mhurhangee/ep-ind-claims huggingface dataset:
An apparatus comprising: an acquisition unit (155, 235) configured to acquire information indicating a plurality of second base stations located within coverage of a first base station connected to a wired backhaul; a grouping unit (153, 233) configured to perform grouping of the plurality of second base stations based on - information relating to traffic of each of the plurality of second base stations, and/or - a measurement result obtained by measurement of a reference signal by each of the plurality of second base stations, wherein the measurement result includes measurements of each of different sets of the reference signal, wherein the second base stations capable of having mutually independent paths in wireless communication with the first base station are placed in a same group; and a controller (157, 237) configured to control establishment of a wireless backhaul between the first base station and each of second base stations in the group. an acquisition unit (155, 235) configured to acquire information indicating a plurality of second base stations located within coverage of a first base station connected to a wired backhaul; a grouping unit (153, 233) configured to perform grouping of the plurality of second base stations based on - information relating to traffic of each of the plurality of second base stations, and/or - a measurement result obtained by measurement of a reference signal by each of the plurality of second base stations, wherein the measurement result includes measurements of each of different sets of the reference signal, - information relating to traffic of each of the plurality of second base stations, and/or - a measurement result obtained by measurement of a reference signal by each of the plurality of second base stations, wherein the measurement result includes measurements of each of different sets of the reference signal, wherein the second base stations capable of having mutually independent paths in wireless communication with the first base station are placed in a same group; and a controller (157, 237) configured to control establishment of a wireless backhaul between the first base station and each of second base stations in the group.
An ultrasonic tool or instrument, comprising: a probe shaft having a proximal end portion and a distal end portion, said distal end portion having an axis of symmetry; a coupling at a proximal end of said shaft for connecting the probe to a source of ultrasonic vibrational energy; and a head at a distal end of said distal end portion of said shaft, said head extending eccentrically in a transverse direction to one side of said shaft, said head having an operative tip or surface spaced laterally from said axis, whereby said distal end portion and said proximal end portion of said shaft are straight or linear, said distal end portion of said shaft being connected to said proximal end portion at a bend junction, said distal end portion being disposed at an angle (θ) relative to said proximal end portion; said head extends eccentrically in a transverse direction to one side of said distal end portion of said shaft; said operative tip or surface of said head is a knurled surface for use in bone abrasion; said head is formed with one through hole for reducing mass of said head and concomitantly eccentric mass of the probe, said head having a proximal edge forming a corner (30, 26) with said operative tip or surface, said proximal edge extending at least partially transversely to said axis of symmetry, said head having a distal edge extending at least partially transversely to said axis of symmetry, said through hole being disposed eccentrically relative to said head, closer to said proximal edge than said distal edge or in said corner (30, 26). a probe shaft having a proximal end portion and a distal end portion, said distal end portion having an axis of symmetry; a coupling at a proximal end of said shaft for connecting the probe to a source of ultrasonic vibrational energy; and a head at a distal end of said distal end portion of said shaft, said head extending eccentrically in a transverse direction to one side of said shaft, said head having an operative tip or surface spaced laterally from said axis, whereby said distal end portion and said proximal end portion of said shaft are straight or linear, said distal end portion of said shaft being connected to said proximal end portion at a bend junction, said distal end portion being disposed at an angle (θ) relative to said proximal end portion; said head extends eccentrically in a transverse direction to one side of said distal end portion of said shaft; said operative tip or surface of said head is a knurled surface for use in bone abrasion; said head is formed with one through hole for reducing mass of said head and concomitantly eccentric mass of the probe, said head having a proximal edge forming a corner (30, 26) with said operative tip or surface, said proximal edge extending at least partially transversely to said axis of symmetry, said head having a distal edge extending at least partially transversely to said axis of symmetry, said through hole being disposed eccentrically relative to said head, closer to said proximal edge than said distal edge or in said corner (30, 26).
