mhurhangee/ep-ind-claims huggingface dataset:
A non-electrolytic apparatus for treating an aqueous sample stream including analyte ions and matrix ions of opposite charge, said apparatus comprising first and second charged ion exchange membrane sheets(14,16) capable of passing only ions of opposite charge to said analyte ions, a sample stream flow channel defined by said membrane sheets, a first and second aqueous stream ion receiving flow channels(20,22) adjacent opposed sides of said sample stream flow channel and separated therefrom by said first and second ion exchange membrane sheets(14, 16), respectively, a stationary flow-through first packing of ion exchange material disposed in said sample stream flow channel of said same charge as said first and second membrane sheets and having a first ion exchange capacity for said matrix ions, a second flow-through packing(24,26) of ion exchange material disposed in said first and second ion receiving flow channels, wherein said second packing is of opposite charge to said first packing, wherein said first and second ion receiving channels have an ion exchange capacity for said matrix ions less than about 25% of said first ion exchange capacity of said sample channel for said matrix ions, and wherein said apparatus does not include electrodes disposed to apply an electric field between said sample stream flow channel and said first ion receiving flow channel.
An electrosurgical apparatus comprising: an electrosurgical instrument (106, 112, 118) for delivering RF energy and/or microwave frequency energy into biological tissue; and an interface cable for conveying radiofrequency and/or microwave frequency energy between an electrosurgical generator and the electrosurgical instrument (106, 112, 118), wherein there is an electrical connection between the interface cable and the electrosurgical instrument (106, 112, 118); wherein the electrosurgical instrument (106, 112, 118) comprises a connection interface that is cooperable with a terminal connector of the interface cable, and the electrosurgical apparatus further comprises an electrically insulating tubular body secured around the circumference of the terminal connector of the interface cable, the tubular body having a passage therethrough which is open at a first end to expose an end of the terminal connector and through which the interface cable extends, characterised in that: the electrosurgical instrument further comprises a sterile barrier sheath surrounding the connection interface, the sterile barrier sheath being extendable over a portion of the interface cable to surround a connection between the connection interface and terminal connector. an electrosurgical instrument (106, 112, 118) for delivering RF energy and/or microwave frequency energy into biological tissue; and an interface cable for conveying radiofrequency and/or microwave frequency energy between an electrosurgical generator and the electrosurgical instrument (106, 112, 118), wherein there is an electrical connection between the interface cable and the electrosurgical instrument (106, 112, 118); wherein the electrosurgical instrument (106, 112, 118) comprises a connection interface that is cooperable with a terminal connector of the interface cable, and the electrosurgical apparatus further comprises an electrically insulating tubular body secured around the circumference of the terminal connector of the interface cable, the tubular body having a passage therethrough which is open at a first end to expose an end of the terminal connector and through which the interface cable extends,
A treatment system, comprising: a tension relief layer comprising a central elastic region and a pair of opposing wings, the central elastic region being coupled between the pair of opposing wings, wherein at least a portion of each of the opposing wings have adhesive lower surfaces, and wherein the opposing wings can be stretched away from one another towards a first tensile configuration and when held in the first tensile configuration can be adhered to skin on opposing sides of an incision or wound; a skin interface for positioning in direct contact with the incision or wound, wherein the skin interface has a porous portion; a first spacer element positioned immediately above an upper surface of the skin interface such that the first spacer element is sandwiched between the skin interface and a lower surface of the central elastic region; an indicator layer comprising opposing pull tabs respectively coupled to at least a portion of an upper surface of the opposing wings, the opposing pull tabs each having elongate extension portions that mate in an interlocked arrangement which aids to prevent the opposing wings from being stretched beyond a maximum distance; a porous region within the central elastic region that allows for the passage of material from the incision or wound to an upper surface of the tension relief layer; and a conformable sealing layer for application over the tension relief layer and adhered forming a sealed space around at least a portion of the incision or wound. a tension relief layer comprising a central elastic region and a pair of opposing wings, the central elastic region being coupled between the pair of opposing wings, wherein at least a portion of each of the opposing wings have adhesive lower surfaces, and wherein the opposing wings can be stretched away from one another towards a first tensile configuration and when held in the first tensile configuration can be adhered to skin on opposing sides of an incision or wound; a skin interface for positioning in direct contact with the incision or wound, wherein the skin interface has a porous portion; a first spacer element positioned immediately above an upper surface of the skin interface such that the first spacer element is sandwiched between the skin interface and a lower surface of the central elastic region; an indicator layer comprising opposing pull tabs respectively coupled to at least a portion of an upper surface of the opposing wings, the opposing pull tabs each having elongate extension portions that mate in an interlocked arrangement which aids to prevent the opposing wings from being stretched beyond a maximum distance; a porous region within the central elastic region that allows for the passage of material from the incision or wound to an upper surface of the tension relief layer; and a conformable sealing layer for application over the tension relief layer and adhered forming a sealed space around at least a portion of the incision or wound.
