mhurhangee/ep-ind-claims huggingface dataset:
A system for the simulation of a percutaneous medical procedure, the system comprising: a simulated vasculature including: a first component configured to allow for introduction of a medical device into the system through an introductory port; a second component connected to the first component and shaped to simulate a portion of a human vasculature; and a third component connected to the second component and shaped to simulate a delivery site for the medical procedure, and a first tank that is unsealed and open to the atmosphere at a top end; and a second tank that is sealed and not open to the atmosphere, wherein the system is configured to allow for a medical device to be delivered to the third component by passing through the introductory port of the first component and passing through the second component, wherein the system is configured to replicate simulated conditions of use for the medical procedure, and wherein the second component is fluidly connected to the first and second tank (36, 38), and wherein the second component is connected to the first tank via a conduit that is vertically oriented and sized to provide a desired back pressure to the second component and via a conduit comprising a valve to serve as a fast pace bypass conduit of the third component. a simulated vasculature including: a first component configured to allow for introduction of a medical device into the system through an introductory port; a second component connected to the first component and shaped to simulate a portion of a human vasculature; and a third component connected to the second component and shaped to simulate a delivery site for the medical procedure, and a first tank that is unsealed and open to the atmosphere at a top end; and a second tank that is sealed and not open to the atmosphere, a first component configured to allow for introduction of a medical device into the system through an introductory port; a second component connected to the first component and shaped to simulate a portion of a human vasculature; and a third component connected to the second component and shaped to simulate a delivery site for the medical procedure, and a first tank that is unsealed and open to the atmosphere at a top end; and a second tank that is sealed and not open to the atmosphere, wherein the system is configured to allow for a medical device to be delivered to the third component by passing through the introductory port of the first component and passing through the second component, wherein the system is configured to replicate simulated conditions of use for the medical procedure, and wherein the second component is fluidly connected to the first and second tank (36, 38), and wherein the second component is connected to the first tank via a conduit that is vertically oriented and sized to provide a desired back pressure to the second component and via a conduit comprising a valve to serve as a fast pace bypass conduit of the third component.
A method of controlling a device by a server, the method being performed by the server and comprising the steps of: receiving, from a first external device, information regarding a second external device, wherein the information was received by the first external device from the second external device; authenticating the second external device based on the information regarding the second external device; detecting position information regarding the second external device; characterized in that the method further comprises the steps of: transmitting, to the first external device, control information regarding the first external device to control a sensor of the first external device based on the position information, the control information being used in controlling the sensor of the first external device; and providing a service relating to the sensor of the first external device after transmitting the control information. receiving, from a first external device, information regarding a second external device, wherein the information was received by the first external device from the second external device; authenticating the second external device based on the information regarding the second external device; detecting position information regarding the second external device; transmitting, to the first external device, control information regarding the first external device to control a sensor of the first external device based on the position information, the control information being used in controlling the sensor of the first external device; and providing a service relating to the sensor of the first external device after transmitting the control information.
A battery module, comprising: - a plurality of battery cells, which are in a form of pouch cells, and which are stacked and/or piled next to each other in a horizontal direction; - each battery cell comprising a positive terminal tab and a negative terminal tab extruding from opposite edges of the battery cell, or from a same edge of the battery cell; characterized in that the battery module further comprises: - a fastening portion per one battery cell, which fastening portion is a longitudinally shaped element, and where the fastening portion is placed along the edge of the battery cell where the positive or the negative terminal tab (7, 8) locates, right adjacent to the respective terminal tab (7, 8); - the positive and negative terminal tabs (7, 8) are configured to be in a bent fashion on top of a surface of the longitudinal shaped fastening portion; wherein - the fastening portion is configured to hinder movement of the battery cells in an orthogonal direction compared to the longest dimension of the fastening portion; and wherein - a desired number of battery cells are configured to be placed adjacently within the battery module so that respective fastening portions aligned in a parallel direction create support for the battery module. - a plurality of battery cells, which are in a form of pouch cells, and which are stacked and/or piled next to each other in a horizontal direction; - each battery cell comprising a positive terminal tab and a negative terminal tab extruding from opposite edges of the battery cell, or from a same edge of the battery cell; - a fastening portion per one battery cell, which fastening portion is a longitudinally shaped element, and where the fastening portion is placed along the edge of the battery cell where the positive or the negative terminal tab (7, 8) locates, right adjacent to the respective terminal tab (7, 8); - the positive and negative terminal tabs (7, 8) are configured to be in a bent fashion on top of a surface of the longitudinal shaped fastening portion; wherein - the fastening portion is configured to hinder movement of the battery cells in an orthogonal direction compared to the longest dimension of the fastening portion; and wherein - a desired number of battery cells are configured to be placed adjacently within the battery module so that respective fastening portions aligned in a parallel direction create support for the battery module.
