mhurhangee/ep-ind-claims huggingface dataset:
A blower housing part with an inlet opening for sucking in blower air and with a bearing support held in the inlet opening for accommodating a blower motor, wherein the bearing support has a bearing bush open toward a blower motor side, which is designed to accommodate at least one motor shaft bearing of the blower motor, wherein conically tapered ribs are formed in the bearing bush, which reduce a cross-sectional area of an accommodating space of the bearing bush in the axial direction, characterised in that in the bearing bush a bush-shaped elastomeric element is arranged, which is designed to accommodate the at least one motor shaft bearing of the blower motor.
A device for detecting the axial position of a rotary shaft of a rotary machine, the device comprising a target of ferromagnetic material placed at the end of said rotary shaft, an induction coil associated with a stationary magnetic circuit secured to a structure of the rotary machine and placed facing said target while leaving an airgap, and a power supply circuit for powering said induction coil, the device being characterized in that the circuit for powering the induction coil comprises an AC voltage source connected between a first end of the induction coil and a zone situated at a reference voltage (0 V), at least one capacitor connected between said first end of the induction coil and a second end of the induction coil, and a detector device interposed between said second end of the induction coil and said zone situated at said reference voltage (0 V), in order to deliver on a line information (i L) about the magnitude of the current flowing between said second end of the induction coil and said zone situated at the reference voltage (0 V), said information (i L) representing the value of a modification x to the width of said airgap that presents a predetermined nominal value e 0.
A method comprising: configuring a plurality of transceiver modules (702, 704, 706, 708) in an antenna array with assigned receive signal weighting factors for distributed signal combining, wherein the transceiver modules (702, 704, 706, 708) are interconnected with serial high-speed data communication buses, and wherein each transceiver module is positioned adjacent to a respective antenna element in the antenna array; configuring the plurality of transceiver modules (702, 704, 706, 708) into a plurality of transceiver - module groups, each transceiver module group including a group of transceiver modules (702, 704, 706, 708) that are serially connected and intercommunicating via the associated serial high-speed data communication buses; receiving a plurality of wireless radio frequency, RF, modulated data signals at the plurality of transceiver modules (702, 704, 706, 708) and responsively generating a corresponding plurality of receive in-phase, I, and quadrature, Q, baseband data signals; generating a plurality of received beamformed signals using the plurality of transceiver module groups by combining subsets of the receive I and Q baseband data signals within each transceiver module group using the assigned receive signal weighting factors, wherein the combining includes transmitting weighted receive I and Q baseband data signals between the transceiver modules within the transceiver module group; and demodulating the received beamformed signals. configuring a plurality of transceiver modules (702, 704, 706, 708) in an antenna array with assigned receive signal weighting factors for distributed signal combining, wherein the transceiver modules (702, 704, 706, 708) are interconnected with serial high-speed data communication buses, and wherein each transceiver module is positioned adjacent to a respective antenna element in the antenna array; configuring the plurality of transceiver modules (702, 704, 706, 708) into a plurality of transceiver - module groups, each transceiver module group including a group of transceiver modules (702, 704, 706, 708) that are serially connected and intercommunicating via the associated serial high-speed data communication buses; receiving a plurality of wireless radio frequency, RF, modulated data signals at the plurality of transceiver modules (702, 704, 706, 708) and responsively generating a corresponding plurality of receive in-phase, I, and quadrature, Q, baseband data signals; generating a plurality of received beamformed signals using the plurality of transceiver module groups by combining subsets of the receive I and Q baseband data signals within each transceiver module group using the assigned receive signal weighting factors, wherein the combining includes transmitting weighted receive I and Q baseband data signals between the transceiver modules within the transceiver module group; and demodulating the received beamformed signals.
