mhurhangee/ep-ind-claims huggingface dataset:
Arrangement for operating a hydraulic consumer, comprising a hydraulic control valve having a main slide valve, a pressure compensation valve and an orifice plate, wherein, by means of the main slide valve, a hydraulic volume flow in the direction of hydraulic connections provided for operation of the hydraulic consumer is able to be defined, wherein the pressure compensation valve is controlled on the basis of a pressure difference that drops at the orifice plate when the volume flow passes through, such that said pressure compensation valve adopts an at least partially closing control position when the hydraulic pressure upstream of the orifice plate in the direction of the volume flow is greater than that downstream of the orifice plate, including a restoring spring force of a spring element preloading the pressure compensation valve into a fully open position, wherein a sensor arrangement senses the pressure difference and transmits a pressure difference value derived therefrom to a control unit, characterized in that the control unit, by evaluating the pressure difference value, extrapolates a mismatch of the hydraulic supply on the part of the hydraulic control valve when the pressure difference is smaller than a control value given by the restoring spring force, wherein the main slide valve is closed by the control unit, through actuation of an electric actuating device, irrespective of a hydraulic demand at the hydraulic control valve that results in particular from an input at an operator terminal, until the pressure difference sensed by sensor means is greater than the control value given by the restoring spring force or until said main slide valve adopts a fully closing valve position, wherein the control unit opens the main slide valve for test purposes following a predefined waiting time by actuating the electric actuating device on the basis of a hydraulic demand at the hydraulic control valve that results in particular from an input at an operator terminal.
An isolated anti-vascular endothelial growth factor (VEGF) antibody wherein the antibody comprises six hypervariable regions (HVRs) selected from: (i) an HVR-L1 comprising the amino acid sequence of X 1 X 2 R X 3 SL wherein X 1 is G or A; X 2 is V or I; and X 3 is T or R; (ii) an HVR-L2 comprising the amino acid sequence of DASSLA (SEQ ID NO:6); (iii) an HVR-L3 comprising the amino acid sequence of SYKSPL (SEQ ID NO:7); (iv) an HVR-H1 comprising the amino acid sequence of SISGSWIF (SEQ ID NO:1); (v) an HVR-H2 comprising the amino acid sequence of GAIWPFGGYTH (SEQ ID NO:2); and (vi) an HVR-H3 comprising the amino acid sequence of RWGHSTSPWAMDY (SEQ ID NO:3). (i) an HVR-L1 comprising the amino acid sequence of X 1 X 2 R X 3 SL wherein X 1 is G or A; X 2 is V or I; and X 3 is T or R; (ii) an HVR-L2 comprising the amino acid sequence of DASSLA (SEQ ID NO:6); (iii) an HVR-L3 comprising the amino acid sequence of SYKSPL (SEQ ID NO:7); (iv) an HVR-H1 comprising the amino acid sequence of SISGSWIF (SEQ ID NO:1); (v) an HVR-H2 comprising the amino acid sequence of GAIWPFGGYTH (SEQ ID NO:2); and (vi) an HVR-H3 comprising the amino acid sequence of RWGHSTSPWAMDY (SEQ ID NO:3).
A ram air turbine system, comprising: a main generator; a RAT power generation unit; first circuitry by which the main generator and the RAT power generation unit are connectable to an aircraft bus, the first circuitry comprising a first switch which is controllable such that power is selectively provided to the aircraft bus from one of the main generator and the RAT power generation unit; a storage device; second circuitry by which the storage device is connectable to the aircraft bus, the second circuitry comprising a second switch which is controllable such that power is selectively provided to the aircraft bus from the storage device; and third circuitry by which the RAT power generation unit provides power to the storage device. a main generator; a RAT power generation unit; first circuitry by which the main generator and the RAT power generation unit are connectable to an aircraft bus, the first circuitry comprising a first switch which is controllable such that power is selectively provided to the aircraft bus from one of the main generator and the RAT power generation unit; a storage device; second circuitry by which the storage device is connectable to the aircraft bus, the second circuitry comprising a second switch which is controllable such that power is selectively provided to the aircraft bus from the storage device; and third circuitry by which the RAT power generation unit provides power to the storage device.
A latex glove comprising an outer surface and an inner surface; at least a portion of said outer surface having a surface texture in a latex layer, said surface texture comprising a plurality of geometrically defined indentations indicating sharply defined internal edges, wherein the indentations comprise indentations having re-entrant surfaces and the interior opening is larger than the surface opening of the indentation on the outer surface of the glove.
