mhurhangee/ep-ind-claims huggingface dataset:
Method for plasma treatment of containers by means of a plasma module having several plasma stations on a plasma wheel, wherein each plasma station comprises at least one plasma chamber with at least one treatment point, with the steps of: ▪ inserting and positioning at least one container with a container interior (5.1) in the plasma chamber on the treatment point of a corresponding plasma station, ▪ at least partially evacuating the respective plasma chamber and the at least one container interior (5.1), ▪ at least partially charging the container interior (5.1) inside the at least partially evacuated plasma chamber with a process gas, wherein the at least partial charging is effected at the same time at least at one plasma station through a central process gas feed, ▪ providing at least the container interior (5.1) with an inner coating by means of plasma treatment, and ▪ carrying out a ventilation step after the plasma treatment, in which both the plasma chamber and the at least one container interior (5.1) of the container are at least partially ventilated, characterized in that in the case of an operational malfunction and/or a cut-out in at least one treatment point of one of the plasma stations the process gas is at least partially, but in particular completely, discharged by means of a bypass line before being supplied to the treatment point and/or the container held there. ▪ inserting and positioning at least one container with a container interior (5.1) in the plasma chamber on the treatment point of a corresponding plasma station, ▪ at least partially evacuating the respective plasma chamber and the at least one container interior (5.1), ▪ at least partially charging the container interior (5.1) inside the at least partially evacuated plasma chamber with a process gas, wherein the at least partial charging is effected at the same time at least at one plasma station through a central process gas feed, ▪ providing at least the container interior (5.1) with an inner coating by means of plasma treatment, and ▪ carrying out a ventilation step after the plasma treatment, in which both the plasma chamber and the at least one container interior (5.1) of the container are at least partially ventilated,
Method for monitoring and fault diagnosis of a rotating electric machine which is fed by a converter, wherein a current signature (I 1, I 2, I 3) of output signals of the converter is recorded, a transformation of the current signature (I 1, I 2, I 3) is carried out and the transformed current signature is evaluated in at least one frequency band in order to detect damage to the machine, wherein the transformation of the current signature (I 1, I 2, I 3) comprises at least one fast Fourier transform using a filter function, wherein a transformed reference current signature is ascertained which represents a damage-free state of the machine, and that the transformed current signature is compared during the evaluation with the transformed reference current signature, wherein in order to detect damage to the machine a frequency-dependent tolerance band is predetermined in a value range of the transformed current signature and damage is concluded to have occurred if the transformed current signature lies outside the tolerance band in the case of at least one frequency.
A method for processing an image, carried out by a data processing device with at least one processor and a memory, the method comprising: performing edge-preserving filtering on an original image to obtain a first processed image (S201, S701); obtaining a detail feature of the original image (S202, S702) by determining a color difference between the original image and the first processed image, and determining the detail feature according to the color difference; wherein the determining the detail feature according to the color difference comprises: enhancing the color difference according to an adjustment coefficient to obtain an enhanced color difference, and determining the enhanced color difference as the detail feature; determining a second processed image according to the detail feature and the first processed image (S203, S703); characterized in that the method further comprises: processing the second processed image in a guidance image filtering manner by using the original image as a first guidance image to obtain a third processed image, and outputting the third processed image to be displayed (S204, S704). performing edge-preserving filtering on an original image to obtain a first processed image (S201, S701); obtaining a detail feature of the original image (S202, S702) by determining a color difference between the original image and the first processed image, and determining the detail feature according to the color difference; wherein the determining the detail feature according to the color difference comprises: enhancing the color difference according to an adjustment coefficient to obtain an enhanced color difference, and determining the enhanced color difference as the detail feature; determining a second processed image according to the detail feature and the first processed image (S203, S703); characterized in that the method further comprises: processing the second processed image in a guidance image filtering manner by using the original image as a first guidance image to obtain a third processed image, and outputting the third processed image to be displayed (S204, S704).
