mhurhangee/ep-ind-claims huggingface dataset:
An intravenous drip monitoring device, comprising: a processor; a weight sensor electrically connected to the processor, configured for detecting a weight information of drip, and transmitting the weight information to the processor; a communication module electrically connected to the processor, configured for transmitting a drip monitoring information to a first server; an alarm module electrically connected to the processor, configured for generating a warning signal; a power supply module electrically connected to the processor, the weight sensor, the communication module, and the alarm module, configured for supplying power source to the processor, the weight sensor, the communication module, and the alarm module; wherein the processor is configured for determining whether the weight information is less than or equal to a warning value, if the weight information is less than or equal to the warning value, controlling the alarm module to generate the warning signal, characterized in that the communication module is configured for receiving the warning value and a control information transmitted from the server and the processor is configured for enabling or disabling the alarm module according to the control information. a processor; a weight sensor electrically connected to the processor, configured for detecting a weight information of drip, and transmitting the weight information to the processor; a communication module electrically connected to the processor, configured for transmitting a drip monitoring information to a first server; an alarm module electrically connected to the processor, configured for generating a warning signal; a power supply module electrically connected to the processor, the weight sensor, the communication module, and the alarm module, configured for supplying power source to the processor, the weight sensor, the communication module, and the alarm module; wherein the processor is configured for determining whether the weight information is less than or equal to a warning value, if the weight information is less than or equal to the warning value, controlling the alarm module to generate the warning signal, characterized in that the communication module is configured for receiving the warning value and a control information transmitted from the server and the processor is configured for enabling or disabling the alarm module according to the control information.
An apparatus, comprising: a processor, configured to: receive one or more medical images that image at least part of an esophagus and at least part of a heart of a patient; receive positions, within the heart, of one or more electrodes that apply Radio Frequency energy to ablate tissue in the heart, in a coordinate system having a vertical axis, wherein the one or more electrodes are at a distal end of a medical device; register the positions of the one or more electrodes with the received medical images; and calculate, based on the registered positions and on the medical images, a subset of one or more smallest heights among respective heights of the electrodes above the esophagus of the patient along the vertical axis; and an output device, configured to present to a user an indication of the smallest heights. a processor, configured to: receive one or more medical images that image at least part of an esophagus and at least part of a heart of a patient; receive positions, within the heart, of one or more electrodes that apply Radio Frequency energy to ablate tissue in the heart, in a coordinate system having a vertical axis, wherein the one or more electrodes are at a distal end of a medical device; register the positions of the one or more electrodes with the received medical images; and calculate, based on the registered positions and on the medical images, a subset of one or more smallest heights among respective heights of the electrodes above the esophagus of the patient along the vertical axis; and receive one or more medical images that image at least part of an esophagus and at least part of a heart of a patient; receive positions, within the heart, of one or more electrodes that apply Radio Frequency energy to ablate tissue in the heart, in a coordinate system having a vertical axis, wherein the one or more electrodes are at a distal end of a medical device; register the positions of the one or more electrodes with the received medical images; and calculate, based on the registered positions and on the medical images, a subset of one or more smallest heights among respective heights of the electrodes above the esophagus of the patient along the vertical axis; and an output device, configured to present to a user an indication of the smallest heights.
A fan section for a gas turbine engine, comprising: a fan case surrounding a fan with fan blades; a liner disposed between the fan case and the fan, spaced a radial distance from the fan case to provide a gap, the liner including an aluminum liner; and at least one torque stop arranged between the fan case and the liner, the at least one torque stop includes rails glued with an adhesive to the aluminum liner and blocks glued with the adhesive to the fan case; wherein the at least one torque stop is frangible, the at least one torque stop prevents rotation of the liner relative to the fan case; and wherein the at least one torque stop and the adhesive can withstand a tangential load given by the equation (1+S)*T Rub /R FanCas /N TorqeStops where S is a safety factor, T Rub is a rub torque generated by a 1.3 Kg (2.5 lb) bird strike, R FanCase is a radius of the fan case, and N TorqeStops is the number of torque stops. a fan case surrounding a fan with fan blades; a liner disposed between the fan case and the fan, spaced a radial distance from the fan case to provide a gap, the liner including an aluminum liner; and at least one torque stop arranged between the fan case and the liner, the at least one torque stop includes rails glued with an adhesive to the aluminum liner and blocks glued with the adhesive to the fan case; wherein the at least one torque stop is frangible, the at least one torque stop prevents rotation of the liner relative to the fan case; and wherein the at least one torque stop and the adhesive can withstand a tangential load given by the equation (1+S)*T Rub /R FanCas /N TorqeStops where S is a safety factor, T Rub is a rub torque generated by a 1.3 Kg (2.5 lb) bird strike, R FanCase is a radius of the fan case, and N TorqeStops is the number of torque stops.
