mhurhangee/patent-ind-claim-en huggingface dataset:
Method for controlling or regulating an operating device, in particular of a railway system, which is fed by an operating network (BN) that is connected to at least one energy supply system (EVN1, EVN2), in order to maintain a desired load profile within the operating network (BN), in particular to avoid or compensate for load peaks, with a load calculator (RL), characterised in that a) the load calculator (RL) is provided with the data of the course of the total load (PG) occurring in the operating network (BN), b) several courses of load components (PSO, PS1, PS2) are determined from the total load (PG); c) the future course (PSOE, PS1E, PS2E) is determined for each of the load components (PSO, PS1, PS2); d) the future courses (PSOE, PS1E, PS2E) determined for the load components (PSO, PS1, PS2) are superimposed to determine a future course (PGE) of the total load (PG) and future load peaks; and e) the operating device and/or the at least one energy supply system (EVN1, EVN2) is controlled or regulated under consideration of the determined future course (PGE) of the total load (PG) and predefined load limits in order to avoid future load peaks or to provide the energy required therefor, wherein in order to determine the load components (PSO, PS1, PS2) within the course of the total load (PG), possibly the averaged total load course (PGG), recursively occurring signal components and/or periodically occurring signal components are determined. a) the load calculator (RL) is provided with the data of the course of the total load (PG) occurring in the operating network (BN), b) several courses of load components (PSO, PS1, PS2) are determined from the total load (PG); c) the future course (PSOE, PS1E, PS2E) is determined for each of the load components (PSO, PS1, PS2); d) the future courses (PSOE, PS1E, PS2E) determined for the load components (PSO, PS1, PS2) are superimposed to determine a future course (PGE) of the total load (PG) and future load peaks; and e) the operating device and/or the at least one energy supply system (EVN1, EVN2) is controlled or regulated under consideration of the determined future course (PGE) of the total load (PG) and predefined load limits in order to avoid future load peaks or to provide the energy required therefor,
A rotary hoe arrangement for weeding a field, the rotary hoe arrangement comprising - a tool bar comprising a plurality of hoe wheels along the tool bar , two foldable wing sections divided by a central bar , each wing section comprises an inner wing connected to an outer wing having a distal wing end , - the tool bar having an operational position , where the central bar , inner wings and outer wings define a straight work line , and a folded position where the wing sections are folded for transportation to and from a field, - each inner wing being pivotably engaged with the central bar , each inner wing pivots in an inner plane between an inner operational position, where the inner wing extends along the straight work line , and an inner folded position, where the inner wing extends vertically upwardly and substantially perpendicularly to the straight work line , characterised in that - each outer wing being pivotably engaged with the corresponding inner wing , each outer wing pivots in an outer plane being tilted relative to the corresponding inner plane between an outer operational position, where the outer wing extends along the straight work line , and an outer folded position, where the distal wing end substantially faces the central bar and the outer wing is parallel to the corresponding inner wing and positioned upwardly in the outer plane, and where each outer plane forms a 35-55 degree angle with the corresponding inner plane. - a tool bar comprising a plurality of hoe wheels along the tool bar , two foldable wing sections divided by a central bar , each wing section comprises an inner wing connected to an outer wing having a distal wing end , - the tool bar having an operational position , where the central bar , inner wings and outer wings define a straight work line , and a folded position where the wing sections are folded for transportation to and from a field, - each inner wing being pivotably engaged with the central bar , each inner wing pivots in an inner plane between an inner operational position, where the inner wing extends along the straight work line , and an inner folded position, where the inner wing extends vertically upwardly and substantially perpendicularly to the straight work line , characterised in that - each outer wing being pivotably engaged with the corresponding inner wing , each outer wing pivots in an outer plane being tilted relative to the corresponding inner plane between an outer operational position, where the outer wing extends along the straight work line , and an outer folded position, where the distal wing end substantially faces the central bar and the outer wing is parallel to the corresponding inner wing and positioned upwardly in the outer plane, and where each outer plane forms a 35-55 degree angle with the corresponding inner plane.
A method performed by a user equipment, comprising: determining, by the user equipment, a quasi co-location source reference signal associated with a configured transmission configuration index state for a physical downlink control channel, wherein the configured transmission configuration index state refers to an aperiodic or semi-persistent reference signal; and including the quasi co-location source reference signal in a set of reference signals to use for radio link monitoring or failure detection if the quasi co-location source reference signal is a periodic reference signal, and the user equipment is not explicitly provided with the set of reference signals. determining, by the user equipment, a quasi co-location source reference signal associated with a configured transmission configuration index state for a physical downlink control channel, wherein the configured transmission configuration index state refers to an aperiodic or semi-persistent reference signal; and including the quasi co-location source reference signal in a set of reference signals to use for radio link monitoring or failure detection if the quasi co-location source reference signal is a periodic reference signal, and the user equipment is not explicitly provided with the set of reference signals.