A tool cartridge for a material removal tool, comprising: a cartridge body; an axial adjustment screw at a first end of the cartridge body; a clamping screw and an opening for the clamping screw proximate the first end of the cartridge body; a seat for a cutting tool insert at a second end of the cartridge body; a recess extending through at least a portion of the cartridge body from a first side toward a second side, a long axis of the recess non-parallel to a long axis of the cartridge body and at least a portion of the recess open to a bottom side of the cartridge body; and a differential screw and a threaded opening for a differential screw proximate the second end and positioned longitudinally between the opening for the clamping screw and at least a portion of the seat, wherein a thread axis of the threaded opening for the differential screw is at an angle G relative to a long axis of the tool cartridge wherein the cartridge includes a pad positioned in the threaded opening for the differential screw at the bottom surface of the cartridge body, and body, wherein the pad is in operative communication with the differential screw at a first end to translate motion of the differential screw to change a protrusion position of a surface of the pad relative to the bottom surface of the cartridge body. a cartridge body; an axial adjustment screw at a first end of the cartridge body; a clamping screw and an opening for the clamping screw proximate the first end of the cartridge body; a seat for a cutting tool insert at a second end of the cartridge body; a recess extending through at least a portion of the cartridge body from a first side toward a second side, a long axis of the recess non-parallel to a long axis of the cartridge body and at least a portion of the recess open to a bottom side of the cartridge body; and a differential screw and a threaded opening for a differential screw proximate the second end and positioned longitudinally between the opening for the clamping screw and at least a portion of the seat,
A method of controlling turbine blade tip-to-static structure clearance in a gas turbine engine that is installed on an aircraft and that includes a turbine shroud and a turbine case, the method comprising the steps of: processing aircraft data to determine when the aircraft is flying at altitude cruise conditions; directing compressor discharge air to impinge upon at least a portion of the turbine shroud when it is determined that the aircraft is not flying at altitude cruise conditions; and upon determining that the aircraft is flying at altitude cruise conditions, directing the compressor discharge air to flow across at least a portion of the turbine case and to impinge upon at least a portion of the turbine shroud, wherein altitude cruise conditions means the aircraft is flying at a substantially constant altitude and the engine is operating at substantially constant engine power. processing aircraft data to determine when the aircraft is flying at altitude cruise conditions; directing compressor discharge air to impinge upon at least a portion of the turbine shroud when it is determined that the aircraft is not flying at altitude cruise conditions; and upon determining that the aircraft is flying at altitude cruise conditions, directing the compressor discharge air to flow across at least a portion of the turbine case and to impinge upon at least a portion of the turbine shroud, wherein altitude cruise conditions means the aircraft is flying at a substantially constant altitude and the engine is operating at substantially constant engine power.
A method for driving an actuator of a circuit breaker, the method comprising the steps of: supplying a coil of the actuator with a first voltage, such that the coil generates a magnetic field which causes an armature to move relative to a stator of the actuator from a closed position to an opened position, characterized in that it further comprises: supplying the coil with a second voltage of reverse polarity with respect to the first voltage while the armature is moving relative to the stator such that the coil generates a reverse magnetic field which decelerates the relative movement of the stator and the armature. supplying a coil of the actuator with a first voltage, such that the coil generates a magnetic field which causes an armature to move relative to a stator of the actuator from a closed position to an opened position, characterized in that it further comprises: supplying the coil with a second voltage of reverse polarity with respect to the first voltage while the armature is moving relative to the stator such that the coil generates a reverse magnetic field which decelerates the relative movement of the stator and the armature. supplying the coil with a second voltage of reverse polarity with respect to the first voltage while the armature is moving relative to the stator such that the coil generates a reverse magnetic field which decelerates the relative movement of the stator and the armature.
