mhurhangee/ep-ind-claims huggingface dataset:
A surgical system configured to determine a size of a vessel within a region proximate to a working end of a surgical instrument, comprising: at least one light emitter disposed at the working end of the surgical instrument; an array of light sensors disposed at the working end of the surgical instrument opposite the at least one light emitter, the array of light sensors comprising at least one row of light sensors; and a controller coupled to the array of light sensors, characterized in that individual light sensors in the row of light sensors of the array of light sensors are adapted to generate a signal comprising a pulsatile component and a non-pulsatile component; and the controller comprises a splitter to separate the pulsatile component from the non-pulsatile component and an analyzer to determine magnitudes of the non-pulsatile components at the individual light sensors in the row of light sensors, to determine a pair of positions of individual light sensors corresponding to a first transition in the non-pulsatile component from a higher magnitude to a lower magnitude and a second transition in the non-pulsatile component from a lower magnitude to a higher magnitude, and to determine a resting outer diameter of the vessel based on the pair of positions. at least one light emitter disposed at the working end of the surgical instrument; an array of light sensors disposed at the working end of the surgical instrument opposite the at least one light emitter, the array of light sensors comprising at least one row of light sensors; and a controller coupled to the array of light sensors, characterized in that individual light sensors in the row of light sensors of the array of light sensors are adapted to generate a signal comprising a pulsatile component and a non-pulsatile component; and the controller comprises a splitter to separate the pulsatile component from the non-pulsatile component and an analyzer to determine magnitudes of the non-pulsatile components at the individual light sensors in the row of light sensors, to determine a pair of positions of individual light sensors corresponding to a first transition in the non-pulsatile component from a higher magnitude to a lower magnitude and a second transition in the non-pulsatile component from a lower magnitude to a higher magnitude, and to determine a resting outer diameter of the vessel based on the pair of positions.
A metal structure for boating structural supports, including a plurality of metal support sections (6, 7) preferably made of aluminium alloy, each of which comprises a portion with a through-cavity having a closed polygonal cross-section and at least one edge portion with a substantially C-shaped cavity formed by two connecting edges extending from and integral with a side of said through-cavity portion, the metal structure further including metal brackets for mechanically assembling said support sections (6, 7) to each other, each of said metal brackets comprising a substantially right-triangular flat portion, at least two fastening holes to fasten the metal support sections (6, 7) to the bracket, and at least two locking tabs, each of which is inserted between said connecting edges of a respective metal support section (6, 7), characterized in that the connecting edges of the at least one edge portion are formed by two parallel side walls, each one extending perpendicularly from a side of the through-cavity portion, said side walls terminating in a pair of fins that extend perpendicularly from the respective sidewall towards each other and that define a groove there between, in that said flat portion rests on the fins of the edge portion of the support sections (6, 7) assembled together, and in that each locking tab is inserted in a groove and engaged between a pair of fins of the connecting edges of a metal support section (6, 7).
A printed circuit board (100, 200) comprising: - a base portion, - at least three finger portions (102, 103, 104) extending in a transversal direction with respect to said base portion and being substantially parallel to each other, wherein two adjacent finger portions (102, 103, 104) define an intermediate aperture with a shape corresponding to at least one of the finger portions, wherein the at least three finger portions (102, 103, 104) each have a plurality of longitudinal protrusions distributed along at least a first side of the at least three finger portions (102, 103, 104), wherein each of the at least three finger portions (102, 103, 104) is provided with a plurality of light emitting elements aligned in a first and a second row and wherein light emitting elements of at least one of the first or the second row are arranged on the protrusions, wherein an intermediate finger portion comprises an end portion protruding longitudinally beyond said plurality of longitudinal protrusions, wherein light emitting elements are arranged on the end portion. - a base portion, - at least three finger portions (102, 103, 104) extending in a transversal direction with respect to said base portion and being substantially parallel to each other,
A wind turbine blade for a wind turbine, the wind turbine blade comprising an electrical conductor extending in a longitudinal direction of the wind turbine blade, and a carbon fiber material (25, 39, 40) being electrically conductive and having a first portion which is arranged beside the electrical conductor, a second portion which is connected to the first portion and is attached and electrically connected to the electrical conductor, and a third portion which is connected to the second portion and at least partially overlaps with the first portion, wherein the third portion comprises one part which overlaps with the first portion and another part which does not overlap with the first portion, characterized in that the one part is triangular shaped.