Gear flow meter for measuring the flow of a fluid, having a gear chamber, in which at least one measuring gear wheel (20, 21) is arranged, a bottom and a cover which delimit the gear chamber on end faces of the at least one measuring gear wheel (20, 21), wherein a respective rotation shaft (30, 31) is provided centrally relative to each measuring gear wheel (20, 21), wherein each measuring gear wheel (20, 21) is rotatably mounted and a fluid is conveyable through the gear chamber to rotate the at least one measuring gear wheel (20, 21), and having a measuring unit to detect a gear rotation and evaluation means to determine a flow of the fluid through the gear chamber on the basis of the gear rotation, wherein a respective receiving area is provided between each measuring gear wheel (20, 21) and the bottom and also between each measuring gear wheel (20, 21) and the cover, in which receiving area rolling elements are arranged for mounting the respective measuring gear wheel (20, 21), characterized in that the rolling elements directly contact the respective measuring gear wheel (20, 21), the respective rotation shaft (30, 31) and the bottom or cover (52, 56), wherein running surfaces of the rolling elements are formed by the measuring gear wheel (20, 21) and the rotation shaft (30, 31) itself, and the rolling elements are each movable as a whole relative to the rotation shaft (30, 31), the measuring gear wheel (20, 21) and the bottom or cover (52, 56) which they contact.
A light module for a motor vehicle, comprising: +) at least one light source (1, 10, 11, 100, 110); +) at least one reflector (2, 20, 21, 200, 210, 2000); +) at least one lens (3, 30, 31, 300, 310); wherein the light emitted by the light source (1, 10, 11, 100, 110) is formed into a light distribution by a reflecting surface (2a, 20a, 21a, 22a, 200a, 210a, 2000a) of the at least one reflector (2, 20, 21, 200, 210, 2000) and - when the light module is fitted in a vehicle - is projected via the at least one lens (3, 30, 31, 300, 310) into an area in front of the vehicle, wherein the reflecting surface (2a, 20a, 21a, 22a, 200a, 210a, 2000a) of the at least one reflector (2, 20, 21, 200, 210, 2000) is formed in such a way that a first focal point of the reflector (2, 20, 21, 200, 210, 2000), in which first local point the at least one light source (1, 10,11, 100, 110) is being located, is located between the reflecting surface (2a, 20a, 21a, 22a, 200a, 210a, 2000a) and the at least one lens (3, 30, 31, 300, 310) and a second focal point is located on the side of the reflector (2, 20, 21, 200, 210, 2000) facing away from the