mhurhangee/ep-ind-claims huggingface dataset:
A prefabricated surrounding frame for a building opening, having an inner face and an outer face, in particular a window frame, comprising a) a circumferential frame body with in each case when used generically, a first lateral boundary element and an opposite second lateral boundary element, an upper boundary element and an opposite lower boundary element, b) a first reveal with a reveal surface and an opposite rear reveal surface and/or a second reveal with a reveal surface and an opposite rear reveal surface and/or a lintel with a lintel surface, c) a sloped wedge or sill receiving unit, each containing a front face, a rear face and a top face, wherein, when the sloped wedge or sill receiving unit is used generically, the top face has or forms a run-off surface that is inclined downwardly in the direction from the rear face to the front face, d) at least one watertight layer, in particular foil, on the upper face of the sloped wedge or sill receiving unit, e) a circumferential collar element made from a plurality of structural units, wherein the structural units rest against the outwardly facing edges of the boundary elements (2, 4, 6, 8) of the circumferential frame body by means of installation stops, and f) a support area for a profile frame, in particular a structurally load-bearing support strip, in particular adapted and arranged to support a door or a window. a) a circumferential frame body with in each case when used generically, a first lateral boundary element and an opposite second lateral boundary element, an upper boundary element and an opposite lower boundary element, b) a first reveal with a reveal surface and an opposite rear reveal surface and/or a second reveal with a reveal surface and an opposite rear reveal surface and/or a lintel with a lintel surface, c) a sloped wedge or sill receiving unit, each containing a front face, a rear face and a top face, wherein, when the sloped wedge or sill receiving unit is used generically, the top face has or forms a run-off surface that is inclined downwardly in the direction from the rear face to the front face, d) at least one watertight layer, in particular foil, on the upper face of the sloped wedge or sill receiving unit, e) a circumferential collar element made from a plurality of structural units, wherein the structural units rest against the outwardly facing edges of the boundary elements (2, 4, 6, 8) of the circumferential frame body by means of installation stops, and f) a support area for a profile frame, in particular a structurally load-bearing support strip, in particular adapted and arranged to support a door or a window.
Syringe for obtaining a target volume of blood, the syringe comprising: a barrel, wherein a plunger is arranged within the barrel to be displaceable along a displacement direction, wherein the plunger comprises a filter, wherein the barrel and the plunger together provide for a first stop and a second stop, wherein the first stop is configured for positioning the filter at a predetermined location along the displacement direction thereby defining a target volume of blood and a buffer volume of blood, and wherein the second stop is configured to stop the plunger from expelling more than the buffer volume for obtaining the target volume of blood when the plunger is pushed towards a distal end of the syringe along the displacement direction, wherein the barrel comprises a proximal end at which a first opening for introducing the plunger into the barrel is located, wherein at the distal end of the barrel a second opening for receiving the target volume of blood is located, and wherein the second stop is located closer to the first opening than the first stop, wherein the filter is configured to be gas-permeable when the filter is not in contact with blood, and wherein the filter is configured to become gas-impermeable when getting in contact with blood, wherein the plunger is fluid-sealing when the filter is gas-impermeable, and wherein the plunger is configured for guiding air out of the barrel and through the filter towards outside the syringe during a self-filling process of the syringe. a barrel, wherein a plunger is arranged within the barrel to be displaceable along a displacement direction, wherein the plunger comprises a filter, wherein the barrel and the plunger together provide for a first stop and a second stop, wherein the first stop is configured for positioning the filter at a predetermined location along the displacement direction thereby defining a target volume of blood and a buffer volume of blood, and wherein the second stop is configured to stop the plunger from expelling more than the buffer volume for obtaining the target volume of blood when the plunger is pushed towards a distal end of the syringe along the displacement direction, wherein the barrel comprises a proximal end at which a first opening for introducing the plunger into the barrel is located, wherein at the distal end of the barrel a second opening for receiving the target volume of blood is located, and wherein the second stop is located closer to the first opening than the first stop, wherein the filter is configured to be gas-permeable when the filter is not in contact with blood, and wherein the filter is configured to become gas-impermeable when getting in contact with blood, wherein the plunger is fluid-sealing when the filter is gas-impermeable, and wherein the plunger is configured for guiding air out of the barrel and through the filter towards outside the syringe during a self-filling process of the syringe.
