mhurhangee/ep-ind-claims huggingface dataset:
A blow molding device including a blow molding mold to which a bottomed tubular preform is fitted, a blow nozzle that is fitted to a mouth tubular portion (PFb) of the preform fitted to the mold, and a pressurized liquid supply unit configured to supply a pressurized liquid (Fp) to the blow nozzle, the preform being to be molded into a shape conforming to a cavity of the mold by filling the liquid (Fp) into the preform through the blow nozzle, the blow molding device comprising: a deaeration mechanism that is connected to the blow nozzle, wherein the liquid (Fp) is filled into the preform through the blow nozzle after air that is present within the preform fitted to the mold is sucked out by the deaeration mechanism, characterised in that the deaeration mechanism has a function of supplying flush air into a flow path connecting the deaeration mechanism and the blow nozzle to return the liquid (Fp) within the flow path to the blow nozzle.
A method for determining at least one astigmatic effect of at least one eye of a person, the method comprising the following steps: a) displaying at least one image to at least one eye of a person, wherein the at least one image comprises at least one line (142, 142'), wherein the at least one line (142, 142') comprises a plurality of sections, wherein an orientation of each section with respect to an optical axis of the image differs from each other; b) recording at least one reaction of the person to the at least one image at at least one point in time; and c) determining at least one value for at least one astigmatic effect of at least one eye of the person by evaluating the at least one reaction of the person at the point in time, characterized in that the at least one reaction of the person to the at least one image comprises indicating a position on the at least one line (142, 142'), wherein the position on the at least one line (142, 142') refers to at least one transition (166, 166') from a first appearance of the at least one line (142, 142') to the person into a second appearance of the at least one line (142, 142') to the person, or vice-versa, wherein the second appearance of the at least one line (142, 142') to the person differs from the first appearance of the at least one line (142, 142') to the person, wherein the at least one transition (166, 166') indicates at least one position on the at least one line (142, 142') in which a first portion in which the at least one line (142, 142') exhibits the first appearance to the eye of the person terminates and at least one adjacent second portion in which the at least one line (142, 142') exhibits the second appearance to the eye of the person commences, or vice-versa, wherein the at least one value for the at least one astigmatic effect is determined from the position of the at least one transition (166, 166') on the at least one line (142, 142'). a) displaying at least one image to at least one eye of a person, wherein the at least one image comprises at least one line (142, 142'), wherein the at least one line (142, 142') comprises a plurality of sections, wherein an orientation of each section with respect to an optical axis of the image differs from each other; b) recording at least one reaction of the person to the at least one image at at least one point in time; and c) determining at least one value for at least one astigmatic effect of at least one eye of the person by evaluating the at least one reaction of the person at the point in time,
A method for producing spatial objects, which comprises: (a) printing a spatial object using a three-dimensional printer and a printing material that comprises polyaryletherketones, wherein the spatial object is printed in an amorphous phase; characterized it further comprises: (b) placing the spatial object in a container and submerging the spatial object in a charging material; (c) heating the container that includes the spatial object and charging material until the spatial object transitions into a semi-crystalline phase. (a) printing a spatial object using a three-dimensional printer and a printing material that comprises polyaryletherketones, wherein the spatial object is printed in an amorphous phase; (b) placing the spatial object in a container and submerging the spatial object in a charging material; (c) heating the container that includes the spatial object and charging material until the spatial object transitions into a semi-crystalline phase.
A method of motoring a gas turbine engine, the method comprising: determining a first speed to motor a gas turbine engine for cooling; determining a first time period to motor the gas turbine engine at the first speed; motoring the gas turbine engine at the first speed; detecting a gap parameter of the gas turbine engine; detecting a speed parameter of the gas turbine engine; detecting a vibration parameter of the gas turbine engine; determining a second speed to motor the gas turbine engine for cooling in response to at least one of the vibration parameter, the gap parameter, and the speed parameter determining a second time period to motor the gas turbine engine at the second speed in response to at least one of the vibration parameter, the gap parameter, and the speed parameter; and motoring the gas turbine at the second speed in response to at least one gap parameter, speed parameter, and vibration parameter. determining a first speed to motor a gas turbine engine for cooling; determining a first time period to motor the gas turbine engine at the first speed; motoring the gas turbine engine at the first speed; detecting a gap parameter of the gas turbine engine; detecting a speed parameter of the gas turbine engine; detecting a vibration parameter of the gas turbine engine; determining a second speed to motor the gas turbine engine for cooling in response to at least one of the vibration parameter, the gap parameter, and the speed parameter determining a second time period to motor the gas turbine engine at the second speed in response to at least one of the vibration parameter, the gap parameter, and the speed parameter; and motoring the gas turbine at the second speed in response to at least one gap parameter, speed parameter, and vibration parameter.