lens (3, 30, 31, 300, 310), wherein the reflecting surface (2a, 20a, 21a, 22a, 200a, 210a, 2000a) of the reflector (2, 20, 21, 200, 210, 2000) is designed in such a way that the light pattern generated comprises at least one light-dark line, characterised in that the reflecting surface (22a, 200a, 210a, 2000a) of the reflector (21, 200, 210, 2000) is designed in such a way that light from the at least one light source (11, 100, 110) reflected along at least one defined curve on the reflecting surface (22a, 200a, 210a, 2000a) is projected in the light pattern as an area with maximum brightness. +) at least one light source (1, 10, 11, 100, 110); +) at least one reflector (2, 20, 21, 200, 210, 2000); +) at least one lens (3, 30, 31, 300, 310);
A compound which is of a formula set out below or is a pharmaceutically acceptable salt thereof: (2S,3R,4R,5S,6R)-2-(4-chloro-3-(4-(2-(2-methoxyethoxy)ethoxy) benzyl)phenyl)-6-(hydroxymethyl)tetrahydro-2H-pyran-3,4,5-triol; (2S,3R,4R,5S,6R)-2-(3-(4-(2-(allyloxy)ethoxy)benzyl)-4-chlorophenyl)-6-(hydroxymethyl)tetrahydro-2H-pyran-3,4,5-triol; (2S,3R,4R,5S,6R)-2-(4-chloro-3-(4-(2-(prop-2-ynyloxy)ethoxy)benzyl)phenyl)-6-(hydroxymethyl)tetrahydro-2H-pyran-3,4,5-triol; (2S,3R,4R,5S,6R)-2-(4-chloro-3-(4-(1-(prop-2-ynyloxy)propan-2-yloxy)benzyl)phenyl)-6-(hydroxymethyl)tetrahydro-2H-pyran-3,4,5-triol; (2S,3R,4R,5S,6R)-2-(4-chloro-3-(4-(2-(cyclopentyloxy)ethoxy)benzyl)phenyl)-6-(hydroxymethyl)tetrahydro-2H-pyran-3,4,5-triol; (2S,3R,4R,5S,6R)-2-(4-chloro-3-(4-(2-cyclopropoxyethoxy)benzyl)phenyl)-6-(hydroxymethyl)tetrahydro-2H-pyran-3,4,5-triol; (2S,3R,4R,5S,6R)-2-(4-chloro-3-(4-(2-(2,2,2-trifluoroethoxy)ethoxy)benzyl)phenyl)-6-(hydroxymethyl)tetrahydro-2H-pyran-3,4,5-triol; (2S,3R,4R,5S,6R)-2-(4-chloro-3-(4-(2-(2-fluoroethoxy)ethoxy)benzyl)phenyl)-6-(hydroxymethyl)tetrahydro-2H-pyran-3,4,5-triol; (2S,3R,4R,5S,6R)-2-(4-chloro-3-(4-(2-(2,2-difluoroethoxy)ethoxy)benzyl)phenyl)-6-(hydroxymethyl)tetrahydro-2H-pyran-3,4,5-triol; (2S,3R,4R,5S,6R)-2-(4-chloro-3-(4-(2-(2-(pyrrolidin-1-yl)ethoxy)ethoxy)benzyl)phenyl)-6-(hydroxymethyl)tetrahydro-2H-pyran-3,4,5-triol; (2S,3R,4R,5S,6R)-2-(4-chloro-3-(4-(2-( -(tetrahydrofuran-3-yloxy)ethoxy)benzyl)phenyl)-6-(hydroxymethyl)tetrahydro-2H-pyran-3,4,5-triol; (2S,3R,4R,5S,6R)-2-(4-chloro-3-(4-(2-cyclobutoxyethoxy)benzyl)phenyl)-6-(hydroxymethyl)tetrahydro-2H-pyran-3,4,5-triol; (2S,3R,4R,5S,6R)-2-(4-chloro-3-(4-(2-(1-methylcyclopropoxy)ethoxy))benzyl)phenyl)-6-(hydroxymethyl)tetrahydro-2H-pyran-3,4,5-triol; (2S,3R,4R,5S,6R)-2-(4-chloro-3-(4-(2-cyclopropoxypropoxy)benzyl)phenyl)-6-(hydroxymethyl)tetrahydro-2H-pyran-3,4,5-triol.