A fullerenic structure comprising a fullerene C 60 chemically bonded to a surface of a carbon material, wherein the carbon material is carbon black.
A product for use in the treatment of a cancer or a blood disorder in a subject, the product comprising a first composition and a second composition, wherein the first composition comprises decitabine, tetrahydrouridine and a pharmaceutically acceptable carrier, the second composition comprises 5-azacytidine, tetrahydrouridine and a pharmaceutically acceptable carrier, and wherein the first and the second compositions are for administration to the subject sequentially or alternately or simultaneously. wherein the first composition comprises decitabine, tetrahydrouridine and a pharmaceutically acceptable carrier, the second composition comprises 5-azacytidine, tetrahydrouridine and a pharmaceutically acceptable carrier, and wherein the first and the second compositions are for administration to the subject sequentially or alternately or simultaneously.
A method for operating a transmitting device using semi-orthogonal multiple access, SOMA, in a wireless local area network, WLAN, wherein the SOMA is a combination of power domain optimization and modulation division multiple access, MDMA, the method comprising: determining , by the transmitting device, a first quadrature amplitude modulation, QAM, bit allocation, a first coding rate, and a first SOMA group for a first receiving device and a second QAM bit allocation, a second coding rate, and a second SOMA group for a second receiving device in accordance with channel information associated with the first receiving device and the second receiving device, wherein SOMA groups are identified by a SOMA group identifier and a SOMA group identifier is used to identify receiving devices participating in a SOMA transmission; generating , by the transmitting device, a frame including indicators of the first and second QAM bit allocations, the first and second coding rates, and the first and second SOMA groups; and sending , by the transmitting device, the frame to the first receiving device and the second receiving device; wherein generating the frame comprises: for each SOMA group, populating a group identifier field with a SOMA group identifier associated with the SOMA group, and populating a modulation and coding scheme, MCS, field with a modulation and coding rate indicator for each receiving device associated with the SOMA group. determining , by the transmitting device, a first quadrature amplitude modulation, QAM, bit allocation, a first coding rate, and a first SOMA group for a first receiving device and a second QAM bit allocation, a second coding rate, and a second SOMA group for a second receiving device in accordance with channel information associated with the first receiving device and the second receiving device, wherein SOMA groups are identified by a SOMA group identifier and a SOMA group identifier is used to identify receiving devices participating in a SOMA transmission; generating , by the transmitting device, a frame including indicators of the first and second QAM bit allocations, the first and second coding rates, and the first and second SOMA groups; and sending , by the transmitting device, the frame to the first receiving device and the second receiving device; for each SOMA group, populating a group identifier field with a SOMA group identifier associated with the SOMA group, and populating a modulation and coding scheme, MCS, field with a modulation and coding rate indicator for each receiving device associated with the SOMA group.
Device for attaching an end of a bracelet to an object, particularly a watch case or a piece of jewellery, comprising; - a support plate formed of a base defining a plane, - a control member , - two pins (4' 4") slidably mounted in the plane of the support plate on the same sliding axis, said pins (4', 4") being able, after actuation of the control member to move between a position of engagement in which the pins (4', 4") are secured to the object, and a retracted position in which the pins (4', 4") are detached from the object, - elastic means connecting the two pins (4', 4") and maintaining said pins (4', 4") in a position of engagement in the absence of actuation of the control member , the device being characterized in that the control member is mounted to move in translation on an arbor, called the translation arbor , which is substantially perpendicular to the plane of the support plate , and in that the control member is offset with respect to the sliding axis of the pins (4', 4") and connected to the latter by connecting elements (5', 5", 6', 6") able to transform the translational movement of the control member into a sliding movement of the pins (4', 4") when the control member is actuated and in that the connecting elements successively include between the control member and the pins (4'. 4"): - two arms (5', 5") articulated at one end about an arbor, called the pivot arbor , the arms (5', 5") being arranged around the control member symmetrically with respect to a line connecting said pivot arbor and the translation arbor of the control member, said line being perpendicular to the sliding axis of the pins (4', 4"), - two connecting rods (6', 6") each mounted to pivot via pegs (9', 9") on the other end of said arms (5', 5"). - a support plate formed of a base defining a plane, - a control member , - two pins (4' 4") slidably mounted in the plane of the support plate on the same sliding axis, said pins (4', 4") being able, after actuation of the control member to move between a position of engagement in which the pins (4', 4") are secured to the object, and a retracted position in which the pins (4', 4") are detached from the object, - elastic means connecting the two pins (4', 4") and maintaining said pins (4', 4") in a position of engagement in the absence of actuation of the control member , - two arms (5', 5") articulated at one end about an arbor, called the pivot arbor , the arms (5', 5") being arranged around the control member symmetrically with respect to a line connecting said pivot arbor and the translation arbor of the control member, said line being perpendicular to the sliding axis of the pins (4', 4"), - two connecting rods (6', 6") each mounted to pivot via pegs (9', 9") on the other end of said arms (5', 5").
