mhurhangee/ep-ind-claims huggingface dataset:
A near field communication device, comprising the following components contained in a housing: a plurality of elements, each configured to perform an independent process, including at least one removable element (62-1, 62-2) and at least one fixed element; a controller configured to control said plurality of elements; and a front end configured to perform near field communication with an external device, the front end being connected to said plurality of elements and configured to perform near field communication of signals from each of said plurality of elements to said external device, wherein said controller is configured to avoid the occurrence of a collision by allocating different time slots corresponding to the plurality of elements when power has been supplied to the device or when any of said elements has been removed or added, wherein said at least one fixed element stores the allocated time slot in a nonvolatile manner, whereas said at least one removable element (62-1, 62-2) stores the time slot in a volatile manner, each of said plurality of elements has a function of performing communication in a randomly timed time slot before the time slot is allocated thereto; and said controller is configured to perform the allocation of the different time slots employing the respective function of performing the communication in the randomly timed time slot. a plurality of elements, each configured to perform an independent process, including at least one removable element (62-1, 62-2) and at least one fixed element; a controller configured to control said plurality of elements; and a front end configured to perform near field communication with an external device, the front end being connected to said plurality of elements and configured to perform near field communication of signals from each of said plurality of elements to said external device, wherein said controller is configured to avoid the occurrence of a collision by allocating different time slots corresponding to the plurality of elements when power has been supplied to the device or when any of said elements has been removed or added, wherein said at least one fixed element stores the allocated time slot in a nonvolatile manner, whereas said at least one removable element (62-1, 62-2) stores the time slot in a volatile manner, each of said plurality of elements has a function of performing communication in a randomly timed time slot before the time slot is allocated thereto; and said controller is configured to perform the allocation of the different time slots employing the respective function of performing the communication in the randomly timed time slot.
A modified antibody or antigen binding fragment thereof, which comprises at least one peptide tag that is a substrate of 4'-phosphopantetheinyl transferase, and is located within a structural loop of said antibody or antigen binding fragment thereof, wherein said 4'-phosphopantetheinyl transferase is Sfp, AcpS, T. maritima PPTase, human PPTase or a mutant or homolog form thereof that retains the 4'-phosphopantetheinyl transferase activity; and wherein the peptide tag is selected from the group consisting of: GDSLSWLLRLLN (SEQ ID NO: 1), GDSLSWL (SEQ ID NO: 2), GDSLSWLVRCLN (SEQ ID NO: 3), GDSLSWLLRCLN (SEQ ID NO: 4), GDSLSWLVRLLN (SEQ ID NO: 5), GDSLSWLLRSLN (SEQ ID NO: 6), GSQDVLDSLEFIASKLA (SEQ ID NO: 7), VLDSLEFIASKLA (SEQ ID NO: 8), DSLEFIASKLA (SEQ ID NO: 9), GDSLDMLEWSLM (SEQ ID NO: 10), GDSLDMLEWSL (SEQ ID NO: 11), GDSLDMLEWS (SEQ ID NO: 12), GDSLDMLEW (SEQ ID NO: 13), DSLDMLEW (SEQ ID NO: 14), GDSLDM (SEQ ID NO: 15), LDSVRMMALAAR (SEQ ID NO: 16), LDSLDMLEWSLR (SEQ ID NO: 17), DSLEFIASKL (SEQ ID NO: 18), DSLEFIASK (SEQ ID NO: 19), DVLDSLEFI (SEQ ID NO: 20), VLDSLEFIAS (SEQ ID NO: 21), and DSLDMLEWSL (SEQ ID NO: 1132), and wherein the peptide tag is inserted between amino acid residues 110 and 111 of the light chain, or the peptide tag is inserted between amino acid residues 119 and 120, or between amino acid residues 120 and 121, or between amino acid residues 135 and 136, or between amino acid residues 136 and 137, or between amino acid residues 138 and 139, or between amino acid residues 162 and 163, or between amino acid residues 164 and 165, or between amino acid residues 165 and 166, or between amino acid residues 194 and 195, or between amino acid residues 195 and 196 of the CH1 domain; or