mhurhangee/ep-ind-claims huggingface dataset:
A superconducting system comprising: a coplanar superconducting circuit comprising: a first ground plane region; a second ground plane region electrically isolated from the first ground plane region by portions of the coplanar superconducting circuit; and a tunable coupler having a first port (P 1) and a second port (P 2), the tunable coupler comprising: a variable inductance coupling element coupled between the first port (P 1) and the second port (P 2); a first termination inductor having a first end coupled to a first end of the variable inductance coupling element, and a second end coupled to the first ground plane region; and a second termination inductor having a first end coupled to a second end of the variable inductance coupling element, and a second end coupled to the second ground plane region. a first ground plane region; a second ground plane region electrically isolated from the first ground plane region by portions of the coplanar superconducting circuit; and a tunable coupler having a first port (P 1) and a second port (P 2), the tunable coupler comprising: a variable inductance coupling element coupled between the first port (P 1) and the second port (P 2); a first termination inductor having a first end coupled to a first end of the variable inductance coupling element, and a second end coupled to the first ground plane region; and a second termination inductor having a first end coupled to a second end of the variable inductance coupling element, and a second end coupled to the second ground plane region. a variable inductance coupling element coupled between the first port (P 1) and the second port (P 2); a first termination inductor having a first end coupled to a first end of the variable inductance coupling element, and a second end coupled to the first ground plane region; and a second termination inductor having a first end coupled to a second end of the variable inductance coupling element, and a second end coupled to the second ground plane region.
An aircraft, comprising: an airframe having a main section, a pylon section and a tail section; a rotor (151, 160), which is disposed at one of the pylon section and the tail section and is rotatable about a rotational axis to provide drive to the airframe; a secondary gearbox, disposed within one of the pylon section and the tail section of the airframe; a primary gearbox, disposed within the main section of the airframe, the primary gearbox comprising an outer housing, rotationally fixed relative to the airframe, and a driveshaft extending through the outer housing, the driveshaft being coupled to the secondary gearbox to thereby drive rotation of the rotor relative to the airframe via the secondary gearbox; and an integral rotor position sensing system, displaced from the pylon and tail sections of the airframe, affixed to the outer housing and the driveshaft and configured to sense rotational characteristics of the driveshaft, characterized in that the driveshaft includes an inner shaft and an outer shaft, and in that the integral rotor position sensing system comprises: a sensor integrally affixed to the outer housing of the primary gearbox, the sensor being rotationally fixed relative to the airframe; and a sensed element, sensed by the sensor, attached to the outer shaft of the driveshaft, wherein the rotational characteristics of the driveshaft are sensed according to signals received from the sensor. an airframe having a main section, a pylon section and a tail section; a rotor (151, 160), which is disposed at one of the pylon section and the tail section and is rotatable about a rotational axis to provide drive to the airframe; a secondary gearbox, disposed within one of the pylon section and the tail section of the airframe; a primary gearbox, disposed within the main section of the airframe, the primary gearbox comprising an outer housing, rotationally fixed relative to the airframe, and a driveshaft extending through the outer housing, the driveshaft being coupled to the secondary gearbox to thereby drive rotation of the rotor relative to the airframe via the secondary gearbox; and an integral rotor position sensing system, displaced from the pylon and tail sections of the airframe, affixed to the outer housing and the driveshaft and configured to sense rotational characteristics of the driveshaft, characterized in that the driveshaft includes an inner shaft and an outer shaft, and in that the integral rotor position sensing system comprises: a sensor integrally affixed to the outer housing of the primary gearbox, the sensor being rotationally fixed relative to the airframe; and a sensed element, sensed by the sensor, attached to the outer shaft of the driveshaft, wherein the rotational characteristics of the driveshaft are sensed according to signals received from the sensor. a sensor integrally affixed to the outer housing of the primary gearbox, the sensor being rotationally fixed relative to the airframe; and a sensed element, sensed by the sensor, attached to the outer shaft of the driveshaft, wherein the rotational characteristics of the driveshaft are sensed according to signals received from the sensor.