An electromagnetic wave emission device comprising: a plurality of emission antennas that emit an electromagnetic wave output from an electromagnetic wave generation device; and a transmission system including an electromagnetic wave transmission line that extends from an output terminal of the electromagnetic wave generation device and that branches to a plurality of branching lines, wherein each of the plurality of the branching lines connects to a corresponding said emission antenna, wherein: the transmission system is configured such that the electromagnetic wave is supplied to a target antenna, wherein the target antenna is a said emission antenna where plasma exists in its neighborhood, and such that the electromagnetic wave distributed to the target antenna and the all or part of electromagnetic wave reflected in a said emission antenna that is different from the target antenna are provided to the target antenna; and the all or part of electromagnetic wave that is distributed to the target antenna and the all or part of the electromagnetic wave that is reflected in the antenna that is different from the target antenna are emitted from the target antenna to the plasma. a plurality of emission antennas that emit an electromagnetic wave output from an electromagnetic wave generation device; and a transmission system including an electromagnetic wave transmission line that extends from an output terminal of the electromagnetic wave generation device and that branches to a plurality of branching lines, wherein each of the plurality of the branching lines connects to a corresponding said emission antenna, the transmission system is configured such that the electromagnetic wave is supplied to a target antenna, wherein the target antenna is a said emission antenna where plasma exists in its neighborhood, and such that the electromagnetic wave distributed to the target antenna and the all or part of electromagnetic wave reflected in a said emission antenna that is different from the target antenna are provided to the target antenna; and the all or part of electromagnetic wave that is distributed to the target antenna and the all or part of the electromagnetic wave that is reflected in the antenna that is different from the target antenna are emitted from the target antenna to the plasma.
An automotive crashworthiness energy absorptive part (1, 11, 15, 21, 23) to be provided at a front portion or a rear portion of an automotive body and configured to be axially crushed when crashworthiness load is input from a front side or a rear side of the automotive body to absorb crashworthiness energy, the automotive crashworthiness energy absorptive part (1, 11, 15, 21, 23) comprising: a tubular member configured to be axially crushed in a longitudinal direction of the tubular member to absorb crashworthiness energy by repeatedly generating buckling deformation in a bellows shape, the tubular member made of a metal sheet having a top portion and side wall portions continuous to the top portion; and a resin (9, 13, 17, 27) configured to coat or patch at least inner surfaces of the top portion and the side wall portions of the tubular member, wherein the coated or patched resin (9, 13, 17, 27) has a thickness of 8 mm or less after being heated and forms at least a part of a peripheral wall portion in a closed cross-sectional space, and adheres to the inner surfaces with an adhesive strength of 10 MPa or more, and the resin (9, 13, 17, 27) is sandwiched between the metal sheets as the intervening object in the convex bending portion of the buckling deformation in a bellows shape so that the bending radius of the convex bending portion is made larger than the fracture limit for bending radius inherent in the metal sheets with the resin (9, 13, 17, 27) intervening, and fractures are prevented from occurring in the bellows-shaped bending portion of the tubular member. a tubular member configured to be axially crushed in a longitudinal direction of the tubular member to absorb crashworthiness energy by repeatedly generating buckling deformation in a bellows shape, the tubular member made of a metal sheet having a top portion and side wall portions continuous to the top portion; and a resin (9, 13, 17, 27) configured to coat or patch at least inner surfaces of the top portion and the side wall portions of the tubular member, wherein the coated or patched resin (9, 13, 17, 27) has a thickness of 8 mm or less after being heated and forms at least a part of a peripheral wall portion in a closed cross-sectional space, and adheres to the inner surfaces with an adhesive strength of 10 MPa or more, and the resin (9, 13, 17, 27) is sandwiched between the metal sheets as the intervening object in the convex bending portion of the buckling deformation in a bellows shape so that the bending radius of the convex bending portion is made larger than the fracture limit for bending radius inherent in the metal sheets with the resin (9, 13, 17, 27) intervening, and fractures are prevented from occurring in the bellows-shaped bending portion of the tubular member.
A compound according to formula I, II, or III where each R 1 is independently hydrogen, hydroxyl, thiol, halogen, lower alkyl, lower alkoxy, or lower alkyl ester; and each R 2, R 3, R 4, and R 5 independently is hydrogen, hydroxyl, thiol, or halogen.
