mhurhangee/ep-ind-claims huggingface dataset:
A method of measuring an electromagnetic wave level of an electronic device, the method comprising: obtaining a relationship equation between a reference electromagnetic level measured by a first measuring device in an electro-magnetic compatibility, EMC, chamber and an electromagnetic level measured by a second measuring device; measuring a first electromagnetic wave level of the electronic device by the second measuring device; and obtaining a second electromagnetic wave level of the electronic device based on the measured first electromagnetic wave level and the relationship equation. obtaining a relationship equation between a reference electromagnetic level measured by a first measuring device in an electro-magnetic compatibility, EMC, chamber and an electromagnetic level measured by a second measuring device; measuring a first electromagnetic wave level of the electronic device by the second measuring device; and obtaining a second electromagnetic wave level of the electronic device based on the measured first electromagnetic wave level and the relationship equation.
Device for dosing or counting objects, comprising: - a plate provided with a plurality of recesses each suitable for receiving a single object, said recesses being arranged in at least two series of at least two rows (R1-R2; R3-R4) disposed in parallel along a longitudinal axis such that, in a same series (R1-R2; R3-R4), the recesses in a first row (R1; R3) are offset longitudinally relative to the recesses in the second row (R2; R4) by a non-zero pitch; - a pull element arranged to slide relative to the plate along said longitudinal axis, said pull element comprising at least two adjacent tongues (20, 21; 2001-2003), each designed to cover or uncover a corresponding series of rows, said tongues (20, 21) being arranged to slide relative to one another over a distance equal to said pitch and coupled by a drive mechanism configured such that the sliding of the pull element along the longitudinal axis over a distance greater than said pitch causes the simultaneous movement of the two tongues (20, 21). - a plate provided with a plurality of recesses each suitable for receiving a single object, said recesses being arranged in at least two series of at least two rows (R1-R2; R3-R4) disposed in parallel along a longitudinal axis such that, in a same series (R1-R2; R3-R4), the recesses in a first row (R1; R3) are offset longitudinally relative to the recesses in the second row (R2; R4) by a non-zero pitch; - a pull element arranged to slide relative to the plate along said longitudinal axis, said pull element comprising at least two adjacent tongues (20, 21; 2001-2003), each designed to cover or uncover a corresponding series of rows, said tongues (20, 21) being arranged to slide relative to one another over a distance equal to said pitch and coupled by a drive mechanism configured such that the sliding of the pull element along the longitudinal axis over a distance greater than said pitch causes the simultaneous movement of the two tongues (20, 21).
A method of dosing a treatment chemical with an encapsulated tracer dye, wherein the encapsulated dye is encapsulated by mixing the dye with a surfactant, whereby the surfactant is a (polyethylene oxide)-(polypropylene oxide)-(polyethylene oxide) tri-block copolymer in water solution and the dye is selected from the list of derivatives of xanthene, oxazine, cyanine, styryl, coumarin, porphine, perylene, phthalocyanine, and any combinations thereof or wherein the dye is a xanthene derivative, including rhodamine WT, sulforhodamine B, rhodamine B and any combinations thereof, the method comprising the step of introducing the encapsulated dye and the treatment chemical into a process system, wherein the spectrometry properties of the encapsulated dye are not substantially altered by the materials in process system or by being co-present with the treatment chemical, and wherein the treatment chemical is one selected from coagulants, flocculants, anti-scaling agents, anti-corrosion agents, biocide, oxygen scavengers, hardness removal agents, and any combination thereof, or in which the treatment chemical is inorganic, organic and blend of inorganic and organic coagulants, or in which the treatment chemical is inorganic coagulant or blend of inorganic and organic coagulants containing aluminum or iron salt.
A particulate collecting device attachable to a vehicle for collecting and capturing particulates that are released from a tyre or a wheel of the vehicle through wear on or against a driving surface when the vehicle is driven on the driving surface, comprising: an electrostatic filter unit for collecting or capturing the particulates in a flow by electrostatic attraction, the electrostatic filter unit mountable in an operative position in close proximity to the tyre of the vehicle for receiving a flow of particulates from a contact point between the tyre or wheel and the driving surface, the filter unit comprising one or more electrostatically chargeable collector electrodes to attract charged particulates in the flow when the one or more collector electrodes are charged, so as to collect or capture the particulates; a charging circuit connected to the one or more collector electrodes for electrostatically charging the one or more collector electrodes; and a control module connectable to the charging circuit to selectively activate and deactivate charging of the one or more collecting electrodes in response to one or more detected driving conditions. an electrostatic filter unit for collecting or capturing the particulates in a flow by electrostatic attraction, the electrostatic filter unit mountable in an operative position in close proximity to the tyre of the vehicle for receiving a flow of particulates from a contact point between the tyre or wheel and the driving surface, the filter unit comprising one or more electrostatically chargeable collector electrodes to attract charged particulates in the flow when the one or more collector electrodes are charged, so as to collect or capture the particulates; a charging circuit connected to the one or more collector electrodes for electrostatically charging the one or more collector electrodes; and a control module connectable to the charging circuit to selectively activate and deactivate charging of the one or more collecting electrodes in response to one or more detected driving conditions.