the peptide tag is inserted between amino acid residues 388 and 389 of the CH3 domain; wherein the amino acids are numbered according to the Eu numbering system. GDSLSWLLRLLN (SEQ ID NO: 1), GDSLSWL (SEQ ID NO: 2), GDSLSWLVRCLN (SEQ ID NO: 3), GDSLSWLLRCLN (SEQ ID NO: 4), GDSLSWLVRLLN (SEQ ID NO: 5), GDSLSWLLRSLN (SEQ ID NO: 6), GSQDVLDSLEFIASKLA (SEQ ID NO: 7), VLDSLEFIASKLA (SEQ ID NO: 8), DSLEFIASKLA (SEQ ID NO: 9), GDSLDMLEWSLM (SEQ ID NO: 10), GDSLDMLEWSL (SEQ ID NO: 11), GDSLDMLEWS (SEQ ID NO: 12), GDSLDMLEW (SEQ ID NO: 13), DSLDMLEW (SEQ ID NO: 14), GDSLDM (SEQ ID NO: 15), LDSVRMMALAAR (SEQ ID NO: 16), LDSLDMLEWSLR (SEQ ID NO: 17), DSLEFIASKL (SEQ ID NO: 18), DSLEFIASK (SEQ ID NO: 19), DVLDSLEFI (SEQ ID NO: 20), VLDSLEFIAS (SEQ ID NO: 21), and DSLDMLEWSL (SEQ ID NO: 1132),
A composition for use in the treatment of an ear disorder comprising (+)-azasetron, of Formula -I: or a pharmaceutically acceptable salt and/or solvate thereof, and at least one pharmaceutically acceptable excipient, wherein the composition comprises at least a 90: 10 w/w mixture of (+)-azasetron of Formula -I:(-)-azasetron, or pharmaceutically acceptable salts and/or solvates thereof. and at least one pharmaceutically acceptable excipient, wherein the composition comprises at least a 90: 10 w/w mixture of (+)-azasetron of Formula -I:(-)-azasetron, or pharmaceutically acceptable salts and/or solvates thereof.
A swing control device that controls a rotary body rotated by an electric motor, wherein a velocity command value generated to rotate the rotary body at a predetermined target velocity is substantially constant; and characterised in that an absolute value of a second torque command value generated based on the velocity command value when the velocity command value is changed is controlled to be larger than an absolute value of a first torque command value generated based on the velocity command value when a measured velocity of the rotary body is changed.
A biological fluid collection device, comprising: an inlet portion; an outlet portion; an outer wall spanning the inlet portion and the outlet portion, the outer wall including a top wall and a bottom wall; a first inner wall disposed within the outer wall and spanning the top wall and the bottom wall, the first inner wall including a first inner wall first end and a first inner wall second end; a second inner wall disposed within the outer wall and spanning the top wall and the bottom wall, the second inner wall including a second inner wall first end and a second inner wall second end; a first flow channel disposed between a first portion of the outer wall and the first inner wall, the first flow channel in fluid communication with the inlet portion; a second flow channel disposed between a second portion of the outer wall and the second inner wall, the second flow channel in fluid communication with the inlet portion; a mixing portion disposed between the first inner wall second end and the outlet portion; and a sample stabilizer disposed within a portion of an interior of the outer wall, wherein the first inner wall and the second inner wall together define a chamber therebetween, the chamber in fluid communication with the inlet portion. an inlet portion; an outlet portion; an outer wall spanning the inlet portion and the outlet portion, the outer wall including a top wall and a bottom wall; a first inner wall disposed within the outer wall and spanning the top wall and the bottom wall, the first inner wall including a first inner wall first end and a first inner wall second end; a second inner wall disposed within the outer wall and spanning the top wall and the bottom wall, the second inner wall including a second inner wall first end and a second inner wall second end; a first flow channel disposed between a first portion of the outer wall and the first inner wall, the first flow channel in fluid communication with the inlet portion; a second flow channel disposed between a second portion of the outer wall and the second inner wall, the second flow channel in fluid communication with the inlet portion; a mixing portion disposed between the first inner wall second end and the outlet portion; and a sample stabilizer disposed within a portion of an interior of the outer wall, wherein the first inner wall and the second inner wall together define a chamber therebetween, the chamber in fluid communication with the inlet portion.