A method of manufacturing an arthroplasty jig, the method comprising: generating two-dimensional images of at least a portion of a bone (18, 20) forming a joint using an imaging machine, receiving said two-dimensional images extending an open-loop contour line along an arthroplasty target region in at least some of the two-dimensional images; generating a three-dimensional computer model of the arthroplasty target region from the open-loop contour lines; generating from the three-dimensional computer model surface contour data pertaining to the arthroplasty target area; comparing dimensions of the at least a portion of the bone to candidate jig blanks; selecting from the candidate jig blanks a jig blank (50A, 50B) with the smallest dimensions that are able to accommodate the dimensions of the at least a portion of the bone; providing the selected jig blank to a manufacturing machine and using the surface contour data at the manufacturing machine to manufacture the arthroplasty jig.
A needle guard for protecting a human or animal from accidental contact with a needle connected to said needle guard, comprising: a mounting base for the needle; a hinge structure connecting the mounting base to a needle shield, the hinge structure being adapted to pivot the needle shield relative to the mounting base from an open position in which the needle shield is separated from the needle, to a closed position in which the needle shield encloses the needle; and a needle shield hinge adjacent to the hinge structure and needle shield, the needle shield hinge being adapted to pivot the needle shield relative to the hinge structure, characterized in that the hinge structure comprises: a spring member connected to the mounting base; and a spring plate connected to the spring member for cooperating with the needle shield during use with the needle. a mounting base for the needle; a hinge structure connecting the mounting base to a needle shield, the hinge structure being adapted to pivot the needle shield relative to the mounting base from an open position in which the needle shield is separated from the needle, to a closed position in which the needle shield encloses the needle; and a needle shield hinge adjacent to the hinge structure and needle shield, the needle shield hinge being adapted to pivot the needle shield relative to the hinge structure, characterized in that the hinge structure comprises: a spring member connected to the mounting base; and a spring plate connected to the spring member for cooperating with the needle shield during use with the needle.
Jet regulator having a jet-splitting device which divides the incoming water flow into a multiplicity of individual jets, of which at least one individual jet impinges on a nodal point of mutually crossing grid bars (4, 5) of a downstream grid network, wherein the jet regulator is an aerated jet regulator with a jet regulator housing which has at least one aeration opening on the housing periphery thereof, characterised in that the jet regulator housing has, on the housing inner periphery thereof in the flow direction below the at least one aeration opening, at least one deflection projection to keep the water jet away from the aeration opening.
A turbine engine stator assembly circumferentially spaced apart about a turbine engine rotary blading assembly across a gap having a first radial gap length prior to turbine engine operation, the stator assembly comprising a circumferential shroud having a shroud inner surface defining a first radial boundary of the gap, and the rotary blading assembly comprising blading members having a blading member outer surface defining a second radial boundary of the gap, wherein: the circumferential shroud is movable radially; the stator assembly includes at least one gap control member comprising a plurality of discrete shape memory alloy portions (38, 40, 42/44, 46) in combination with fluid flow means to deliver fluid at pre-selected temperatures to the SMA of the gap control member the plurality of discrete SMA portions (38,40,42/44,46) comprising at least two different SMA; each SMA of the gap control member being selected and preconditioned to deform pre-selected amounts during engine operation, responsive to temperature of the fluid, to move the circumferential shroud and the shroud inner surface radially in relation to the blading member outer surface to change the first radial gap length pre-selected amounts during engine operation. the circumferential shroud is movable radially; each SMA of the gap control member being selected and preconditioned to deform pre-selected amounts during engine operation, responsive to temperature of the fluid, to move the circumferential shroud and the shroud inner surface radially in relation to the blading member outer surface to change the first radial gap length pre-selected amounts during engine operation.
Thumb orthosis comprising a spreading body which serves for spreading a thumb and a pointer finger, characterized by a first holding device by which a first end portion of the spreading body can be held at the thumb and a second holding device by which a second end portion of the spreading body can be held at the pointer finger, the thumb orthosis being exclusively held by the two holding devices (22, 23) at the hand of the user wearing the thumb orthosis.
