mhurhangee/patent-ind-claim-en huggingface dataset:
A transistor comprising: a nanowire channel , wherein the nanowire channel includes nanowires and the nanowires are about 15 or less angstroms apart, characterized in that the nanowires are created from a MXene material. a nanowire channel , wherein the nanowire channel includes nanowires and the nanowires are about 15 or less angstroms apart, characterized in that the nanowires are created from a MXene material.
A receiving frame for immobilizing a cartridge having a connection feature to an automatic injector housing, the cartridge having a needle at its distal end, and is mechanically coupled in its proximal end to a plunger driver , comprising: a ventral side for fitting into a base portion of said automatic injector; and a dorsal side having: a cartridge mount for receiving said cartridge from above, said cartridge mount comprises a interference element with a distal stop , the interference element sized to slidably link to said connection feature and allow said cartridge to slide up to said distal stop , and a snap element allowing the interference element to receive the connection feature, but inhibiting disconnection of said cartridge ; and a driver mount , for fixedly containing said plunger driver , said driver mount comprising a walled container sized to at least partially surround said plunger driver and having an open top for receiving said plunger driver from above; wherein said cartridge and said driver mount are mechanically coupled through said plunger driver . a ventral side for fitting into a base portion of said automatic injector; and a dorsal side having: a cartridge mount for receiving said cartridge from above, said cartridge mount comprises a interference element with a distal stop , the interference element sized to slidably link to said connection feature and allow said cartridge to slide up to said distal stop , and a snap element allowing the interference element to receive the connection feature, but inhibiting disconnection of said cartridge ; and a driver mount , for fixedly containing said plunger driver , said driver mount comprising a walled container sized to at least partially surround said plunger driver and having an open top for receiving said plunger driver from above; a cartridge mount for receiving said cartridge from above, said cartridge mount comprises a interference element with a distal stop , the interference element sized to slidably link to said connection feature and allow said cartridge to slide up to said distal stop , and a snap element allowing the interference element to receive the connection feature, but inhibiting disconnection of said cartridge ; and a driver mount , for fixedly containing said plunger driver , said driver mount comprising a walled container sized to at least partially surround said plunger driver and having an open top for receiving said plunger driver from above; wherein said cartridge and said driver mount are mechanically coupled through said plunger driver .
A lithium-ion secondary battery comprising a positive electrode , a negative electrode , and a non-aqueous liquid electrolyte, the positive electrode comprising as a primary component of its positive electrode active material a lithium-containing olivine compound, the negative electrode comprising a negative current collector and a negative electrode active material layer formed on the negative current collector, the negative electrode active material layer comprising carbon particles as a negative electrode active material, the amount of the negative electrode active material contained in the negative electrode active material layer being 95 % by mass to 99 % by mass; the lithium-ion secondary battery being characterized in that the positive electrode further comprises 2 to 20 parts by mass of an activated carbon relative to 100 parts by mass of the positive electrode active material, the activated carbon has an average particle diameter of 0,1 μm to 50 μm, and the olivine compound is contained in an amount accounting for 80% by mass or greater of the positive electrode active material.
A SIK3 inhibitor for use in the treatment of a proliferative disorder, which is a cancer or tumour, in a subject, by inhibiting SIK3 and sensitising cells involved with the proliferative disorder to a cell-mediated immune response, the treatment comprising administering the SIK3 inhibitor to the subject; wherein: (i) the subject has a plasma concentration of TNF greater than 2 pg/mL; and/or (ii) the proliferative disorder is a solid tumour that, in the subject, has an intratumoural concentration of TNF greater than 0.5 pg/mL.
A wearable heart activity sensor device comprising: a substrate of optically transparent material arranged to face a skin of a user when the sensor device is worn by the user; at least one light emitting diode , LED, arranged on the substrate and arranged to emit light through the substrate; at least one photo sensor arranged on the substrate as spatially separated from the at least one LED and arranged to absorb light through the substrate, wherein the at least one LED and the at least one photo sensor are comprised in a photoplethysmogram sensor of the heart activity sensor device; characterized in that the wearable heart activity sensor device further comprises an overmold of optically non-transparent thermoplastic material covering the at least one light emitting diode, the at least one photo sensor and a space between the at least one light emitting diode and the at least one photo sensor. a substrate of optically transparent material arranged to face a skin of a user when the sensor device is worn by the user; at least one light emitting diode , LED, arranged on the substrate and arranged to emit light through the substrate; at least one photo sensor arranged on the substrate as spatially separated from the at least one LED and arranged to absorb light through the substrate, wherein the at least one LED and the at least one photo sensor are comprised in a photoplethysmogram sensor of the heart activity sensor device; characterized in that the wearable heart activity sensor device further comprises an overmold of optically non-transparent thermoplastic material covering the at least one light emitting diode, the at least one photo sensor and a space between the at least one light emitting diode and the at least one photo sensor.