A composite brake disc for a disc brake of a utility vehicle having: - two friction rings (2, 3), - a pot-or neck-shaped connecting element that extends axially from an inner circumference of the friction rings (2, 3) to an axis of rotation of the composite brake disc and serves to fasten the composite brake disc to a wheel axle, - the connecting element having an outer surface that has extending from a front edge a plurality of first and second lugs (6, 7), the ends (8, 9) of which are alternately received in the friction rings (2, 3), - the ends of the first lugs being moulded into a first friction ring close to the outer surface of the connecting element and the ends of the second lugs being moulded into a second friction ring distant from the outer surface of the connecting element, - the lugs (6, 7) extending away from the outer surface of the connecting element axially in relation to the axis of rotation of the composite brake disc, characterised in that - the first lugs have a u-shaped bend in a region between the outer surface of the connecting element and the ends received in the friction ring, - at least some the first and second lugs (6, 7) being provided with at least one channel. - two friction rings (2, 3), - a pot-or neck-shaped connecting element that extends axially from an inner circumference of the friction rings (2, 3) to an axis of rotation of the composite brake disc and serves to fasten the composite brake disc to a wheel axle, - the connecting element having an outer surface that has extending from a front edge a plurality of first and second lugs (6, 7), the ends (8, 9) of which are alternately received in the friction rings (2, 3), - the ends of the first lugs being moulded into a first friction ring close to the outer surface of the connecting element and the ends of the second lugs being moulded into a second friction ring distant from the outer surface of the connecting element, - the lugs (6, 7) extending away from the outer surface of the connecting element axially in relation to the axis of rotation of the composite brake disc, - the first lugs have a u-shaped bend in a region between the outer surface of the connecting element and the ends received in the friction ring, - at least some the first and second lugs (6, 7) being provided with at least one channel.
A fastener cartridge assembly for use with a surgical instrument, wherein the fastener cartridge assembly comprises: a cartridge body including a deck with a longitudinal slot and a plurality of fastener cavities formed therein; at least one fastener removably positioned in each said fastener cavity; a sled configured to move along said longitudinal slot during a firing stroke, wherein said sled is positioned in a starting position prior to the firing stroke; and a cover removably positioned over at least a portion of said deck, wherein said cover comprises a locating fin structured and dimensioned to fit within said longitudinal slot, wherein said locating fin comprises a proximal portion; said sled comprising a distal edge, and characterized in that said proximal portion of said locating fin comprises a holding surface configured to retainingly engage said distal edge when said sled is in said starting position. a cartridge body including a deck with a longitudinal slot and a plurality of fastener cavities formed therein; at least one fastener removably positioned in each said fastener cavity; a sled configured to move along said longitudinal slot during a firing stroke, wherein said sled is positioned in a starting position prior to the firing stroke; and a cover removably positioned over at least a portion of said deck, wherein said cover comprises a locating fin structured and dimensioned to fit within said longitudinal slot, wherein said locating fin comprises a proximal portion; said sled comprising a distal edge, and characterized in that said proximal portion of said locating fin comprises a holding surface configured to retainingly engage said distal edge when said sled is in said starting position.
A method of bonding first and second glass panels to one another, so as to hermetically seal and isolate a cavity defined therebetween, the method comprising, a. providing a first homogeneous powder glass sealing composition comprising: i. 25-65 mol% Bi 2 O 3, ii. 3-60 mol% ZnO, iii. 4-65 mol% B 2 O 3, iv. no intentionally added oxides of silicon, and v. no intentionally added oxides of aluminum vi. 0.1-25 mol% of at least one selected from the group consisting of CuO, Fe 2 O 3, Co 2 O 3, MnO, NiO, Cr 2 O 3; b. providing a second homogeneous powder glass sealing composition comprising: i. 25-65 mol% Bi 2 O 3, ii. 3-60 mol% ZnO, iii. 4-65 mol% B 2 O 3, iv. no intentionally added oxides of silicon, and v. no intentionally added oxides of aluminum vi. 0.1-25 mol% of at least one colorant selected from the group consisting of CuO, Fe 2 O 3, Co 2 O 3, MnO, NiO, Cr 2 O 3, c. mixing the first and second powders to form a mixture, d. applying the mixture to at least one of the first and second glass panels, e. positioning the first and second glass panels such that the first and second powders come into contact with both glass panels, f. firing at a temperature of 350-550 °C to sinter and flow the first and second powders, and wherein the second homogeneous glass powder is different from the first homogeneous glass powder. a. providing a first homogeneous powder glass sealing composition comprising: i. 25-65 mol% Bi 2 O 3, ii. 3-60 mol% ZnO, iii. 4-65 mol% B 2 O 3, iv. no intentionally added oxides of silicon, and v. no intentionally added oxides of aluminum vi. 0.1-25 mol% of at least one selected from the group consisting of CuO, Fe 2 O 3, Co 2 O 3, MnO, NiO, Cr 2 O 3; i. 25-65 mol% Bi 2 O 3, ii. 3-60 mol% ZnO, iii. 4-65 mol% B 2 O 3, iv. no intentionally added oxides of silicon, and v. no intentionally added oxides of aluminum vi. 0.1-25 mol% of at least one selected