mhurhangee/ep-ind-claims huggingface dataset:
A method for obtaining an x-ray image of an object, comprising steps of: providing a first wireless digital radiography receiver panel having unique encoded information for identification; applying a first label onto one or more surfaces of the panel, the first label having an alphanumeric coding element that is readable for identifying the first panel to an operator of the first panel; storing a first association among the first panel, the alphanumeric coding element on the first label and an x-ray imaging room in which the x-ray image is to be obtained; displaying an operator interface comprising a display that displays at least the alphanumeric coding element and further comprises a selector panel that provides a selection utility for designating as an active panel the first panel having the first association; responding to an instruction from the operator by designating the first panel having the first association as the active panel in the room; transmitting wireless instructions to the active panel to capture x-ray image data upon exposure of the object to x-radiation in the room; and obtaining the x-ray image data from the active panel. providing a first wireless digital radiography receiver panel having unique encoded information for identification; applying a first label onto one or more surfaces of the panel, the first label having an alphanumeric coding element that is readable for identifying the first panel to an operator of the first panel; storing a first association among the first panel, the alphanumeric coding element on the first label and an x-ray imaging room in which the x-ray image is to be obtained; displaying an operator interface comprising a display that displays at least the alphanumeric coding element and further comprises a selector panel that provides a selection utility for designating as an active panel the first panel having the first association; responding to an instruction from the operator by designating the first panel having the first association as the active panel in the room; transmitting wireless instructions to the active panel to capture x-ray image data upon exposure of the object to x-radiation in the room; and obtaining the x-ray image data from the active panel.
A communication component comprising: - a far field transceiver for exchanging far field signals with a cellular mobile telecommunication device, the far field transceiver being a WLAN transceiver for exchanging WLAN signals, - an NFC transceiver for exchanging NFC signals and for powering the communication component, the NFC transceiver being operable to exchange the NFC signals (150, 154) with the NFC terminal - converter means (132, 134) for converting a received far field signal to an NFC signal and for converting a received NFC signal to a far field signal, characterised in that, the communication component further comprises a reader into which a security token, such as a SIM card, is inserted, the security token having a storage for storing a symmetric key or an asymmetric cryptographic key pair for authentication and encryption of the communication between the communication component and the cellular mobile telecommunication device and the NFC terminal. - a far field transceiver for exchanging far field signals with a cellular mobile telecommunication device, the far field transceiver being a WLAN transceiver for exchanging WLAN signals, - an NFC transceiver for exchanging NFC signals and for powering the communication component, the NFC transceiver being operable to exchange the NFC signals (150, 154) with the NFC terminal - converter means (132, 134) for converting a received far field signal to an NFC signal and for converting a received NFC signal to a far field signal,
A breathing circuit for use with a first gas set and a second gas set, said circuit comprising means for keeping separate the FGS and SGS, and a means for sequentially delivering to a patient, first the FGS, and, on inspiration, when the patient inspires so as to deplete the supply of FGS in the circuit, substantially the SGS for the balance of inspiration, the circuit comprising: a) an inspiratory limb (32, 59, 220, 500) having a port for entry of FGS (30, 218), a FGS reservoir (37, 215) and a FGS flow control means comprising at least one of a uni-directional valve (31, 219) that opens toward the patient and a FGS controlled valve activated by a FGS valve control means, said FGS valve control being configured to open said FGS controlled valve during inspiration until the inspiratory reservoir (37, 215) has been depleted and then to close it until the end of expiration; and b) an expiratory limb (39, 51, 202, 501) containing an exit port (19, 41, 209) for exhaled gas, an SGS reservoir (18, 36, 207), and SGS flow control means comprising an exhalation valve (33, 203) on the expiratory limb (39, 51, 202, 501) for controlling the flow of SGS towards the SGS reservoir during exhalation, and a bypass valve (35, 206) on a bypass limb (34, 221) connected to the expiratory limb for controlling flow of SGS in the expiratory limb towards the patient during a portion of inspiration, said bypass limb (34, 221) bypassing said exhalation valve(33, 203), whereby said bypass valve (35, 206) is opened during inspiration only once the FGS reservoir (37, 215) has been emptied thus providing to the patient sequential delivery of FGS followed by substantially SGS when the patient's rate of ventilation exceeds the rate of entry of the FGS into the breathing circuit. a) an inspiratory limb (32, 59, 220, 500) having a port for entry of FGS (30, 218), a FGS reservoir (37, 215) and a FGS flow control means comprising at least one of a uni-directional valve (31, 219) that opens toward the patient and a FGS controlled valve activated by a FGS valve control means, said FGS valve control being configured to open said FGS controlled valve during inspiration until the inspiratory reservoir (37, 215) has been depleted and then to close it until the end of expiration; and b) an expiratory limb (39, 51, 202, 501) containing an exit port (19, 41, 209) for exhaled gas, an SGS reservoir (18, 36, 207), and SGS flow control means comprising an exhalation valve (33, 203) on the expiratory limb (39, 51, 202, 501) for controlling the flow of SGS towards the SGS reservoir during exhalation, and a bypass valve (35, 206) on a bypass limb (34, 221) connected to the expiratory limb for controlling flow of SGS in the expiratory limb towards the patient during a portion of inspiration, said bypass limb (34, 221) bypassing said exhalation valve(33, 203), whereby said bypass valve (35, 206) is opened during inspiration only once the FGS reservoir (37, 215) has been emptied thus providing to the patient sequential delivery of FGS followed by substantially SGS when the patient's rate of ventilation exceeds the rate of entry of the FGS into the breathing circuit.