An aerostat system that allows for improved control in a variety of wind conditions, passive alignment into the wind, and autonomous docking, the system comprising: an aerostat including a shroud; multiple tether groups arranged on the shroud so that there is defined a substantial separation distance between tether attachment points (104(a), 104(b), 108(a), 108(b)) in each of a longitudinal direction and a lateral direction, of said shroud; and a base station located with respect to a ground surface including a rotating platform, the platform being interconnected to the multiple tether groups, characterized in that each of the multiple tether groups is independently actuated by a respective winch assembly, and the platform includes a rail assembly that selectively engages the aerostat in a docked configuration with respect to the platform. an aerostat including a shroud; multiple tether groups arranged on the shroud so that there is defined a substantial separation distance between tether attachment points (104(a), 104(b), 108(a), 108(b)) in each of a longitudinal direction and a lateral direction, of said shroud; and a base station located with respect to a ground surface including a rotating platform, the platform being interconnected to the multiple tether groups,
Patient interface for affixment on onto a patient eye, said patient interface including - a negative pressure cavity with a top wall and a circumferential outer wall, - an optical passage, wherein the top wall circumferentially surrounds the optical passage and wherein the circumferential outer wall projects from the top wall and circumferentially surrounds the optical passage; - a number of rib members, the rib members projecting separately from each other from the top wall into the negative pressure cavity between the circumferential outer wall and the optical passage, characterized in that the rib members are arranged along tangents to a common circumferential curve, the circumferential curve being equidistant to the circumferential outer wall. - a negative pressure cavity with a top wall and a circumferential outer wall, - an optical passage, wherein the top wall circumferentially surrounds the optical passage and wherein the circumferential outer wall projects from the top wall and circumferentially surrounds the optical passage; - a number of rib members, the rib members projecting separately from each other from the top wall into the negative pressure cavity between the circumferential outer wall and the optical passage, characterized in that the rib members are arranged along tangents to a common circumferential curve, the circumferential curve being equidistant to the circumferential outer wall.
A water soluble photo-curable antistatic resin composition, comprising: in relation to total weight of the composition, 5 to 15wt.% of conductive fine particles containing carbon nanotubes; 0.1 to 5wt.% of fumed silica; 10 to 20wt.% of water soluble epoxy or urethane acrylate based oligomer; 20 to 75wt.% of mono-functional monomer or multi-functional monomer; 0.1 to 5wt.% of photo-polymerization initiator; 0.1 to 5wt.% of additive including at least one selected from a group consisting of adhesion enhancer, dispersing agent, defoaming agent, leveling agent and the like; and 50 to 150 parts by weight of pure water relative to total 100 weight of the above ingredients; wherein the conductive fine particles have 0.004 to 80wt.% of carbon nanotubes and further include antimony-doped tin oxide; wherein the conductive fine particles have particle diameter in the range of 5 to 200 nm.
A method for wireless communications performed by a user equipment, comprising: receiving, from a network entity, cell information for neighbor cells, wherein the cell information comprises a list of cell identifiers for a subset of neighbor cells operating in intra or inter frequency bands relative to a frequency band on which a serving cell is operating and time synchronization information for the neighbor cells; searching for synchronization symbols from the neighbor cells based on the cell information; based on the synchronization symbols from the neighbor cells, identifying one of the neighbor cells to perform a handover to; and initiating a handover from the serving cell to the identified one of the neighbor cells. receiving, from a network entity, cell information for neighbor cells, wherein the cell information comprises a list of cell identifiers for a subset of neighbor cells operating in intra or inter frequency bands relative to a frequency band on which a serving cell is operating and time synchronization information for the neighbor cells; searching for synchronization symbols from the neighbor cells based on the cell information; based on the synchronization symbols from the neighbor cells, identifying one of the neighbor cells to perform a handover to; and initiating a handover from the serving cell to the identified one of the neighbor cells.
A method for performing a chromatin immunoprecipitation assay using an antibody, comprising: a) isolating chromatin from a sample, by passing a liquid sample comprising chromatin through a rigid porous matrix on which a ligand is immobilized, wherein the ligand binds to a protein associated with the chromatin, and wherein the rigid porous matrix comprises sintered thermoplastic polymer particles in the form of a filter disc or frit; b) recovering DNA from the chromatin; and c) analysing the DNA. a) isolating chromatin from a sample, by passing a liquid sample comprising chromatin through a rigid porous matrix on which a ligand is immobilized, wherein the ligand binds to a protein associated with the chromatin, and wherein the rigid porous matrix comprises sintered thermoplastic polymer particles in the form of a filter disc or frit; b) recovering DNA from the chromatin; and c) analysing the DNA.