A kit for carrying out an infiltration of dental enamel, with the constituents: a) a conditioner for etching enamel lesions which comprises a1) 4 to 80% by weight of at least one acid which has a pKa of 2 or less; a2) a protic solvent; wherein the acid having a saturation vapor pressure at 20° C of 120 mbar or less, for use as conditioning agent for etching enamel lesions; b) an infiltrant. a) a conditioner for etching enamel lesions which comprises a1) 4 to 80% by weight of at least one acid which has a pKa of 2 or less; a2) a protic solvent; wherein the acid having a saturation vapor pressure at 20° C of 120 mbar or less, for use as conditioning agent for etching enamel lesions; a1) 4 to 80% by weight of at least one acid which has a pKa of 2 or less; a2) a protic solvent; wherein the acid having a saturation vapor pressure at 20° C of 120 mbar or less, for use as conditioning agent for etching enamel lesions; b) an infiltrant.
A plasma microreactor comprising: - a support, made at least partially of a dielectric material, the support comprising a gas inlet, adapted to be connected to a gas reservoir, a liquid inlet, adapted to be connected to a liquid reservoir and at least a fluid outlet adapted to be connected to a receiver containing gas and/or liquid, - a liquid microchannel in the support adapted to allow a liquid flow from the liquid inlet to the fluid outlet, - a gas channel, in the support adapted to allow a gas flow from the gas inlet to the fluid outlet, - at least a ground electrode, - at least a high voltage electrode, separated from the gas channel by the dielectric material of the support, wherein said ground electrode and said high voltage electrode are arranged on opposite sides of the gas channel so as to be able to create an electric field inside the gas channel, wherein the liquid microchannel and the gas channel are contiguous and at least an opening is arranged between the liquid microchannel and the gas channel so as to form a fluid channel and to cause the liquid flow contact the gas flow and wherein the liquid flow is retained within the liquid microchannel by capillarity action. - a support, made at least partially of a dielectric material, the support comprising a gas inlet, adapted to be connected to a gas reservoir, a liquid inlet, adapted to be connected to a liquid reservoir and at least a fluid outlet adapted to be connected to a receiver containing gas and/or liquid, - a liquid microchannel in the support adapted to allow a liquid flow from the liquid inlet to the fluid outlet, - a gas channel, in the support adapted to allow a gas flow from the gas inlet to the fluid outlet, - at least a ground electrode, - at least a high voltage electrode, separated from the gas channel by the dielectric material of the support,
A gas turbine engine, comprising: an inner case including an inner case flange; an outer case including an outer case flange connected to the inner case flange; a heat shield arranged aft of the inner case flange, the heat shield having a first end connected to the inner case at an inner connecting point and a second end connected to the outer case at an outer connecting point, the outer connecting point arranged aft of the outer case flange, and a bulge extending in an aft direction from a radially inner upstream portion, characterised in that: the heat shield has a windback shape which trails along the shape of the inner case; the outer connecting point is aft of the inner connecting point; and the first end of the heat shield curves in the aft direction, wherein a landing in the form of a ring is attached to the interior of the outer case at the outer connecting point, the landing being configured to receive the heat shield, wherein the landing allows the heat shield to be supported by the outer case but remain spaced apart from the outer case. an inner case including an inner case flange; an outer case including an outer case flange connected to the inner case flange; a heat shield arranged aft of the inner case flange, the heat shield having a first end connected to the inner case at an inner connecting point and a second end connected to the outer case at an outer connecting point, the outer connecting point arranged aft of the outer case flange, and a bulge extending in an aft direction from a radially inner upstream portion, characterised in that: the heat shield has a windback shape which trails along the shape of the inner case; the outer connecting point is aft of the inner connecting point; and the first end of the heat shield curves in the aft direction, the outer connecting point is aft of the inner connecting point; and the first end of the heat shield curves in the aft direction, wherein a landing in the form of a ring is attached to the interior of the outer case at the outer connecting point, the landing being configured to receive the heat shield, wherein the landing allows the heat shield to be supported by the outer case but remain spaced apart from the outer case.