A method for providing reservoir based details comprising the steps of: a. isolating a subterranean rock sample capable of bearing a liquid hydrocarbon; b. combining a liquid hydrocarbon fraction with the subterranean rock sample under conditions capable of producing a first interface between the subterranean rock sample and the liquid hydrocarbon fraction, creating an interfacial liquid hydrocarbon fraction; c. performing measurements proximate the interfacial liquid hydrocarbon fraction and subterranean rock sample; d. combining a brine solution with the liquid hydrocarbon fraction under conditions capable of producing a second interface between the brine solution and the liquid hydrocarbon fraction; and e. performing measurements proximate the interfacial liquid hydrocarbon fraction and brine solution, wherein the measurements are made using spectroscopic and interfacial techniques including microscopic, rheometric and tensiometric measurements selected from the group consisting of: atomic force microscopy, Brewster angle microscopy, imaging ellipsometry, scanning electron microscopy, cryo-scanning electron microscopy, environmental scanning electron microscopy, transmission electron microscopy, surface force measurements, surface pressure measurements, surface potential measurements, confocal microscopy, molecular structural analyses, magnetic resonance measurements, rheometry, tensiometry, and combinations thereof. a. isolating a subterranean rock sample capable of bearing a liquid hydrocarbon; b. combining a liquid hydrocarbon fraction with the subterranean rock sample under conditions capable of producing a first interface between the subterranean rock sample and the liquid hydrocarbon fraction, creating an interfacial liquid hydrocarbon fraction; c. performing measurements proximate the interfacial liquid hydrocarbon fraction and subterranean rock sample; d. combining a brine solution with the liquid hydrocarbon fraction under conditions capable of producing a second interface between the brine solution and the liquid hydrocarbon fraction; and e. performing measurements proximate the interfacial liquid hydrocarbon fraction and brine solution,
A solar cell, comprising: a p-n structure having a first conductive semiconductor substrate, a second conductive semiconductor layer formed on the first conductive semiconductor substrate and having a conduction opposite to the first conductive semiconductor substrate, and a p-n junction formed at an interface between the first conductive semiconductor substrate and the second conductive semiconductor layer; a first anti-reflection film formed directly on the second conductive semiconductor layer and composed of SiNx:H thin film with a thickness of 40 nm to 100 nm; a second anti-reflection film formed directly on the first anti-reflection film and composed of silicon oxy-nitride; a front electrode formed on the second anti-reflection film according to a predetermined pattern and connected to the second conductive semiconductor layer through the first and second anti-reflection films (205, 206); and a rear electrode formed at an opposite side to the front electrode with the first conductive semiconductor substrate being interposed therebetween so as to be connected to the first conductive semiconductor substrate, wherein the first anti-reflection film has a refractive index of 1.5 to 3.4, wherein the second anti-reflection film has a refractive index of 1.45 to 2.4 and a thickness of 10nm to 200 nm, and wherein the refractive index of the first anti-reflection film is greater than the refractive index of the second anti-reflection film. a p-n structure having a first conductive semiconductor substrate, a second conductive semiconductor layer formed on the first conductive semiconductor substrate and having a conduction opposite to the first conductive semiconductor substrate, and a p-n junction formed at an interface between the first conductive semiconductor substrate and the second conductive semiconductor layer; a first anti-reflection film formed directly on the second conductive semiconductor layer and composed of SiNx:H thin film with a thickness of 40 nm to 100 nm; a second anti-reflection film formed directly on the first anti-reflection film and composed of silicon oxy-nitride; a front electrode formed on the second anti-reflection film according to a predetermined pattern and connected to the second conductive semiconductor layer through the first and second anti-reflection films (205, 206); and a rear electrode formed at an opposite side to the front electrode with the first conductive semiconductor substrate being interposed therebetween so as to be connected to the first conductive semiconductor substrate, wherein the first anti-reflection film has a refractive index of 1.5 to 3.4, wherein the second anti-reflection film has a refractive index of 1.45 to 2.4 and a thickness of 10nm to 200 nm, and wherein the refractive index of the first anti-reflection film is greater than the refractive index of the second anti-reflection film.
