mhurhangee/ep-ind-claims huggingface dataset:
A variable nozzle mechanism for a variable geometry turbocharger, comprising: a first annular member; a second annular member disposed so as to face the first annular member and forming an exhaust gas flow passage having an annular shape between the first annular member and the second annular member, for guiding exhaust gas to a turbine rotor of the turbo charger from a scroll flow passage formed on a radially outer side of the turbine rotor; and a plurality of nozzle vanes supported rotatably on the first annular member and configured to be capable of adjusting a flow passage area of the exhaust gas flow passage, wherein the first annular member has a plurality of support holes for supporting the plurality of nozzle vanes rotatably, the support holes being disposed at intervals in a circumferential direction of the turbine rotor, wherein an inner peripheral edge of the first annular member includes a plurality of first inner edge portions belonging to an angular range (A, B, C, D) in which the support holes exist in the circumferential direction of the turbine rotor and a plurality of second inner edge portions belonging to an angular range (A, B, C, D) in which the support holes do not exist in the circumferential direction of the turbine rotor, and wherein at least one second inner edge portion of the plurality of second inner edge portions comprises a recess portion recessed outward in a radial direction of the turbine rotor, the recess portion extending in an axial direction of the turbine rotor from the side of the exhaust gas flow passage. a first annular member; a second annular member disposed so as to face the first annular member and forming an exhaust gas flow passage having an annular shape between the first annular member and the second annular member, for guiding exhaust gas to a turbine rotor of the turbo charger from a scroll flow passage formed on a radially outer side of the turbine rotor; and a plurality of nozzle vanes supported rotatably on the first annular member and configured to be capable of adjusting a flow passage area of the exhaust gas flow passage, wherein the first annular member has a plurality of support holes for supporting the plurality of nozzle vanes rotatably, the support holes being disposed at intervals in a circumferential direction of the turbine rotor, wherein an inner peripheral edge of the first annular member includes a plurality of first inner edge portions belonging to an angular range (A, B, C, D) in which the support holes exist in the circumferential direction of the turbine rotor and a plurality of second inner edge portions belonging to an angular range (A, B, C, D) in which the support holes do not exist in the circumferential direction of the turbine rotor, and wherein at least one second inner edge portion of the plurality of second inner edge portions comprises a recess portion recessed outward in a radial direction of the turbine rotor, the recess portion extending in an axial direction of the turbine rotor from the side of the exhaust gas flow passage.
A mounting base for an articulator in dental technology for creating and handling plaster models that are free from retention plates, which has a base body with a mounting surface facing the articulator in a mounting state and a holding surface facing away therefrom, and wherein at least one permanently magnetic holding element is provided in the holding surface, characterised in that the mounting base - has at least one recess in the holding surface and at least one impression element each of which is movably placed into the recess, and - has at least one lifting element which is inserted between the mounting surface and the holding surface, wherein the at least one lifting element is in operative connection with the at least one impression element and can be actuated from outside the mounting base in order to carry out a lifting movement and a lowering movement of the at least one impression element, and wherein the at least one lifting element is configured to move the at least one impression element between two predefined maximum positions and to position the same at least in the two predefined maximum positions, wherein, in a first maximum position, the impression element protrudes farthest out of the holding surface and, in a second maximum position, is flush with the holding surface. - has at least one recess in the holding surface and at least one impression element each of which is movably placed into the recess, and - has at least one lifting element which is inserted between the mounting surface and the holding surface,
A method for controlling a particular loudness characteristic of an audio signal, wherein the particular loudness characteristic is either a specific loudness, which is a measure of perceptual loudness as a function of frequency and time, or a partial specific loudness, which is a measure of perceptual loudness of the audio signal in the presence of a secondary interfering signal as a function of frequency and time, comprising receiving from a transmission or reproducing from a storage medium the audio signal and frequency- and time-variant modification parameters for modifying the audio signal, and modifying the audio signal in response to the received modification parameters in order to reduce the difference between the particular loudness characteristic of the audio signal and a target specific loudness, wherein said frequency- and time-variant modification parameters are obtainable by: deriving, as a function of the audio signal, said target specific loudness, and deriving the frequency- and time-variant modification parameters usable for modifying the audio signal in order to reduce the difference between its particular loudness characteristic and the target specific loudness. deriving, as a function of the audio signal, said target specific loudness, and deriving the frequency- and time-variant modification parameters usable for modifying the audio signal in order to reduce the difference between its particular loudness characteristic and the target specific loudness.