. An aerosol-generating device comprising: an air inlet; an air outlet; an air flow passage extending in a first direction between the air inlet and the air outlet; a heating element in the air flow passage for heating an aerosol-forming substrate; a first temperature sensor for measuring a first temperature at a first position along the air flow passage, wherein said first position is a position at the heating element and the first temperature is a temperature of the heating element at the first position; a second temperature sensor spaced apart in the first direction from the first sensor for measuring a second temperature at a second position along the air flow passage, wherein said second position is a position downstream of the heating element and said second temperature is an ambient temperature of the airflow passage at said second position; a third temperature sensor for measuring a third temperature at a third position along the airflow passage, wherein said third position is a position upstream of the heating element and said third temperature is an ambient temperature of the airflow passage at said third position; and a controller configured to control an operational parameter of the device based on the measured first temperature, the measured second temperature and the measured third temperature. an air inlet; an air outlet; an air flow passage extending in a first direction between the air inlet and the air outlet; a heating element in the air flow passage for heating an aerosol-forming substrate; a first temperature sensor for measuring a first temperature at a first position along the air flow passage, wherein said first position is a position at the heating element and the first temperature is a temperature of the heating element at the first position; a second temperature sensor spaced apart in the first direction from the first sensor for measuring a second temperature at a second position along the air flow passage, wherein said second position is a position downstream of the heating element and said second temperature is an ambient temperature of the airflow passage at said second position; a third temperature sensor for measuring a third temperature at a third position along the airflow passage, wherein said third position is a position upstream of the heating element and said third temperature is an ambient temperature of the airflow passage at said third position; and a controller configured to control an operational parameter of the device based on the measured first temperature, the measured second temperature and the measured third temperature.
Method for transmitting data in a network comprising a plurality M of communication apparatuses (20, 30), with M ≥ 2, wherein the plurality M comprises a first communication apparatus and a second communication apparatus, which are connected via a network connection section for the purpose of transmitting data, comprising: a) the first communication apparatus and the second communication apparatus each ascertaining a time-of-flight property of data transmitted between the first communication apparatus and the second communication apparatus via the network connection section, wherein the network connection section is in the form of a wired network connection section or in the form of an optical network connection section, b) the first communication apparatus and the second communication apparatus each deriving a secret by using the respective ascertained time-of-flight property, and c) transmitting a message protected by means of the derived secret between the first and the second communication apparatus (20, 30). a) the first communication apparatus and the second communication apparatus each ascertaining a time-of-flight property of data transmitted between the first communication apparatus and the second communication apparatus via the network connection section, wherein the network connection section is in the form of a wired network connection section or in the form of an optical network connection section, b) the first communication apparatus and the second communication apparatus each deriving a secret by using the respective ascertained time-of-flight property, and c) transmitting a message protected by means of the derived secret between the first and the second communication apparatus (20, 30).
A construction vehicle comprising a system for tracking a position of a working edge on an implement of the construction vehicle, the construction vehicle comprising the implement coupled to the construction vehicle at a pivot poin between a rigid member of the construction vehicle and the implement, a hydraulic mechanism coupled to the rigid member and configured to provide rotational movement of the implement, the system comprising: an angle sensor coupled to the implement and configured to determine rotation of the implement; a mounting mechanism on the rigid member, and a survey pole coupled to the mounting mechanism, wherein the mounting mechanism is configured for attaching the survey pole to the rigid member; a global navigation satellite system, GNSS, unit coupled to the survey pole, the mounting mechanism arranged relative to the rigid member so that the GNSS unit remains free from contact with any part of the construction vehicle, the implement, or the rigid member during a full range of motion of the rigid member, the GNSS unit arranged in a known spatial relationship with the pivot point between the rigid member of the construction vehicle and the implement, the GNSS unit configured to determine a position, a tilt, and a heading of the GNSS unit; characterised by a mobile controller configured for wireless communications with the GNSS unit and the angle sensor, the mobile controller configured to receive the position, the tilt, and the heading from the GNSS unit, and to receive the rotation of the implement from the angle sensor, the mobile controller configured to determine coordinates of the working edge of the implement in a real world coordinate frame. an angle sensor coupled to the implement and configured to determine rotation of the implement; a mounting mechanism on the rigid member, and a survey pole coupled to the mounting mechanism, wherein the mounting mechanism is configured for attaching the survey pole to the rigid member; a global navigation satellite system, GNSS, unit coupled to the survey pole, the mounting mechanism arranged relative to the rigid member so that the GNSS unit remains free from contact with any part of the construction vehicle, the implement, or the rigid member during a full range of motion of the rigid member, the GNSS unit arranged in a known spatial relationship with the pivot point between the rigid member of the construction vehicle and the implement, the GNSS unit configured to determine a position, a tilt, and a heading of the GNSS unit; characterised by a mobile controller configured for wireless communications with the GNSS unit and the angle sensor, the mobile controller configured to receive the position, the tilt, and the heading from the GNSS unit, and to receive the rotation of the implement from the angle sensor, the mobile controller configured to determine coordinates of the working edge of the implement in a real world coordinate frame.