mhurhangee/ep-ind-claims huggingface dataset:
An antenna line device installed in an antenna apparatus of a multiple antenna system, the antenna apparatus comprising at least one multi-band antenna array, the antenna line device comprising: an input port having input power terminals and input control data communication terminals and an output port having output power terminals and output control data communication terminals, where the input power terminals and output power terminals are connected via an operating power transfer path and where the input control data communication terminals and output control data communication terminals are connected via a control data transfer path, a control part configured to perform a control according to a control signal received from a base station body; and at least two of a DC ping part, an RF ping part and a domain detection part, wherein the DC ping part is configured to include an electrical element (322, D1) installed in the operating power transfer path to cause a voltage drop, and to detect an operating power level before or after the voltage drop caused by the electrical element (322, D1) under the control of the control part, wherein the RF ping part is configured to check a connection of a feeder line to the antenna array by detecting a signal inputted through the feeder line under the control of the control part, and wherein the domain detection part comprises a switch configured to be installed in the control data transfer path and to be turned on/off under the control of the control part for identifying an antenna apparatus that covers each coverage sector. an input port having input power terminals and input control data communication terminals and an output port having output power terminals and output control data communication terminals, where the input power terminals and output power terminals are connected via an operating power transfer path and where the input control data communication terminals and output control data communication terminals are connected via a control data transfer path, a control part configured to perform a control according to a control signal received from a base station body; and at least two of a DC ping part, an RF ping part and a domain detection part,
Size-adjustable, pivotable triple-connection device comprising: a first element comprising an upper hole and a lower hole; and a second element comprising an upper and a lower hole characterized by the second element being pivotable in relation to an axis of alignment of upper holes of the first and second elements, and aligning, when not connected by its lower hole, in relation to a vertical axis of the first element. a first element comprising an upper hole and a lower hole; and a second element comprising an upper and a lower hole characterized by the second element being pivotable in relation to an axis of alignment of upper holes of the first and second elements, and aligning, when not connected by its lower hole, in relation to a vertical axis of the first element.
A charging device provided between a chargeable electrical device and an electric power source for supplying charging electric power to said electrical device, comprising: an electric power supply path (PL11, PL12, PL21, PL22) for supplying said charging electric power from said electric power source to said electrical device; an interrupting circuit configured to be operable to interrupt said electric power supply path (PL11, PL12, PL21, PL22); a leakage detecting circuit for detecting electrical leakage occurring in said electric power supply path (PL11, PL12, PL21, PL22) during charging; and an examining circuit for detecting the interruption of said electric power supply path (PL11, PL12, PL21, PL22) caused by said interrupting circuit and for examining said leakage detecting circuit after confirming the interruption of said electric power supply path (PL11, PL12, PL21, PL22) caused by said interrupting circuit. an electric power supply path (PL11, PL12, PL21, PL22) for supplying said charging electric power from said electric power source to said electrical device; an interrupting circuit configured to be operable to interrupt said electric power supply path (PL11, PL12, PL21, PL22); a leakage detecting circuit for detecting electrical leakage occurring in said electric power supply path (PL11, PL12, PL21, PL22) during charging; and an examining circuit for detecting the interruption of said electric power supply path (PL11, PL12, PL21, PL22) caused by said interrupting circuit and for examining said leakage detecting circuit after confirming the interruption of said electric power supply path (PL11, PL12, PL21, PL22) caused by said interrupting circuit.
A computer implemented method of generating a 3-D patient-specific musculoskeletal model to be executed on an ultrasound medical imaging system, the method comprising: transmitting ultrasound signals the frequency of which changes with respect to time using a predetermined excitation function as part of an ultrasound scan; acquiring a plurality of raw radio frequency signals from the ultrasound scan, the plurality of raw RF signals including a first raw RF signal and a second raw RF signal, each raw RF signal representing a reflected ultrasound signal; generating an envelope signal (392a, 392b) from each of the raw RF signals (390a, 390b), each envelope signal (392a, 392b) including one or more peaks (442a, 442b); generating a contour line based on the peaks (442a, 442b) of the envelope signals (392a, 392b); determining a position of the ultrasound transducer corresponding to each of the plurality of raw RF signals (390a, 390b); transforming the contour line into a point cloud based at least in part on the positions of the ultrasound transducer; and optimizing a 3-D bone model with respect to the point cloud to generate the 3-D patient-specific musculoskeletal model. transmitting ultrasound signals the frequency of which changes with respect to time using a predetermined excitation function as part of an ultrasound scan; acquiring a plurality of raw radio frequency signals from the ultrasound scan, the plurality of raw RF signals including a first raw RF signal and a second raw RF signal, each raw RF signal representing a reflected ultrasound signal; generating an envelope signal (392a, 392b) from each of the raw RF signals (390a, 390b), each envelope signal (392a, 392b) including one or more peaks (442a, 442b); generating a contour line based on the peaks (442a, 442b) of the envelope signals (392a, 392b); determining a position of the ultrasound transducer corresponding to each of the plurality of raw RF signals (390a, 390b); transforming the contour line into a point cloud based at least in part on the positions of the ultrasound transducer; and optimizing a 3-D bone model with respect to the point cloud to generate the 3-D patient-specific musculoskeletal model.