An exhaust grille comprising an array of air flow redirecting members positioned relative to each other in spaced overlapping relation to define passages therebetween so that substantially all the air incident on said grille is diverted by said air flow redirecting members through said passages whilst sound waves are reflected by said air flow redirecting members to prevent the sound waves from passing through said passages, characterised in that said air flow redirecting members are positioned relative to each other and shaped so that there is substantially no linear air flow path through the passages between said air flow redirecting members irrespective of the direction or angle of incidence of the air flow toward said air flow redirecting members.
A nasal cannula assembly for respiratory therapy, the assembly comprising: - a console having a display screen, controls, a first gas supply tube port, and a second gas supply tube port, wherein the console outputs breathing gas from the first gas supply tube port and the second gas supply tube port; - a first gas supply tube coupled to the first gas supply tube port and having a first connector; - a second gas supply tube coupled to the second gas supply port and having a second connector; and - a nasal cannula body comprising: - a first end coupled to the first connector; - a second end coupled to the second connector; - a longitudinal axis extending from the first end to the second end; - a first nasal prong in fluid communication with the first gas supply tube; and - a second nasal prong in fluid communication with the second gas supply tube; wherein - the first nasal prong is rotatable about the longitudinal axis relative to a position of the second nasal prong. - a console having a display screen, controls, a first gas supply tube port, and a second gas supply tube port, wherein the console outputs breathing gas from the first gas supply tube port and the second gas supply tube port; - a first gas supply tube coupled to the first gas supply tube port and having a first connector; - a second gas supply tube coupled to the second gas supply port and having a second connector; and - a nasal cannula body comprising: - a first end coupled to the first connector; - a second end coupled to the second connector; - a longitudinal axis extending from the first end to the second end; - a first nasal prong in fluid communication with the first gas supply tube; and - a second nasal prong in fluid communication with the second gas supply tube; - a first end coupled to the first connector; - a second end coupled to the second connector; - a longitudinal axis extending from the first end to the second end; - a first nasal prong in fluid communication with the first gas supply tube; and - a second nasal prong in fluid communication with the second gas supply tube; - the first nasal prong is rotatable about the longitudinal axis relative to a position of the second nasal prong.
An oligo-DNA chip comprising an oligo-DNA and a self-assembled monolayer solid substrate and prepared by fixing said oligo-DNA on the self-assembled monolayer solid substrate through multi-molecular recognition, characterized in that: - said oligo-DNA has 9 - 12 consecutive guanine bases attached thereto; - said self-assembled monolayer solid substrate comprises a solid substrate selected from gold and a self-assembled monolayer attached on the solid substrate; and - said self-assembled monolayer solid substrate is formed by attaching an aminocalixarene represented by Formula 6 to the solid substrate; and wherein, R 1, R 2, R 3, R 4, R 5, R 6, R 7, R 8, R' 1, R' 2, R' 3, R' 4, R' 5, R' 6, R' 7, R' 8 are independently selected from the group consisting of -H, -CH 3, -C 2 H 5, -C 3 H 7, -OCH 3, -Cl, -C 6 H 5,-OH, -OCH 2 CH 3, -Br, -CF 3, -OCH 2 C 6 H 5, -OC 6 H 5, -OC 6 H 4 CH 3, -OC 6 H 4 C(CH 3) 3, -OC 6 H 4 CF 3, -OC 6 H 4 Cl, -OCOCH 3,-NHCOCH 3, -CONHCH 3, -CN, COOH, and -COOR, wherein R represents -CH 3 or -C 2 H 5; and said Y 1, Y 2, Y 3 and Y 4 are independently selected from the group consisting of -H, and -(CH 2) n -SH, wherein, n= 2-15, and -C6H4- and -C6H5 are defined as a phenyl group, wherein the aminocalixarene having a thiol group at its terminal group is attached to the gold substrate to form said self assembled monolayer solid substrate. - said oligo-DNA has 9 - 12 consecutive guanine bases attached thereto; - said self-assembled monolayer solid substrate comprises a solid substrate selected from gold and a self-assembled monolayer attached on the solid substrate; and - said self-assembled monolayer solid