from the group consisting of CuO, Fe 2 O 3, Co 2 O 3, MnO, NiO, Cr 2 O 3; b. providing a second homogeneous powder glass sealing composition comprising: i. 25-65 mol% Bi 2 O 3, ii. 3-60 mol% ZnO, iii. 4-65 mol% B 2 O 3, iv. no intentionally added oxides of silicon, and v. no intentionally added oxides of aluminum vi. 0.1-25 mol% of at least one colorant selected from the group consisting of CuO, Fe 2 O 3, Co 2 O 3, MnO, NiO, Cr 2 O 3, i. 25-65 mol% Bi 2 O 3, ii. 3-60 mol% ZnO, iii. 4-65 mol% B 2 O 3, iv. no intentionally added oxides of silicon, and v. no intentionally added oxides of aluminum vi. 0.1-25 mol% of at least one colorant selected from the group consisting of CuO, Fe 2 O 3, Co 2 O 3, MnO, NiO, Cr 2 O 3, c. mixing the first and second powders to form a mixture, d. applying the mixture to at least one of the first and second glass panels, e. positioning the first and second glass panels such that the first and second powders come into contact with both glass panels, f. firing at a temperature of 350-550 °C to sinter and flow the first and second powders, and
A calibration method for a channel simulator, in which channels are formed with respect to all paths between P base stations, P being an integer more than 2, and Q terminals, Q being an integer more than 2, the calibration method comprising: (a) inputting a base station signal having equal power after connecting the P base stations with one terminal; (b) capturing and measuring A/D converter, ADC, powers of base station interface cards connected with the base stations; (c) performing calibration so that the ADC powers measured in step (b) are equal to each other; (d) checking reference signal received power or a path loss value of each terminal after inputting the base station signal in a state that one base station is connected with the Q terminals; and (e) performing the calibration so that D/A converter values of terminal interface cards connected with the terminals are equal to each other using the RSRP and the path loss value, wherein the calibration in step (c) is performed by adjusting a gain of an amplifier or an attenuation degree of an attenuator of the base station interface cards; and the calibration in step (e) is performed by adjusting a gain of an amplifier or an attenuation degree of an attenuator of the terminal interface card, characterized in that the calibrated ADC power of each of the base station interface cards, PLADC, is defined as follows: P L ADC = A ADC o P L ADC ′, wherein A ADC = a ADC,1 ⋯ a ADC, P, wherein P L ADC ′ = PL ADC,1 ′ ⋯ PL ADC, P ′, and wherein AADC is a calibration matrix and PLADC' is a measured ADC power matrix, and further characterized in that the calibrated DAC power of each of the terminal interface cards, PLDAC, is defined as follows: P L DAC = A DAC o P L DAC ′ wherein A DAC = a DAC,1 ⋯ a DAC, Q, wherein P L DAC ′ = PL DAC,1 ′ ⋯ PL DAC, Q ′, and wherein ADAC is another calibration matrix and PL DAC' is a measured DAC power matrix. (a) inputting a base station signal having equal power after connecting the P base stations with one terminal; (b) capturing and measuring A/D converter, ADC, powers of base station interface cards connected with the base stations; (c) performing calibration so that the ADC powers measured in step (b) are equal to each other; (d) checking reference signal received power or a path loss value of each terminal after inputting the base station signal in a state that one base station is connected with the Q terminals; and (e) performing the calibration so that D/A converter values of terminal interface cards connected with the terminals are equal to each other using the RSRP and the path loss value,
A turbine engine component comprising: a shroud ring; and a stationary airfoil coupled to the shroud ring, the stationary airfoil comprising: a leading edge and a trailing edge interconnected by a concave pressure sidewall and a convex suction sidewall; and an end portion forming a slip joint with the shroud ring, the slip joint permitting radial movement of the stationary airfoil relative to the shroud ring characterised in that the end portion is generally C-shaped and includes a pair of inwardly deformable opposing flanges to define the slip joint, the end portion has a pair of sloping curved side surface areas (266, 268) that first curve radially outwardly from the concave and convex sidewalls (122, 124) and then curve inwardly to define the opposing flanges and the generally C-shaped end portion. a shroud ring; and a stationary airfoil coupled to the shroud ring, the stationary airfoil comprising: a leading edge and a trailing edge interconnected by a concave pressure sidewall and a convex suction sidewall; and an end portion forming a slip joint with the shroud ring, the slip joint permitting radial movement of the stationary airfoil relative to the shroud ring characterised in that the end portion is generally C-shaped and includes a pair of inwardly deformable opposing flanges to define the slip joint, the end portion has a pair of sloping curved side surface areas (266, 268) that first curve radially outwardly from the concave and convex sidewalls (122, 124) and then curve inwardly to define the opposing flanges and the generally C-shaped end portion. a leading edge and a trailing edge interconnected by a concave pressure sidewall and a convex suction sidewall; and an end portion forming a slip joint with the shroud ring, the slip joint permitting radial movement of the stationary airfoil relative to the shroud ring characterised in that the end portion is generally C-shaped and includes a pair of inwardly deformable opposing flanges to define the slip joint, the end portion has a pair of sloping curved side surface areas (266, 268) that first curve radially outwardly from the concave and convex sidewalls (122, 124) and then curve inwardly to define the opposing flanges and the generally C-shaped end portion.