A device for use in a gas turbine combustor, the device comprising: primary nozzles; and a secondary nozzle comprising: a flange; an elongated nozzle body extending from the flange; and a plurality of premix fuel injectors spaced radially from the nozzle body, the injectors extending axially from the flange and generally parallel to the nozzle body for a portion of the length of the nozzle body, wherein the plurality of premix fuel injectors is arranged in an annular array around the nozzle body, wherein the primary nozzles are arranged in an annular array around the secondary nozzle and the premix fuel injectors are disposed between the nozzle body and the primary nozzles, characterized in that there is an equal number of premix fuel injectors and primary nozzles. primary nozzles; and a secondary nozzle comprising: a flange; an elongated nozzle body extending from the flange; and a plurality of premix fuel injectors spaced radially from the nozzle body, the injectors extending axially from the flange and generally parallel to the nozzle body for a portion of the length of the nozzle body, wherein the plurality of premix fuel injectors is arranged in an annular array around the nozzle body, a flange; an elongated nozzle body extending from the flange; and a plurality of premix fuel injectors spaced radially from the nozzle body, the injectors extending axially from the flange and generally parallel to the nozzle body for a portion of the length of the nozzle body, wherein the plurality of premix fuel injectors is arranged in an annular array around the nozzle body,
A method of refining beam patterns of a base station antenna configured to communicate with a plurality of aircraft using a plurality of beams, to reduce interference between adjacent beams from the base station, comprising: receiving position locations from each of the plurality of aircraft; receiving an attitude of each of the plurality of aircraft from each of the plurality of aircraft; receiving reports of measurements of pilot signals from each of the plurality of aircraft, the pilot signals having been transmitted by the base station; and adjusting, at the base station, an amplitude and a phase of a signal driving at least one antenna transmit element to refine the beam patterns, the adjusting based at least in part on the received reports of measurements of pilot signals, the received position locations, and the received attitude from each of the plurality of aircraft; and forwarding at least one of the received position locations of at least one of the plurality of aircraft to another base station for handoff; or forwarding the attitude of at least one of the plurality of aircraft to another base station for handoff. receiving position locations from each of the plurality of aircraft; receiving an attitude of each of the plurality of aircraft from each of the plurality of aircraft; receiving reports of measurements of pilot signals from each of the plurality of aircraft, the pilot signals having been transmitted by the base station; and adjusting, at the base station, an amplitude and a phase of a signal driving at least one antenna transmit element to refine the beam patterns, the adjusting based at least in part on the received reports of measurements of pilot signals, the received position locations, and the received attitude from each of the plurality of aircraft; and forwarding at least one of the received position locations of at least one of the plurality of aircraft to another base station for handoff; or forwarding the attitude of at least one of the plurality of aircraft to another base station for handoff.
An arrangement comprising a superconducting device cooled by a two-stage cryogenic refrigerator, having a first stage and a second stage, such that, in operation the second stage is cooled to a cooler temperature than the first stage; and a current lead for supplying current to the superconducting device, the current lead comprising an HTS conductor extending along a length of the current lead, the HTS conductor being thermally and electrically joined to an electrical shunt, respective voltage taps (30, 32) being connected to respective ends of the HTS conductor for connection to a quench heater in thermal contact with the superconducting device, such that a quench in the HTS conductor will give rise to a voltage appearing between the voltage taps, such voltage being applied to the quench heater to give rise to quench within the superconducting device, the current lead comprising first, second and third (17/24) stages attached in an electrically- and thermally-conductive manner with the HTS conductor overlapping each stage, the first stage of the current lead being cooled by the first stage of the cryogenic refrigerator; the second stage being the electrical shunt; and the third stage being cooled by the second stage of the cryogenic refrigerator, wherein the superconducting device comprises a plurality of superconducting coils, and each of the superconducting coils is provided with a quench heater in thermal contact therewith and connected to receive the voltage appearing between the voltage taps. the current lead comprising first, second and third (17/24) stages attached in an electrically- and thermally-conductive manner with the HTS conductor overlapping each stage, the first stage of the current lead being cooled by the first stage of the cryogenic refrigerator; the second stage being the electrical shunt; and the third stage being cooled by the second stage of the cryogenic refrigerator, wherein the superconducting device comprises a plurality of superconducting coils, and each of the superconducting coils is provided with a quench heater in thermal contact therewith and connected to receive the voltage appearing between the voltage taps.
A label cutting device comprising: a conveyance path through which label paper is conveyed; a cutting unit having wire pins and a wire pin moving mechanism that drives the wire pins forward and back; a cutting controller configured to drive the wire pin moving mechanism to advance the wire pins, strike the label paper on the conveyance path with the wire pins, and cut the label paper based on print data; and a striking force controller configured to adjust the striking force of the wire pins striking the label paper, characterized in that the striking force controller has a gap adjusting mechanism configured to adjust a gap between the cutting unit and the conveyance path. a conveyance path through which label paper is conveyed; a cutting unit having wire pins and a wire pin moving mechanism that drives the wire pins forward and back; a cutting controller configured to drive the wire pin moving mechanism to advance the wire pins, strike the label paper on the conveyance path with the wire pins, and cut the label paper based on print data; and a striking force controller configured to adjust the striking force of the wire pins striking the label paper, characterized in that the striking force controller has a gap adjusting mechanism configured to adjust a gap between the cutting unit and the conveyance path.