substrate is formed by attaching an aminocalixarene represented by Formula 6 to the solid substrate; and wherein, R 1, R 2, R 3, R 4, R 5, R 6, R 7, R 8, R' 1, R' 2, R' 3, R' 4, R' 5, R' 6, R' 7, R' 8 are independently selected from the group consisting of -H, -CH 3, -C 2 H 5, -C 3 H 7, -OCH 3, -Cl, -C 6 H 5,-OH, -OCH 2 CH 3, -Br, -CF 3, -OCH 2 C 6 H 5, -OC 6 H 5, -OC 6 H 4 CH 3, -OC 6 H 4 C(CH 3) 3, -OC 6 H 4 CF 3, -OC 6 H 4 Cl, -OCOCH 3,-NHCOCH 3, -CONHCH 3, -CN, COOH, and -COOR, wherein R represents -CH 3 or -C 2 H 5; and said Y 1, Y 2, Y 3 and Y 4 are independently selected from the group consisting of -H, and -(CH 2) n -SH, wherein, n= 2-15, and -C6H4- and -C6H5 are defined as a phenyl group, wherein the aminocalixarene having a thiol group at its terminal group is attached to the gold substrate to form said self assembled monolayer solid substrate.
An aerosol-generating device comprising: a housing having a chamber sized to receive at least a portion of an aerosol-forming article; a first helical inductor coil disposed at least partially around, or adjacent to, the chamber; a second helical inductor coil disposed at least partially around, or adjacent to, the chamber, wherein the first helical inductor coil is part of a first circuit having a first resonant frequency and the second helical inductor coil forms part of a resonant circuit having a second resonant frequency, and an elongate susceptor element inductively heatable by one or both of the first and second helical inductor coils to heat at least a portion of an aerosol-forming substrate which is part of the aerosol-forming article, when the aerosol-forming substrate is at least partially received in the chamber. a housing having a chamber sized to receive at least a portion of an aerosol-forming article; a first helical inductor coil disposed at least partially around, or adjacent to, the chamber; a second helical inductor coil disposed at least partially around, or adjacent to, the chamber, wherein the first helical inductor coil is part of a first circuit having a first resonant frequency and the second helical inductor coil forms part of a resonant circuit having a second resonant frequency, and an elongate susceptor element inductively heatable by one or both of the first and second helical inductor coils to heat at least a portion of an aerosol-forming substrate which is part of the aerosol-forming article, when the aerosol-forming substrate is at least partially received in the chamber.
A method for rapid acquisition of MRI data at multiple points in time in an MRI scan, said method comprising the steps of: (a) repeatedly applying an RF excitation module consisting of an RF excitation pulse, a slice-selective magnetic field gradient pulse and a gradient blip in a primary phase encoding direction, whereby the same slice is excited by each RF excitation pulse; (b) acquiring an aliased k-space dataset at a point in time, whereby distinct k-space points are tagged and overlapped by application of said RF excitation modules by varying the amplitude and phase of the RF excitation pulses in time to obtain a k-t dataset; (c) undoing k-space aliasing in the acquired k-space datasets by Fourier transforming them along the time axis to separate the overlapped k-space points, the step of undoing k-space aliasing including a filtering process to separate the k-space points to produce an un-aliased k-t space dataset; and (d) performing a Fourier transformation along one or more axes of the un-aliased k-space datasets to generate image frames for the different time points at which data was acquired. (a) repeatedly applying an RF excitation module consisting of an RF excitation pulse, a slice-selective magnetic field gradient pulse and a gradient blip in a primary phase encoding direction, whereby the same slice is excited by each RF excitation pulse; (b) acquiring an aliased k-space dataset at a point in time, whereby distinct k-space points are tagged and overlapped by application of said RF excitation modules by varying the amplitude and phase of the RF excitation pulses in time to obtain a k-t dataset; (c) undoing k-space aliasing in the acquired k-space datasets by Fourier transforming them along the time axis to separate the overlapped k-space points, the step of undoing k-space aliasing including a filtering process to separate the k-space points to produce an un-aliased k-t space dataset; and (d) performing a Fourier transformation along one or more axes of the un-aliased k-space datasets to generate image frames for the different time points at which data was acquired.
