mhurhangee/ep-ind-claims huggingface dataset:
Temperature monitoring system for power transformers submerged in oil, wherein the system is adapted to carry out the temperature monitoring of power transformers based on the oil, coil and charging switch temperatures, wherein the oil temperature measurement is made redundantly, the system being characterized in that, in order to perform said redundant oil temperature measurement, the system comprises two RTD-type temperature sensors (1A, 1B) installable next to each other in the transformer lid that are connected to two independent measurement inlets in the temperature monitoring system, and in that: - if the two RTD-type temperature sensors (1A, 1B) measure approximately the same temperature, the system considers it is working under normal operation conditions and the arithmetic average of the measurements of both RTD-type temperature sensors (1A, 1B) is considered as oil temperature; and - if a maximum value admissible for a temperature difference in the measurement of both RTD-type temperature sensors (1A, 1B) is exceeded, the system considers that it is working under abnormal operation conditions due to problems in the measurement of one of the RTD-type temperature sensors (1A, 1B), wherein said maximum value admissible for the temperature difference of both RTD-type temperature sensors (1A, 1B) is programmed in the temperature monitoring system such that in the event of a defect of one of said sensors the measurement of that sensor is disregarded and the temperature monitoring system continues to operate by using the other sensor. - if the two RTD-type temperature sensors (1A, 1B) measure approximately the same temperature, the system considers it is working under normal operation conditions and the arithmetic average of the measurements of both RTD-type temperature sensors (1A, 1B) is considered as oil temperature; and - if a maximum value admissible for a temperature difference in the measurement of both RTD-type temperature sensors (1A, 1B) is exceeded, the system considers that it is working under abnormal operation conditions due to problems in the measurement of one of the RTD-type temperature sensors (1A, 1B), wherein said maximum value admissible for the temperature difference of both RTD-type temperature sensors (1A, 1B) is programmed in the temperature monitoring system
Portable crease removal apparatus comprising a handle and a steam-emitting head connected to an upper end of the handle, the steam-emitting head comprising a front end comprising a treatment face, provided with at least one steam outlet hole, intended to vertically face a piece of clothing to have creases removed when the apparatus is held in a vertical crease removal position, with the handle located under the head, the apparatus comprising an instant vaporisation chamber and a water reservoir supplying, by gravity, said instant vaporisation chamber when the apparatus occupies the vertical crease removal position, characterised in that the reservoir comprises a vent circuit which ensures that the reservoir is vented, both when the apparatus occupies the vertical crease removal position and when the apparatus occupies a horizontal crease removal position in which the treatment face is disposed in a horizontal plane and is oriented downwards.
An array substrate, comprising a base substrate and a plurality of pixel units arranged in matrix on the base substrate characterized in that, a first electrode groove and a second electrode groove separated from each other are arranged in a region of the base substrate corresponding to one of the pixel units, the first electrode groove and the second electrode groove respectively extending from an upper surface of the base substrate towards a lower surface of the base substrate; and the pixel unit includes a pixel electrode and a common electrode, the pixel electrode being arranged in the first electrode groove, and the common electrode being arranged in the second electrode groove.
A method for producing an anti-resonant hollow-core fiber which comprises a hollow core extending along a longitudinal axis of the fiber and a casing region that surrounds the hollow core and comprises a plurality of anti-resonant elements, comprising the method steps of: (a) providing a sheath tube which comprises a sheath tube inner bore and a sheath tube longitudinal axis, along which a sheath tube wall extends which is delimited by an inner face and an outer face, (b) providing a number of anti-resonant element preforms, (c) arranging the anti-resonant element preforms at desired positions on the inner face of the sheath tube wall to form a primary preform for the hollow-core fiber, which primary preform comprises a hollow core region and a casing region, and (d) further processing the primary preform to form a secondary preform from which the hollow-core fiber is drawn, the further processing comprising carrying out one or more of the following hot-forming processes once or repeatedly: (i) elongation, (ii) collapse, (iii) collapse and simultaneous elongation, (iv) collapse of additional casing material, (v) collapse of additional casing material and subsequent elongation, (vi) collapse of additional casing material and simultaneous elongation, characterized in that the provision of the sheath tube according to method step (a) comprises a machining measure in which the sheath tube wall is provided, by machining in the region of the target positions, with a longitudinal structure which extends in the direction of the sheath tube longitudinal axis and has longitudinal slots distributed around the circumference