A method of marking sheet metal for use in sheet metal work, the method comprising the following steps: - preparing marking information in digital format; - transmitting the marking information to a control unit of a marking system also comprising a sheet metal driving system; a sheet metal braking system; and a marking head; the sheet metal having a thickness of less than 10 mm, preferably between 0.4 mm and 1.5 mm; - inserting the sheet metal into the braking system and into the drive system; - exerting on the sheet metal, using the drive system, a drive force in a drive direction; - exerting a braking force on the sheet metal with the braking system opposing the driving force, so as to tension and flatten the sheet metal; and - marking the marking information on the tensioned sheet metal by means of the marking head placed in a marking plane between the drive system and the braking system, the marking plane being at a distance d from the sheet metal. - preparing marking information in digital format; - transmitting the marking information to a control unit of a marking system also comprising a sheet metal driving system; a sheet metal braking system; and a marking head; the sheet metal having a thickness of less than 10 mm, preferably between 0.4 mm and 1.5 mm; - inserting the sheet metal into the braking system and into the drive system; - exerting on the sheet metal, using the drive system, a drive force in a drive direction; - exerting a braking force on the sheet metal with the braking system opposing the driving force, so as to tension and flatten the sheet metal; and - marking the marking information on the tensioned sheet metal by means of the marking head placed in a marking plane between the drive system and the braking system, the marking plane being at a distance d from the sheet metal.
Method for an automatic calibration of a multistatic antenna array comprising N t transmitters and N r receivers, wherein a correction coefficient is determined for each combination of each transmitter T i with each receiver R j at each operation frequency by a calibration measurement represented by a matrix element T i j of a calibration matrix T, wherein an m th estimation for a refined calibration matrix T̂ m is determined by the step i. measuring initial matrix elements T ij, wherein T ij is the ratio of the measured magnitude and phase of a signal at receiver R j, which is emitted by transmitter T i and reflected by a known calibration object, to an expected received signal at receiver R j, wherein the m th estimation for the refined calibration matrix T̂ m is calculated from a preceding estimation T̂ m-1 by the operation T ^ m = 1 N t ⋅ N r ⋅ T ^ m − 1 ⋅ Λ T ^ m − 1 ⋅ T ^ m − 1 of matrix T̂ m-1 and an element-wise inverted and transposed matrix of matrix T̂ m-1 divided by a normalization factor, which equals to the total number of transmitters N t multiplied by the total number of receivers N r, wherein Λ is an elementwise inversion of transposed matrix T̂ m -1, wherein the first estimation is started with T̂ 0 which comprises the initial calibration matrix elements T ij measured in step i. i. measuring initial matrix elements T ij, wherein T ij is the ratio of the measured magnitude and phase of a signal at receiver R j, which is emitted by transmitter T i and reflected by a known calibration object, to an expected received signal at receiver R j,
A method, performed by a wireless device, of wireless communication between the wireless device and a network comprising a first node communicatively linked to the wireless device using a first communication link and a second node communicatively linked to the wireless device using a second communication link, the method comprising: sending from the wireless device uplink control signals for the first node indirectly via the second node using the second communication link; receiving by said wireless device downlink control signals originating from said first node directly using the first communication link; sending from said wireless device uplink control signals for said second node to said second node directly using said second communication link; receiving by said wireless device downlink control signals originating from said second node indirectly via said first node using said first communication link; sending from said wireless device uplink data signals to said first node indirectly via said second node using said second communication link; and receiving by said wireless device downlink data signals from said first node directly using said first communication link; wherein said uplink data signals and said uplink control signals are multiplexed onto a physical uplink shared channel, PUSCH, of said second communication link and wherein said downlink data signals and said downlink control signals are multiplexed onto a physical downlink shared channel, PDSCH, of said first communication link. sending from the wireless device uplink control signals for the first node indirectly via the second node using the second communication link; receiving by said wireless device downlink control signals originating from said first node directly using the first communication link; sending from said wireless device uplink control signals for said second node to said second node directly using said second communication link; receiving by said wireless device downlink control signals originating from said second node indirectly via said first node using said first communication link; sending from said wireless device uplink data signals to said first node indirectly via said second node using said second communication link; and receiving by said wireless device downlink data signals from said first node directly using said first communication link; wherein said uplink data signals and said uplink control signals are multiplexed onto a physical uplink shared channel, PUSCH, of said second communication link and wherein said downlink data signals and said downlink control signals are multiplexed onto a physical downlink shared channel, PDSCH, of said first communication link.
