding to a second line, based on whether at least one of the first handwriting input or the second handwriting input satisfies at least one specified condition, determine to merge the second line into the first line or maintain the second line, based on a result of the determining convert the handwriting input into text by merging the second line into the first line or maintaining the second line, and control the display (160, 260) to display the converted handwriting input, acquire the handwriting input sensed by the sensing panel and displayed on the display (160, 260), the handwriting input comprising a first handwriting input corresponding to a first line and a second handwriting input corresponding to a second line, based on whether at least one of the first handwriting input or the second handwriting input satisfies at least one specified condition, determine to merge the second line into the first line or maintain the second line, based on a result of the determining convert the handwriting input into text by merging the second line into the first line or maintaining the second line, and control the display (160, 260) to display the converted handwriting input,
A method for measuring tread thickness from tread surface (Ts) to belt surface located in a radially outermost position within a tire by emitting ultrasonic waves to the tread surface immersed in a liquid and receiving reflected waves, the method comprising the steps of: measuring a profile of the tread surface (Ts); identifying bottom positions (N1 to N6) of circumferentially extending grooves (M1 to M6) from the profile obtained in the step of measuring a profile; estimating depths (d1 to d6) from the groove bottoms (N1 to N6) to belt surface from the groove bottoms identified in the step of identifying bottom positions and pre-created tire design data; predicting thicknesses (Dp) by calculating predicted thicknesses from the tread surface (Ts) to the belt surface from a relationship between the thicknesses from the groove bottoms (N1 to N6) identified in the step of identifying bottom positions to a virtual tread surface corresponding to the groove bottoms (N1 to N6), which is set by interpolating the values of the tread surface (Ts) before and after the grooves (M1 to M6), and the depths (d1 to d6) from the groove bottoms (N1 to N6) to the belt surface estimated in the step of estimating depths; and setting amplification factors for received reflected waves according to an amplification factor-thickness data map prepared beforehand in correspondence to the predicated thicknesses. measuring a profile of the tread surface (Ts); identifying bottom positions (N1 to N6) of circumferentially extending grooves (M1 to M6) from the profile obtained in the step of measuring a profile; estimating depths (d1 to d6) from the groove bottoms (N1 to N6) to belt surface from the groove bottoms identified in the step of identifying bottom positions and pre-created tire design data; predicting thicknesses (Dp) by calculating predicted thicknesses from the tread surface (Ts) to the belt surface from a relationship between the thicknesses from the groove bottoms (N1 to N6) identified in the step of identifying bottom positions to a virtual tread surface corresponding to the groove bottoms (N1 to N6), which is set by interpolating the values of the tread surface (Ts) before and after the grooves (M1 to M6), and the depths (d1 to d6) from the groove bottoms (N1 to N6) to the belt surface estimated in the step of estimating depths; and setting amplification factors for received reflected waves according to an amplification factor-thickness data map prepared beforehand in correspondence to the predicated thicknesses.
A method for modifying a print job to be printed onto a plurality of sheets of a medium as part of creating a print product, comprising the steps of automatically: a) receiving print project data comprising a print job to be printed onto a plurality of individual sheets of a medium and further comprising process data indicating how the print job is to be processed for creating the print product; b) determining, based on the print project data, a first intermediate state during the creating of the print product at which an intermediate product is to be cut in a manual cutting step; c) determining, based on the print project data, a reference object and/or reference geometrical feature of the intermediate product in the first intermediate state; d) determining, based on the print project data, a cut line (A-A, B-B, C-C, D-D) along which the intermediate product in the first intermediate state is to be cut in the manual cutting step; e) determining, based on the print project data, a distance (dV, dX, dY, dZ) from the reference object or reference geometrical feature of the intermediate product in the first intermediate state to the determined cut line (A-A, B-B, C-C, D-D); f) determining, based on the print project data, an indicator position comprised by the intermediate product in the first intermediate state but not comprised by the end product; g) modifying the print job such that a cut distance information item indicating the determined distance numerically is to be printed in the determined indicator position; and h) executing the modified print job. a) receiving print project data comprising a print job to be printed onto a plurality of individual sheets of a medium and further comprising process data indicating how the print job is to be processed for creating the print product; b) determining, based on the print project data, a first intermediate state during the creating of the print product at which an intermediate product is to be cut in a manual cutting step; c) determining, based on the print project data, a reference object and/or reference geometrical feature of the intermediate product in the first intermediate state; d) determining, based on the print project data, a cut line (A-A, B-B, C-C, D-D) along which the intermediate product in the first intermediate state is to be cut in the manual cutting step; e) determining, based on the print project data, a distance (dV, dX, dY, dZ) from the reference object or reference geometrical feature of the intermediate product in the first intermediate state to the determined cut line (A-A, B-B, C-C, D-D); f) determining, based on the print project data, an indicator position comprised by the intermediate product in the first intermediate state but not comprised by the end product; g) modifying the print job such that a cut distance information item indicating the determined distance numerically is to be printed in the determined indicator position; and h) executing the modified print job.