Control system of a propulsion unit of a watercraft comprising: an engine electronic control unit configured to control an operating state of an engine ; a remote controller having a control lever and being capable of transmitting a control signal to the engine electronic control unit to achieve a target operating state; and an electronic remote control unit comprising an operating state determination means configured to determine whether the engine is in an operating state, a shift position detector configured to detect whether the shift is in neutral, and a lever position detector configured to detect whether the control lever is in a neutral position, characterised in that the electronic remote control unit is configured to control a shift actuator either to maintain or to change a shift position of the engine when a supply of electrical power from an electrical power source to the engine is stopped or resumed depending on whether the engine is in an operating state, and on a shift position, and on an operating position of the control lever . an engine electronic control unit configured to control an operating state of an engine ; a remote controller having a control lever and being capable of transmitting a control signal to the engine electronic control unit to achieve a target operating state; and an electronic remote control unit comprising an operating state determination means configured to determine whether the engine is in an operating state, a shift position detector configured to detect whether the shift is in neutral, and a lever position detector configured to detect whether the control lever is in a neutral position, characterised in that the electronic remote control unit is configured to control a shift actuator either to maintain or to change a shift position of the engine when a supply of electrical power from an electrical power source to the engine is stopped or resumed depending on whether the engine is in an operating state, and on a shift position, and on an operating position of the control lever .
Copolymer obtainable from the free-radical copolymerization at least of components a), b) and c) a) 25.0 to 80.0 mol% of one or more cationic monomers selected from the group consisting of cationic (meth)acrylamide monomers and diallyldimethylammonium chloride, and b) 1.0 to 50.0 mol% and preferably 1.0 to 10.0 mol% of one or more polyethylene glycol macromonomers, and c) 15.0 to 74.0 mol% of one or more uncharged acrylamide monomers, characterized in that the one or more polyethylene glycol macromonomers of component b) is/are selected from monomers of the formula (IV) H 2 C=CR x -Z-O-(C 3 H 6 O) l - (CH 2 CH 2 O) p -H (IV) in which R x is H or methyl, Z is O(CH 2 ) 4 , l on molar average is a number from 0 to 7 and preferably from 0 to 6, and p on molar average is a number from 1 to 150, preferably from 11 to 150 and more preferably from 12 to 150. a) 25.0 to 80.0 mol% of one or more cationic monomers selected from the group consisting of cationic (meth)acrylamide monomers and diallyldimethylammonium chloride, and b) 1.0 to 50.0 mol% and preferably 1.0 to 10.0 mol% of one or more polyethylene glycol macromonomers, and c) 15.0 to 74.0 mol% of one or more uncharged acrylamide monomers, R x is H or methyl, Z is O(CH 2 ) 4 , l on molar average is a number from 0 to 7 and preferably from 0 to 6, and p on molar average is a number from 1 to 150, preferably from 11 to 150 and more preferably from 12 to 150.
An aircraft comprising a gas turbine engine , a fuselage and at least one wing extending from the fuselage ; the gas turbine engine having a nacelle attached to the at least one wing , a fan received within the nacelle ; and an engine core received within the nacelle ; and the nacelle having a longitudinal centre line , an inboard end defined as an end proximate a fuselage , an outboard end defined as an end that is azimuthally opposite to the inboard end , a leading edge , a trailing edge , and a nacelle length (L nac ) defined as an axial distance between the leading edge and the trailing edge ; wherein an azimuthal angle (θ) is defined about the longitudinal centre line , and wherein the nacelle length (L nac ) varies azimuthally; the aircraft being characterised in that the nacelle length (L nac ) decreases azimuthally at the leading edge of the nacelle from the inboard end of the nacelle to the outboard end of the nacelle . the gas turbine engine having a nacelle attached to the at least one wing , a fan received within the nacelle ; and an engine core received within the nacelle ; and the nacelle having a longitudinal centre line , an inboard end defined as an end proximate a fuselage , an outboard end defined as an end that is azimuthally opposite to the inboard end , a leading edge , a trailing edge , and a nacelle length (L nac ) defined as an axial distance between the leading edge and the trailing edge ; wherein an azimuthal angle (θ) is defined about the longitudinal centre line , and wherein the nacelle length (L nac ) varies azimuthally; the aircraft being characterised in that the nacelle length (L nac ) decreases azimuthally at the leading edge of the nacelle from the inboard end of the nacelle to the outboard end of the nacelle .