A method for transforming a prilling section comprising a prilling tower, intended to convert a liquid phase into a solid product, the method comprising at least the steps of: a) removing means for spraying said liquid originally provided in said tower; b) making a tubular, or substantially tubular, vertical wall inside said tower, said wall defining a vertical channel inside the tower, and wherein said wall is permeable to air, or at least an upper portion of said wall is permeable to air; c) installing a set of new nozzles on top of said tower, said nozzles being adapted to generate a polydispersed flow of liquid drops, with a descending motion, inside said channel, the newly installed nozzles having orifices of various diameters to generate said polydispersed flow; d) providing means for feeding said new nozzles with at least a part of the available liquid phase; e) providing means for distributing air (3, 3a) in a gap that is defined between the outer casing of the tower and said wall, or between the outer casing of the tower and a portion permeable to air of the wall itself. a) removing means for spraying said liquid originally provided in said tower; b) making a tubular, or substantially tubular, vertical wall inside said tower, said wall defining a vertical channel inside the tower, and wherein said wall is permeable to air, or at least an upper portion of said wall is permeable to air; c) installing a set of new nozzles on top of said tower, said nozzles being adapted to generate a polydispersed flow of liquid drops, with a descending motion, inside said channel, the newly installed nozzles having orifices of various diameters to generate said polydispersed flow; d) providing means for feeding said new nozzles with at least a part of the available liquid phase; e) providing means for distributing air (3, 3a) in a gap that is defined between the outer casing of the tower and said wall, or between the outer casing of the tower and a portion permeable to air of the wall itself.
Aircraft comprising a skin forming an outer surface of the aircraft, the aircraft being equipped with a system for estimating the parameters of an impact comprising an array of sensors attached to the skin and a central processing unit connected to said array and configured for assessing the parameters ( F, I, T) of an impact, said parameters comprising at least the position of the point of impact, the intensity and the duration of the impact, the sensor array comprising a first set of sensors providing data relating to the elastic waves, the sensors of the first set of sensors being located at neutral points of the skin of the aircraft relative to the discriminant vibration eigenmodes of said skin, the central processing unit assessing the parameters ( F, I, T) of an impact from the data of the array of sensors and a response model of the skin to external excitations calculated from the modal properties of the skin.
Device (10; 20) for determining the velocity of a bullet travelling in a direction from a point of fire to a target, comprising: first and second electro-acoustic sensors (12a, 12b; 22a, 22b) arranged at a predetermined distance from each other; a processing unit arranged to receive a first electrical signal from the first electro-acoustic sensor (12a; 22a) and a second electrical signal from the second electro-acoustic sensor (12b; 22b) to determine a time frame between the reception of the first and second electrical signals and to determine the velocity of the bullet in a direction parallel to the alignment of the first and second electro-acoustic sensors (12a, 12b; 22a, 22b), whereupon the velocity of the bullet in a direction parallel to the alignment of the first and second electro-acoustic sensors (12a, 12b; 22a, 22b) is determined; and velocity presentation means; characterized in that the first and second electro-acoustic sensors (12a, 12b; 22a, 22b), the processing unit and the velocity presentation means are mounted in a common housing, the housing being formed so that the device (10; 20) for determining the velocity of the bullet is portable; a sighting means is attached to the housing for aligning the first and second electro-acoustic sensors (12a, 12b; 22a, 22b) parallel to the direction from the point of fire to the target; and that each of the first and second electro-acoustic sensors (12a, 12b; 22a, 22b) is arranged to detect acoustic energy in the ultrasonic range of a shock wave generated by the bullet when travelling at supersonic speed in the direction from the point of fire to the target and to transduce the acoustic energy in the ultrasonic range into an electrical signal. first and second electro-acoustic sensors (12a, 12b; 22a, 22b) arranged at a predetermined distance from each other; a processing unit arranged to receive a first electrical signal from the first electro-acoustic sensor (12a; 22a) and a second electrical signal from the second electro-acoustic sensor (12b; 22b) to determine a time frame between the reception of the first and second electrical signals and to determine the velocity of the bullet in a direction parallel to the alignment of the first and second electro-acoustic sensors (12a, 12b; 22a, 22b), whereupon the velocity of the bullet in a direction parallel to the alignment of the first and second electro-acoustic sensors (12a, 12b; 22a, 22b) is determined; and velocity presentation means;