Differential protection device for detecting leakage current or fault current in an electrical installation powered by at least one phase conductor (P1, P2, P3) of a network and at least one neutral and/or earth conductor of said network, said device comprising, on the one hand, a transformer with a preferentially toroidal core made of ferromagnetic material, with a primary winding composed of at least two of the aforementioned conductors (P1, P2, P3, N) and with at least one secondary winding across the terminals of which is established a signal induced when a differential fault occurs at the primary winding and, on the other hand, at least one processing and control circuit designed to process the induced signal and, in the event that a predefined threshold value is exceeded, to control an electromagnetic actuator, a relay or an analogue means for disconnecting or opening the device, said processing and control circuit(s) being connected to the terminals of the secondary winding in question, the differential protection device being characterized in that a passive circuit comprising one inductor at least, and at least one resistor and/or at least one capacitor connected in series with said at least one inductor, is connected to the terminals of the secondary winding, in parallel with the latter, the inductor that forms part of the passive circuit being dimensioned in such a way that, for fault current frequencies greater than approximately 20 kHz, the triggering threshold of the circuit is less than or equal to 420 mA. said device comprising, on the one hand, a transformer with a preferentially toroidal core made of ferromagnetic material, with a primary winding composed of at least two of the aforementioned conductors (P1, P2, P3, N) and with at least one secondary winding across the terminals of which is established a signal induced when a differential fault occurs at the primary winding and, on the other hand, at least one processing and control circuit designed to process the induced signal and, in the event that a predefined threshold value is exceeded, to control an electromagnetic actuator, a relay or an analogue means for disconnecting or opening the device, said processing and control circuit(s) being connected to the terminals of the secondary winding in question, the differential protection device being characterized in that a passive circuit comprising one inductor at least, and at least one resistor and/or at least one capacitor connected in series with said at least one inductor, is connected to the terminals of the secondary winding, in parallel with the latter, the inductor that forms part of the passive circuit being dimensioned in such a way that, for fault current frequencies greater than approximately 20 kHz, the triggering threshold of the circuit is less than or equal to 420 mA.
An electromagnetic driven membrane pump for pumping of fluids or gases, comprised of a pump housing inside which at least one, to at least one intake and at least one outlet connected pump chamber is formed and delimited between a gable of the pump housing and at least one to the pump housing's wall attached and completely sealed membrane, that is attached to a, in the pump housing's axial direction running axle, that is suspended in at least two suspensions separated in the axle's longitudinal direction, at least one of the suspensions being comprised of a flat spring attached to the axle, which flat spring runs in a radial direction out towards the pump housing's wall and is attached to this wall, the axle being partly or entirely comprised of, includes or carries a magnetic material to be driven by a magnetic field from an electromagnet in order to oscillate in its longitudinal direction and move the membrane in a corresponding oscillating movement, characterized in that the flat spring is comprised of a ring-shaped inner part and a ring-shaped outer part, the outer part being attached to the pump housing and the inner part to the axle, the inner part being fixed to the outer part by four elastic legs arranged around the point where the flat spring is attached to the axle, half of the legs being mirror-inverted in relation to the other half of the legs; and that another one of said suspensions is comprised of the membrane.
Agitator ball mill having a grinding chamber, a rotatably mounted agitator shaft, which protrudes at least partly into the grinding chamber and on which agitator elements (10, 20, 30) are arranged spaced apart from one another axially inside the grinding chamber, and having an inlet for supplying material to be ground and grinding bodies and an outlet for removal of the ground material, wherein the agitator elements (10, 20, 30) each have at least one conveyor chamber and are constructed in such a way that, during operation, they convey a mixture consisting of material to be ground or dispersed and grinding bodies through their at least one conveyor chamber outwards away from the agitator shaft, characterized in that in the grinding chamber there are arranged return conveyor elements (17, 27, 37; 47; 57) which are joined to the agitator shaft for conjoint rotation therewith and which, during operation, convey the mixture laterally alongside and/or between the agitator elements (10, 20, 30) inwards towards the agitator shaft.
A dental implant device in the form of an interface member having a coupling interface that is complementary to the coupling interface provided on a dental implant anchor, said interface member having an apical end, an occlusal end and a lumen defined therebetween; i) wherein said apical end having an external surface forming portion that provides for interfacing with the dental implant anchor; ii) wherein said occlusal end defines an elevated rim extending from said external surface portion, said elevated rim has a length of at least 0.5 mm and up to a length of 7mm and wherein said interface member is adjustable about said elevated rim to define a flange that supports the margins of a restoration associated thereon and wherein said flange is configured to be parallel to the occlusal plane and wherein said flange has an oval cross-sectional profile; and wherein an internal surface of said lumen features inner grooves. i) wherein said apical end having an external surface forming portion that provides for interfacing with the dental implant anchor; ii) wherein said occlusal end defines an elevated rim extending from said external surface portion, said elevated rim has a length of at least 0.5 mm and up to a length of 7mm and wherein said interface member is adjustable about said elevated rim to define a flange that supports the margins of a restoration associated thereon and wherein said flange is configured to be parallel to the occlusal plane and wherein said flange has an oval cross-sectional profile; and wherein an internal surface of said lumen features inner grooves.