A method performed by an aircraft, comprising: operating a global position satellite landing system to generate control signals for flying an aircraft; obtaining aircraft inertial data using an inertial measuring unit on the aircraft; receiving, from a landing site, which is a ship, radar derived location data indicating a relative location of the aircraft to the ship as well as ship inertial data; and providing the generated control signals to a piloting system for automatically landing the aircraft; wherein in a normal operating state, the GPS landing system uses aircraft GPS data determined using a GPS receiver on the aircraft and ship GPS data received from the ship as an input; wherein, upon determining the GPS signals are unreliable, the GPS landing system switches to a backup operating state, wherein the GPS landing system uses the radar derived location data in combination with the aircraft inertial data and the ship inertial data as the input, in lieu of the GPS signals, and wherein the GPS signals are not used during the backup operating state and the radar derived location data is not used during the normal operating state. operating a global position satellite landing system to generate control signals for flying an aircraft; obtaining aircraft inertial data using an inertial measuring unit on the aircraft; receiving, from a landing site, which is a ship, radar derived location data indicating a relative location of the aircraft to the ship as well as ship inertial data; and providing the generated control signals to a piloting system for automatically landing the aircraft; wherein in a normal operating state, the GPS landing system uses aircraft GPS data determined using a GPS receiver on the aircraft and ship GPS data received from the ship as an input; wherein, upon determining the GPS signals are unreliable, the GPS landing system switches to a backup operating state, wherein the GPS landing system uses the radar derived location data in combination with the aircraft inertial data and the ship inertial data as the input, in lieu of the GPS signals, and wherein the GPS signals are not used during the backup operating state and the radar derived location data is not used during the normal operating state.
A qubit device comprising: a first group of superconducting capacitor pads positioned about a defined location of the qubit device, wherein the first group of superconducting capacitor pads comprise two or more superconducting capacitor pads having a first polarity; a second group of superconducting capacitor pads positioned about the defined location of the qubit device in an alternating arrangement with the first group of superconducting capacitor pads, wherein the second group of superconducting capacitor pads comprise two or more superconducting capacitor pads having a second polarity that is opposite the first polarity;. a first set of connectors that electrically couples respective ones of the first group of superconducting capacitor pads; and a second set of connectors that electrically couples respective ones of the second group of superconducting capacitor pads; characterized in that the qubit device further comprises an oxide barrier formed onto a least a portion of a surface of the first set of connectors, and wherein at least a portion of the second set of connectors is formed onto a surface of the oxide barrier that is opposite the first set of connectors, thereby defining a Josephson junction between the first set of connectors and the second set of connectors. a first group of superconducting capacitor pads positioned about a defined location of the qubit device, wherein the first group of superconducting capacitor pads comprise two or more superconducting capacitor pads having a first polarity; a second group of superconducting capacitor pads positioned about the defined location of the qubit device in an alternating arrangement with the first group of superconducting capacitor pads, wherein the second group of superconducting capacitor pads comprise two or more superconducting capacitor pads having a second polarity that is opposite the first polarity;. a first set of connectors that electrically couples respective ones of the first group of superconducting capacitor pads; and a second set of connectors that electrically couples respective ones of the second group of superconducting capacitor pads; characterized in that the qubit device further comprises an oxide barrier formed onto a least a portion of a surface of the first set of connectors, and wherein at least a portion of the second set of connectors is formed onto a surface of the oxide barrier that is opposite the first set of connectors, thereby defining a Josephson junction between the first set of connectors and the second set of connectors.