A computer-implemented method comprising: (i) receiving first data from a first sensor, the first data comprising values for a first parameter of an aircraft; (ii) determining whether damage has occurred to the aircraft using the values of the first data; (iii) receiving second data from a second sensor, the second data comprising values for a second parameter of the aircraft; (iv) determining whether damage has occurred to the aircraft using the values of the second data; (v) determining whether damage has occurred to the aircraft using the determinations of whether damage has occurred at steps (ii) and (iv); (vi) receiving third data from a third sensor, the third data comprising values for a third parameter of the aircraft; (vii) determining whether damage has occurred to the aircraft using the values of the third data; (viii) determining whether damage has occurred to the aircraft using the determination of whether damage has occurred at steps (v) and (vii); and (ix) controlling output of a signal comprising data indicating the occurrence of damage to the aircraft using the occurrence of damage determined at step (viii), wherein step (ix) is performed subsequent to the determination of damage occurrence at step (v) and at step (viii). (i) receiving first data from a first sensor, the first data comprising values for a first parameter of an aircraft; (ii) determining whether damage has occurred to the aircraft using the values of the first data; (iii) receiving second data from a second sensor, the second data comprising values for a second parameter of the aircraft; (iv) determining whether damage has occurred to the aircraft using the values of the second data; (v) determining whether damage has occurred to the aircraft using the determinations of whether damage has occurred at steps (ii) and (iv); (vi) receiving third data from a third sensor, the third data comprising values for a third parameter of the aircraft; (vii) determining whether damage has occurred to the aircraft using the values of the third data; (viii) determining whether damage has occurred to the aircraft using the determination of whether damage has occurred at steps (v) and (vii); and (ix) controlling output of a signal comprising data indicating the occurrence of damage to the aircraft using the occurrence of damage determined at step (viii), wherein step (ix) is performed subsequent to the determination of damage occurrence at step (v) and at step (viii).
An arc extinguishing unit for a molded case circuit breaker (MCCB) including a casing, a stator connected to a load or a power source, and a mover rotatably installed within the casing such that it is brought into contact with or separated from the stator, the arc extinguishing unit for a molded case circuit breaker comprising: a plurality of grids arranged at predetermined intervals,; a pair of side plates including two-stage flat plates having a step cross-section and including a first flat plate fixing one end portions of the grids to form an arc chute and a second flat plate forming an arc chamber together with a lower surface of the grids; and a pair of lateral magnets fixedly installed on rear surfaces of the second plates, characterized by an intermediate protrusion formed on a lateral surface of each of the grids has a first stop projection formed on one side thereof, a second stop projection formed on a lower surface of each grid, a first installation hole formed on the first plate to allow the intermediate protrusion to be inserted therein, and a connection portion formed between the first flat plate and the second flat plate has a second installation hole to which the second projection is inserted. a plurality of grids arranged at predetermined intervals,; a pair of side plates including two-stage flat plates having a step cross-section and including a first flat plate fixing one end portions of the grids to form an arc chute and a second flat plate forming an arc chamber together with a lower surface of the grids; and a pair of lateral magnets fixedly installed on rear surfaces of the second plates, characterized by an intermediate protrusion formed on a lateral surface of each of the grids has a first stop projection formed on one side thereof, a second stop projection formed on a lower surface of each grid, a first installation hole formed on the first plate to allow the intermediate protrusion to be inserted therein, and a connection portion formed between the first flat plate and the second flat plate has a second installation hole to which the second projection is inserted.
A clock circuit comprising: a phase locked loop having a phase locked loop output for providing an output signal, a phase locked loop input for receiving a first reference signal and a feedback input for receiving a phase-adjusted feedback signal, and the phase locked loop further comprising means configured to derive a feedback signal from said output signal, a phase rotator configured to receive the feedback signal, the phase rotator configured to apply a phase shift to the feedback signal and to provide a first phase-shifted feedback signal; a delay element configured to receive the first phase-shifted feedback signal and provide the phase-adjusted feedback signal, wherein the phase rotator and the delay element both provide control of the feedback signal, wherein the phase rotator is adapted to perform frequency tracking by applying said phase shift to the feedback signal and the delay element is a fine controlled delay element adapted to perform phase tracking by applying an amount of phase delay or an amount of phase advance to the first phase-shifted feedback signal, and a phase detector, configured to compare the output signal to a second reference signal and provide, based on said comparison, both: a) a control signal to the phase rotator, via an integral control path for integral phase control, and b) a copy of said control signal to the delay element, via a proportional control path for proportional phase control. a phase locked loop having a phase locked loop output for providing an output signal, a phase locked loop input for receiving a first reference signal and a feedback input for receiving a phase-adjusted feedback signal, and the phase locked loop further comprising means configured to derive a feedback signal from said output signal, a phase rotator configured to receive the feedback signal, the phase rotator configured to apply a phase shift to the feedback signal and to provide a first phase-shifted feedback signal; a delay element configured to receive the first phase-shifted feedback signal and provide the phase-adjusted feedback signal, wherein the phase rotator and the delay element both provide control of the feedback signal, wherein the phase rotator is adapted to perform frequency tracking by applying said phase shift to the feedback signal and the delay element is a fine controlled delay element adapted to perform phase tracking by applying an amount of phase delay or an amount of phase advance to the first phase-shifted feedback signal, and a phase detector, configured to compare the output signal to a second reference signal and provide, based on said comparison, both: a) a control signal to the phase rotator, via an integral control path for integral phase control, and b) a copy of said control signal to the delay element, via a proportional control path for proportional phase control. a) a control signal to the phase rotator, via an integral control path for integral phase control, and b) a copy of said control signal to the delay element, via a proportional control path for proportional phase control.