Shaft feedthrough of a housing, in particular of an intake manifold, of an internal combustion engine in particular of a motor vehicle, with a bearing ring support, which is disposed in a wall of the housing, and with a bearing ring for a shaft, in particular a flap shaft of a flap control, which is inserted coaxially into the bearing ring support, wherein at the bearing ring at least one claw is disposed, which extends obliquely to the axis of the bearing ring beyond its radially outer circumferential side and which clings with its free end oppositely to an insertion direction of the bearing ring to a radially inner circumferential side of the bearing ring support, wherein the at least one claw, possibly the claw ring, is cast integrally in the bearing ring.
Electric power supply system for a vehicle fleet, comprising a first base station that can be attached to a first fleet vehicle, and a second base station that can be attached to a second fleet vehicle, there being spanned between the two base stations (14, 18) a carrier rope that is variable in length and on which an electric power transmission cable is run in loops, of fixed length in each case, by means of holding elements (26-1,...,26-6) that are displaceable along the carrier rope, characterized in that, for the purpose of altering the length of the carrier rope, the first base station comprises a winding drum that can be driven in rotation by means of a motor drive, the electric power supply system further having a control unit and a rotary position transducer, assigned to the winding drum, for acquiring a drum rotation executed by means of the motor drive, the control unit extrapolating, from the number of acquired drum rotations, a current distance between the two base stations (14, 18).
A system for controlling a high-lift device of an aircraft, wherein a high-lift device comprises a leading edge device or a trailing edge device and wherein the system comprises; an interface for placement in a flight deck of an aircraft wherein the interface is configured to receive an input from a flight crew and/or provide feedback to the flight crew and wherein the interface includes: a first edge control device for controlling a position of a high-lift device of the aircraft and operable to: select any of a plurality of control device positions, each one of the plurality of control device positions corresponding to a different flight phase of the aircraft; and engage, in response to a selection of a first control device position, a command mode for actuating the high-lift device in an automated manner based on the flight phase associated with the first control device position; wherein the system further comprises: a flight control computer communicatively coupled to the interface and configured to compute a high-lift device setting for the high-lift device; and an actuation system configured to automatically actuate the high-lift device to the high-lift device setting if the command mode is engaged; characterized in that the interface further includes: a second edge control device operable to select a desired setting for the high-lift device different from the computed high-lift device setting without movement of the first edge control device from the first control device position. a first edge control device for controlling a position of a high-lift device of the aircraft and operable to: select any of a plurality of control device positions, each one of the plurality of control device positions corresponding to a different flight phase of the aircraft; and engage, in response to a selection of a first control device position, a command mode for actuating the high-lift device in an automated manner based on the flight phase associated with the first select any of a plurality of control device positions, each one of the plurality of control device positions corresponding to a different flight phase of the aircraft; and engage, in response to a selection of a first control device position, a command mode for actuating the high-lift device in an automated manner based on the flight phase associated with the first control device position; a flight control computer communicatively coupled to the interface and configured to compute a high-lift device setting for the high-lift device; and an actuation system configured to automatically actuate the high-lift device to the high-lift device setting if the command mode is engaged; characterized in that the interface further includes: a second edge control device operable to select a desired setting for the high-lift device different from the computed high-lift device setting without movement of the first edge control device from the first control device position. a second edge control device operable to select a desired setting for the high-lift device different from the computed high-lift device setting without movement of the first edge control device from the first control device position.
A fluid reservoir configured for releasable engagement with an ultrasonic surgical instrument, the fluid reservoir comprising: a housing including a body, a leading end, and a trailing end enclosing a fluid chamber configured for storing fluid therein; inflow and outflow ports (342, 344) disposed at the leading end of the housing; and a heat exchanger disposed at the trailing end of the housing and external to the instrument when the fluid reservoir is in engagement with the instrument. a housing including a body, a leading end, and a trailing end enclosing a fluid chamber configured for storing fluid therein; inflow and outflow ports (342, 344) disposed at the leading end of the housing; and a heat exchanger disposed at the trailing end of the housing and external to the instrument when the fluid reservoir is in engagement with the instrument.