A method of detecting prostate cancer in a biological sample comprising: (a) combining the biological sample with at least a first and a second oligonucleotide primer under hybridizing conditions, wherein the first oligonucleotide primer contains a sequence that hybridizes to a first sequence in a target sequence from EPC2 (SEQ ID NO:5) and the second oligonucleotide primer contains a sequence that hybridizes to a second sequence in a nucleic acid strand complementary to the target sequence, wherein the first sequence does not overlap with the second sequence, wherein the target sequence comprises nucleotides 127 to 807 of SEQ ID NO: 5; (b) amplifying a plurality of amplification products when the target sequence is present in the biological sample by adding at least one polymerase activity to the biological sample containing the first and second oligonucleotide primers; (c) immobilizing the plurality of amplification products; (d) combining an oligonucleotide probe with the immobilized plurality of amplification products to thereby permit the probe to hybridize to at least one immobilized amplification product; and (e) detecting whether a signal results from hybridization between the oligonucleotide probe and at least one amplification product, wherein detection of the signal indicates the expression of EPC2 (SEQ ID NO:5) and the presence of prostate cancer in the biological sample. (a) combining the biological sample with at least a first and a second oligonucleotide primer under hybridizing conditions, wherein the first oligonucleotide primer contains a sequence that hybridizes to a first sequence in a target sequence from EPC2 (SEQ ID NO:5) and the second oligonucleotide primer contains a sequence that hybridizes to a second sequence in a nucleic acid strand complementary to the target sequence, wherein the first sequence does not overlap with the second sequence, wherein the target sequence comprises nucleotides 127 to 807 of SEQ ID NO: 5; (b) amplifying a plurality of amplification products when the target sequence is present in the biological sample by adding at least one polymerase activity to the biological sample containing the first and second oligonucleotide primers; (c) immobilizing the plurality of amplification products; (d) combining an oligonucleotide probe with the immobilized plurality of amplification products to thereby permit the probe to hybridize to at least one immobilized amplification product; and (e) detecting whether a signal results from hybridization between the oligonucleotide probe and at least one amplification product, wherein detection of the signal indicates the expression of EPC2 (SEQ ID NO:5) and the presence of prostate cancer in the biological sample.
A method of reducing mucus attributable to poly-gamma-glutamate, wherein the protein YwtB (CapA, PgsA) encoded by the ywtB gene and having an amino acid sequence which is at least 90% identical to the amino acid sequence set forth in SEQ ID NO. 8 is prevented from functioning as an enzyme involved in the formation of polyamino acids or as a subunit of such an enzyme.
Polyaxial bone anchoring device including a bone anchoring element comprising a head and a shank; a receiving part (4, 4', 4", 4"') for receiving a rod for coupling the rod to the bone anchoring element, the receiving part comprising a first end, an opposite second end and a central axis extending through the first end and the second end, and a channel for receiving the rod and an accommodation space for receiving the head; a pressure element (6, 6', 6") arranged in the receiving part and configured to exert pressure onto the head; wherein the pressure element (6, 6') comprises at least one flexible section (66a, 66b; 66a', 66b'), characterized in that the at least one flexible section (66a, 66b; 66a', 66b'; 66a", 66b") has a free end portion (69a, 69b; 69a', 69b', 69a", 69b") that cooperates with an inclined surface portion (15a, 15b; 32a, 32b; 15a", 15b") or with a protruding edge (151a, 151b) of the receiving part (4, 4'; 4", 4"') such as to hold the pressure element (6, 6'; 6") in a position in which it exerts a pre-load onto the head before the head is locked.
A self-drilling expansion fastener being integrally formed of a sheet metal material for use with an externally threaded element to tightly lock multiple layers of sheet workpieces to one another, comprising: an expansion structure being integrally formed to have an internally threaded body portion and a barrel body portion, wherein the internally threaded body portion is a cylindrical hollow body and includes a plurality of internal threads, and wherein the barrel body portion is a hexagonal hollow body, internally defines a hex bore and includes a plurality of laterally spaced force-distributing bars; and a drill structure being integrally formed at a head of the expansion structure; the drill structure including a chip guard connected to the expansion structure for covering the head of the expansion structure, and a drill forward projected from the chip guard for self-drilling a hole on the multiple layers of sheet workpieces, so that the expansion structure can be extended through the sheet workpieces and tightly received in the drilled hole with the force-distributing bars fully located behind the sheet workpieces; whereby when the externally threaded element is screwed deeper into the expansion structure to mesh with the internal threads, the force-distributing bars are gradually pulled backward to expand outward and are finally compressed into a fully folded state to tightly press against an inner side of the multiple layers of sheet workpieces, so that the sheet workpieces are firmly locked together. an expansion structure being integrally formed to have an internally threaded body portion and a barrel body portion, wherein the internally threaded body portion is a cylindrical hollow body and includes a plurality of internal threads, and wherein the barrel body portion is a hexagonal hollow body, internally defines a hex bore and includes a plurality of laterally spaced force-distributing bars; and a drill structure being integrally formed at a head of the expansion structure; the drill structure including a chip guard connected to the expansion structure for covering the head of the expansion structure, and a drill forward projected from the chip guard for self-drilling a hole on the multiple layers of sheet workpieces, so that the expansion structure can be extended through the sheet workpieces and tightly received in the drilled hole with the force-distributing bars fully located behind the sheet workpieces; whereby when the externally threaded element is screwed deeper into the expansion structure to mesh with the internal threads, the force-distributing bars are gradually pulled backward to expand outward and are finally compressed into a fully folded state to tightly press against an inner side of the multiple layers of sheet workpieces, so that the sheet workpieces are firmly locked together.