Plug adapter having a first plug-side end and a second plug-side end, wherein the first plug-side end is configured as a first electrical interface having a first mechanical interface geometry and at least one first inner conductor part and at least one first outer conductor part and the second plug-side end is configured as a second electrical interface having a second mechanical interface geometry and at least one second inner conductor part and at least one second outer conductor part, wherein the first and second mechanical interface geometries have different designs, wherein at least one first inner conductor part and one second inner conductor part are configured, in each case, integral with one another, characterised in that the first electrical interface comprises a first outer conductor part which is configured circular or elliptical in cross-section, wherein the first mechanical interface geometry is configured such that the first inner conductor parts are arranged on a circumferential line and that the second electrical interface comprises a second outer conductor part which is configured rectangular or polygonal in cross-section wherein the second interface geometry is configured such that the plug-side ends of the second inner conductor parts are arranged on a line in one plane.
A ventricular assist system, the system comprising: an implantable ventricular assist device comprising an energy storage component and a secondary coil electrically coupled to the energy storage component; and an inductive coupling device for transcutaneously charging the ventricular assist device, the inductive coupling device comprising: a flexible housing defining an internal volume; a resonant circuit comprising a coil disposed within the internal volume of the housing, wherein the coil is deformable; characterized by a plurality of sensors coupled to the coil; and a processor operably coupled to the plurality of sensors, wherein the processor is configured to determine a deformation of the coil based on at least one signal received from at least one of the plurality of sensors. an implantable ventricular assist device comprising an energy storage component and a secondary coil electrically coupled to the energy storage component; and an inductive coupling device for transcutaneously charging the ventricular assist device, the inductive coupling device comprising: a flexible housing defining an internal volume; a resonant circuit comprising a coil disposed within the internal volume of the housing, wherein the coil is deformable; characterized by a plurality of sensors coupled to the coil; and a processor operably coupled to the plurality of sensors, wherein the processor is configured to determine a deformation of the coil based on at least one signal received from at least one of the plurality of sensors. a flexible housing defining an internal volume; a resonant circuit comprising a coil disposed within the internal volume of the housing, wherein the coil is deformable; characterized by a plurality of sensors coupled to the coil; and a processor operably coupled to the plurality of sensors, wherein the processor is configured to determine a deformation of the coil based on at least one signal received from at least one of the plurality of sensors.
A data analytics method, comprising: Obtaining, by a user plane data processing network element, information about at least one feature set from a data analytics network element, wherein information about each feature set in the information about the at least one feature set corresponds to at least one service type or at least one execution rule; Obtaining, by the user plane data processing network element, a feature parameter of user plane data based on the information about the at least one feature set; Sending, by the user plane data processing network element, the feature parameter to the data analytics network element; Obtaining, by the user plane data processing network element, a response result of the feature parameter from the data analytics network element; and Obtaining, by the user plane data processing network element based on the response result, a service type associated with the user plane data or an execution rule associated with the user plane data; wherein the information about the feature set is a set of feature indexes; and the obtaining, by the user plane data processing network element, a feature parameter of the user plane data based on the information about the at least one feature set comprises: determining, by the user plane data processing network element based on a feature index in the set of feature indexes, a feature corresponding to the feature index, and obtaining, by the user plane data processing network element the feature parameter that is of the user plane data and that corresponds to the feature. Obtaining, by a user plane data processing network element, information about at least one feature set from a data analytics network element, wherein information about each feature set in the information about the at least one feature set corresponds to at least one service type or at least one execution rule; Obtaining, by the user plane data processing network element, a feature parameter of user plane data based on the information about the at least one feature set; Sending, by the user plane data processing network element, the feature parameter to the data analytics network element; Obtaining, by the user plane data processing network element, a response result of the feature parameter from the data analytics network element; and Obtaining, by the user plane data processing network element based on the response result, a service type associated with the user plane data or an execution rule associated with the user plane data; wherein the information about the feature set is a set of feature indexes; and the obtaining, by the user plane data processing network element, a feature parameter of the user plane data based on the information about the at least one feature set comprises: determining, by the user plane data processing network element based on a feature index in the set of feature indexes, a feature corresponding to the feature index, and obtaining, by the user plane data processing network element the feature parameter that is of the user plane data and that corresponds to the feature.