A compound having the structure of Formula I wherein X is: 1) C(R i)(R j), or 2) oxygen; T is: 1) CH 2, 2) CH 2 CH 2, or 3) absent; R 1 and R 2 are independently: 1) -CH 3, or 2) -CH 2 CH 3; R 3 is: 1) hydrogen, 2) -CH 3, or 3) -CH 2 CH 3; R 4 is: 1) hydrogen, or 2) -CH 3; R a and R b are each independently: 1) hydrogen, 2) -CH 3, or 3) -CH 2 CH 3; R i and R j are each independently: 1) hydrogen, 2) deuterium, 3) hydroxyl, 4) fluoro, 5) alkoxy, 6) C 1-10 alkyl, or 7) C 1-10 haloalkyl; and R i and R j can be taken together as oxo (=O): B is: 1) 2) 3) 4) R e, R f, R g, R h and R k are each independently: 1) hydrogen, 2) C 1-10 alkyl, 3) C 1-10 haloalkyl, 4) halogen, 5) nitro, 6) hydroxy, 7) alkoxy, 8) nitrile, 9) carboxamido, 10) arylcarbonyl, 11) carbamoyl, 12) amidyl, 13) amino, 14) alkylcarbonyl, or 15) urea or 16) -C NH 2; R l, R m and R n are: 1) -CR e, or 2) nitrogen; but wherein at least one of R l, R m and R n is nitrogen, Z is: 1) oxygen, or 2) sulfur; all alkyl may be substituted with one or more of the following: hydroxy, ester, amidyl, oxo, carboxyl, carboxamido, halo, cyano, nitrate, nitrite, thionitrate, thionitrite, sulfhydryl and amino groups; including pharmaceutically acceptable salts, solvates and hydrates thereof. wherein X is: 1) C(R i)(R j), or 2) oxygen; 1) C(R i)(R j), or 2) oxygen; T is: 1) CH 2, 2) CH 2 CH 2, or 3) absent; 1) CH 2, 2) CH 2 CH 2, or 3) absent; R 1 and R 2 are independently: 1) -CH 3, or 2) -CH 2 CH 3; 1) -CH 3, or 2) -CH 2 CH 3; R 3 is: 1) hydrogen, 2) -CH 3, or 3) -CH 2 CH 3; 1) hydrogen, 2) -CH 3, or 3) -CH 2 CH 3; R 4 is: 1) hydrogen, or 2) -CH 3; 1) hydrogen, or 2) -CH 3; R a and R b are each independently: 1) hydrogen, 2) -CH 3, or 3) -CH 2 CH 3; 1) hydrogen, 2) -CH 3, or 3) -CH 2 CH 3; R i and R j are each independently: 1) hydrogen, 2) deuterium, 3) hydroxyl, 4) fluoro, 5) alkoxy, 6) C 1-10 alkyl, or 7) C 1-10 haloalkyl; 1) hydrogen, 2) deuterium, 3) hydroxyl, 4) fluoro, 5) alkoxy, 6) C 1-10 alkyl, or 7) C 1-10 haloalkyl; and R i and R j can be taken together as oxo (=O): B is: 1) 2) 3) 4) B is: 1) 2) 3) 4) 1) 2) 3) 4) R e, R f, R g, R h and R k are each independently: 1) hydrogen, 2) C 1-10 alkyl, 3) C 1-10 haloalkyl, 4) halogen, 5) nitro, 6) hydroxy, 7) alkoxy, 8) nitrile, 9) carboxamido, 10) arylcarbonyl, 11) carbamoyl, 12) amidyl, 13) amino, 14) alkylcarbonyl, or 15) urea or 16) -C NH 2; 1) hydrogen, 2) C 1-10 alkyl, 3) C 1-10 haloalkyl, 4) halogen, 5) nitro, 6) hydroxy, 7) alkoxy, 8) nitrile, 9) carboxamido, 10) arylcarbonyl, 11) carbamoyl, 12) amidyl, 13) amino, 14) alkylcarbonyl, or 15) urea or 16) -C NH 2; R l, R m and R n are: 1) -CR e, or 2) nitrogen; 1) -CR e, or 2) nitrogen; but wherein at least one of R l, R m and R n is nitrogen, Z is: 1) oxygen, or 2) sulfur; 1) oxygen, or 2) sulfur; all alkyl may be substituted with one or more of the following: hydroxy, ester, amidyl, oxo, carboxyl, carboxamido, halo, cyano, nitrate, nitrite, thionitrate, thionitrite, sulfhydryl and amino groups; including pharmaceutically acceptable salts, solvates and hydrates thereof.