A powered threader device comprising: a frame assembly and a releasable chuck assembly (31, 55) adapted for retaining and rotating a workpiece about a workpiece central axis; characterized by a brushless DC electric motor supported by the frame assembly, the motor providing a powered rotary output in engagement with the chuck assembly (31, 55) to thereby rotate the workpiece; a positionable die assembly for forming threads in the workpiece, the die assembly including a universal die head; a current sensor to measure electrical current to the brushless DC electric motor; control provisions to limit electrical current to the brushless DC electric motor; wherein the brushless DC electric motor is an electronically commutated motor, wherein the control provisions limit electrical current to the brushless DC electric motor based on information from the current sensor, to thereby limit torque of the powered rotary output of the brushless DC electric motor. a frame assembly and a releasable chuck assembly (31, 55) adapted for retaining and rotating a workpiece about a workpiece central axis; characterized by a brushless DC electric motor supported by the frame assembly, the motor providing a powered rotary output in engagement with the chuck assembly (31, 55) to thereby rotate the workpiece; a positionable die assembly for forming threads in the workpiece, the die assembly including a universal die head; a current sensor to measure electrical current to the brushless DC electric motor; control provisions to limit electrical current to the brushless DC electric motor; wherein the brushless DC electric motor is an electronically commutated motor, wherein the control provisions limit electrical current to the brushless DC electric motor based on information from the current sensor, to thereby limit torque of the powered rotary output of the brushless DC electric motor.
An assembly comprising: - an exhaust casing, said casing being of revolution about a turbine engine drive axis (X-X), and comprising a fastening flange to a support, and - a sealing plate of revolution around the axis (X-X), characterized in that the plate is attached on the fastening flange of the exhaust casing, and has a radial section comprising: - a radially internal end part, - a radially external end part, and - an elbow extending between the two end parts, said parts together forming an angle comprised between 80 and 100 degrees, and the radially external end part having a length in an axial direction (L 34) comprised between 15 and 35% of the height of the plate measured in the radial direction around the axis of revolution, and the radially external end part extending substantially parallel to said axis, and in that said elbow is angularly open to downstream in the axial direction relative to the airflow in the turbine engine. - an exhaust casing, said casing being of revolution about a turbine engine drive axis (X-X), and comprising a fastening flange to a support, and - a sealing plate of revolution around the axis (X-X), - a radially internal end part, - a radially external end part, and - an elbow extending between the two end parts,
A fastener (10, 110) for attaching a decking member to a support member, comprising a body (12, 112) extending from a front end to a rear end and including a generally flat portion defining a plane extending between two opposing lateral edges, the body defining an attachment opening (18, 118) extending from a top surface to a bottom surface thereof, a first shoulder extending from one lateral edge and transitioning to a downwardly projecting first leg (14, 114) and an opposite second shoulder extending from the opposing lateral edge to a downwardly projecting second leg (15, 115), characterized by each leg (14, 114, 15, 115) having a front edge that is angled obliquely relative to the plane in the forward direction and having a rear edge with an undercut portion.