A process to produce IPP and VPP from a protein source that comprises the -I-P-P-and -V-P-P- sequence in its protein sequence and whereby at least 40% of - I-P-P-sequence present in the protein source is converted into the peptide IPP and at least 40% of the -V-P-P- sequence present in the protein source is converted into the peptide VPP, which comprises the use of a proline specific endoprotease and an amino peptidase, whereby the proline specific endoprotease and the amino peptidase are incubated together in a single step.
A truck for a railroad vehicle, the truck comprising: - at least two wheels (1 A, 1 B), each supported by an axle box (2A, 2B), and - a side frame for mechanically connecting the axle boxes (2A, 2B), - a beam extending between the axle boxes (2A, 2B) and supporting a device for transmitting electrical current to a rail of a railroad track, characterized in that: - the beam extends along a curved line that has a curve radius varying continually along the curved line, - the beam is made from a metal alloy and does not have a weld perpendicular to the curved line, and - along the curved line, centers of curved circles tangent to the curved line are situated on the same side of a curved surface that passes through the curved line and is parallel to the rotation axes (X1A, X1 B) of the wheels (1A, 1 B). - at least two wheels (1 A, 1 B), each supported by an axle box (2A, 2B), and - a side frame for mechanically connecting the axle boxes (2A, 2B), - a beam extending between the axle boxes (2A, 2B) and supporting a device for transmitting electrical current to a rail of a railroad track, - the beam extends along a curved line that has a curve radius varying continually along the curved line, - the beam is made from a metal alloy and does not have a weld perpendicular to the curved line, and - along the curved line, centers of curved circles tangent to the curved line are situated on the same side of a curved surface that passes through the curved line and is parallel to the rotation axes (X1A, X1 B) of the wheels (1A, 1 B).
A system for vacuum bagging a composite layup comprising: a tool surface having an inside corner; and a vacuum bag assembly comprising: a bagging film having a bagging film length, the bagging film being positioned over a composite layup and sealed to the tool surface; a tube bag having opposing tube ends and a tube bag length, the tube bag being positioned over the composite layup along a length of the inside corner; and each one of the tube ends being sealed to the tool surface along a first portion of a tube end perimeter edge and being sealed to the bagging film along a second portion of the tube end perimeter edge such that each one of the tube ends is open to atmosphere. a tool surface having an inside corner; and a vacuum bag assembly comprising: a bagging film having a bagging film length, the bagging film being positioned over a composite layup and sealed to the tool surface; a tube bag having opposing tube ends and a tube bag length, the tube bag being positioned over the composite layup along a length of the inside corner; and each one of the tube ends being sealed to the tool surface along a first portion of a tube end perimeter edge and being sealed to the bagging film along a second portion of the tube end perimeter edge such that each one of the tube ends is open to atmosphere. a bagging film having a bagging film length, the bagging film being positioned over a composite layup and sealed to the tool surface; a tube bag having opposing tube ends and a tube bag length, the tube bag being positioned over the composite layup along a length of the inside corner; and each one of the tube ends being sealed to the tool surface along a first portion of a tube end perimeter edge and being sealed to the bagging film along a second portion of the tube end perimeter edge such that each one of the tube ends is open to atmosphere.
Co-micronization product comprising: - an active ingredient selected from the group consisting of ulipustal acetate, a metabolite of ulipristal acetate, and mixtures thereof, and - a pharmaceutically acceptable solid surfactant selected from C 8 -C 20 alkyl sulfate salts and mixtures thereof. - an active ingredient selected from the group consisting of ulipustal acetate, a metabolite of ulipristal acetate, and mixtures thereof, and - a pharmaceutically acceptable solid surfactant selected from C 8 -C 20 alkyl sulfate salts and mixtures thereof.
A composition comprising a first mRNA encoding the heavy chain of an antibody and a second mRNA encoding the light chain of the antibody at a molar ratio ranging from 2:1 to 1:2 for use in therapy in a patient, wherein the first mRNA and the second mRNA (i) each comprise a 5' cap structure, a 3' poly-A tail, a 5' untranslated region and a 3' untranslated region and (ii) are encapsulated within liposomes comprising a cationic lipid, a neutral lipid, a cholesterol-based lipid, and a PEG-modified lipid and having a size no greater than 150 nm, wherein the first mRNA encoding the heavy chain and the second mRNA encoding the light chain are encapsulated in the same liposome, wherein the antibody is a tetramer and each tetramer is composed of two identical pairs of polypeptide chains, each pair having one light chain of approximately 25 kD and one heavy chain of approximately 50-70 kD, and wherein the composition is administered intravenously to the patient and the antibody is distributed systemically in the patient.