A downforce system for a vehicle, the downforce system comprising: a restrictor configured to restrict a flow of air into a region that is defined at least in part by the restrictor and a ground surface on which the vehicle is disposed, a rim disposed on the restrictor and configured to form at least a partial seal with the ground surface; a dedicated pressure source disposed outside the restrictor and connected to the restrictor via an air flow path , the pressure source being configured to generate a pressure differential across the restrictor; the downforce system being characterised by a preload mechanism configured to apply a preload force to the rim to press the rim against the ground surface, wherein the preload mechanism includes an actuator for varying the preload force applied by the preload mechanism. a restrictor configured to restrict a flow of air into a region that is defined at least in part by the restrictor and a ground surface on which the vehicle is disposed, a rim disposed on the restrictor and configured to form at least a partial seal with the ground surface; a dedicated pressure source disposed outside the restrictor and connected to the restrictor via an air flow path , the pressure source being configured to generate a pressure differential across the restrictor; the downforce system being characterised by a preload mechanism configured to apply a preload force to the rim to press the rim against the ground surface, wherein the preload mechanism includes an actuator for varying the preload force applied by the preload mechanism.
An organic compound represented by formula : wherein R 1 to R 24 are each independently selected from the group consisting of a hydrogen atom, a halogen atom, a substituted or unsubstituted alkyl group, a substituted or unsubstituted alkoxy group, a substituted or unsubstituted amino group, a substituted or unsubstituted aryl group, a substituted or unsubstituted heterocyclic group, a substituted or unsubstituted aryloxy group, a silyl group, and a cyano group.
A multi-layered ceramic product having a sintered first layer and a buckled or mounded second layer integrated on top of the first layer , wherein the second layer is obtained from a geopolymer and/or a zeolite powder.
A method of determining an isotope ratio of ions from a source of ions using mass spectrometry comprising: obtaining a plurality of mass spectra of ions, wherein obtaining each mass spectrum of the plurality of mass spectra comprises: generating ions from a first source of ions; guiding the generated ions through a device having a mass transfer function that varies with ion current; providing at least some of the ions to a mass analyser; using the mass analyser to obtain a mass spectrum of the ions provided to the mass analyser; and determining the ion current of the ions provided to the mass analyser; wherein the mass spectra are obtained for different measured ion currents; determining an isotope ratio of ions provided to the mass analyser from each mass spectrum; using the determined isotope ratio and determined ion current for each mass spectrum to determine a calibration relationship that characterises a variation of the determined isotope ratios and the measured ion currents across the mass spectra; and adjusting a measured isotope ratio obtained at a determined ion current by using the calibration relationship to adjust the measured isotope ratio to an adjusted isotope ratio corresponding to a selected ion current. obtaining a plurality of mass spectra of ions, wherein obtaining each mass spectrum of the plurality of mass spectra comprises: generating ions from a first source of ions; guiding the generated ions through a device having a mass transfer function that varies with ion current; providing at least some of the ions to a mass analyser; using the mass analyser to obtain a mass spectrum of the ions provided to the mass analyser; and determining the ion current of the ions provided to the mass analyser; generating ions from a first source of ions; guiding the generated ions through a device having a mass transfer function that varies with ion current; providing at least some of the ions to a mass analyser; using the mass analyser to obtain a mass spectrum of the ions provided to the mass analyser; and determining the ion current of the ions provided to the mass analyser; wherein the mass spectra are obtained for different measured ion currents; determining an isotope ratio of ions provided to the mass analyser from each mass spectrum; using the determined isotope ratio and determined ion current for each mass spectrum to determine a calibration relationship that characterises a variation of the determined isotope ratios and the measured ion currents across the mass spectra; and adjusting a measured isotope ratio obtained at a determined ion current by using the calibration relationship to adjust the measured isotope ratio to an adjusted isotope ratio corresponding to a selected ion current.