Gas supply cock(1; 101; 201; 301; 401; 501) of the type comprising a body (2;102; 202; 302; 402; 502) of cock (1; 101; 201; 301; 401; 501) in which are provided at least one gas inlet conduit (3; 103; 203; 303) and at least one gas outlet conduit (4, 5; 104,105; 204, 205; 304, 305; 404, 405), and in which a plug is lodged for the purpose of regulating, as a function of its angular position, the flow of the gas coming from said at least one inlet conduit to said at least one outlet conduit, said plug being rotatable between an initial position and a final position, and means (7, 8a, 8b, 9a, 9b, 10a, 10b; 107, 108, 109, 110, 114; 207, 208, 209, 210, 214, 215; 307, 309, 310, 314; 407, 409, 410, 414; 507, 509, 510, 514) for preventing stable positioning of said rotatable plug in correspondence of at least one predefined angular interval, characterized in that said at least one predefined angular interval being distant from said initial and final positions, and said plug being stably displaceable in any angular position between said initial and final positions, except that within said at least one predefined angular interval.
A method for distinguishing between a blood sample and a control solution sample, the method comprising the steps of: (a) introducing a sample having an analyte into an electrochemical cell to initiate a reaction with a reagent in the cell, the electrochemical cell comprising first and second electrodes in a spaced apart relationship; (b) applying a first test potential, with a time interval of between 0.05 seconds and 1.0 second, having a first polarity, between the first and second electrodes, and measuring a current from the electrodes; (c) summing at least two current values measured during the first test potential to generate an interferent index; (d) using the interferent index to distinguish between a blood sample and a control solution sample. (a) introducing a sample having an analyte into an electrochemical cell to initiate a reaction with a reagent in the cell, the electrochemical cell comprising first and second electrodes in a spaced apart relationship; (b) applying a first test potential, with a time interval of between 0.05 seconds and 1.0 second, having a first polarity, between the first and second electrodes, and measuring a current from the electrodes; (c) summing at least two current values measured during the first test potential to generate an interferent index; (d) using the interferent index to distinguish between a blood sample and a control solution sample.
An internal combustion engine including an internal combustion engine main body formed with a combustion chamber, and an ignition device configured to ignite a fuel air mixture in said combustion chamber, said internal combustion engine being configured to execute a repetitive combustion cycle including an ignition of said fuel air mixture by said ignition device and combustion of said fuel air mixture therein, wherein said internal combustion engine comprises: an electromagnetic wave emission device configured to emit an electromagnetic wave to said combustion chamber during a propagation of a flame following said ignition of said fuel air mixture; and a control unit configured to control a frequency of said electromagnetic wave emitted to said combustion chamber from said electromagnetic wave emission device in accordance with an operation condition of said internal combustion engine main body, is characterised in that said control unit has a control map for acquiring a target value of the oscillation frequency as an output value when a load and a rotation speed of said internal combustion engine main body are inputted as input values, and in said control map, said target value of said oscillation frequency is configured to increase as the operation condition moves from a low load and a low rotation speed regions toward a high load and a high rotation speed regions. an electromagnetic wave emission device configured to emit an electromagnetic wave to said combustion chamber during a propagation of a flame following said ignition of said fuel air mixture; and a control unit configured to control a frequency of said electromagnetic wave emitted to said combustion chamber from said electromagnetic wave emission device in accordance with an operation condition of said internal combustion engine main body, is characterised in that said control unit has a control map for acquiring a target value of the oscillation frequency as an output value when a load and a rotation speed of said internal combustion engine main body are inputted as input values, and in said control map, said target value of said oscillation frequency is configured to increase as the operation condition moves from a low load and a low rotation speed regions toward a high load and a high rotation speed regions.