A stylus comprising: a stylus body; a tip disposed at the distal end of, and slidably connected to, the stylus body; a force sensor disposed inside the stylus body, the force sensor having a first terminal and a second terminal, the first terminal electrically connected to a first exposed pad and the second terminal electrically connected to a second exposed pad; and a conductive pad configured to contact the first exposed pad and the second exposed pad when a force is applied to the tip, wherein a circuit is completed when the conductive pad contacts the first exposed pad and the second exposed pad, and characterized in that the force sensor is calibrated to measure a point in time when the electrical circuit is completed by measurement of a step-function wherein a measured current remains at zero or near zero while the circuit is broken, then steps up to a measured level when the circuit has been completed and measures the change in resistance at the force sensor after the circuit has been completed, independent of the magnitude of the measured resistance, and to report a zero value at the point in time when the conductive pad contacts the first exposed pad and the second exposed pad. a stylus body; a tip disposed at the distal end of, and slidably connected to, the stylus body; a force sensor disposed inside the stylus body, the force sensor having a first terminal and a second terminal, the first terminal electrically connected to a first exposed pad and the second terminal electrically connected to a second exposed pad; and a conductive pad configured to contact the first exposed pad and the second exposed pad when a force is applied to the tip, wherein a circuit is completed when the conductive pad contacts the first exposed pad and the second exposed pad, and characterized in that the force sensor is calibrated to measure a point in time when the electrical circuit is completed by measurement of a step-function wherein a measured current remains at zero or near zero while the circuit is broken, then steps up to a measured level when the circuit has been completed and measures the change in resistance at the force sensor after the circuit has been completed, independent of the magnitude of the measured resistance, and to report a zero value at the point in time when the conductive pad contacts the first exposed pad and the second exposed pad.
A lithographic printing plate precursor comprising a support the surface of which has a water droplet contact angle in air of ≥ 70°, and a photosensitive layer, wherein the support has on its surface a compound (Cx) having a functional group X capable of being substituted for a functional group Y when X is contacted with a compound (Cy) having the functional group Y, to fix Y on the surface of the support so as to decrease the water droplet contact angle in air on its surface to ≤ 30°, and wherein the compound (Cx) is a compound having an electrophilic functional group represented by formula: L 2 (̵CH 2 -W) m wherein W is a Cl, Br, I or -OSO 2 R 1, wherein R 1 is alkyl, aryl, alkenyl or alkynyl, L 2 is an m-valent organic residue, and m is a natural number. W is a Cl, Br, I or -OSO 2 R 1, wherein R 1 is alkyl, aryl, alkenyl or alkynyl, L 2 is an m-valent organic residue, and m is a natural number.
Use of an oil agent in the form of dicarbitol succinate, said oil agent having a viscosity of 5 - 200 mPa.s at 25°C (measured using a Brookfield viscometer DV-II+ Spindle No. 2, 12 rpm) for the manufacturing of a preparation for external use on skin, hair, mucosa and wounds.
Method for safe supervising train integrity, in particular at SIL4-level, the train comprising a first carriage and a second carriage (C1, C2), the method comprising: a) acquiring first position data of the first carriage via a first SIL4-proved tracking unit which is installed on-board of the first carriage and acquiring second position data of the second carriage via a second SIL4-proved tracking unit which is installed on-board of the second carriage, wherein the position data (P1, P2), is related to a rail route coordinate system; b) determining a deviation (Δ) between a reference value which depends on the length of the train and a position value which is determined by subtraction of the first and the second rail route coordinate system related position data (P1, P2); c) detecting whether train integrity is given by analyzing the deviation; d) Repeating steps a) through c); wherein the tracking units (TU1, TU2) are part of on-board units (OBU1, OBU2) of an automatic train protection system; and wherein each tracking unit (TU1, TU2) determines expected position data of the respective other tracking unit (TU1, TU2) and transmits the expected position data to the other tracking unit (TU1, TU2). a) acquiring first position data of the first carriage via a first SIL4-proved tracking unit which is installed on-board of the first carriage and acquiring second position data of the second carriage via a second SIL4-proved tracking unit which is installed on-board of the second carriage, wherein the position data (P1, P2), is related to a rail route coordinate system; b) determining a deviation (Δ) between a reference value which depends on the length of the train and a position value which is determined by subtraction of the first and the second rail route coordinate system related position data (P1, P2); c) detecting whether train integrity is given by analyzing the deviation; d) Repeating steps a) through c); wherein the tracking units (TU1, TU2) are part of on-board units (OBU1, OBU2) of an automatic train protection system; and wherein each tracking unit (TU1, TU2) determines expected position data of the respective other tracking unit (TU1, TU2) and transmits the expected position data to the other tracking unit (TU1, TU2).