A method for operating a replication control module, the method comprising: - determining that a handover takes place by which a data session exchanged via a cellular network between a serving application instance and a user equipment is transferred from the serving application instance to a target application instance selected from a plurality of application instances located in a cloud environment, wherein session state data comprise a session state of the data session, wherein the session state data is externalized from the data session and stored on a replica - determining a location of the target application instance in the cloud environment, - determining target replica locations of the replica of the session state data individually on a per session basis for said data session during its runtime while taking into account the location of the target application instance, wherein the replica comprises a master replica and at least one slave replica and the target replica location is determined for the master replica and the at least one slave replica, wherein the master replica is collocated at a first node as close as possible to the serving application instance, and wherein the at least one slave replica is located in at least one second node which is a direct neighbor to the first node - transmitting location information about the determined locations for the replica locations to a data handling module allowing the data handling module to distribute the replica to the determined target replica locations. - determining that a handover takes place by which a data session exchanged via a cellular network between a serving application instance and a user equipment is transferred from the serving application instance to a target application instance selected from a plurality of application instances located in a cloud environment, wherein session state data comprise a session state of the data session, wherein the session state data is externalized from the data session and stored on a replica - determining a location of the target application instance in the cloud environment, - determining target replica locations of the replica of the session state data individually on a per session basis for said data session during its runtime while taking into account the location of the target application instance, wherein the replica comprises a master replica and at least one slave replica and the target replica location is determined for the master replica and the at least one slave replica, wherein the master replica is collocated at a first node as close as possible to the serving application instance, and wherein the at least one slave replica is located in at least one second node which is a direct neighbor to the first node - transmitting location information about the determined locations for the replica locations to a data handling module allowing the data handling module to distribute the replica to the determined target replica locations.
A PET data processing method for interpolating positron emission tomography data for reconstructing a PET image, comprising: acquiring PET event data, which was obtained by scanning an object using a PET scanner; generating a raw sinogram from the acquired PET event data; determining a plurality of triangles connecting a plurality of sampling points within the raw sinogram, wherein: the plurality of sampling points are arranged in rows based on an arrangement of a plurality of scintillation crystals in the PET scanner; and determining the plurality of triangles comprises connecting adjacent sampling points to construct triangles horizontally between a first row and a second row such that each consecutive triangle formed between the first row and the second row has an opposite orientation; and determining a uniformly sampled sinogram from the raw sinogram using the determined plurality of triangles. acquiring PET event data, which was obtained by scanning an object using a PET scanner; generating a raw sinogram from the acquired PET event data; determining a plurality of triangles connecting a plurality of sampling points within the raw sinogram, wherein: the plurality of sampling points are arranged in rows based on an arrangement of a plurality of scintillation crystals in the PET scanner; and determining the plurality of triangles comprises connecting adjacent sampling points to construct triangles horizontally between a first row and a second row such that each consecutive triangle formed between the first row and the second row has an opposite orientation; and the plurality of sampling points are arranged in rows based on an arrangement of a plurality of scintillation crystals in the PET scanner; and determining the plurality of triangles comprises connecting adjacent sampling points to construct triangles horizontally between a first row and a second row such that each consecutive triangle formed between the first row and the second row has an opposite orientation; and determining a uniformly sampled sinogram from the raw sinogram using the determined plurality of triangles.
A method of detecting leakage in a compressed air system having a compressor, the method comprising: configuring an electrical monitor to measure one or more electrical parameters indicative of operation of the compressor; identifying periods of time during which the compressed air system is not in use; analyzing running times and intervals of the compressor between compressor operations during one or more of identified periods of time to establish a baseline for constant air leakage, the baseline being derived from a regular pattern of brief air compressor operations; continuing to analyze running times and intervals of the compressor between compressor operations when the compressor is not in use; and notifying one or more users when running times and intervals between compressor operations vary from the baseline, wherein analyzing the running times and intervals of the compressor between compressor operations includes monitoring the lengths of the periods of running times and the lengths of intervals of non-operation of the compressor. configuring an electrical monitor to measure one or more electrical parameters indicative of operation of the compressor; identifying periods of time during which the compressed air system is not in use; analyzing running times and intervals of the compressor between compressor operations during one or more of identified periods of time to establish a baseline for constant air leakage, the baseline being derived from a regular pattern of brief air compressor operations; continuing to analyze running times and intervals of the compressor between compressor operations when the compressor is not in use; and notifying one or more users when running times and intervals between compressor operations vary from the baseline, wherein analyzing the running times and intervals of the compressor between compressor operations includes monitoring the lengths of the periods of running times and the lengths of intervals of non-operation of the compressor.