A transmitter comprising: means for generating a drive waveform signal ; power supply means ; amplifier means connected to the power supply and the means for generating a drive waveform signal for producing an output drive signal based on the drive waveform signal ; output means for acting on the output drive signal to generate an output signal having a current and a voltage; and feedback means for providing feedback to the means for generating a drive waveform signal on the basis of the output signal; characterised in that the feedback comprises in-phase and quadrature components of the current and voltage of the output signal. means for generating a drive waveform signal ; power supply means ; amplifier means connected to the power supply and the means for generating a drive waveform signal for producing an output drive signal based on the drive waveform signal ; output means for acting on the output drive signal to generate an output signal having a current and a voltage; and feedback means for providing feedback to the means for generating a drive waveform signal on the basis of the output signal; characterised in that the feedback comprises in-phase and quadrature components of the current and voltage of the output signal.
A component of an integrally detachable valve clamp and delivery system thereof, characterized in that , a control handle, a delivery catheter connected to the control handle, and a valve clamp connected to the delivery catheter , wherein the valve clamp is equipped with an inner catheter and an outer catheter , both of which are equipped with detachable connection mechanisms ; the delivery catheter comprises a first delivery catheter , a central control unit , and a second delivery catheter ; the distal parts of both the first delivery catheter and the second delivery catheter are equipped with releasable connection mechanisms that match the detachable connection mechanisms ; when pre-installed, the detachable connection mechanism on the inner catheter is connected to the releasable connection mechanism on the first delivery catheter through the central control unit , forming a first disassembly part , while the detachable connection mechanism on the outer catheter is connected to the releasable connection mechanism on the second delivery catheter through the central control unit , forming a second disassembly part ; when the central control unit is moved away from the first disassembly part and the second disassembly part , the first delivery catheter separates from the inner catheter , and the second delivery catheter separates from the outer catheter .
A thermoelectric conversion module comprising: n-type thermoelectric conversion elements and p-type thermoelectric conversion elements , each of which is alternately connected in series through an electrode plate , wherein the n-type thermoelectric conversion elements and the p-type thermoelectric conversion elements are formed of materials having different thermal expansion coefficients, one surface side of each of the n-type thermoelectric conversion elements and one surface side of each of the p-type thermoelectric conversion elements are aligned and joined on one surface side of an insulating substrate , characterised in that a thermal conductive member is formed independently on each of other surface sides of the n-type thermoelectric conversion elements and on each of other surface sides of the p-type thermoelectric conversion elements. n-type thermoelectric conversion elements and p-type thermoelectric conversion elements , each of which is alternately connected in series through an electrode plate , wherein the n-type thermoelectric conversion elements and the p-type thermoelectric conversion elements are formed of materials having different thermal expansion coefficients, one surface side of each of the n-type thermoelectric conversion elements and one surface side of each of the p-type thermoelectric conversion elements are aligned and joined on one surface side of an insulating substrate , characterised in that
A method of deploying a constellation of spacecraft, the method comprising: releasing a cluster of spacecraft from a launch vehicle at a first orbit ; separating spacecraft in the cluster of spacecraft from each other to minimize overlapping visibility periods from a ground station ; and raising each of the spacecraft as separated simultaneously in a synchronized ascent to a respective final orbit ; the method characterised in that raising each of the spacecraft as separated simultaneously in the synchronized ascent to the respective final orbit comprises: sending a timed command to each of the spacecraft, when visible to the ground station, indicating to maneuver to the respective final orbit, wherein the timed command indicates when to begin the maneuver in order to achieve the synchronized ascent and to maintain the relative phasing of each spacecraft to each other. releasing a cluster of spacecraft from a launch vehicle at a first orbit ; separating spacecraft in the cluster of spacecraft from each other to minimize overlapping visibility periods from a ground station ; and raising each of the spacecraft as separated simultaneously in a synchronized ascent to a respective final orbit ; the method characterised in that raising each of the spacecraft as separated simultaneously in the synchronized ascent to the respective final orbit comprises: sending a timed command to each of the spacecraft, when visible to the ground station, indicating to maneuver to the respective final orbit, wherein the timed command indicates when to begin the maneuver in order to achieve the synchronized ascent and to maintain the relative phasing of each spacecraft to each other.