Linking device configured to connect an aircraft engine and a primary structure of an aircraft pylon, comprising: - a support configured to be connected to the primary structure, - a spreader, extending between first and second ends (58.1, 58.2), that has a central part (58.3) connected to the support by a principal link comprising a principal rotation axis, - a first thrust rod comprising a first end (52.1) connected to the first end (58.1) of the spreader by a first secondary link and a second end configured to be connected to the engine, - a second thrust rod comprising a first end (52.1') connected to the second end (58.2) of the spreader by a second secondary link and a second end configured to be connected to the engine, - first and second fittings (74, 74'), secured to the support, comprising upper and lower branches (76, 78), between which the spreader is positioned, characterized in that the linking device generates a deflection of the spreader that is configured to pivot about a deflection rotation axis perpendicular to the principal rotation axis and contained in a plane of symmetry (Ps) passing via the principal rotation axis and in that the linking device comprises at least one system for limiting the deflection of the spreader comprising an extension secured to the spreader and also upper and lower stops (84, 86), secured to the first or second fitting (74, 74'), between which the extension is positioned. - a support configured to be connected to the primary structure, - a spreader, extending between first and second ends (58.1, 58.2), that has a central part (58.3) connected to the support by a principal link comprising a principal rotation axis, - a first thrust rod comprising a first end (52.1) connected to the first end (58.1) of the spreader by a first secondary link and a second end configured to be connected to the engine, - a second thrust rod comprising a first end (52.1') connected to the second end (58.2) of the spreader by a second secondary link and a second end configured to be connected to the engine, - first and second fittings (74, 74'), secured to the support, comprising upper and lower branches (76, 78), between which the spreader is positioned,
A healthcare product package (10;110;210;310;410;510) comprising: (a) a container (2;102;202;302;402;502) for containing a healthcare product, and (b) an information unit (1;101;201;301;401;501) which is located inside the container, characterised in that the information unit comprises a carrier (3;103;203;303;403;503;603;703;803;903) and at least one information article (4,6,8;104,110,112;204,206,208;304;404;423) releasably attached to the carrier, and that the information unit does not include means enclosing the at least one information article. (a) a container (2;102;202;302;402;502) for containing a healthcare product, and (b) an information unit (1;101;201;301;401;501) which is located inside the container,
An infrastructure equipment forming part of a mobile communications network configured to transmit signals to and receive signals from one or more communications devices, the infrastructure equipment comprising a receiver configured to receive signals on the uplink from the one or more communications devices via a wireless access interface of the mobile communications network, a transmitter configured to transmit signals on the downlink to the one or more communications devices via the wireless access interface, and a controller configured to control the receiver to receive the signals and to control the transmitter to transmit the signals, wherein the controller is configured in combination with the receiver and the transmitter to determine whether a duration of reception of signals from one of the communications devices exceeds a predetermined threshold, wherein the predetermined threshold is configured by the infrastructure equipment based on measurements performed by the infrastructure equipment, and if so subsequently to delay transmission of data or control signals to the one of the communications devices for a predetermined re-synchronisation period following the reception of the signals from the one of the communications devices, wherein the length of the predetermined re-synchronisation period is configured by the infrastructure equipment based on measurements performed by the infrastructure equipment. a receiver configured to receive signals on the uplink from the one or more communications devices via a wireless access interface of the mobile communications network, a transmitter configured to transmit signals on the downlink to the one or more communications devices via the wireless access interface, and a controller configured to control the receiver to receive the signals and to control the transmitter to transmit the signals, wherein the controller is configured in combination with the receiver and the transmitter to determine whether a duration of reception of signals from one of the communications devices exceeds a predetermined threshold, wherein the predetermined threshold is configured by the infrastructure equipment based on measurements performed by the infrastructure equipment, and if so subsequently to delay transmission of data or control signals to the one of the communications devices for a predetermined re-synchronisation period following the reception of the signals from the one of the communications devices, wherein the length of the predetermined re-synchronisation period is configured by the infrastructure equipment based on measurements performed by the infrastructure equipment.
Prosthesis for repositioning and fixating acetabulum fractures, comprising: a cup member formed and configured to be fixable into a portion of a fractured acetabular socket (A,C); a hook member formed and configured to be fixable onto an edge of the other portion of the fractured acetabular socket (B,C); the prosthesis being characterized in that the cup member and the hook member are formed and configured to be retractable into one another; and in that the prosthesis comprises a hook retraction member comprising at least one cable arranged and configured for retracting the hook member into the cup member by which the portions of the fractured acetabular socket (A, B, C) are retracted towards one another. a cup member formed and configured to be fixable into a portion of a fractured acetabular socket (A,C); a hook member formed and configured to be fixable onto an edge of the other portion of the fractured acetabular socket (B,C); the prosthesis being characterized in that the cup member and the hook member are formed and configured to be retractable into one another; and in that the prosthesis comprises a hook retraction member comprising at least one cable arranged and configured for retracting the hook member into the cup member by which the portions of the fractured acetabular socket (A, B, C) are retracted towards one another.