Multi-antenna broadband system for mobile communications consisting of at least two antennas with the same shape and same size, placed above an earth plane, the antennas are connected respectively to a modem, and the part most distant from the earth plane of each antenna is folded one or more times so that the folded part or the last folded part of the antenna forms an angle with the non-folded part of the antenna of between 10 and 100 degrees, characterised in that the multi-antenna system comprises an odd number of antennas comprising a first antenna and second antennas, the first antenna being placed at a point above the earth plane at the same distance from the earth plane as the distance from the second antennas to the earth plane and each second antenna is symmetrical with another second antenna in accordance with a central symmetry, the centre of the symmetry being the point at which the first antenna is placed.
A battery management apparatus for managing a chargeable and dischargeable battery, comprising: a battery state calculator that calculates a state of charge, a capacity deterioration degree, and a resistance deterioration degree of the battery; a mid voltage calculator that corrects the calculated resistance deterioration degree, corrects a mid resistance of the battery corresponding to a respective mid voltage according to a correction coefficient in accordance with the corrected resistance deterioration degree, and calculates a mid voltage that is present between a charge-discharge voltage in a current state of charge of the battery, and a charge-discharge voltage in a minimum state of charge or a maximum state of charge of the battery, based on the corrected mid resistance; a remaining capacity calculator that calculates a remaining capacity or a chargeable capacity of the battery, based on the calculated state of charge and the capacity deterioration degree; and an available energy calculator that calculates available energy or chargeable energy of the battery, based on the calculated mid voltage and the remaining capacity, or on the calculated mid voltage and the chargeable capacity. a battery state calculator that calculates a state of charge, a capacity deterioration degree, and a resistance deterioration degree of the battery; a mid voltage calculator that corrects the calculated resistance deterioration degree, corrects a mid resistance of the battery corresponding to a respective mid voltage according to a correction coefficient in accordance with the corrected resistance deterioration degree, and calculates a mid voltage that is present between a charge-discharge voltage in a current state of charge of the battery, and a charge-discharge voltage in a minimum state of charge or a maximum state of charge of the battery, based on the corrected mid resistance; a remaining capacity calculator that calculates a remaining capacity or a chargeable capacity of the battery, based on the calculated state of charge and the capacity deterioration degree; and an available energy calculator that calculates available energy or chargeable energy of the battery, based on the calculated mid voltage and the remaining capacity, or on the calculated mid voltage and the chargeable capacity.
A bolus for non-surgical, non-therapeutic intravenous (IV) administration comprising a liquid solution of a radioactive compound having a radioactive half-life of less than 21 minutes for use in blood flow imaging, characterized in that said bolus has a radioactivity concentration of between 180-220 MBq/ml, such as 200 MBq/ml, and said radioactive compound is radioactive water, such as 0-15 H 2 O or 0-14 H 2 O.
An ice protection system for an airfoil comprising: an electrical heating mat comprising an electrically resistive material, wherein the electrically resistive material is configured to define a first spanwise zone of the airfoil and a first chordwise zone of the airfoil, wherein at least one of the first spanwise zone or the first chordwise zone include a first busbar portion (604A-1) contiguous with the electrically resistive material, and characterized in that wherein the electrical heating mat is etched such that each of the first spanwise zone, the first chordwise zone, and the first busbar portion are coplanar in a first layer of the ice protection system; and an anti-ice strip zone , wherein the anti-ice strip zone is etched in a second layer different from the first layer, and wherein the anti-ice strip zone is overlaid across the first spanwise zone and the first chordwise zone such that the anti-ice strip zone is configured to extend along a leading edge axis and to coincide with a leading edge . an electrical heating mat comprising an electrically resistive material, wherein the electrically resistive material is configured to define a first spanwise zone of the airfoil and a first chordwise zone of the airfoil, wherein at least one of the first spanwise zone or the first chordwise zone include a first busbar portion (604A-1) contiguous with the electrically resistive material, and characterized in that wherein the electrical heating mat is etched such that each of the first spanwise zone, the first chordwise zone, and the first busbar portion are coplanar in a first layer of the ice protection system; and an anti-ice strip zone , wherein the anti-ice strip zone is etched in a second layer different from the first layer, and wherein the anti-ice strip zone is overlaid across the first spanwise zone and the first chordwise zone such that the anti-ice strip zone is configured to extend along a leading edge axis and to coincide with a leading edge .