An electrolysis apparatus comprising an inert anode system comprising at least one inert anode having a lower portion in contact with a molten salt bath, where at least an upper portion of the inert anode contacts and is circumscribed by a solid material subject to attack by gases from the bath, wherein the solid material is selected from the group consisting of alumina-based cement and cryolite-alumina, both of which will dissolve in the presence of the molten salt bath.
A method in a first network node for enabling soft combination in a wireless communication device, wherein the wireless communication device is connected to a plurality of network nodes including the first network node, the method comprising: transmitting a data packet to the wireless communication device; generating assistance information indicating to the wireless communication device when to search for the same data packet from one or more second network nodes of the plurality of network nodes for soft combination, wherein when the first network node and the second network node transmit the same data packet to the wireless communication device in an asynchronous manner, the assistance information includes information regarding a search window within which the wireless communication device searches for the same data packet from the second network node, and wherein the information regarding the search window is used by the wireless communication device to derive the search window; and transmitting the assistance information to the wireless communication device, wherein the search window is indicated by [(x-y 1) ms, (x+y 2) ms], x ms representing a timing delay of the second network node relative to the first network node, y 1 ms representing a first scheduling window within which the first network node schedules the data packet and y 2 ms representing a second scheduling window within which the second network node schedules the same data packet, wherein y 1 and y 2 can be the same or different. transmitting a data packet to the wireless communication device; generating assistance information indicating to the wireless communication device when to search for the same data packet from one or more second network nodes of the plurality of network nodes for soft combination, wherein when the first network node and the second network node transmit the same data packet to the wireless communication device in an asynchronous manner, the assistance information includes information regarding a search window within which the wireless communication device searches for the same data packet from the second network node, and wherein the information regarding the search window is used by the wireless communication device to derive the search window; and transmitting the assistance information to the wireless communication device, wherein the search window is indicated by [(x-y 1) ms, (x+y 2) ms], x ms representing a timing delay of the second network node relative to the first network node, y 1 ms representing a first scheduling window within which the first network node schedules the data packet and y 2 ms representing a second scheduling window within which the second network node schedules the same data packet, wherein y 1 and y 2 can be the same or different.
Propulsion system for an aircraft, including a dual-flow turbojet and a mounting structure intended to mount this turbojet to the wing surface or to the fuselage of the aircraft, where the said mounting structure includes an aft aerodynamic fairing including a thermal protection floor to protect the said mounting structure from the heat of a primary airstream channelled by an exhaust nozzle of the said turbojet, the said propulsion system including means for extracting a cooling airstream from a secondary airstream of the said turbojet, together with air circulation means fed by the said extraction means and having at least one outlet aperture (64, 68) emerging into a space between the said thermal protection floor (32, 53) and the said exhaust nozzle, wherein the said extraction means include at least one air inlet connected to the said air circulation means and formed in an aerodynamic wall (44, 56) of the said propulsion system, which is closely followed by the said secondary airstream during operation, and which extends longitudinally and facing another similar aerodynamic wall (44, 56) of the said propulsion system, with which it delimits a cavity (41, 62) essentially isolated from the said secondary airstream, characterized in that the said aerodynamic fairing extends in the extension of a bifurcation formed of two bifurcation walls mutually connecting two annular nacelle cases which delimit, respectively internally and externally, an annular space for a secondary airstream to flow in the said turbojet, and in that the said aerodynamic walls are the said bifurcation walls or side walls of the said aft aerodynamic fairing.
A movement device for self-propelled lawn mower robots comprising: - a main wheel which can be coupled to a power pick-up of a motor; - at least one auxiliary wheel which can be coupled to the main wheel to receive from said main wheel a mechanical power; - coupling means configured for securely fixing the at least one auxiliary wheel to said main wheel, in such a way that the at least one auxiliary wheel is rotationally integral with the main wheel; comprising at least one drive wheel, having a main body substantially circular and a plurality of drive fingers extending radially away from said main body, characterized in that it comprises a protective element which can be coupled to a lateral surface of an auxiliary wheel or of the main wheel facing directly toward a working area of the lawn mower robot, in such a way as to cover at least partly said surface. - a main wheel which can be coupled to a power pick-up of a motor; - at least one auxiliary wheel which can be coupled to the main wheel to receive from said main wheel a mechanical power; - coupling means configured for securely fixing the at least one auxiliary wheel to said main wheel, in such a way that the at least one auxiliary wheel is rotationally integral with the main wheel; comprising at least one drive wheel, having a main body substantially circular and a plurality of drive fingers extending radially away from said main body, characterized in that it comprises a protective element which can be coupled to a lateral surface of an auxiliary wheel or of the main wheel facing directly toward a working area of the lawn mower robot, in such a way as to cover at least partly said surface. characterized in that it comprises a protective element which can be coupled to a lateral surface of an auxiliary wheel or of the main wheel facing directly toward a working area of the lawn mower robot, in such a way as to cover at least partly said surface.