Method for registering and monitoring autonomous vehicles having at least one hardware component and/or at least one software component for providing an autonomous driving function, comprising the steps of: a. transmitting a data set to a central device, wherein the data set contains details of the at least one hardware component and/or the at least one software component of the autonomous vehicle, b. the central device receiving the data set and storing the data set together with an identifier assigned to the autonomous vehicle, c. the central device sending a confirmation of the successful storage to the autonomous vehicle, d. the autonomous vehicle receiving and storing the confirmation, e. the autonomous vehicle enabling the autonomous driving function provided by the at least one hardware component and/or at least one software component on the basis of the stored confirmation, f. the autonomous vehicle transmitting the stored unique identifier assigned to the autonomous vehicle, g. receiving the transmitted unique identifier assigned to the autonomous vehicle, h. comparing the data set stored in the central device for this identifier or details decoded from the identifier with information relating to faulty hardware components and/or software components, i. transmitting a signal to the autonomous vehicle to initiate an action if a faulty hardware component and/or software component was determined during the comparison according to step h), j. the autonomous vehicle receiving the signal and performing the required action, characterized in that the transmission of the data set according to step a) is carried out after replacing a hardware component and/or after updating a software component. a. transmitting a data set to a central device, wherein the data set contains details of the at least one hardware component and/or the at least one software component of the autonomous vehicle, b. the central device receiving the data set and storing the data set together with an identifier assigned to the autonomous vehicle, c. the central device sending a confirmation of the successful storage to the autonomous vehicle, d. the autonomous vehicle receiving and storing the confirmation, e. the autonomous vehicle enabling the autonomous driving function provided by the at least one hardware component and/or at least one software component on the basis of the stored confirmation, f. the autonomous vehicle transmitting the stored unique identifier assigned to the autonomous vehicle, g. receiving the transmitted unique identifier assigned to the autonomous vehicle, h. comparing the data set stored in the central device for this identifier or details decoded from the identifier with information relating to faulty hardware components and/or software components, i. transmitting a signal to the autonomous vehicle to initiate an action if a faulty hardware component and/or software component was determined during the comparison according to step h), j. the autonomous vehicle receiving the signal and performing the required action,
Endoscope protection device including a sheath with a rigid cylindrical tubular part and an associated flexible sleeve, characterized in that the rigid cylindrical tubular part is produced in a material able to transport light, in that the rigid cylindrical tubular part is treated to guide light from a light source from its proximal end to its distal end, and in that the distal end of the cylindrical tubular part includes means (14, 16) for scattering and/or orienting light guided by the cylindrical tubular part.
Extractor hood device with edge extraction, comprising at least one gap-shaped intake opening for sucked air, which extends along an edge of a central air-impermeable cover plate, a hood screen having at least one central air-permeable grease filter which closes off an exhaust shaft or funnel, at least a central region of the grease filter and of the hood screen being shielded from a cooking zone by the cover plate during operation and is connected to the gap-shaped intake opening by an air duct, the inner boundary surfaces of which are air-impermeable surfaces of the hood screen and the cover plate, and wherein the inner boundary surfaces are shaped such that the boundary surfaces opposite to the gap-shaped intake opening deflect an air flow entering through the gap-shaped intake opening by at least 45 degrees, wherein deflecting portions of the boundary surfaces opposite to the gap-shaped intake opening form at least partially the boundary surfaces of the air duct, characterized in that the extractor hood device comprises at least one insert part which forms the deflecting parts and can be separated from the rest of the hood screen and the cover plate and reinserted.