An electronic self-destructing fuse structure comprising: a lower plate structure comprising a first guide hole vertically penetrating therethrough and a first pin inserted into the first guide hole to vertically move; a substrate module disposed at a lower side of the lower plate structure, the substrate module comprising a first through-hole positioned corresponding to a position of the first pin, the first through-hole having a reserve battery mounted therein to be activated when struck by the first pin, a second through-hole comprising a first conductive wire formed thereacross and configured to detect a short circuit, a third through-hole comprising a second conductive wire formed thereacross and configured to detect a short circuit, and an electric detonator mounted at a lower side thereof, the electric detonator outputting, toward a lower side, an electrical detonation signal in response to the short circuit of the second conductive wire and detonating according to the electrical detonation signal; and a first safety structure disposed at a lower side of the substrate module, the first safety structure comprising a centrifugal force weight configured to be moved outwards from a center by centrifugal force and to short-circuit the first conductive wire, an impact weight configured to ascend and descend by inertia and to short-circuit the second conductive wire, and a first detonator hole formed to allow the electric detonator to be close to a spit-back. a lower plate structure comprising a first guide hole vertically penetrating therethrough and a first pin inserted into the first guide hole to vertically move; a substrate module disposed at a lower side of the lower plate structure, the substrate module comprising a first through-hole positioned corresponding to a position of the first pin, the first through-hole having a reserve battery mounted therein to be activated when struck by the first pin, a second through-hole comprising a first conductive wire formed thereacross and configured to detect a short circuit, a third through-hole comprising a second conductive wire formed thereacross and configured to detect a short circuit, and an electric detonator mounted at a lower side thereof, the electric detonator outputting, toward a lower side, an electrical detonation signal in response to the short circuit of the second conductive wire and detonating according to the electrical detonation signal; and a first safety structure disposed at a lower side of the substrate module, the first safety structure comprising a centrifugal force weight configured to be moved outwards from a center by centrifugal force and to short-circuit the first conductive wire, an impact weight configured to ascend and descend by inertia and to short-circuit the second conductive wire, and a first detonator hole formed to allow the electric detonator to be close to a spit-back.
A separator comprising: a porous polymer substrate having a plurality of pores; a separator base including a porous coating layer formed on at least one surface of the porous polymer substrate, said porous coating layer comprising a plurality of inorganic particles and a binder polymer disposed partially or totally on the surface of the inorganic particles to connect and fix the inorganic particles with each other; and an adhesive porous layer formed on at least one surface of the separator base, said adhesive porous layer comprising an adhesive resin which shows adhesive property through heating at a temperature lower than a melting point of the porous polymer substrate, wherein the adhesive porous layer is provided with a porous structure formed by phase separation caused by an evaporation rate of a solvent and that of a non-solvent, when applying and drying a coating composition including the adhesive resin, the solvent and the non-solvent on at least one surface of the separator base, characterized in that the inorganic particles are a combination of boehmite particles and alumina particles, the boehmite particles having a smaller average particle diameter and a smaller density than the alumina particles. a porous polymer substrate having a plurality of pores; a separator base including a porous coating layer formed on at least one surface of the porous polymer substrate, said porous coating layer comprising a plurality of inorganic particles and a binder polymer disposed partially or totally on the surface of the inorganic particles to connect and fix the inorganic particles with each other; and an adhesive porous layer formed on at least one surface of the separator base, said adhesive porous layer comprising an adhesive resin which shows adhesive property through heating at a temperature lower than a melting point of the porous polymer substrate, wherein the adhesive porous layer is provided with a porous structure formed by phase separation caused by an evaporation rate of a solvent and that of a non-solvent, when applying and drying a coating composition including the adhesive resin, the solvent and the non-solvent on at least one surface of the separator base, characterized in that the inorganic particles are a combination of boehmite particles and alumina particles, the boehmite particles having a smaller average particle diameter and a smaller density than the alumina particles.