Belt buckle for a safety belt system with a spring-loaded latch mechanism for locking a belt tongue inserted into a lock housing and with a push button guided displaceably on the lock housing under spring action for acting on the latch mechanism as required to unlock the belt buckle, wherein a cable attaching the belt buckle to a vehicle is attached by an attachment device riveted to the lock housing and the attachment device comprises a plate-shaped basic body, from the base surface of which an abutment projection with a radial arcuate abutment surface for a loop formed by the cable protrudes in an axial direction and a rivet pin protrudes in the axial direction from the abutment projection, characterised by that the rivet pin is offset eccentrically to an apex of the arcuate abutment surface of the abutment projection, which surface is encircled by the cable, wherein the distance of the apex of the abutment surface to the centre point of the rivet pin is smaller than the radius of curvature of the abutment surface at the apex.
A device for supplying power to a wired drone, including at least: - one power converter on the ground, - one power converter at the level of the drone, - one wire connecting the power converters (4 and 2), the device being characterized in that a regulation of the power converter on the ground ensures that the voltage U B delivered by the power converter on the ground increases when the current I B delivered by the power converter on the ground increases, and this over the power range of normal use of the drone. - one power converter on the ground, - one power converter at the level of the drone, - one wire connecting the power converters (4 and 2),
Control panel, in particular for a motor vehicle, including a cover which is mounted on a support and which is provided with at least one tactile pressing detection zone (Z1, Z2, Z3, Z4, Z5, Z6) forming a control button (B1, B2, B3, B4, B5), in which a force sensor having a pressure-sensitive zone is arranged between the cover and the support, behind the detection zone (Z1, Z2, Z3, Z4, Z5, Z6), so as to detect the actuation of the control button (B1, B2, B3, B4, B5) to produce an electrical control signal when a user applies a determined tactile pressing force to the detection zone (Z1, Z2, Z3, Z4, Z5, Z6), the tactile pressing force being transmitted axially towards the sensitive zone via a spacer plate made of elastically compressible material which is intercalated between the sensor and the cover, characterised by the fact that the inner surface of the cover includes a series (S1, S2, S3, S4, S5, S6) of relief elements which are distributed over the inner surface of the cover opposite the sensitive zone so as to form a plurality of zones of localised excess pressure on the spacer plate, the said zones of localised excess pressure being uniformly distributed so that the spacer plate applies a substantially even prestressing force over the sensitive zone.
A controller for providing pulse-width modulation control of an interleaved power converter having at least a first phase leg and a second phase leg, the controller characterised by: a random value generator that randomly generates values; a summer that adds the values generated by the random value generator to a nominal value to define a period of a carrier signal; a carrier signal generator that generates a first carrier signal having a period defined by the output of the summer, wherein the period of the carrier signal is varied from a nominal period by the addition of the random value provided by the random value generator to the nominal value; a phase adjustor (26, 28) that generates a second carrier signal shifted in phase relative to the first carrier signal; a first comparator that compares the first carrier signal to a reference signal to generate first pulse-width modulated signals used to control a state of the first phase leg of the interleaved power converter; and a second comparator that compares the second carrier signal to the reference signal to generate second PWM signals used to control a state of the second phase leg of the interleaved power converter. a random value generator that randomly generates values; a summer that adds the values generated by the random value generator to a nominal value to define a period of a carrier signal; a carrier signal generator that generates a first carrier signal having a period defined by the output of the summer, wherein the period of the carrier signal is varied from a nominal period by the addition of the random value provided by the random value generator to the nominal value; a phase adjustor (26, 28) that generates a second carrier signal shifted in phase relative to the first carrier signal; a first comparator that compares the first carrier signal to a reference signal to generate first pulse-width modulated signals used to control a state of the first phase leg of the interleaved power converter; and a second comparator that compares the second carrier signal to the reference signal to generate second PWM signals used to control a state of the second phase leg of the interleaved power converter.