A method for operating an aircraft having two or more engines (102, 104), the method comprising: operating the two or more engines (102, 104) of the aircraft in an asymmetric operating regime, wherein a first of the engines (102, 104) is in an active mode to provide motive power to the aircraft and a second of the engines (102, 104) is in a standby mode to provide substantially no motive power to the aircraft; and governing the first engine (102, 104) in the active mode using a first governing logic, characterised in that the method further comprises: governing the second engine (102, 104) in the standby mode using a second governing logic different from the first governing logic, the second governing logic based on a trimmed target compressor speed and trimmed variable geometry mechanism settings, the trimmed target compressor speed including a nominal target compressor speed adjusted using a first engine-specific trim value, the trimmed VGM settings including nominal VGM settings adjusted using a second engine-specific trim value, and the first engine-specific trim value and the second engine-specific trim value being specific to the second engine (102, 104) and dependent on at least one parameter of the second engine (102, 104) in the standby mode, the at least one parameter comprising fuel consumption. operating the two or more engines (102, 104) of the aircraft in an asymmetric operating regime, wherein a first of the engines (102, 104) is in an active mode to provide motive power to the aircraft and a second of the engines (102, 104) is in a standby mode to provide substantially no motive power to the aircraft; and governing the first engine (102, 104) in the active mode using a first governing logic,
An interspinous process spacer, comprising: a main body including a first securing member extending from a top portion of the main body that engages a first vertebra and a bottom portion of the main body that engages a second vertebra; a first wing pivotably coupled to a distal portion of the main body and including a second securing member extending parallel to the first securing member to form a clamp section in a first position and non-parallel to the first securing member in a second position for securing around a spinous process on the first vertebra; and a screw positionable within the main body and including a distal end that positions the first wing between the first position wherein the clamp section includes a first diameter, and the second position wherein the clamp section includes a second diameter, wherein the screw advances towards the distal portion to position the first wing from the first position to the second position, characterized in that the distal end of the screw includes a curved portion that engages a curved section of the first wing and a proximal end of the screw includes a threaded portion that engages a threaded bore in the main body. a main body including a first securing member extending from a top portion of the main body that engages a first vertebra and a bottom portion of the main body that engages a second vertebra; a first wing pivotably coupled to a distal portion of the main body and including a second securing member extending parallel to the first securing member to form a clamp section in a first position and non-parallel to the first securing member in a second position for securing around a spinous process on the first vertebra; and a screw positionable within the main body and including a distal end that positions the first wing between the first position wherein the clamp section includes a first diameter, and the second position wherein the clamp section includes a second diameter, wherein the screw advances towards the distal portion to position the first wing from the first position to the second position, characterized in that the distal end of the screw includes a curved portion that engages a curved section of the first wing and a proximal end of the screw includes a threaded portion that engages a threaded bore in the main body.
An oligonucleotide which targets a Transcription factor E3 natural antisense transcript for use as a therapeutic compound, wherein the oligonucleotide increases the expression of Transcription factor E3 and/or Insulin Receptor Substrate 2, and wherein the natural antisense transcript has the nucleic acid sequence as set forth in SEQ ID NO:3, or a variant thereof which retains the function of the natural antisense transcript of SEQ ID NO: 3.
A method for operating a radar device that implements built-in self-test (BIST), the radar device (200, 300) having a transmitter (105, 110, 115) and a receiver (120, 125), the method comprising: generating a noise signal; mixing the noise signal with a transmitter output radio frequency, RF, signal to produce an intermediate signal, wherein the transmitter output RF signal is a version of a local oscillator, LO, signal having linearly increasing frequency; attenuating the intermediate signal to produce a test signal; adding the test signal to a receiver input RF signal to produce a combined receiver input RF signal; downmixing an amplified version of the combined receiver input RF signal with the LO signal to produce a combined low frequency signal; and correlating the combined low frequency signal with the noise signal to produce an error detection signal. generating a noise signal; mixing the noise signal with a transmitter output radio frequency, RF, signal to produce an intermediate signal, wherein the transmitter output RF signal is a version of a local oscillator, LO, signal having linearly increasing frequency; attenuating the intermediate signal to produce a test signal; adding the test signal to a receiver input RF signal to produce a combined receiver input RF signal; downmixing an amplified version of the combined receiver input RF signal with the LO signal to produce a combined low frequency signal; and correlating the combined low frequency signal with the noise signal to produce an error detection signal.
Storage tank for receiving a medium capable of freezing, in particular a reducing agent, having at least one aeration/ventilation line (38, 36; 72) and a cup-shaped container introduced into the storage tank, characterized in that an air space in the cup-shaped container is connected via a ventilation line to an air chamber of the storage tank, which is aerated and ventilated via the at least one aeration/ventilation line (38, 36; 72), wherein the ventilation line extends from a first connection above the air space in the cup-shaped container to a second connection, wherein the second connection is connected to the air space of the storage tank, and in that the first connection is arranged on a lid of the cup-shaped container and the second connection is arranged on a tank lid of the storage tank.
Flipper for container spreaders, totally or partially constructed with elastic materials, wherein the flipper comprises three portions screwed to each other, namely a portion that couples to the spreader, a sheet acting as a centring element, and a central area comprising a spring plate, characterized in that the spring plate is made of two or more elastomeric material sheets of the type of synthetic rubber.