A fuel pressure sensing system (400, 500) for a gas turbine engine comprising: a first fuel splitter (408, 504) configured to split a primary fuel stream (404, 534) into a first (410, 506) and second stream (422, 508); a first (414, 512) and second (426, 522) flow controller, wherein the first flow controller (414, 512) is configured to move the first stream (410, 506) at a first flow rate and the second flow controller (426, 522) is configured to move the second stream (422, 508) at the first flow rate; a first (418, 518) and second (430, 528) fuel nozzle respectively downstream from the respective first (414, 512) and second (426, 522) flow controllers; a first pressure sensor (420, 516) positioned downstream from the first flow controller (414, 512) and upstream from the first fuel nozzle (418, 518), wherein the first pressure sensor (420, 516) is configured to sense a first fuel stream pressure between the first flow controller (414, 512) and the first fuel nozzle (418, 518); a second pressure sensor (432, 526) positioned downstream from the second flow controller (426, 522) and upstream from the second fuel nozzle (430, 528), wherein the second pressure sensor (432, 526) is configured to sense a second fuel stream pressure between the second flow controller (426, 522) and the second fuel nozzle (430, 528); and characterized by comprising a common drive (434, 530) coupled to the first (414, 512) and second (426, 522) flow controllers and configured to drive the first (414, 512) and second (426, 522) flow controllers at a same speed. a first fuel splitter (408, 504) configured to split a primary fuel stream (404, 534) into a first (410, 506) and second stream (422, 508); a first (414, 512) and second (426, 522) flow controller, wherein the first flow controller (414, 512) is configured to move the first stream (410, 506) at a first flow rate and the second flow controller (426, 522) is configured to move the second stream (422, 508) at the first flow rate; a first (418, 518) and second (430, 528) fuel nozzle respectively downstream from the respective first (414, 512) and second (426, 522) flow controllers; a first pressure sensor (420, 516) positioned downstream from the first flow controller (414, 512) and upstream from the first fuel nozzle (418, 518), wherein the first pressure sensor (420, 516) is configured to sense a first fuel stream pressure between the first flow controller (414, 512) and the first fuel nozzle (418, 518); a second pressure sensor (432, 526) positioned downstream from the second flow controller (426, 522) and upstream from the second fuel nozzle (430, 528), wherein the second pressure sensor (432, 526) is configured to sense a second fuel stream pressure between the second flow controller (426, 522) and the second fuel nozzle (430, 528); and characterized by comprising a common drive (434, 530) coupled to the first (414, 512) and second (426, 522) flow controllers and configured to drive the first (414, 512) and second (426, 522) flow controllers at a same speed.
A method for dyeing artificial fibers comprising: a preparation step to prepare an artificial fiber; a mix step to add a dyestuff, a crosslinking agent, and water into a tank for mixture to obtain a dye liquor; a dye step to immerse the artificial fiber in the tank to obtain a dyed artificial fiber, wherein the dye step further includes disposing a pressing member above the tank, and adjusting a height of the pressing member relative to the tank; a press step to press the dyed artificial fiber by a roller set, wherein the roller set has two opposing rollers; and a dry step to dry out the dyed artificial fiber. a preparation step to prepare an artificial fiber; a mix step to add a dyestuff, a crosslinking agent, and water into a tank for mixture to obtain a dye liquor; a dye step to immerse the artificial fiber in the tank to obtain a dyed artificial fiber, wherein the dye step further includes disposing a pressing member above the tank, and adjusting a height of the pressing member relative to the tank; disposing a pressing member above the tank, and adjusting a height of the pressing member relative to the tank; a press step to press the dyed artificial fiber by a roller set, wherein the roller set has two opposing rollers; and a dry step to dry out the dyed artificial fiber.
