mhurhangee/patent-ind-claim-en huggingface dataset:
A downlink control channel monitoring method, comprising: sending first indication information to a network device, wherein the first indication information indicates N groups of monitoring capability parameters of a terminal device, wherein each group of monitoring capability parameters in the N groups of monitoring capability parameters comprise a reference value of an interval between monitoring spans and a reference value of duration of a monitoring span, N is a positive integer, and a reference value of a monitoring capability in the monitoring span, which comprises a maximum quantity of candidate downlink control channels and/or a maximum quantity of non-overlapping control channel elements; determining K monitoring spans in a first time unit based on the reference values of intervals between monitoring spans and/or the reference values of duration of monitoring spans in the N groups of monitoring capability parameters, wherein K is a positive integer; determining monitoring capabilities in the K monitoring spans based on the reference values of monitoring capabilities in monitoring spans in the N groups of monitoring capability parameters; and performing blind detection on a downlink control channel in the K monitoring spans based on the monitoring capabilities in the K monitoring spans; wherein a monitoring capability in each of the K monitoring spans is a maximum value of the reference values of the monitoring capabilities in the monitoring spans in the N groups of monitoring capability parameters. sending first indication information to a network device, wherein the first indication information indicates N groups of monitoring capability parameters of a terminal device, wherein each group of monitoring capability parameters in the N groups of monitoring capability parameters comprise a reference value of an interval between monitoring spans and a reference value of duration of a monitoring span, N is a positive integer, and a reference value of a monitoring capability in the monitoring span, which comprises a maximum quantity of candidate downlink control channels and/or a maximum quantity of non-overlapping control channel elements; determining K monitoring spans in a first time unit based on the reference values of intervals between monitoring spans and/or the reference values of duration of monitoring spans in the N groups of monitoring capability parameters, wherein K is a positive integer; determining monitoring capabilities in the K monitoring spans based on the reference values of monitoring capabilities in monitoring spans in the N groups of monitoring capability parameters; and performing blind detection on a downlink control channel in the K monitoring spans based on the monitoring capabilities in the K monitoring spans; wherein a monitoring capability in each of the K monitoring spans is a maximum value of the reference values of the monitoring capabilities in the monitoring spans in the N groups of monitoring capability parameters.
Connecting assembly for connecting two structures of an aircraft , the connecting assembly comprising: - a central element having a through-hole , preferably a bore, designed to make a connection with one of said two structures by virtue of a fastener element comprising a shank inserted into the through-hole , - a plurality of deformable shock-absorbing elements , referred to as first shock-absorbing elements, each of the first shock-absorbing elements being, on the one hand, secured to said central element and, on the other hand, configured to bear against a surface of the other structure of the two structures , - at least two other shock-absorbing elements , referred to as second shock-absorbing elements, manufactured from a deformable material, and, on the one hand, secured to the central element and, on the other hand, extending as far as a predetermined distance away from a surface of the other structure , the second shock-absorbing elements potentially comprising one or more metal inserts or inserts made from a material other than said deformable material, and/or one or more cavities arranged in the deformable material, the connecting assembly being characterized in that : - said first shock-absorbing elements each extend outwards, from the central element , in a direction perpendicular to a longitudinal axis of said through-hole, and in that : - said second shock-absorbing elements each extend outwards, from the central element , in a direction perpendicular to the longitudinal axis of said through-hole , which direction is different from the direction in which the first shock-absorbing elements extend. - a central element having a through-hole , preferably a bore, designed to make a connection with one of said two structures by virtue of a fastener element comprising a shank inserted into the through-hole , - a plurality of deformable shock-absorbing elements , referred to as first shock-absorbing elements, each of the first shock-absorbing elements being, on the one hand, secured to said central element and, on the other hand, configured to bear against a surface of the other structure of the two structures , - at least two other shock-absorbing elements , referred to as second shock-absorbing elements, manufactured from a deformable material, and, on the one hand, secured to the central element and, on the other hand, extending as far as a predetermined distance away from a surface of the other structure , the second shock-absorbing elements potentially comprising one or more metal inserts or inserts made from a material other than said deformable material, and/or one or more cavities arranged in the deformable material, - said first shock-absorbing elements each extend outwards, from the central element , in a direction perpendicular to a longitudinal axis of said through-hole, and in that : - said second shock-absorbing elements each extend outwards, from the central element , in a direction perpendicular to the longitudinal axis of said through-hole , which direction is different from the direction in which the first shock-absorbing elements extend.