A method of detecting the alignment of a substrate used to form a solar cell device during a sequence of printing steps, comprising: - detecting in a detection unit a position of at least one printing track selected between a finger and a busbar, said printing tracks (15, 16) forming a first pattern printed onto a surface of the substrate in a first printing station and comprising a plurality of first tracks substantially parallel to each other, which are connected to each other by second tracks, - determining at least one reference point in at least a portion of said printing track (15, 16), wherein the at least one reference point is determined in at least a point of intersection between one of said first tracks and one of said second tracks, - comparing in the detection unit the actual position of said at least one reference point with an expected or previously detected position of said at least one reference point; - determining an offset between the actual position and the expected or previously detected position of said at least one reference point; - adjusting the reciprocal position between the printing head of a second printing station and the substrate for to account for the determined offset; and - printing a second pattern onto the first pattern. - detecting in a detection unit a position of at least one printing track selected between a finger and a busbar, said printing tracks (15, 16) forming a first pattern printed onto a surface of the substrate in a first printing station and comprising a plurality of first tracks substantially parallel to each other, which are connected to each other by second tracks, - determining at least one reference point in at least a portion of said printing track (15, 16), wherein the at least one reference point is determined in at least a point of intersection between one of said first tracks and one of said second tracks, - comparing in the detection unit the actual position of said at least one reference point with an expected or previously detected position of said at least one reference point; - determining an offset between the actual position and the expected or previously detected position of said at least one reference point; - adjusting the reciprocal position between the printing head of a second printing station and the substrate for to account for the determined offset; and - printing a second pattern onto the first pattern.
A microwave oven comprising: a tray rotatably installed inside a cooking chamber; a temperature measuring apparatus comprising a driving unit configured to generate a rotation force, and a sensing unit configured to measure the temperatures of a plurality of temperature measurement points, which is provided at an upper side of the tray, characterised by having a temperature measurement angle thereof changed through the rotation force of the driving unit; and by a control unit configured to control the temperature measuring apparatus to measure the plurality of temperature measurement points provided at the upper side of the tray according to a temperature measurement pattern that is set in advance at each rotation period of the tray, such that at least adjacent rotation periods of the tray form different temperature measuring patterns from each other by allowing the rotation period of the tray to be asynchronous with the temperature measurement pattern of the temperature measuring apparatus. a tray rotatably installed inside a cooking chamber; a temperature measuring apparatus comprising a driving unit configured to generate a rotation force, and a sensing unit configured to measure the temperatures of a plurality of temperature measurement points, which is provided at an upper side of the tray, characterised by having a temperature measurement angle thereof changed through the rotation force of the driving unit; and by a control unit configured to control the temperature measuring apparatus to measure the plurality of temperature measurement points provided at the upper side of the tray according to a temperature measurement pattern that is set in advance at each rotation period of the tray, such that at least adjacent rotation periods of the tray form different temperature measuring patterns from each other by allowing the rotation period of the tray to be asynchronous with the temperature measurement pattern of the temperature measuring apparatus.
An in vitro method of modulating a metabolic response comprising contacting an adipose cell with transforming growth factor alpha (TGFA) to increase thermogenesis by the adipose cell.