A method (600, 1200, 1300, 1400) for wireless communication, the method performed by a base station, the method comprising: identifying (610, 925, 1020, 1205, 1305, 1405) a set of synchronization signals, wherein the set of synchronization signals comprises primary synchronization signals, PSSs, secondary synchronization signals, SSSs, or a combination thereof, and multiplexing each PSS and each SSS of the set of synchronization signals using time division multiplexing; selecting (615, 930, 1025, 1210, 1310, 1315, 1320, 1415) a phase offset from a set of phase offsets for each synchronization signal of the set of synchronization signals, the set of phase offsets including a first phase offset and a second phase offset; and transmitting (620, 935, 1030, 1215, 1325, 1420) each synchronization signal of the set of synchronization signals on different component carriers of a set of component carriers using the selected phase offset, the set of synchronization signals being simultaneously transmitted using frequency division multiplexing, wherein each synchronization signal is associated with a different component carrier of the set of component carriers, and wherein a first synchronization signal of the set of synchronization signals is phase shifted according to the first phase offset and a second synchronization signal of the set of synchronization signals is phase shifted according to the second phase offset, wherein the first phase offset is different to the second phase offset. identifying (610, 925, 1020, 1205, 1305, 1405) a set of synchronization signals, wherein the set of synchronization signals comprises primary synchronization signals, PSSs, secondary synchronization signals, SSSs, or a combination thereof, and multiplexing each PSS and each SSS of the set of synchronization signals using time division multiplexing; selecting (615, 930, 1025, 1210, 1310, 1315, 1320, 1415) a phase offset from a set of phase offsets for each synchronization signal of the set of synchronization signals, the set of phase offsets including a first phase offset and a second phase offset; and transmitting (620, 935, 1030, 1215, 1325, 1420) each synchronization signal of the set of synchronization signals on different component carriers of a set of component carriers using the selected phase offset, the set of synchronization signals being simultaneously transmitted using frequency division multiplexing, wherein each synchronization signal is associated with a different component carrier of the set of component carriers, and wherein a first synchronization signal of the set of synchronization signals is phase shifted according to the first phase offset and a second synchronization signal of the set of synchronization signals is phase shifted according to the second phase offset, wherein the first phase offset is different to the second phase offset.
An injector having an injector head comprising a cylindrical body; and a middle cylinder embodied in the form of a cylindrical elevation on said body, further comprising a modular portion whereon information belonging to the injector is written, characterized in that said modular portion comprises an upper piece positioned on one side of the middle cylinder and embodied in semi-circle form, and that the modular portion comprises a lower piece positioned on the other side of the middle cylinder and embodied in semi-circle form.
Passenger seat arrangement for a passenger aircraft, comprising: a passenger seat assembly having at least one passenger seat (1, 2) and a seat supporting frame (3, 4); at least one seat fastening rail which can be installed in a cabin floor of the passenger aircraft and in which the seat supporting frame (3, 4) is mounted; a first electronic housing in which electrical power converter components are arranged and which is mounted on the seat fastening rail and which has a rail mounting adapter so that the vector of the weight force of the first electronic housing runs through the rail mounting adapter into the seat fastening rail; a second electronic housing in which electrical output ports for connecting electronic terminal devices are arranged and which is mounted on the passenger seat assembly; and wired cabling which electrically connects a supply port of the electrical power converter components of the first electronic housing to the electrical output ports of the second electronic housing. a passenger seat assembly having at least one passenger seat (1, 2) and a seat supporting frame (3, 4); at least one seat fastening rail which can be installed in a cabin floor of the passenger aircraft and in which the seat supporting frame (3, 4) is mounted; a first electronic housing in which electrical power converter components are arranged and which is mounted on the seat fastening rail and which has a rail mounting adapter so that the vector of the weight force of the first electronic housing runs through the rail mounting adapter into the seat fastening rail; a second electronic housing in which electrical output ports for connecting electronic terminal devices are arranged and which is mounted on the passenger seat assembly; and wired cabling which electrically connects a supply port of the electrical power converter components of the first electronic housing to the electrical output ports of the second electronic housing.