A pattern structure comprising: a plurality of pattern structure units arranged on a same plane, wherein each of the plurality of pattern structure units has a first surface and a second surface, which are opposite to each other, and a microstructure is defined on the first surface of each of the plurality of pattern structure units; and a flattening layer disposed on the second surface of each of the plurality of pattern structure units, wherein the flattening layer connects the plurality of pattern structure units with each other, wherein microstructures of the plurality of pattern structure units are located at a same height and, wherein a vertical step difference exists between second surfaces of the plurality of pattern structure units. a plurality of pattern structure units arranged on a same plane, wherein each of the plurality of pattern structure units has a first surface and a second surface, which are opposite to each other, and a microstructure is defined on the first surface of each of the plurality of pattern structure units; and a flattening layer disposed on the second surface of each of the plurality of pattern structure units, wherein the flattening layer connects the plurality of pattern structure units with each other, wherein microstructures of the plurality of pattern structure units are located at a same height and, wherein a vertical step difference exists between second surfaces of the plurality of pattern structure units.
Ceramic component with at least one electrical bushing, comprising a ceramic body, through which a borehole extends, a metal conductor, which is arranged at least in part in the borehole and is secured in the borehole, sealing said borehole by means of an active brazing solder, wherein the metal conductor comprises tantalum, platinum or Kovar, wherein the active brazing solder is a Zr-Ni-Ti alloy, wherein the active brazing solder fills in an annular gap between the metal conductor and the ceramic body, characterized in that the active brazing solder has a chemical composition that is variable radially, in that the concentration of nickel is higher at the boundary to the metal electrical conductor than at the boundary to the ceramic body, and in that the concentration of titanium in the active brazing solder at the boundary to the ceramic body is higher than at the boundary to the metal conductor.
A support assembly for a deep tissue temperature probe comprising a substrate, the substrate being a sheet of flexible, thermally insulative material with two sides; at least three contiguous sections (502,504,506) defined in the sheet, in which each section is joined to at least one adjacent section at a peripheral location common to two adjacent sections; two thermal sensors (508,510), each supported on a respective one of two adjacent sections; a heater (524,534) supported on a third section; and, an identical pattern of slits (542, 513) in each of the sections adapted for aligning with the slits of the other sections when the sections are folded together and open through all of the sections.
A tire tread having at least one tread element, the at least one tread element having a sipe therein, the sipe having a first portion having a first and second opposed side (25, 27), and a third side joining said first and second side (25, 27), and said sipe further including a continuous tubular pathway (i) bordering said first, second and third side (23, 25, 27) or (ii) extending along the third side and at least partially extending along at least one of the first and second side (25, 27), characterized in that the first portion has a section having a three dimensional configuration comprising a series of protrusions and recesses (15a, 15b).
Tank system for an aircraft having a longitudinal direction, said tank system comprising: - a tank intended to contain a liquid, - a drainage line that is housed and fixed in the bottom part of the tank, extends parallel to the longitudinal direction, and has a drainage port at each end, - for each drainage port, a funnel secured to the drainage line, wherein the axis of the funnel is parallel to the longitudinal direction and wherein the top of the funnel opens into the drainage port, wherein the funnel has a wall, through which at least one window passes, - a body mounted to be able to move in translation parallel to the longitudinal direction, - for each funnel, a plug that is secured to the body and arranged to be able to move inside said funnel alternately between an open position in which the plug blocks off neither the windows in the funnel nor the drainage port and a closed position in which the plug blocks off at least the drainage port, and - an arm, a first end of which is mounted in an articulated manner to the tank above the body and a second end of which is mounted in an articulated manner on the body via a connection combining a connection that pivots about an axis perpendicular to the longitudinal direction and horizontal and a connection that slides perpendicular to the longitudinal direction in a plane perpendicular to said axis. - a tank intended to contain a liquid, - a drainage line that is housed and fixed in the bottom part of the tank, extends parallel to the longitudinal direction, and has a drainage port at each end, - for each drainage port, a funnel secured to the drainage line, wherein the axis of the funnel is parallel to the longitudinal direction and wherein the top of the funnel opens into the drainage port, wherein the funnel has a wall, through which at least one window passes, - a body mounted to be able to move in translation parallel to the longitudinal direction, - for each funnel, a plug that is secured to the body and arranged to be able to move inside said funnel alternately between an open position in which the plug blocks off neither the windows in the funnel nor the drainage port and a closed position in which the plug blocks off at least the drainage port, and - an arm, a first end of which is mounted in an articulated manner to the tank above the body and a second end of which is mounted in an articulated manner on the body via a connection combining a connection that pivots about an axis perpendicular to the longitudinal direction and horizontal and a connection that slides perpendicular to the longitudinal direction in a plane perpendicular to said axis.