of the sheath tube wall and in that the anti-resonant element preforms are each arranged on a longitudinal slot. (a) providing a sheath tube which comprises a sheath tube inner bore and a sheath tube longitudinal axis, along which a sheath tube wall extends which is delimited by an inner face and an outer face, (b) providing a number of anti-resonant element preforms, (c) arranging the anti-resonant element preforms at desired positions on the inner face of the sheath tube wall to form a primary preform for the hollow-core fiber, which primary preform comprises a hollow core region and a casing region, and (d) further processing the primary preform to form a secondary preform from which the hollow-core fiber is drawn, the further processing comprising carrying out one or more of the following hot-forming processes once or repeatedly: (i) elongation, (ii) collapse, (iii) collapse and simultaneous elongation, (iv) collapse of additional casing material, (v) collapse of additional casing material and subsequent elongation, (vi) collapse of additional casing material and simultaneous elongation, (i) elongation, (ii) collapse, (iii) collapse and simultaneous elongation, (iv) collapse of additional casing material, (v) collapse of additional casing material and subsequent elongation, (vi) collapse of additional casing material and simultaneous elongation,
System for a wind turbine, the system comprising a first wind turbine structure, a second wind turbine structure, wherein the first wind turbine structure and the second wind turbine structure are rotatable with respect to each other, characterized in that the system comprises a safety bearing element (104, 104', 104") which is mounted to the first wind turbine structure such that the second wind turbine structure is in slideable contact with a contact surface of the safety bearing element (104, 104', 104") if a distance between the first wind turbine structure and the second wind turbine structure is reduced below a predetermined reference value, wherein the safety bearing element (104, 104', 104") comprises an electrical indicating circuitry with an indicating conductor, and wherein the electrical indicating circuitry is connectable to a wear controller system such that a signal is generatable by the electrical indicating circuitry and transmitted to the wear controller system until the indicating conductor is damaged due to the slideable contact of second wind turbine structure with the safety bearing element (104, 104', 104").
A gas reforming device comprising: a gas flow passage forming body; first and second cathodes (64, 65) which are arranged opposite to each other in said gas flow passage, individually having a grid shape and at least the surfaces thereof are made of an insulator; a common anode sandwiched between the respective surfaces of said first and second cathodes (64, 65) so as to be spaced apart therefrom in the direction parallel to the direction of gas flow in the gas flow passage, and a pulse power supply for applying a pulse voltage between the first cathode and said common anode and to between the second cathode and said common anode, so as to generate ion sheath layers spread on the respective surfaces of the first and second cathodes (64, 65), wherein said first and second cathodes (64, 65) are individually accompanied by grounding electrodes arranged on peripheral portions thereof so as, in operation, to contact end portions of said ion sheath layers thereby grounding said ion sheath layers, wherein in operation said pulse power supply is configured to form individually, from a process gas introduced in a direction parallel to a direction of shortest inter-electrode distances between said first cathode and said common anode and between said second cathode and said common anode, non-thermal equilibrium low-temperature plasmas between said first cathode and said common anode and between said second cathode and said common anode, and wherein said non-thermal equilibrium low-temperature plasmas are configured to activate the process gas so as to generate a reform gas. a gas flow passage forming body; first and second cathodes (64, 65) which are arranged opposite to each other in said gas flow passage, individually having a grid shape and at least the surfaces thereof are made of an insulator; a common anode sandwiched between the respective surfaces of said first and second cathodes (64, 65) so as to be spaced apart therefrom in the direction parallel to the direction of gas flow in the gas flow passage, and a pulse power supply for applying a pulse voltage between the first cathode and said common anode and to between the second cathode and said common anode, so as to generate ion sheath layers spread on the respective surfaces of the first and second cathodes (64, 65), wherein said first and second cathodes (64, 65) are individually accompanied by grounding electrodes arranged on peripheral portions thereof so as, in operation, to contact end portions of said ion sheath layers thereby grounding said ion sheath layers, wherein in operation said pulse power supply is configured to form individually, from a process gas introduced in a direction parallel to a direction of shortest inter-electrode distances between said first cathode and said common anode and between said second cathode and said common anode, non-thermal equilibrium low-temperature plasmas between said first cathode and said common anode and between said second cathode and said common anode, and wherein said non-thermal equilibrium low-temperature plasmas are configured to activate the process gas so as to generate a reform gas.