A fitting assembly (1, 1') for attaching an elongate member to a surface within a shower or bath area, the fitting assembly (1, 1') comprising: a clamp (3, 3') comprising a collar arranged to receive and abut the elongate member, the collar having an axially extending split, the clamp (3, 3') further comprising a finger (9a, 9b, 9a', 9b') extending outwardly from the collar adjacent one side of the split; a cover (4, 4') comprising an aperture arranged to receive the elongate member, the cover (4, 4') arranged to retain the clamp (3, 3') within such that the collar is axially aligned with the aperture and further arranged to prevent rotation of the clamp (3, 3') with respect to the cover (4, 4'); and a bracket (2, 2') arranged to be fixed to the surface and to receive and retain the cover (4, 4') containing the clamp (3, 3'), the bracket (2, 2') comprising a receiving portion arranged to urge the finger (9a, 9b, 9a', 9b') so as to compress the collar portion at the split, thereby clamping the elongate member within the collar. a clamp (3, 3') comprising a collar arranged to receive and abut the elongate member, the collar having an axially extending split, the clamp (3, 3') further comprising a finger (9a, 9b, 9a', 9b') extending outwardly from the collar adjacent one side of the split; a cover (4, 4') comprising an aperture arranged to receive the elongate member, the cover (4, 4') arranged to retain the clamp (3, 3') within such that the collar is axially aligned with the aperture and further arranged to prevent rotation of the clamp (3, 3') with respect to the cover (4, 4'); and a bracket (2, 2') arranged to be fixed to the surface and to receive and retain the cover (4, 4') containing the clamp (3, 3'), the bracket (2, 2') comprising a receiving portion arranged to urge the finger (9a, 9b, 9a', 9b') so as to compress the collar portion at the split, thereby clamping the elongate member within the collar.
A method for detecting a shaft event of a gas turbine engine, the method comprising: monitoring at least one engine parameter and comparing the at least one engine parameter to a schedule for the at least one parameter defining a first threshold and a second threshold greater than the first threshold; applying a limit to the at least one engine parameter when the at least one engine parameter is inside a parameter limiting region between the first threshold and the second threshold, the first threshold separating the parameter limiting region from a normal operating region, the second threshold separating the parameter limiting region from a hazardous operating region; and detecting the shaft event when the at least one engine parameter crosses the second threshold and issuing a signal in response to the detecting. monitoring at least one engine parameter and comparing the at least one engine parameter to a schedule for the at least one parameter defining a first threshold and a second threshold greater than the first threshold; applying a limit to the at least one engine parameter when the at least one engine parameter is inside a parameter limiting region between the first threshold and the second threshold, the first threshold separating the parameter limiting region from a normal operating region, the second threshold separating the parameter limiting region from a hazardous operating region; and detecting the shaft event when the at least one engine parameter crosses the second threshold and issuing a signal in response to the detecting.
A method of identifying a data transmission technology used in a network link between a first node and a second node, said method comprising: transmitting a first set of data packets from the first node to the second node over the network link, and receiving the first set of data packets at the second node, wherein the first set of data packets comprises a plurality of data packets of a first size, and the plurality of data packets are transmitted with a fixed transmitted inter-packet gap; calculating latency values associated with the first set of data packets, wherein each latency value is equal to the difference in the received inter-packet gap of the data packet and the fixed transmitted inter-packet gap; repeating the transmitting and calculating steps with a second set of data packets, wherein the second set of data packets comprises a plurality of data packets of a second size, and wherein the second size is different to the first size; generating a fingerprint for the network link comprising a distribution of latency values for each packet size; comparing the generated fingerprint with a plurality of predetermined fingerprints to determine the data transmission technology used in the network link, wherein each predetermined fingerprint corresponds to data transmission technology type. transmitting a first set of data packets from the first node to the second node over the network link, and receiving the first set of data packets at the second node, wherein the first set of data packets comprises a plurality of data packets of a first size, and the plurality of data packets are transmitted with a fixed transmitted inter-packet gap; calculating latency values associated with the first set of data packets, wherein each latency value is equal to the difference in the received inter-packet gap of the data packet and the fixed transmitted inter-packet gap; repeating the transmitting and calculating steps with a second set of data packets, wherein the second set of data packets comprises a plurality of data packets of a second size, and wherein the second size is different to the first size; generating a fingerprint for the network link comprising a distribution of latency values for each packet size; comparing the generated fingerprint with a plurality of predetermined fingerprints to determine the data transmission technology used in the network link, wherein each predetermined fingerprint corresponds to data transmission technology type.