A method for stabilizing the rotation speed of a hydraulic machine in turbine mode, the machine comprising a distributor adapted to modify a water flow, wherein the method comprises the steps of: - calculating a speed difference (ε) between the rotational speed (N) of the hydraulic machine and a target rotational speed (N_sp), processing said speed difference (ε) to output an orientation (γ) of the distributor; - orienting the distributor according to said orientation (γ); and - processing said speed difference (ε) by an electric torque controller to output an electric torque and applying said electric torque (Telec) to the machine , wherein the method comprises a step of coupling the hydraulic machine to a grid , which step comprises opening an electric torque circuit breaker between the source of the electric torque and the machine . - calculating a speed difference (ε) between the rotational speed (N) of the hydraulic machine and a target rotational speed (N_sp), processing said speed difference (ε) to output an orientation (γ) of the distributor; - orienting the distributor according to said orientation (γ); and - processing said speed difference (ε) by an electric torque controller to output an electric torque and applying said electric torque (Telec) to the machine , wherein the method comprises a step of coupling the hydraulic machine to a grid , which step comprises opening an electric torque circuit breaker between the source of the electric torque and the machine .
A flame-retardant foamable styrene-based resin composition comprising (A) a styrene-based resin, (B) a mixture of (B1) tetrabromobisphenol A-bis(2,3-dibromo-2-methylpropyl ether) and (B2) a different bromine-containing flame retardant, (C) zinc-modified hydrotalcite, (D) zeolite, and (G) a foaming agent, wherein 0.005 to 0.08 parts by weight of the zinc-modified hydrotalcite (C) are contained per 100 parts by weight of the styrene-based resin (A).
A system for treating a neural site in a body comprising: a therapeutic substance ; a catheter comprising a lumen coupled to at least one delivery tip ; a controller configured to project the at least one delivery tip outwards from the catheter into a treatment site within the body upon deployment and to deliver a bolus of the therapeutic substance through the lumen and the at least one delivery tip during use; wherein the at least one delivery tip comprises at least one of one or more electrodes (1720; 1780) and one or more sensors, the one or more electrodes being configured to monitor a margin of migration of the bolus of the therapeutic substance delivered through the lumen into the treatment site. a therapeutic substance ; a catheter comprising a lumen coupled to at least one delivery tip ; a controller configured to project the at least one delivery tip outwards from the catheter into a treatment site within the body upon deployment and to deliver a bolus of the therapeutic substance through the lumen and the at least one delivery tip during use; wherein the at least one delivery tip comprises at least one of one or more electrodes (1720; 1780) and one or more sensors, the one or more electrodes being configured to monitor a margin of migration of the bolus of the therapeutic substance delivered through the lumen into the treatment site.
A wind power installation with - a tower , - an aerodynamic rotor , wherein the aerodynamic rotor - can be operated with a variable rotor speed (n) and - has a number of rotor blades respectively with an adjustable rotor blade angle (α), - a generator (Gen) for generating an electrical output power, wherein - for operating the wind power installation an operating characteristic , which indicates a relationship between the rotor speed (n) and the output power (P), is specified and - a controller, which sets the output power (P) in a way corresponding to the operating characteristic in dependence on the rotor speed (n), is provided, wherein - selectable as the operating characteristic is a reduced-tonality operating characteristic , which is designed such that an excitation of a system resonance of the wind power installation is reduced as compared with an optimum-power operating characteristic , without however excluding a speed that excites this system resonance and characterized in that - it is provided with a pitch control, which sets the rotor blade angle (α) in dependence on the generated output power in partial-load operation in a way corresponding to a pitch characteristic , and wherein the pitch characteristic is adapted in dependence on the selected operating characteristic , in particular is selectable from a number of pitch characteristics , in particular a dedicated pitch characteristic is provided for each operating characteristic. - a tower , - an aerodynamic rotor , wherein the aerodynamic rotor - can be operated with a variable rotor speed (n) and - has a number of rotor blades respectively with an adjustable rotor blade angle (α), - a generator (Gen) for generating an electrical output power, - for operating the wind power installation an operating characteristic , which indicates a relationship between the rotor speed (n) and the output power (P), is specified and - a controller, which sets the output power (P) in a way corresponding to the operating characteristic in dependence on the rotor speed (n), is provided, wherein - selectable as the operating characteristic is a reduced-tonality operating characteristic , which is designed such that an excitation of a system resonance of the wind power installation is reduced as compared with an optimum-power operating characteristic , without however excluding a speed that excites this system resonance and characterized in that - it is provided with a pitch control, which sets the rotor blade angle (α) in dependence on the generated output power in partial-load operation in a way corresponding to a pitch characteristic , and wherein the pitch characteristic is adapted in dependence on the selected operating characteristic , in particular is selectable from a number of pitch characteristics , in particular a dedicated pitch characteristic is provided for each operating characteristic.