A gas turbine engine comprising: a casing a blade outer air seal (BOAS) attached to said casing, said BOAS comprising: a seal body having a radially inner face facing toward the blade tip of a blade and a radially outer face facing the casing that axially extend between a leading edge portion and a trailing edge portion said seal body attached to said casing; a trough disposed on said radially inner face; and an abradable seal received within said trough, wherein said trough is open to expose a leading edge of said abradable seal to a core flow path of the gas turbine engine; characterised in that: said casing includes at least a first surface and a second surface that is different from said first surface, wherein each of said first surface and said second surface of a radially inner portion of the casing include a thermal barrier coating wherein said thermal barrier coating on said first surface axially overlaps said thermal barrier coating of said second surface. a casing a blade outer air seal (BOAS) attached to said casing, said BOAS comprising: a seal body having a radially inner face facing toward the blade tip of a blade and a radially outer face facing the casing that axially extend between a leading edge portion and a trailing edge portion said seal body attached to said casing; a trough disposed on said radially inner face; and an abradable seal received within said trough, wherein said trough is open to expose a leading edge of said abradable seal to a core flow path of the gas turbine engine; characterised in that: said casing includes at least a first surface and a second surface that is different from said first surface, wherein each of said first surface and said second surface of a radially inner portion of the casing include a thermal barrier coating wherein said thermal barrier coating on said first surface axially overlaps said thermal barrier coating of said second surface. a seal body having a radially inner face facing toward the blade tip of a blade and a radially outer face facing the casing that axially extend between a leading edge portion and a trailing edge portion said seal body attached to said casing; a trough disposed on said radially inner face; and an abradable seal received within said trough, wherein said trough is open to expose a leading edge of said abradable seal to a core flow path of the gas turbine engine; characterised in that: said casing includes at least a first surface and a second surface that is different from said first surface, wherein each of said first surface and said second surface of a radially inner portion of the casing include a thermal barrier coating wherein said thermal barrier coating on said first surface axially overlaps said thermal barrier coating of said second surface.
A method comprising: receiving a temperature indication, the temperature indication being a function of a temperature of a power pack of a portable electronic device; determining (54, 56), as a function of the temperature indication, whether the temperature is within an elevated operating temperature range; and when the temperature is within the elevated operating temperature range, reducing (52, 66) a charge termination voltage and a charging current and increasing a termination current, wherein the charging current is reduced to between 0.5C and 0.75C; and wherein the reduced charging current is a constant current, at which the power pack is charged until a voltage of the power pack reaches the charge termination voltage. receiving a temperature indication, the temperature indication being a function of a temperature of a power pack of a portable electronic device; determining (54, 56), as a function of the temperature indication, whether the temperature is within an elevated operating temperature range; and when the temperature is within the elevated operating temperature range, reducing (52, 66) a charge termination voltage and a charging current and increasing a termination current, wherein the charging current is reduced to between 0.5C and 0.75C; and wherein the reduced charging current is a constant current, at which the power pack is charged until a voltage of the power pack reaches the charge termination voltage.
Process for detecting the presence and position of defects in metal bars, comprising the following steps: - detecting the longitudinal sound propagation velocity v of a metal bar with the same structural composition as the one under examination; - acquiring the Fourier spectrum of an intact, defect-free metal bar with the same structural composition and length as the metal bar under examination; - acquiring the Fourier spectrum of the metal bar under examination; - comparing the two spectra obtained and identifying the presence of any extra spectral lines present and caused by the presence of defects in the metal bar under examination; and in the case wherein said extra spectral lines are present: - identifying the frequency f of said extra spectral lines; - applying the formula f=v/2x to the extra spectral lines present in the spectrum of the bar under examination to obtain the distance x of said defect from one end of the metal bar under examination, knowing the sound propagation velocity v and the frequency f. - detecting the longitudinal sound propagation velocity v of a metal bar with the same structural composition as the one under examination; - acquiring the Fourier spectrum of an intact, defect-free metal bar with the same structural composition and length as the metal bar under examination; - acquiring the Fourier spectrum of the metal bar under examination; - comparing the two spectra obtained and identifying the presence of any extra spectral lines present and caused by the presence of defects in the metal bar under examination; and - identifying the frequency f of said extra spectral lines; - applying the formula f=v/2x to the extra spectral lines present in the spectrum of the bar under examination to obtain the distance x of said defect from one end of the metal bar under examination, knowing the sound propagation velocity v and the frequency f.
A pivot connection type assembly comprising a shaft and first and second connection parts (12A, 40) that are dissociated from each other, each having a bore receiving the shaft so as to enable the first and second connection parts (12A, 40) to pivot relative to each other, the first connection part being arranged axially between a first end of the shaft and a radial plane, while the second connection part is arranged axially between said radial plane and the other end of the shaft, the assembly being characterized in that the shaft is hollow and includes an inside section that presents a radial dimension at least in a first axial plane and over a first segment of the shaft extending axially between the first end and the radial plane, which radial dimension varies, decreasing on axially approaching the radial plane, and in that the assembly includes a ring (20A, 20A') interposed radially between the shaft and the bore of the first connection part, and presenting radial thickness (E, E1, E2) that varies, wherein the radial thickness of the ring increases on axially approaching the radial plane, at least in the first axial plane.