A fuel spray nozzle comprising a fuel injector and an annular air swirler, the fuel injector comprising; a fuel passage arranged centrally of the annular air swirler and having at least one inlet and at least one outlet, the outlet configured for accelerating fuel exiting the fuel passage into a jet of fuel and the annular air swirler comprising one or more swirl passages converging to a single outlet chamber in which the fuel passage outlet(s) sits, wherein the fuel passage is arranged along a co-axial centreline of the fuel passage and annular air swirler and configured such that the jet of fuel exiting the fuel passage through the at least one outlet is directed across a stream of air exiting the one or more swirl passages at the outlet chamber.
A horizontal agitator for producing a flow in a clarifier, a propeller being connected to a submersible motor which is axially offset in relation thereto, wherein the propeller and the submersible motor are designed such that a flow in a direction from the propeller towards the submersible motor is produced when the submersible motor is operated, and wherein plate-shaped flow guide elements (5, 7) are provided downstream of the propeller and extend in at least an axial plane running substantially parallel to the propeller axis, characterised in that the submersible motor is supported on a bottom of the clarifier via at least two first flow guide elements, wherein the first flow guide elements are interconnected via at least one carrier plate (4a, 4b) receiving the submersible motor, wherein the carrier plate (4a, 4b) with the first flow guide elements installed thereon forms a mount, on which an assembly unit formed from the submersible motor and the propeller is detachably fastened by means of a coupling device (8a, 8b, 9a, 9b).
Gas burner for a cooking hob, comprising at least one hollow structure in which an inlet chamber for the inlet of an air/gas mixture, an expansion chamber for the expansion of the air/gas mixture arranged above said inlet chamber, and an annular slot for the outlet of the air/gas mixture arranged above said expansion chamber and configured for supplying the air/gas mixture to an annular laminar flame exiting from the gas burner are defined, said at least one hollow structure comprising at least one inlet opening for the inlet of secondary air, wherein said inlet opening is arranged beneath said inlet chamber, wherein said at least one hollow structure comprises a diaphragm interposed between said expansion chamber and said inlet chamber, characterised in that said expansion chamber is delimited at a bottom part thereof by said diaphragm and at a side part thereof by a first ring nut configured to be associated with said cooking hob and in abutment on said diaphragm and by a second ring nut arranged at a radially inner position with respect to said first ring nut and in abutment on said diaphragm.
A method for dispensing a gas to a receiving vessel, the method comprising: transferring a first quantity of the gas from at least one of a first plurality of storage vessels (102, 103) or a gas source to at least one storage vessel of a second plurality of storage vessels via a compressor; and transferring a fourth quantity of the gas from the at least one storage vessel of the second plurality of storage vessels to the receiving vessel using a respective pressure difference between the gas in the at least one storage vessel of the second plurality of storage vessels and the gas in the receiving vessel to transfer the fourth quantity of the gas, wherein the fourth quantity of the gas comprises at least a portion of the first quantity of the gas; characterized in that a second quantity of the gas is transferred from the gas source to a first storage vessel of the first plurality of storage vessels without a compressor by using a pressure difference between the gas in the gas source and the gas in the first storage vessel to transfer the second quantity of the gas while simultaneously transferring a third quantity of the gas from the gas source to the receiving vessel without a compressor by using a respective pressure difference between the gas of the gas source and the gas in the receiving vessel to transfer the third quantity of the gas. transferring a first quantity of the gas from at least one of a first plurality of storage vessels (102, 103) or a gas source to at least one storage vessel of a second plurality of storage vessels via a compressor; and transferring a fourth quantity of the gas from the at least one storage vessel of the second plurality of storage vessels to the receiving vessel using a respective pressure difference between the gas in the at least one storage vessel of the second plurality of storage vessels and the gas in the receiving vessel to transfer the fourth quantity of the gas, wherein the fourth quantity of the gas comprises at least a portion of the first quantity of the gas; characterized in that a second quantity of the gas is transferred from the gas source to a first storage vessel of the first plurality of storage vessels without a compressor by using a pressure difference between the gas in the gas source and the gas in the first storage vessel to transfer the second quantity of the gas while simultaneously transferring a third quantity of the gas from the gas source to the receiving vessel without a compressor by using a respective pressure difference between the gas of the gas source and the gas in the receiving vessel to transfer the third quantity of the gas.