A puncture tool guiding device for guiding a puncture tool to form a pilot hole through which a pedicle screw is buried in a pedicle, the puncture tool guiding device comprising: a linear reference pin that is disposed forward from a rear side of a spine toward a target point of a pedicle base and serves as a reference, a tubular sleeve having a sleeve central axis disposed at a predetermined insertion angle to the reference pin, and having a distal end that is open toward the target point and through which the puncture tool is passed and guided, and a rod member that couples a proximal side of the reference pin to the sleeve and maintains the sleeve central axis at the predetermined insertion angle to the reference pin, characterised in that slit for confirming, by an X-ray fluoroscopic image, whether or not the puncture tool guiding device is installed accurately on the pedicle is formed in a side surface of the sleeve, and the slit is formed such that a cutting direction of the slit is orthogonal to the reference pin. a linear reference pin that is disposed forward from a rear side of a spine toward a target point of a pedicle base and serves as a reference, a tubular sleeve having a sleeve central axis disposed at a predetermined insertion angle to the reference pin, and having a distal end that is open toward the target point and through which the puncture tool is passed and guided, and a rod member that couples a proximal side of the reference pin to the sleeve and maintains the sleeve central axis at the predetermined insertion angle to the reference pin, characterised in that slit for confirming, by an X-ray fluoroscopic image, whether or not the puncture tool guiding device is installed accurately on the pedicle is formed in a side surface of the sleeve, and the slit is formed such that a cutting direction of the slit is orthogonal to the reference pin.
A process for increasing the proportion of the 7β-epimer in an 7α/7β-epimer mixture of a 7-substituted 6α,14α-ethenomorphinan or a 7-substituted 6α,14α-ethanomorphinan, said process comprising: contacting a solution of the 7α/7β-epimer mixture with an acid to provide a precipitate, and isolating the precipitate to provide an isolated precipitate and a mother liquor, wherein the acid is an achiral acid, and wherein the acid is an aliphatic monocarboxylic acid which is optionally substituted. contacting a solution of the 7α/7β-epimer mixture with an acid to provide a precipitate, and isolating the precipitate to provide an isolated precipitate and a mother liquor, wherein the acid is an achiral acid, and wherein the acid is an aliphatic monocarboxylic acid which is optionally substituted.
A temperature measuring device comprising: an electrical temperature measuring instrument comprising a temperature sensitive section and wires connected with the temperature sensitive section , and configured to measure a temperature of the temperature sensitive section electrically; a heat transfer part formed of an elastomer in which the temperature sensitive section is embedded; and a heat insulation part formed of an elastomer covering a single surface of the heat transfer part , the heat transfer part having a thermal conductivity that is greater than a thermal conductivity of the heat insulation part , a mounting section being formed at the heat insulation part , the mounting section being to be mounted at a mounting location , characterized in that the electrical temperature measuring instrument comprises a flexible printed substrate onto which the wires are fixed, end portions of the wires and an end portion of the flexible printed substrate being embedded in the heat insulation part and the heat transfer part . an electrical temperature measuring instrument comprising a temperature sensitive section and wires connected with the temperature sensitive section , and configured to measure a temperature of the temperature sensitive section electrically; a heat transfer part formed of an elastomer in which the temperature sensitive section is embedded; and a heat insulation part formed of an elastomer covering a single surface of the heat transfer part , the heat transfer part having a thermal conductivity that is greater than a thermal conductivity of the heat insulation part , a mounting section being formed at the heat insulation part , the mounting section being to be mounted at a mounting location , characterized in that the electrical temperature measuring instrument comprises a flexible printed substrate onto which the wires are fixed, end portions of the wires and an end portion of the flexible printed substrate being embedded in the heat insulation part and the heat transfer part .
A heat-absorbing soda lime silica glass plate containing iron, tin, selenium, cobalt and sulfur, wherein the mass ratio of divalent iron as calculated as Fe 2 O 3 to total iron as calculated as Fe 2 O 3 is at least 55%, as represented by mass% based on oxides total iron as calculated as Fe 2 O 3 : 0.01 to 1.0%, total tin as calculated as SnO 2 : 0.02 to 0.3%, Se : 0.0003 to 0.0020%, CoO : 0.0010 to 0.0060%, and total sulfur as calculated as SO 3 : 0.001 to 0.1%, the ratio Tv/Te of the visible light transmittance Tv (by illuminant A, 2° visual field) as defined in JIS R3106 calculated as 4 mm thickness of the glass plate to the solar transmittance Te as defined in JIS R3106 calculated as 4 mm thickness of the glass plate, is at least 1.5, the visible light transmittance Tv (by illuminant A, 2° visual field) is at most 65% as defined in JIS R3106 calculated as 4 mm thickness of the glass plate, the excitation purity Pe is at most 7% as defined in JIS Z8701 calculated as 4 mm thickness of the glass plate, the dominant wavelength Dw of the transmitted light calculated as 4 mm thickness of the glass plate, as defined in JIS Z8701 , is at most 510 nm, and the ratio of SnO 2 /SO 3 to Fe-redox ((SnO 2 /SO 3 )/Fe-redox) is at least 0.20.