A connector for a generator of an active implantable medical device, comprising a substantially cylindrical cavity intended to receive a multipolar lead of the device, the cavity including a stack of annular electrical contact elements alternately separated by annular elements (220; 320) of isolation of the electrical contact elements, wherein: - the isolation elements (220; 320) comprise an annular rigid sleeve and an annular flexible gasket (222; 322) arranged, in an internal region of the sleeve, against an inner annular face of the sleeve; - the sleeve and the gasket comprise respective means (2212, 2213, 2222, 2223) for immobilizing the gasket with respect to the sleeve in the axial direction, by means of conjugated profiles defined on an inner annular face of the sleeve and an outer annular face of the gasket, respectively; and characterized in that: - the gasket extends axially from a lateral face of the sleeve to the other in said internal region of the sleeve; and - each of the lateral faces (2225, 2226) of the flexible gasket protrudes with respect to the corresponding lateral face of the sleeve. - the isolation elements (220; 320) comprise an annular rigid sleeve and an annular flexible gasket (222; 322) arranged, in an internal region of the sleeve, against an inner annular face of the sleeve; - the sleeve and the gasket comprise respective means (2212, 2213, 2222, 2223) for immobilizing the gasket with respect to the sleeve in the axial direction, by means of conjugated profiles defined on an inner annular face of the sleeve and an outer annular face of the gasket, respectively; and characterized in that: - the gasket extends axially from a lateral face of the sleeve to the other in said internal region of the sleeve; and - each of the lateral faces (2225, 2226) of the flexible gasket protrudes with respect to the corresponding lateral face of the sleeve.
A chlorine-containing polymer composition comprising: - a chlorine-containing polymer; and - a wax comprising - a fraction consisting of oxidized hydrocarbons; and - a fraction consisting of non-oxidized hydrocarbons, wherein both fractions have - an average number of carbon atoms (number average) per molecule between 40 to 100 carbon atoms; and - an amount of molecules in which the carbon chain is linear of more than 75 wt.-%. - a chlorine-containing polymer; and - a wax comprising - a fraction consisting of oxidized hydrocarbons; and - a fraction consisting of non-oxidized hydrocarbons, wherein both fractions have - an average number of carbon atoms (number average) per molecule between 40 to 100 carbon atoms; and - an amount of molecules in which the carbon chain is linear of more than 75 wt.-%. - a fraction consisting of oxidized hydrocarbons; and - a fraction consisting of non-oxidized hydrocarbons, wherein both fractions have - an average number of carbon atoms (number average) per molecule between 40 to 100 carbon atoms; and - an amount of molecules in which the carbon chain is linear of more than 75 wt.-%. - an average number of carbon atoms (number average) per molecule between 40 to 100 carbon atoms; and - an amount of molecules in which the carbon chain is linear of more than 75 wt.-%.
An aerospace engine lubricating fluid level annunciation system comprising: a first fluid level sensor (202; 214A) for a first engine (100; 212A), the first fluid level sensor (202; 214A) having a critical level of reliability where deterministic tests and analyses can ensure correct functional performance under all foreseeable operating conditions with no anomalous behaviour; a first low-level detector (204; 216A) coupled to the first fluid level sensor (202; 214A), the first low-level detector (204; 216A) having the critical level of reliability; a first low-level indicator coupled to the first low-level detector (204; 216A) for annunciating a fluid level of the first engine (100; 212A) below a minimum operating level, the first low-level indicator having the critical level of reliability; and an annunciation and display system coupled to the first low-level detector (204; 216A) and configured for performing lubricant-related functions other than annunciating the fluid level of the first engine (100; 212A) below the minimum operating level, the annunciation and display system having a non-critical level of reliability. a first fluid level sensor (202; 214A) for a first engine (100; 212A), the first fluid level sensor (202; 214A) having a critical level of reliability where deterministic tests and analyses can ensure correct functional performance under all foreseeable operating conditions with no anomalous behaviour; a first low-level detector (204; 216A) coupled to the first fluid level sensor (202; 214A), the first low-level detector (204; 216A) having the critical level of reliability; a first low-level indicator coupled to the first low-level detector (204; 216A) for annunciating a fluid level of the first engine (100; 212A) below a minimum operating level, the first low-level indicator having the critical level of reliability; and an annunciation and display system coupled to the first low-level detector (204; 216A) and configured for performing lubricant-related functions other than annunciating the fluid level of the first engine (100; 212A) below the minimum operating level, the annunciation and display system having a non-critical level of reliability.