A method for transmitting a sounding reference signal, SRS, at a user equipment in a wireless communication system, the method comprising: receiving, from a base station, a downlink control information, DCI, through a Physical Downlink Control Channel, PDCCH, in a first subframe; detecting a sounding reference signal triggering indicator in the DCI; and transmitting, to the base station, the SRS in a transmission resource which is cell-specifically defined first after a second subframe, wherein the DCI includes an uplink grant or a downlink grant, wherein if the DCI includes the uplink grant, the second subframe is a subframe in which a Physical Uplink Shared Channel, PUSCH, indicated by the uplink grant is transmitted, and wherein if the DCI includes the downlink grant, the second subframe is a subframe in which a Physical Uplink Control Channel, PUCCH, corresponding to the downlink grant is transmitted. receiving, from a base station, a downlink control information, DCI, through a Physical Downlink Control Channel, PDCCH, in a first subframe; detecting a sounding reference signal triggering indicator in the DCI; and transmitting, to the base station, the SRS in a transmission resource which is cell-specifically defined first after a second subframe, wherein the DCI includes an uplink grant or a downlink grant, wherein if the DCI includes the uplink grant, the second subframe is a subframe in which a Physical Uplink Shared Channel, PUSCH, indicated by the uplink grant is transmitted, and wherein if the DCI includes the downlink grant, the second subframe is a subframe in which a Physical Uplink Control Channel, PUCCH, corresponding to the downlink grant is transmitted.
A knotless suture anchor guide device (10, 100, 200), comprising: a handle (12, 112, 212) and a shaft (14, 114, 214) extending distally from the handle (12, 112, 212), the shaft (14, 114, 214) having an inner lumen with a cross-sectional shape that includes a primary region (20, 20a, 20b) configured to receive a drill bit therethrough, and an offset region (22, 22a, 22b) configured to seat a length of suture such that the suture seats outside of the primary portion (20a, 20b) and thus does not come into contact with a cutting portion of the drill bit, characterised in that at least one of the shaft (14, 114, 214) and the handle (12, 112, 212) includes a suture-engaging feature (18, 118, 19) for engaging a suture extending through the inner lumen, and the shaft (14, 114, 214) includes a distal end with a relief cut-out (28, 128) formed therein for seating a suture extending through the inner lumen. a handle (12, 112, 212) and a shaft (14, 114, 214) extending distally from the handle (12, 112, 212), the shaft (14, 114, 214) having an inner lumen with a cross-sectional shape that includes a primary region (20, 20a, 20b) configured to receive a drill bit therethrough, and an offset region (22, 22a, 22b) configured to seat a length of suture such that the suture seats outside of the primary portion (20a, 20b) and thus does not come into contact with a cutting portion of the drill bit, characterised in that at least one of the shaft (14, 114, 214) and the handle (12, 112, 212) includes a suture-engaging feature (18, 118, 19) for engaging a suture extending through the inner lumen, and the shaft (14, 114, 214) includes a distal end with a relief cut-out (28, 128) formed therein for seating a suture extending through the inner lumen.
Method for controlling the attitude guidance of a satellite with respect to an orthogonal orbital reference system ( OXYZ) comprising a velocity axis, an orbital axis, and a Nadir axis, along a portion of its orbit around the Earth, said orbit portion being illuminated by solar radiation; the satellite moving in the direction of the velocity axis, the satellite comprising a main body, an optical instrument having a fixed observation axis relative to the main body, at least one solar generator that is fixed relative to the main body and defining a functional surface whose normal ( N, Na, Nb) has at least one component perpendicular to the velocity axis, at least one attitude control device, and a control unit connected to the attitude control device, said method comprising a first step of transmitting guidance commands from the control unit to the attitude control unit in order to direct the observation axis of the optical instrument towards the regions to be imaged, characterized in that the method comprises a second step of transmitting guidance commands from the control unit to the attitude control unit so as to orient the normal ( N, Na, Nb) to the functional surface in the direction of the solar radiation, and in that the guidance commands of the first and second steps are commands to rotate the satellite about the velocity axis only, the angle of rotation about the orbital axis and the Nadir axis within the orbital reference system being kept substantially at zero. characterized in that the method comprises a second step of transmitting guidance commands from the control unit to the attitude control unit so as to orient the normal ( N, Na, Nb) to the functional surface in the direction of the solar radiation, and in that the guidance commands of the first and second steps are commands to rotate the satellite about the velocity axis only, the angle of rotation about the orbital axis and the Nadir axis within the orbital reference system being kept substantially at zero.