A hose extrusion head for producing a hose, with (a) a head housing, (b) a duct, which is formed in the head housing, for supplying a hose material, (c) a pin, which is arranged in the duct, (d) a die and (e) at least one securing element, by means of which the die is attached to the head housing, (f) wherein the die is movable for centring relative to the pin and (g) the securing element is attached by one end to the die so that the end follows a movement of the die, characterized in that (h) the securing element is formed by a device which comprises pre-tensioned tension wire cables and which only transfers tensile forces. (a) a head housing, (b) a duct, which is formed in the head housing, for supplying a hose material, (c) a pin, which is arranged in the duct, (d) a die and (e) at least one securing element, by means of which the die is attached to the head housing, (f) wherein the die is movable for centring relative to the pin and (g) the securing element is attached by one end to the die so that the end follows a movement of the die, characterized in that (h) the securing element is formed by a device which comprises pre-tensioned tension wire cables and which only transfers tensile forces.
A method for producing multilayer solid wood panels comprising the following steps of: - barking wood logs; - first slashing the barked wood logs to form bolts; - steaming said bolts; - rotary cutting the bolts after steaming, to form solid wood veneers having a thickness of between 1mm and 10mm; - pre-cutting wood fibres, in said solid wood veneers, into portions on which said wood fibres are stretched; - continuously drying the solid wood veneers; - manually or automatically sorting the solid wood veneers depending on at least one visual quality criterion, to form a first grade of veneers for making up outer layers of the multilayer solid wood panels and a second grade of veneers for making up inner layers of the multilayer solid wood panels; - performing assemblies of solid wood veneers by: i) glue-spreading of the veneer faces to be assembled; ii) composing veneer assemblies comprising a plurality of solid wood veneers disposed against one another, with respective glue-spread faces facing each other, so as to be bonded, each veneer assembly comprising a first grade of veneer for each external layer and, if necessary, one or more second grade veneers as internal layers; iii) pressing the veneer assemblies to form multilayer solid wood panels. - barking wood logs; - first slashing the barked wood logs to form bolts; - steaming said bolts; - rotary cutting the bolts after steaming, to form solid wood veneers having a thickness of between 1mm and 10mm; - pre-cutting wood fibres, in said solid wood veneers, into portions on which said wood fibres are stretched; - continuously drying the solid wood veneers; - manually or automatically sorting the solid wood veneers depending on at least one visual quality criterion, to form a first grade of veneers for making up outer layers of the multilayer solid wood panels and a second grade of veneers for making up inner layers of the multilayer solid wood panels; - performing assemblies of solid wood veneers by: i) glue-spreading of the veneer faces to be assembled; ii) composing veneer assemblies comprising a plurality of solid wood veneers disposed against one another, with respective glue-spread faces facing each other, so as to be bonded, each veneer assembly comprising a first grade of veneer for each external layer and, if necessary, one or more second grade veneers as internal layers; iii) pressing the veneer assemblies to form multilayer solid wood panels. i) glue-spreading of the veneer faces to be assembled; ii) composing veneer assemblies comprising a plurality of solid wood veneers disposed against one another, with respective glue-spread faces facing each other, so as to be bonded, each veneer assembly comprising a first grade of veneer for each external layer and, if necessary, one or more second grade veneers as internal layers; iii) pressing the veneer assemblies to form multilayer solid wood panels.
A structure for sealing a cylinder block and a cylinder head, wherein a cylindrical part protrudes from an upper surface of the cylinder block including a cylinder bore so as to enclose the cylinder bore, and a circular recess having an inner diameter greater than an outer diameter of the cylindrical part is formed on a lower surface of the cylinder head that faces the upper surface of the cylinder block, by mounting the cylinder head on the upper surface of the cylinder block, the cylindrical part is accommodated in the circular recess, and a gasket including an annular rubber elastic member is installed in a space formed between the outer side of the cylindrical part and the inner side of the circular recess, and the gasket is compressed in a radial direction between an outer peripheral surface of the cylindrical part and an inner peripheral surface of the circular recess, and seals the periphery of the cylinder bore between the cylinder block and the cylinder head, characterized in that an upper end surface of the cylindrical part contacts an inner bottom surface of the circular recess.