A method for cutting, in a non-through manner, a body of a thruster of an aerospace vehicle, using water jets, said cutting being made along a cutting path describing a closed loop circuit, characterized in that the method comprises a plurality of passes of a high-pressure water jet (210, 230) along the same cutting path extending across the external perimeter of the thruster body, each water jet passage starting from a starting point located on the cutting path and stopping just after returning on the starting location, characterized in that the starting point of each high-pressure water jet pass is different from the starting points of the other water jet passes.
Apparatus for the separation or liquefaction of a gas at cryogenic temperatures, which comprises an isolated chamber comprising at least one element having to operate at cryogenic temperatures, the element being a distillation column, and also a pipe for transferring fluid coming from or going to the element, the pipe (5, 7) having a diameter D comprising at least one bend for changing the direction of flow of the fluid, characterized in that: - the bend does not comprise a curvature and forms a right angle, or alternatively comprises a curvature for which the ratio of the radius of curvature R to the diameter D of the pipe is y, where y is equal to 0.5 or greater than 0.5 and less than 1 and - profiled deflector vanes are placed inside the bend, with their concavity towards the centre of the bend forming a plurality of parallel curved ducts. - the bend does not comprise a curvature and forms a right angle, or alternatively comprises a curvature for which the ratio of the radius of curvature R to the diameter D of the pipe is y, where y is equal to 0.5 or greater than 0.5 and less than 1 and - profiled deflector vanes are placed inside the bend, with their concavity towards the centre of the bend forming a plurality of parallel curved ducts.
A harvesting apparatus adapted to harvest egg fluid from an egg, the harvesting apparatus comprising: a frame; a harvesting assembly operably engaged with the frame, the harvesting assembly comprising a plurality of nozzles configured to remove egg fluid from an egg; and a suction assembly in fluid communication with the nozzles for harvesting egg fluid from an egg; characterized in that the nozzles are configured to rotate from a vertically off-axis angled position toward a vertical position. a frame; a harvesting assembly operably engaged with the frame, the harvesting assembly comprising a plurality of nozzles configured to remove egg fluid from an egg; and a suction assembly in fluid communication with the nozzles for harvesting egg fluid from an egg;
A device for postural education, comprising: - at least two oscillating elements having respectively: - at least one plantar resting portion for the resting of a foot of a user; - at least one supporting portion opposite to said plantar resting portion and of a substantially convex shape; - connection means of said oscillating elements having an elongated shape and comprise at least one connection element having a first ending part associated with one of said oscillating elements and a second ending part associated with the other of said oscillating elements; in which said supporting portion is adapted to allow the oscillation of the respective said oscillating element as a result of the resting of the foot of said user, wherein said supporting portion comprises a resting surface having a predefined radius of curvature and a substantially hemispherical shape; characterised in that the device further comprises means for the mutual orientation of said oscillating elements, wherein said ending parts (10, 11) are associated in a sliding manner with said oscillating elements. - at least two oscillating elements having respectively: - at least one plantar resting portion for the resting of a foot of a user; - at least one supporting portion opposite to said plantar resting portion and of a substantially convex shape; - at least one plantar resting portion for the resting of a foot of a user; - at least one supporting portion opposite to said plantar resting portion and of a substantially convex shape; - connection means of said oscillating elements having an elongated shape and comprise at least one connection element having a first ending part associated with one of said oscillating elements and a second ending part associated with the other of said oscillating elements;
A communication apparatus comprising: a RFID reader/writer section adapted to perform communication in an ASK modulation format with an RFID tag; and a central processing unit, CPU adapted to set a modulation degree of the ASK modulation of the RFID reader/writer section to a first degree when polling of the RFID tag is performed by the RFID reader/writer section and adapted to set the modulation degree to a second degree, smaller than the first degree, when response information is received from the RFID tag through the RFID reader/writer section. a RFID reader/writer section adapted to perform communication in an ASK modulation format with an RFID tag; and a central processing unit, CPU adapted to set a modulation degree of the ASK modulation of the RFID reader/writer section to a first degree when polling of the RFID tag is performed by the RFID reader/writer section and adapted to set the modulation degree to a second degree, smaller than the first degree, when response information is received from the RFID tag through the RFID reader/writer section.