An airflow control system for a gas turbine system, comprising: a compressor component of a gas turbine system for generating an excess flow of air; a plurality of inlet guide vanes in the air intake section upstream from the compressor component, a flow of air passing through the inlet guide vanes, the inlet guide vanes controlling the flow of air passing through the air intake section to the compressor component, each inlet guide vane being selectively controllable by an independent actuator; a mixing area for receiving an exhaust gas stream produced by the gas turbine system; an air extraction system for extracting at least a portion of the excess flow of air generated by the compressor component of the gas turbine system to provide bypass air, and for diverting the bypass air into the mixing area to reduce a temperature of the exhaust gas stream, the air extraction system including a bypass duct for diverting the bypass air around the gas turbine system into the mixing area to reduce the temperature of the exhaust gas stream in the mixing area; and a selective catalytic reduction system for processing the reduced temperature exhaust gas stream from the mixing area. a compressor component of a gas turbine system for generating an excess flow of air; a plurality of inlet guide vanes in the air intake section upstream from the compressor component, a flow of air passing through the inlet guide vanes, the inlet guide vanes controlling the flow of air passing through the air intake section to the compressor component, each inlet guide vane being selectively controllable by an independent actuator; a mixing area for receiving an exhaust gas stream produced by the gas turbine system; an air extraction system for extracting at least a portion of the excess flow of air generated by the compressor component of the gas turbine system to provide bypass air, and for diverting the bypass air into the mixing area to reduce a temperature of the exhaust gas stream, the air extraction system including a bypass duct for diverting the bypass air around the gas turbine system into the mixing area to reduce the temperature of the exhaust gas stream in the mixing area; and a selective catalytic reduction system for processing the reduced temperature exhaust gas stream from the mixing area.
A gantry comprising: a bending magnet configured to bend a beam orbit; a plurality of first scanning magnets (301, 302) configured to scan the beam orbit in a first direction in order to scan an affected part with the beam; and a second scanning magnet configured to scan the beam orbit in a second direction in order to scan an affected part with the beam, wherein the phase difference between two of the plurality of first scanning magnets (301, 302) is 180n° ± θ, n being a natural number, where θ is equal to or more than 0 and less than 90°, and the bending magnet is arranged between the plurality of first scanning magnets (301, 302). a bending magnet configured to bend a beam orbit; a plurality of first scanning magnets (301, 302) configured to scan the beam orbit in a first direction in order to scan an affected part with the beam; and a second scanning magnet configured to scan the beam orbit in a second direction in order to scan an affected part with the beam, wherein the phase difference between two of the plurality of first scanning magnets (301, 302) is 180n° ± θ, n being a natural number, where θ is equal to or more than 0 and less than 90°, and the bending magnet is arranged between the plurality of first scanning magnets (301, 302).
A method of transmitting multiple data streams (AS,VS) from a transmitting device to a receiving device via a network having a plurality of network layers (14,15, 16,17), the streams (AS,VS) being transmitted via an end-to-end channel between the transmitting device and the receiving device at a transport layer of the network layers (14,15, 16,17) or a process-to-process channel between the transmitting device and the receiving device at an application layer of the network layers (14,15, 16,17), the method comprising: generating at the transmitting device a first data stream that comprises audio data or video data to be played out at the receiving device at a specified playout rate R; determining an end-to-end bandwidth of the end-to-end channel or a process-to-process bandwidth of the process-to-process channel that is available for the first data stream and a second data stream; determining a maximum packet size for the second data stream based on the determined available bandwidth and using playout information, which pertains to the first data stream and conveys the specified playout rate R for the first data stream; generating at the transmitting device, based on the determined maximum packet size, one or more data packets of the second data stream, each of the one or more packets of the second data stream having a packet size no more than the determined maximum packet size; and multiplexing the first data stream and the second data stream onto the available end-to-end channel to enable the multiplexed first data stream and the second data stream to be transmitted over the same channel. generating at the transmitting device a first data stream that comprises audio data or video data to be played out at the receiving device at a specified playout rate R; determining an end-to-end bandwidth of the end-to-end channel or a process-to-process bandwidth of the process-to-process channel that is available for the first data stream and a second data stream; determining a maximum packet size for the second data stream based on the determined available bandwidth and using playout information, which pertains to the first data stream and conveys the specified playout rate R for the first data stream; generating at the transmitting device, based on the determined maximum packet size, one or more data packets of the second data stream, each of the one or more packets of the second data stream having a packet size no more than the determined maximum packet size; and multiplexing the first data stream and the second data stream onto the available end-to-end channel to enable the multiplexed first data stream and the second data stream to be transmitted over the same channel.