An apparatus comprising: a phase-change material having a crystalline structure that manifests changes that increase as a function of time over which the phase-change material and a perishable item have been exposed to an environment having a temperature that is greater than a threshold temperature; and a circuit configured and arranged to respond to the changes by providing a characterization of the exposure of the phase-change material to the environment having the temperature that is greater than the threshold temperature, characterized in that the phase-change material includes a chalcogenide material in an integrated circuit (118, 120) including said circuit, the IC (118, 120) further including an RFID circuit configured and arranged to: harvest electrical power from a wireless signal, and use the harvested electrical power to transmit a wireless signal characterizing exposure of the phase-change material to the environment having the temperature that is greater than the threshold temperature. a phase-change material having a crystalline structure that manifests changes that increase as a function of time over which the phase-change material and a perishable item have been exposed to an environment having a temperature that is greater than a threshold temperature; and a circuit configured and arranged to respond to the changes by providing a characterization of the exposure of the phase-change material to the environment having the temperature that is greater than the threshold temperature, characterized in that the phase-change material includes a chalcogenide material in an integrated circuit (118, 120) including said circuit, the IC (118, 120) further including an RFID circuit configured and arranged to: harvest electrical power from a wireless signal, and use the harvested electrical power to transmit a wireless signal characterizing exposure of the phase-change material to the environment having the temperature that is greater than the threshold temperature.
Light with a carrier unit, at which at least one heat-generating operational unit and/or an illuminant of the light are arranged, and at least one light-guiding element made of plastic, in particular from a thermoplastic, wherein the carrier unit and the light-guiding element are adjacent to one another in a connecting area (8, 12; 10, 14), and, during the operation of the light, the carrier unit and the light-guiding element adopt different temperatures, characterized in that the connecting area (8, 12; 10, 14) limits a heat flow between the carrier unit and the light-guiding element to such a degree that, during the operation of the light, the light-guiding element adopts a temperature distribution in which the greatest temperature difference amounts to a maximum of ΔT = 10K, wherein the contact surface between the carrier unit and the light-guiding element amounts to a maximum of 2%.
Watch comprising a pedometer mechanism for estimating a physical activity level, comprising at least one moving or pivoting weight arranged to drive a ratchet, elastic or friction holding means for holding said ratchet in position between two movements of said moving or pivoting weight, wherein said ratchet drives a gear train displaying, on a display, a value corresponding, to within a multiplicative factor, to the number of pivoting motions of said ratchet, and/or to the value of the cumulative angular rotation of said ratchet, and wherein said pedometer mechanism comprises a limiting means (20; 35; 43) only allowing the pivoting of said ratchet from a minimum threshold corresponding to a minimum travel of said weight if the weight is movable or to a minimum angular rotation value (θ 0) of said weight if the weight pivots, wherein said pedometer mechanism comprises a detection means arranged to detect the direction of movement of said moving or pivoting weight, and comprises a locking means arranged to only allow the pivoting of said ratchet if said detection means has recorded, since the preceding pivoting motion of said ratchet, at least one movement of said moving or pivoting weight in the opposite direction to that which allows the driving of said ratchet, wherein said detection means comprises a first lever arranged to be driven by said moving or pivoting weight and changing angular position according to the direction of movement or pivoting in which the weight is driven, characterized in that said locking means comprises a second lever arranged to be immobilised or released by said first lever, according to the angular position of said first lever, and in that said second lever prevents or allows the pivoting of said ratchet, according to the angular position of said second lever.