A blend consisting essentially of one or more alkoxylated C4-C10 alcohols and one or more siloxane-based defoamers in a weight ratio from 0.1 : 10 to 10 : 0.01 wherein the alkoxylated alcohol is a compound of formula (III), R 3 -O(AO) m -H (III), wherein R 3 is a C4-C10 alkyl group, AO is an alkyleneoxy group having 2-4, preferably 2 carbon atoms, and m is from 1-10, and the term "consisting essentially of" means that the blend comprises more than 90 percent by weight of the alkoxylated alcohol of formula (III) and siloxane defoamer.
A method of linking a two-dimensional design image to a three-dimensional design model, comprising: receiving a 2D design document and a 3D design file, the 2D design document comprising a 2D design image and the 3D design file comprising a 3D design model including one or more design elements; converting the 3D design model to a coded 2D design image, the coded 2D design image comprising one or more coded 2D design elements corresponding to the one or more design elements; determining a unique identifier for each of the one or more design elements based on a code of a coded 2D design element of the one or more coded 2D design elements, the code corresponding to a design element of the one or more design elements; storing each unique identifier in association with the respective design element in the 3D design file; determining an alignment between the 2D design image and the coded 2D design image; receiving a user selection of a point in the 2D design image; determining a reference point in the coded 2D design image that corresponds to the user selection of the point in the 2D design image; and determining a design element data set associated with a design element that corresponds to the reference point, the design element data set being stored in the 3D design file. receiving a 2D design document and a 3D design file, the 2D design document comprising a 2D design image and the 3D design file comprising a 3D design model including one or more design elements; converting the 3D design model to a coded 2D design image, the coded 2D design image comprising one or more coded 2D design elements corresponding to the one or more design elements; determining a unique identifier for each of the one or more design elements based on a code of a coded 2D design element of the one or more coded 2D design elements, the code corresponding to a design element of the one or more design elements; storing each unique identifier in association with the respective design element in the 3D design file; determining an alignment between the 2D design image and the coded 2D design image; receiving a user selection of a point in the 2D design image; determining a reference point in the coded 2D design image that corresponds to the user selection of the point in the 2D design image; and determining a design element data set associated with a design element that corresponds to the reference point, the design element data set being stored in the 3D design file.
Measuring device with a light measuring device having a sensor surface and having a shadow generator which is arranged rotatably in steps with respect to the sensor surface , it being possible for the shadow generator to generate a core shadow and a penumbra for each step, and having an evaluation unit which comprises a data storage device and which is connected to the data storage device in a data-conducting manner, in which a light hardness scale is stored, the light hardness scale having a minimum limit value and a maximum limit value, diffuse light being assigned to the minimum limit value and directional light being assigned to the maximum limit value, and each light hardness value between the limit values corresponding to a specific proportion ratio of diffuse and directional light, and the evaluation unit is connected to the sensor surface in a data-conducting manner, and the sensor surface has a multiplicity of sensors which are distributed over the sensor surface and each measure an illuminance, and illuminance measurement values of the sensors can be fed to the evaluation unit, wherein the evaluation unit determines a course of illuminance along a measuring line of the sensor surface for different positions of the shadow generator , determines the ascending slope (α) along the measuring line of the course of illuminance of the penumbra , determines the steepest ascending slope, selects the steepest ascending slope, and assigns it to a light hardness within the light hardness scale. a light measuring device having a sensor surface and having a shadow generator which is arranged rotatably in steps with respect to the sensor surface , it being possible for the shadow generator to generate a core shadow and a penumbra for each step, and having an evaluation unit which comprises a data storage device and which is connected to the data storage device in a data-conducting manner, in which a light hardness scale is stored, the light hardness scale having a minimum limit value and a maximum limit value, diffuse light being assigned to the minimum limit value and directional light being assigned to the maximum limit value, and each light hardness value between the limit values corresponding to a specific proportion ratio of diffuse and directional light, and the evaluation unit is connected to the sensor surface in a data-conducting manner, and the sensor surface has a multiplicity of sensors which are distributed over the sensor surface and each measure an illuminance, and illuminance measurement values of the sensors can be fed to the evaluation unit, wherein the evaluation unit determines a course of illuminance along a measuring line of the sensor surface for different positions of the shadow generator , determines the ascending slope (α) along the measuring line of the course of illuminance of the penumbra , determines the steepest ascending slope, selects the steepest ascending slope, and assigns it to a light hardness within the light hardness scale.