A scribing wheel (10; 30) comprising: a scribing-wheel base material (11; 31) having a form of a disc with a largest-diameter part and inclined surfaces formed at its periphery, said inclined surfaces forming a vertex in a cutting-edge part of said scribing-wheel base material (11; 31), a diamond film (14; 34) formed on the cutting-edge part of said scribing-wheel base material (11; 31), and a ground region formed by grinding said diamond film by a mechanical grinding technique so as to form a cutting edge, wherein the difference between an angle (α1) of the vertex in the cutting-edge part of said scribing-wheel base material (11; 31) and an angle (α2) of said cutting edge is within a range from 5 to 20 degrees, characterized in that a width of said ground region falls within a range from 10 μm to 30 μm. a scribing-wheel base material (11; 31) having a form of a disc with a largest-diameter part and inclined surfaces formed at its periphery, said inclined surfaces forming a vertex in a cutting-edge part of said scribing-wheel base material (11; 31), a diamond film (14; 34) formed on the cutting-edge part of said scribing-wheel base material (11; 31), and a ground region formed by grinding said diamond film by a mechanical grinding technique so as to form a cutting edge, wherein the difference between an angle (α1) of the vertex in the cutting-edge part of said scribing-wheel base material (11; 31) and an angle (α2) of said cutting edge is within a range from 5 to 20 degrees, characterized in that a width of said ground region falls within a range from 10 μm to 30 μm.
Apparatus for breathing assistance to a subject, comprising: a mask (23,123) adapted to be applied to at least one breathing orifice of said subject; at least one controllable breathing valve connected between said mask and the outside atmosphere to enable spontaneous breathing of said subject; an electro-mechanical controller for controlling the at least one breathing valve; and a sensor for monitoring the subject's breathing cycle, wherein said controller is adapted to control the at least one controllable breathing valve to restrict its flow during a portion of the expiration phase according to information provided by said sensor, characterized in that said portion of the expiration phase excludes the beginning of said expiration phase. a mask (23,123) adapted to be applied to at least one breathing orifice of said subject; at least one controllable breathing valve connected between said mask and the outside atmosphere to enable spontaneous breathing of said subject; an electro-mechanical controller for controlling the at least one breathing valve; and a sensor for monitoring the subject's breathing cycle,
A rotor blade for a turbine of a gas turbine that includes an airfoil, the airfoil having a leading edge, a trailing edge, an outboard tip, and an inboard end that attaches to a root configured to couple the rotor blade to a rotor disc, wherein the airfoil includes a cooling configuration that comprises elongated cooling channels for receiving and directing a coolant through the airfoil, the rotor blade further comprising: a tip shroud connected to the outboard tip of the airfoil; outlet ports defined through an outboard surface of the tip shroud, the outlet ports fluidly communicating with the cooling channels for discharging coolant from the rotor blade; a flow directing structure formed on the outboard surface of the tip shroud, the flow directing structure positioned relative to the outlet ports for affecting the flow of coolant discharged therefrom; and an airfoil profile comprising an outline of the airfoil projected radially on to the outboard surface of the tip shroud; wherein: the flow directing structure comprises a shroud fence; the shroud fence is positioned on the outboard surface so that the shroud fence trails the outlet ports as the rotor blade rotates during operation; characterized in that the shroud fence extends along a path that coincides with a profile of a pressure side of the airfoil. a tip shroud connected to the outboard tip of the airfoil; outlet ports defined through an outboard surface of the tip shroud, the outlet ports fluidly communicating with the cooling channels for discharging coolant from the rotor blade; a flow directing structure formed on the outboard surface of the tip shroud, the flow directing structure positioned relative to the outlet ports for affecting the flow of coolant discharged therefrom; and an airfoil profile comprising an outline of the airfoil projected radially on to the outboard surface of the tip shroud; wherein: the flow directing structure comprises a shroud fence; the shroud fence is positioned on the outboard surface so that the shroud fence trails the outlet ports as the rotor blade rotates during operation; characterized in that the shroud fence extends along a path that coincides with a profile of a pressure side of the airfoil. the flow directing structure comprises a shroud fence; the shroud fence is positioned on the outboard surface so that the shroud fence trails the outlet ports as the rotor blade rotates during operation; characterized in that the shroud fence extends along a path that coincides with a profile of a pressure side of the airfoil.