A dielectric resonator antenna, DRA (3600, 3700, 3800), comprising: an electrically conductive ground structure (3602, 3702, 3802); a plurality of volumes of dielectric materials (3604, 3704, 3804) disposed on the ground structure (3602, 3702, 3802) comprising N volumes, N being an integer equal to or greater than 3, disposed to form successive and sequential layered volumes V i, i being an integer from 1 to N, wherein volume V 1 forms an innermost first volume, wherein a successive volume V i+1 forms a layered shell disposed over and at least partially embedding volume V i, wherein volume V N at least partially embeds all volumes V 1 to V N-1; wherein directly adjacent volumes of the plurality of volumes of dielectric materials (3604, 3704, 3804) have different dielectric constant values that range from a first relative minimum value at volume V 1 to a relative maximum value at one of volumes V 2 to V N-1, back to a second relative minimum value at volume V N back to a second relative minimum value at volume V N, a signal feed (3606, 3706, 3806) electromagnetically coupled to one or more of the plurality of volumes of dielectric materials (3604, 3704, 3804) and wherein a portion of the dielectric material of volume V N bifurcates at least a portion of volumes V 1 to V N-1. an electrically conductive ground structure (3602, 3702, 3802); a plurality of volumes of dielectric materials (3604, 3704, 3804) disposed on the ground structure (3602, 3702, 3802) comprising N volumes, N being an integer equal to or greater than 3, disposed to form successive and sequential layered volumes V i, i being an integer from 1 to N, wherein volume V 1 forms an innermost first volume, wherein a successive volume V i+1 forms a layered shell disposed over and at least partially embedding volume V i, wherein volume V N at least partially embeds all volumes V 1 to V N-1; wherein directly adjacent volumes of the plurality of volumes of dielectric materials (3604, 3704, 3804) have different dielectric constant values that range from a first relative minimum value at volume V 1 to a relative maximum value at one of volumes V 2 to V N-1, back to a second relative minimum value at volume V N back to a second relative minimum value at volume V N, a signal feed (3606, 3706, 3806) electromagnetically coupled to one or more of the plurality of volumes of dielectric materials (3604, 3704, 3804) and wherein a portion of the dielectric material of volume V N bifurcates at least a portion of volumes V 1 to V N-1.
An inertial measurement system for a spinning projectile comprising: a first, roll gyro to be oriented substantially parallel to the spin axis of the projectile; a second gyro and a third gyro with axes arranged with respect to the roll gyro such that they define a three dimensional coordinate system; a controller, arranged to: compute a current projectile attitude from the outputs of the first, second and third gyros (210, 211, 212), the computed attitude comprising a roll angle, a pitch angle and a yaw angle; calculate a roll angle error based on the difference between the computed pitch and yaw angles and expected pitch and yaw angles; provide the roll angle error as an input to a Kalman filter that outputs a roll angle correction and a roll rate scale factor correction; and apply the calculated roll angle correction and roll rate scale factor correction to the output of the roll gyro; characterized in that the Kalman filter models roll angle error as a function of roll rate and one or more wind variables. a first, roll gyro to be oriented substantially parallel to the spin axis of the projectile; a second gyro and a third gyro with axes arranged with respect to the roll gyro such that they define a three dimensional coordinate system; a controller, arranged to: compute a current projectile attitude from the outputs of the first, second and third gyros (210, 211, 212), the computed attitude comprising a roll angle, a pitch angle and a yaw angle; calculate a roll angle error based on the difference between the computed pitch and yaw angles and expected pitch and yaw angles; provide the roll angle error as an input to a Kalman filter that outputs a roll angle correction and a roll rate scale factor correction; and apply the calculated roll angle correction and roll rate scale factor correction to the output of the roll gyro; compute a current projectile attitude from the outputs of the first, second and third gyros (210, 211, 212), the computed attitude comprising a roll angle, a pitch angle and a yaw angle; calculate a roll angle error based on the difference between the computed pitch and yaw angles and expected pitch and yaw angles; provide the roll angle error as an input to a Kalman filter that outputs a roll angle correction and a roll rate scale factor correction; and apply the calculated roll angle correction and roll rate scale factor correction to the output of the roll gyro; characterized in that the Kalman filter models roll angle error as a function of roll rate and one or more wind variables.