Strip, sheet or blank suitable for hot forming at a temperature of 700° C or above, comprising a substrate of hot formable steel, optionally coated with an active corrosion protective coating, characterised in that the optionally coated steel substrate is provided with a ceramic based coating having a thickness of at most 25 micron on the external layer, wherein the ceramic based coating comprises 5 - 80% SiO 2 , 1 - 30% Al 2 O 3 and 1 - 30% MgO 2 , and optionally max 5% CaO, max 10% Fe 2 O 3 and max 10% MnO 2 .
A circuit for recuperating electrical energy from a mechanical resonator comprising: a control circuit ; and a voltage inversion circuit configured to invert the voltage across a capacitance (Cp) of the mechanical resonator, the voltage inversion circuit comprising: a capacitor (Cint); and a charge transfer circuit configured: - to discharge a voltage of a first polarity held by the capacitance of the mechanical resonator to said capacitor during a first period; and - to charge a voltage, of opposite polarity to the first polarity, to the capacitance of the mechanical resonator during a second period using the voltage potential stored by said capacitor during the first period; characterized in that the charge transfer circuit comprises an inductance and at least one switch , the control circuit being configured to switch the at least one switch during the first and/or second period to limit the current passing through the inductance. a control circuit ; and a voltage inversion circuit configured to invert the voltage across a capacitance (Cp) of the mechanical resonator, the voltage inversion circuit comprising: a capacitor (Cint); and a charge transfer circuit configured: - to discharge a voltage of a first polarity held by the capacitance of the mechanical resonator to said capacitor during a first period; and - to charge a voltage, of opposite polarity to the first polarity, to the capacitance of the mechanical resonator during a second period using the voltage potential stored by said capacitor during the first period; characterized in that the charge transfer circuit comprises an inductance and at least one switch , the control circuit being configured to switch the at least one switch during the first and/or second period to limit the current passing through the inductance. a capacitor (Cint); and a charge transfer circuit configured: - to discharge a voltage of a first polarity held by the capacitance of the mechanical resonator to said capacitor during a first period; and - to charge a voltage, of opposite polarity to the first polarity, to the capacitance of the mechanical resonator during a second period using the voltage potential stored by said capacitor during the first period; - to discharge a voltage of a first polarity held by the capacitance of the mechanical resonator to said capacitor during a first period; and - to charge a voltage, of opposite polarity to the first polarity, to the capacitance of the mechanical resonator during a second period using the voltage potential stored by said capacitor during the first period; characterized in that the charge transfer circuit comprises an inductance and at least one switch , the control circuit being configured to switch the at least one switch during the first and/or second period to limit the current passing through the inductance.
Timepiece resonator mechanism comprising a structure and at least one inertial element arranged to oscillate in a pivoting movement around a pivot axis (D) with the centre of inertia of said at least one inertial element aligned on said pivot axis (D), wherein said at least one inertial element is subjected to restoring forces exerted by a plurality of elastic blades , each fixed directly or indirectly to said structure at a first end and fixed directly or indirectly to said at least one inertial element at a second end, and each said elastic blade extends in a perpendicular plane to said pivot axis (D) and is substantially deformable in said perpendicular plane to said pivot axis (D), where said resonator mechanism comprises axial stop means comprising at least a lower axial stop and/or an upper axial stop , and said axial stop means are arranged to cooperate by bearing in abutment with at least one of the movable components for the protection of said blade resonator mechanism against axial shocks in the direction of said pivot axis (D), characterised in that said resonator mechanism comprises a plurality of said inertial elements , which extend over several parallel levels, and in that said resonator mechanism comprises at least one intermediate axial stop, which is arranged between two said adjacent levels of said inertial elements .