A wheel construction for e.g. a construction or agricultural machine, such as a tractor, where the wheel construction at least includes a first wheel rim made up of a first rim ring for mounting a first tyre and further including a first hub plate with an outer periphery, the first hub plate at outer periphery being fixed to the first rim ring at a distance X1 from an annular edge thereof, and extending internally in the first rim ring between the first rim ring and the central axis of the first wheel rim (rotary axis of the first wheel rim), the first hub plate at an inner periphery including a number of holes and a contact face for mechanical and detachable fixing to either a central hub plate or directly to a hub of a vehicle, wherein a possible central hub plate at an outer periphery includes a contact face and holes for direct or indirect joining with the first hub plate at its inner periphery, and at an inner periphery including a contact face and holes for joining with a hub on a vehicle, characterised in that the inner periphery on the first hub plate of the wheel construction is displaced by the distance Y1 along the central axis of the first wheel rim in relation to the outer periphery of the first hub plate, where the outer periphery of the first hub plate is circular/cylindrical as seen in direction of the central axis of the first wheel rim, where the first hub plate) is formed of a plane workpiece, as the workpiece is machined by a suitable cutting tool, such as a laser, plasma, water jet apparatus or the like, and includes a central part, where in radial direction a number of flaps, such as. 4, 6, 8, 10, 12 or more flaps extend from the central part, where part of these flaps are bent in a first direction, each with a design at the outer periphery such that by a set of bent flaps a circular/cylindrical outer periphery with a given diameter is formed.
A magnesium salt selected from one or more of the group consisting of magnesium glycinate, magnesium ascorbate, magnesium chloride, magnesium sulfate, magnesium orotate, magnesium citrate, magnesium fumarate, magnesium malate, magnesium succinate, magnesium tartrate and magnesium carbonate, in a solution comprising, citrate, water, glycerol and choline or phosphatidyl choline, for use in a method of treatment of magnesium deficit.
An adaptive aircraft electrical power distribution system, comprising: an aircraft power source configured to be disposed within an aircraft, the aircraft power source operable to generate and supply electrical power; a power connector configured to be mounted on a fuselage of the aircraft and adapted to connect to an external power cable to receive power from an external power source and to supply power to an external power load; an aircraft power distribution bus configured to be disposed within the aircraft and operable to distribute electrical power to an aircraft electrical load; and a bidirectional power controller configured to be mounted in the aircraft and electrically coupled to the aircraft power source, the aircraft power connector, and the aircraft power distribution bus, the bidirectional power controller configured to: sense when the aircraft power source is generating and supplying electrical power, sense when electrical power is being supplied to the power connector from the external power source, and selectively couple at least one of the aircraft power source or the power connector to the aircraft power distribution system. an aircraft power source configured to be disposed within an aircraft, the aircraft power source operable to generate and supply electrical power; a power connector configured to be mounted on a fuselage of the aircraft and adapted to connect to an external power cable to receive power from an external power source and to supply power to an external power load; an aircraft power distribution bus configured to be disposed within the aircraft and operable to distribute electrical power to an aircraft electrical load; and a bidirectional power controller configured to be mounted in the aircraft and electrically coupled to the aircraft power source, the aircraft power connector, and the aircraft power distribution bus, the bidirectional power controller configured to: sense when the aircraft power source is generating and supplying electrical power, sense when electrical power is being supplied to the power connector from the external power source, and selectively couple at least one of the aircraft power source or the power connector to the aircraft power distribution system.