An annular combustion chamber for an aircraft turbomachine, this chamber comprising two coaxial annular walls, respectively, an internal and an external, which are connected upstream by an annular bottom wall of the chamber, an injection device passing through an axis and comprising an air injection system and a frustoconical bowl which is flared downstream and comprising air passage orifices, the chamber further comprising an annular deflector placed downstream of the annular bottom wall, substantially parallel to the latter, the air injection system, the annular bottom wall, the deflector and the bowl are integrally formed, the deflector comprising an annular portion substantially parallel to the annular bottom wall and separated from the annular bottom wall by a first space, the annular portion comprising an internal end with respect to the axis connected to the bowl and to the annular bottom wall, characterised in that the bowl comprises a first frustoconical wall and a second frustoconical wall substantially parallel and separated from each other by a second space, the annular bottom wall and the first frustoconical wall of the bowl comprising an air passage bores (20, 20') in said first and second spaces (140, 198), said orifices of the bowl extending through the frustoconical walls (192, 194) until they open into the chamber, said outlets of the orifices of the bowl being located at the junctions between a wall of the annular portion of the deflector and the second frustoconical wall of the bowl. the air injection system, the annular bottom wall, the deflector and the bowl are integrally formed, the deflector comprising an annular portion substantially parallel to the annular bottom wall and separated from the annular bottom wall by a first space, the annular portion comprising an internal end with respect to the axis connected to the bowl and to the annular bottom wall, characterised in that the bowl comprises a first frustoconical wall and a second frustoconical wall substantially parallel and separated from each other by a second space, the annular bottom wall and the first frustoconical wall of the bowl comprising an air passage bores (20, 20') in said first and second spaces (140, 198), the deflector comprising an annular portion substantially parallel to the annular bottom wall and separated from the annular bottom wall by a first space, the annular portion comprising an internal end with respect to the axis connected to the bowl and to the annular bottom wall, characterised in that the bowl comprises a first frustoconical wall and a second frustoconical wall substantially parallel and separated from each other by a second space, the annular bottom wall and the first frustoconical wall of the bowl comprising an air passage bores (20, 20') in said first and second spaces (140, 198), said orifices of the bowl extending through the frustoconical walls (192, 194) until they open into the chamber, said outlets of the orifices of the bowl being located at the junctions between a wall of the annular portion of the deflector and the second frustoconical wall of the bowl.
NANOEMULSION characterized by comprising an oily phase dispersed in an aqueous phase, the oily phase containing a combination of the emulsifiers lecithin, fatty acid diester and the product of the condensation of methylglucose with polyglyceryl-3, PEG-40 Sorbitan Peroleate as fatty acid ester and condensed sorbitol with ethylene oxide; in a total concentration equivalent to 1.3% to 46.0% in mass of the total oil content of the composition.
A multilayer heat-shrinkable film, with a number of layers from 4 to 9, comprising: a) an outer heat sealable layer, comprising at least a polyolefin or an EA/AO copolymer and their blends b) at least one layer comprising a blend of from 80 to 50 weight percent of ethylene homopolymer and/or ethylene-alfa olefin copolymers with from 20 to 50 weight percent ethylene vinyl acetate copolymer, c) at least one internal gas-barrier layer, and d)at least one internal layer comprising an acrylic acid-based resin blended with ethylene homopolymer and/or ethylene/alpha-olefin (E/AO) copolymer and/or adhesive materials, in which the acrylic resin is from 80 to 20 percent by weight. a) an outer heat sealable layer, comprising at least a polyolefin or an EA/AO copolymer and their blends b) at least one layer comprising a blend of from 80 to 50 weight percent of ethylene homopolymer and/or ethylene-alfa olefin copolymers with from 20 to 50 weight percent ethylene vinyl acetate copolymer, c) at least one internal gas-barrier layer, and d)at least one internal layer comprising an acrylic acid-based resin blended with ethylene homopolymer and/or ethylene/alpha-olefin (E/AO) copolymer and/or adhesive materials, in which the acrylic resin is from 80 to 20 percent by weight.