Arrangement for the vibration isolation of Bowden-cable-actuated components, comprising a Bowden cable, an actuating element, attached to the end of the Bowden cable, with a mounting eye, a damping element arranged in a form-fitting manner in the mounting eye, and a deflectable transducer element, mounted within the damping element, for actuating the Bowden cable, wherein the damping element is configured as an elastic bushing (38, 60) with a cutout (40, 42) lying in a predefined deflection direction of the transducer element, such that the transducer element, in an unactuated state, takes up a centred position within the elastic bushing (38, 60), characterized in that the transducer element, upon application of a deflecting actuating force (F b), is able to be brought directly into contact with the mounting eye in the region of the cutout (40, 42) under compression of the elastic bushing (38, 60).
A connection arrangement between a body of a vehicle and a frame of a bogie, the connection arrangement comprising a secondary suspension for the vertical suspension of the body relative to the frame, the secondary suspension comprising two levers provided to be mounted pivoting on one of the frame and the body about parallel rotation axes, each lever provided to bear on the other among the frame and the body, and at least one resilient suspension member arranged to oppose pivoting of each lever caused by a downward vertical movement of the body relative to the frame, the resilient suspension member being arranged so as to exert, on each lever, a force oriented substantially horizontally.
A trim piece assembly comprising: a trim piece having an upper margin, a lower margin, an exterior surface, and an interior surface; a drawstring channel positioned on the trim piece; a first set of apertures providing access to the drawstring channel, the first set of apertures positioned at a first distance away from a front centerline of the trim piece; and a second set of apertures extending from the exterior surface to the interior surface of the trim piece, the second set of apertures positioned at a second distance away from the front centerline of the trim piece, characterized in that the second set of apertures is positioned inferior or superior to the first set of apertures with respect to the upper margin of the trim piece assembly.
Warp-knitting machine for producing warp-knitted fabric, having the following features: a) a plurality of lever shafts (3, 4, 5, 6), the axes of which extend in the machine width direction (z) and which run largely parallel to one another, b) a plurality of bar supports which can be driven by the lever shafts (3, 4, 5, 6) to perform pivoting movements in the plane which is spanned by the machine height direction (y) and the machine depth direction (x), c) at least one guide bar which supports thread guiding elements, d) wherein the at least one guide bar is mounted and driven in the warp-knitting machine in such a way that it executes an oscillating offset movement, which is superimposed on its pivoting movement, in the machine width direction (z) during operation, e) the relative position of the lever shaft, with which the at least one guide bar can be driven, to the further lever shafts (4, 5, 6), with which in each case at least one further bar can be driven, can be adjusted in the machine height direction (y) and/or in the machine depth direction (x), f) wherein the warp-knitting machine comprises a machine frame which supports a plurality of lever shafts (3, 4, 5, 6), g) the machine frame comprises a machine upper part and a machine lower part, h) and the machine upper part comprises at least the lever shaft of the guide bars and the components that can be driven by it, characterized in that i) the machine upper part and the machine lower part can be adjusted relative to one another in the machine height direction (y) and/or in the machine depth direction (x). a) a plurality of lever shafts (3, 4, 5, 6), the axes of which extend in the machine width direction (z) and which run largely parallel to one another, b) a plurality of bar supports which can be driven by the lever shafts (3, 4, 5, 6) to perform pivoting movements in the plane which is spanned by the machine height direction (y) and the machine depth direction (x), c) at least one guide bar which supports thread guiding elements, d) wherein the at least one guide bar is mounted and driven in the warp-knitting machine in such a way that it executes an oscillating offset movement, which is superimposed on its pivoting movement, in the machine width direction (z) during operation, e) the relative position of the lever shaft, with which the at least one guide bar can be driven, to the further lever shafts (4, 5, 6), with which in each case at least one further bar can be driven, can be adjusted in the machine height direction (y) and/or in the machine depth direction (x), f) wherein the warp-knitting machine comprises a machine frame which supports a plurality of lever shafts (3, 4, 5, 6), g) the machine frame comprises a machine upper part and a machine lower part, h) and the machine upper part comprises at least the lever shaft of the guide bars and the components that can be driven by it, characterized in that i) the machine upper part and the machine lower part can be adjusted relative to one another in the machine height direction (y) and/or in the machine depth direction (x).