An apparatus for a gas turbine engine comprising: a conduit comprising a first end, a second end, and a longitudinal axis, wherein the conduit defines an inner channel and is configured to extend through a vane cavity of a vane in a radial direction of the gas turbine engine; and a damping finger comprising a first portion coupled to the conduit and a second portion, wherein the damping finger is resiliently flexible and the second portion of the damping finger is configured to contact an inner surface of the vane, characterised in that the second portion is diverging outward from the first portion at an angle relative to the longitudinal axis of the conduit; and in that the first portion outward of the second portion in the radial direction when assembled within the gas turbine engine. a conduit comprising a first end, a second end, and a longitudinal axis, wherein the conduit defines an inner channel and is configured to extend through a vane cavity of a vane in a radial direction of the gas turbine engine; and a damping finger comprising a first portion coupled to the conduit and a second portion, wherein the damping finger is resiliently flexible and the second portion of the damping finger is configured to contact an inner surface of the vane, characterised in that the second portion is diverging outward from the first portion at an angle relative to the longitudinal axis of the conduit; and in that the first portion outward of the second portion in the radial direction when assembled within the gas turbine engine.
Analysis unit comprising a frontal plane, from which the analysis unit is accessible, and parallel mounting planes, which are arranged perpendicularly to the frontal plane; and a gas measurement device, characterized in that the gas measurement device has at least one connection housing part, through which an inlet channel extends from the mounting plane to a connection plane and through which an outlet channel extends from the connection plane to the one mounting plane; and a main housing part with a connection plane that corresponds to the connection plane of the connection housing part and on which the main housing part rests against the connection housing part, wherein the main housing part is equipped with an inflow channel, which is in fluid communication with the inlet channel of the connection housing part via the connection plane, and a recirculation channel, which is in fluid communication with the outlet channel of the connection housing part via the connection plane, wherein the corresponding connection planes are tilted at an angle of 45° from the mounting plane in direction of the frontal plane.
A method for detecting in real time in a living body an oxidation-reduction reaction of an endogenous biomolecule selected from a group consisting of ubiquinone and flavin adenine dinucleotide, which has been administered together with an electron donor to the living body, the method comprising observing an in vivo dynamics of a radical intermediate of said biomolecule, indicative of said oxidation-reduction reaction, by either (i) repeatedly applying an Overhauser MRI method and each time generating a corresponding MR image, wherein, for acquisition of MR data for each image, an electron spin resonance is excited in said radical intermediate, or (ii) repeatedly applying an EPR imaging method and each time generating a corresponding EPR image of said radical intermediate, a change of signal intensities in succesive MR or EPR images, respectively, being indicative of said oxidation-reduction reaction. (i) repeatedly applying an Overhauser MRI method and each time generating a corresponding MR image, wherein, for acquisition of MR data for each image, an electron spin resonance is excited in said radical intermediate, or (ii) repeatedly applying an EPR imaging method and each time generating a corresponding EPR image of said radical intermediate,
Method for serial data transfer from at least one slave, which provides the data bits of a measurement value acquired by at least one sensor to a master for bit-wise serial transmission, wherein the master requests a measurement value from the slave by means of a clock burst (38, 40) that comprises several clock cycles (TCLK), with their number being adapted to the number of the data bits that are to be transferred, characterized in that the number of data bits to be transferred from the slave to the master is adaptively determined and defined in the slave based on the number of clock cycles (TCLK) of a clock burst (38, 40) in the slave that is transferred from the master to the slave as preset by the master.