A horizontal directional drilling rig system, comprising: a horizontal directional drilling rig that is configured to be electrically powered by both line power or one or more electric generators, characterized in that the horizontal directional drilling rig includes: a traverse carrier with electrically powered drive motors (54, 62) thereon, a vise carrier with at least one electrically powered vise carrier drive motor, and an electrical buss bar that directs electrical power to the traverse carrier and the vise carrier; a plurality of power control components, each one of the power control component is electrically connected to a respective one of the electrically powered drive motors (54, 62, 76) via the electrical buss bar. a horizontal directional drilling rig that is configured to be electrically powered by both line power or one or more electric generators, characterized in that the horizontal directional drilling rig includes: a traverse carrier with electrically powered drive motors (54, 62) thereon, a vise carrier with at least one electrically powered vise carrier drive motor, and an electrical buss bar that directs electrical power to the traverse carrier and the vise carrier; a plurality of power control components, each one of the power control component is electrically connected to a respective one of the electrically powered drive motors (54, 62, 76) via the electrical buss bar.
A power generator comprising: a generator housing for an aircraft; and a fluid passage assembly for the power generator, the fluid passage assembly comprising: an inlet conduit for receiving a fluid; a plenum fluidly coupled to the inlet conduit; and at least one distribution conduit fluidly coupled to and extending from the plenum for dispensing the fluid to the power generator; wherein a cross-section (150, 152, 154) of the at least one distribution conduit has at least one corner; wherein: the cross-section (150, 152, 154) further comprises an interior cross-section (150, 152, 154) with radiused corners; and the fluid passage assembly is a coolant fluid passage assembly integral with the generator housing. a generator housing for an aircraft; and a fluid passage assembly for the power generator, the fluid passage assembly comprising: an inlet conduit for receiving a fluid; a plenum fluidly coupled to the inlet conduit; and at least one distribution conduit fluidly coupled to and extending from the plenum for dispensing the fluid to the power generator; wherein a cross-section (150, 152, 154) of the at least one distribution conduit has at least one corner; wherein: the cross-section (150, 152, 154) further comprises an interior cross-section (150, 152, 154) with radiused corners; and the fluid passage assembly is a coolant fluid passage assembly integral with the generator housing. an inlet conduit for receiving a fluid; a plenum fluidly coupled to the inlet conduit; and at least one distribution conduit fluidly coupled to and extending from the plenum for dispensing the fluid to the power generator; wherein a cross-section (150, 152, 154) of the at least one distribution conduit has at least one corner; wherein: the cross-section (150, 152, 154) further comprises an interior cross-section (150, 152, 154) with radiused corners; and the fluid passage assembly is a coolant fluid passage assembly integral with the generator housing. the cross-section (150, 152, 154) further comprises an interior cross-section (150, 152, 154) with radiused corners; and the fluid passage assembly is a coolant fluid passage assembly integral with the generator housing.
Sealing film for application to a substrate, comprising a carrier film and a plurality of functional layers, wherein the functional layers comprise at least two color display layers (5, 6) and at least two adhesion-controlling layers (8, 9), wherein the sealing film has an adhesive layer for fastening to the substrate, wherein the functional layers are arranged between the carrier film and the adhesive layer, wherein the carrier film is at least partially detachable from the functional layers, in particular from the at least two color display layers (5, 6), in order to bring the sealing film from a first state into a second state, wherein the sealing film comprises, in the second state, a peeled-off layer and a residue, wherein, in the second state, at least one symbol arrangement is optically visible at least in the residue, which at least one symbol arrangement is arranged in a first partial region and a second partial region, wherein the at least two adhesion-controlling layers (8, 9) are provided in order to separate defined regions from the at least two color display layers (5, 6) and to make the at least one symbol arrangement optically visible when the carrier film is detached, characterized in that the functional layers and the adhesive layer are at least partially translucent, and in that the functional layers comprise at least one further color display layer and at least one further adhesion-controlling layer, wherein, as a result of the at least partially translucent design of the functional layers, the at least one symbol arrangement is optically more visible in the first partial region on a light background than in the second partial region and the at least one symbol arrangement is optically more visible in the second partial region on a dark background than in the first partial region, wherein the light background is optically lighter than the dark background.