A method for crystallising a substance, namely macromolecule, dissolved in a solvent, having the steps: - introducing a volume of solvent containing the substance into a chamber with a pre-set temperature, atmospheric humidity and gas composition, - adding a predetermined volume of a precipitant to the volume of solvent containing the substance, - allowing the solvent to evaporate while simultaneously observing changes in structure in the volume of solvent containing the substance and the precipitant by means of dynamic light scattering, - detecting weight changes and determining the molarities, - associating with the location in the phase diagram on the basis of the dynamic light scattering measurement and the results of the determination of molarity, - allowing a predetermined number of crystal nuclei to form by adding solvent or adding precipitant, - converting the volume of solvent containing the substance and the precipitant into a metastable state by adding solvent and/or protein solution or by allowing the concentration of the dissolved substance to reduce by allowing nucleation cores to form, - maintaining the metastable state by adding a predetermined quantity of the substance to the volume of solvent containing the substance and the precipitant or allowing the solvent to evaporate until at least one crystal of a predetermined size is formed. - introducing a volume of solvent containing the substance into a chamber with a pre-set temperature, atmospheric humidity and gas composition, - adding a predetermined volume of a precipitant to the volume of solvent containing the substance, - allowing the solvent to evaporate while simultaneously observing changes in structure in the volume of solvent containing the substance and the precipitant by means of dynamic light scattering, - detecting weight changes and determining the molarities, - associating with the location in the phase diagram on the basis of the dynamic light scattering measurement and the results of the determination of molarity, - allowing a predetermined number of crystal nuclei to form by adding solvent or adding precipitant, - converting the volume of solvent containing the substance and the precipitant into a metastable state by adding solvent and/or protein solution or by allowing the concentration of the dissolved substance to reduce by allowing nucleation cores to form, - maintaining the metastable state by adding a predetermined quantity of the substance to the volume of solvent containing the substance and the precipitant or allowing the solvent to evaporate until at least one crystal of a predetermined size is formed.
A multi-band communication device, the multi-band communication device comprising: a first wireless signal processing circuit for operating multiple first band signals; a second wireless signal processing circuit for operating multiple second band signals; an antenna switch module in communication with the first wireless signal processing circuit and the second wireless signal processing circuit for switching the first band signals and a first portion of the second band signals; a first antenna unit in communication with the antenna switch module; and a second antenna unit in communication with the second wireless signal processing circuit, wherein the frequency bands respectively supported by the first antenna unit and the second antenna do not overlap and characterized in that the second antenna unit is directly in communication with the second wireless signal processing circuit. a first wireless signal processing circuit for operating multiple first band signals; a second wireless signal processing circuit for operating multiple second band signals; an antenna switch module in communication with the first wireless signal processing circuit and the second wireless signal processing circuit for switching the first band signals and a first portion of the second band signals; a first antenna unit in communication with the antenna switch module; and a second antenna unit in communication with the second wireless signal processing circuit, wherein the frequency bands respectively supported by the first antenna unit and the second antenna do not overlap and characterized in that the second antenna unit is directly in communication with the second wireless signal processing circuit.
A tool for seating a tubeless tire on a rim using pressurized gas, the tool comprising: a portable cylindrical pressure vessel with an input port, said input port suitable for filling the cylindrical pressure vessel with said pressurized gas; a nozzle pneumatically coupled to an outlet on a distal end of the cylindrical pressure vessel, said nozzle configured to blow the pressurized gas between a rim and a tire bead; a gas valve configured to control a flow of the pressurized gas from the outlet on the distal end of the cylindrical pressure vessel; a pistol grip extending radially from the cylindrical pressure vessel; and a release control located at a position within 15 centimeters (cm) of the pistol grip; wherein the gas valve is configured to open in response to actuation of the release control, allowing the pressurized gas to flow through the outlet on the distal end of the cylindrical pressure vessel and out the nozzle. a portable cylindrical pressure vessel with an input port, said input port suitable for filling the cylindrical pressure vessel with said pressurized gas; a nozzle pneumatically coupled to an outlet on a distal end of the cylindrical pressure vessel, said nozzle configured to blow the pressurized gas between a rim and a tire bead; a gas valve configured to control a flow of the pressurized gas from the outlet on the distal end of the cylindrical pressure vessel; a pistol grip extending radially from the cylindrical pressure vessel; and a release control located at a position within 15 centimeters (cm) of the pistol grip; wherein the gas valve is configured to open in response to actuation of the release control, allowing the pressurized gas to flow through the outlet on the distal end of the cylindrical pressure vessel and out the nozzle.