mhurhangee/patent-ind-claim-en huggingface dataset:
Inner container for a refrigeration appliance, comprising: walls (8; 9), which surround a storage compartment ; a pivotable door; two recesses (17; 29) formed on the inner container ; two pegs , which are hollow and are manufactured together with the inner container by deep-drawing; two adapters , which are arranged in the pegs in each case; wherein the recesses (17; 29) are arranged in the adapters in each case; a bearing bushing , which is optionally able to be installed in one or the other recess (17; 29); wherein one of the recesses (17; 29) specifies a pivot axis of the door and the other receives a latch of the door . walls (8; 9), which surround a storage compartment ; a pivotable door; two recesses (17; 29) formed on the inner container ; two pegs , which are hollow and are manufactured together with the inner container by deep-drawing; two adapters , which are arranged in the pegs in each case; wherein the recesses (17; 29) are arranged in the adapters in each case; a bearing bushing , which is optionally able to be installed in one or the other recess (17; 29); wherein one of the recesses (17; 29) specifies a pivot axis of the door and the other receives a latch of the door .
A container production method by liquid blow molding, comprising: a liquid blow molding step of supplying a pressurized liquid into a preform (PF) disposed in a metal mold to mold the preform (PF) into a container (C) having a trunk (Ca) that has a flat shape in which a width (Wa) in a long axis direction is larger than a width (Wb) in a short axis direction perpendicular to the long axis direction in a plan view, and the trunk (Ca) holding the liquid (L); and a transferring step of taking the container (C) out from the mold and transferring the container (C) in an approximate short axis direction of the trunk (Ca). a liquid blow molding step of supplying a pressurized liquid into a preform (PF) disposed in a metal mold to mold the preform (PF) into a container (C) having a trunk (Ca) that has a flat shape in which a width (Wa) in a long axis direction is larger than a width (Wb) in a short axis direction perpendicular to the long axis direction in a plan view, and the trunk (Ca) holding the liquid (L); and a transferring step of taking the container (C) out from the mold and transferring the container (C) in an approximate short axis direction of the trunk (Ca).
A glass atomizer, comprising a member for e-liquid injection and vapor discharge, wherein the member for e-liquid injection and vapor discharge comprises an outer glass tube and an inner glass tube disposed in the outer glass tube ; the inner glass tube comprises a top end; characterised in that an outer edge of the top end comprises a plurality of grooves ; and the top end is integrated with an inner wall of the outer glass tube .
An on-vehicle battery pack comprising: a battery module comprising: a unit cell , and a module case in which the unit cell is housed, the module case including a plane being set as a gas release plane from which to release a gas discharged from the unit cell ; a pack case including a sidewall portion , wherein the battery module is housed in the pack case with the gas release plane facing an inner surface of the sidewall portion with a space therebetween; and a restriction plate configured to keep the gas released from the gas release plane from rising directly to an upper portion of inside of the pack case , the restriction plate comprising a first plate portion fixed to an upper surface of the module case and protruding toward the sidewall portion of the pack case at a height position higher than at least an upper edge of the gas release plane , and a second plate portion extending downwards in the space continuously from a front edge of the first plate portion in a direction in which the first plate portion protrudes. a battery module comprising: a unit cell , and a module case in which the unit cell is housed, the module case including a plane being set as a gas release plane from which to release a gas discharged from the unit cell ; a unit cell , and a module case in which the unit cell is housed, the module case including a plane being set as a gas release plane from which to release a gas discharged from the unit cell ; a pack case including a sidewall portion , wherein the battery module is housed in the pack case with the gas release plane facing an inner surface of the sidewall portion with a space therebetween; and a restriction plate configured to keep the gas released from the gas release plane from rising directly to an upper portion of inside of the pack case , the restriction plate comprising a first plate portion fixed to an upper surface of the module case and protruding toward the sidewall portion of the pack case at a height position higher than at least an upper edge of the gas release plane , and a second plate portion extending downwards in the space continuously from a front edge of the first plate portion in a direction in which the first plate portion protrudes.
A wireless device comprising: at least one antenna ; a main receiver , having first automatic gain control circuitry for controlling a gain applied to signals received by means of the at least one antenna; and an auxiliary receiver , configured to monitor a power of a periodic reference signal received by means of the at least one antenna, and further configured to send power information to the main receiver , wherein the main receiver is configured, on waking up, to use the power information received from the auxiliary receiver to assist in operation of the first automatic gain control circuitry characterized in that the auxiliary receiver comprises second automatic gain control circuitry , and wherein said power information comprises information corresponding to a gain applied by the second automatic gain control circuitry . at least one antenna ; a main receiver , having first automatic gain control circuitry for controlling a gain applied to signals received by means of the at least one antenna; and an auxiliary receiver , configured to monitor a power of a periodic reference signal received by means of the at least one antenna, and further configured to send power information to the main receiver , wherein the main receiver is configured, on waking up, to use the power information received from the auxiliary receiver to assist in operation of the first automatic gain control circuitry characterized in that the auxiliary receiver comprises second automatic gain control circuitry , and wherein said power information comprises information corresponding to a gain applied by the second automatic gain control circuitry .
An impregnation unit configured to receive at least first and second spreaded fiber layers and to disperse the first and second spreaded fiber layers into a matrix material, the impregnation unit comprising: an extruder configured to supply a sheet or film of the matrix material between the first and second spreaded fiber layers , the extruder being configured to supply the sheet or film of matrix material to an upper surface of the second spreaded fiber layer to form a coated spreaded fiber layer ; a first pressing element disposed downstream of the extruder , the first pressing element having a convex surface configured to press the first spreaded fiber layer into the matrix material; and a second pressing element disposed downstream of the extruder , the second pressing element having a convex surface configured to press the second spreaded fiber layer into the matrix material, wherein the second pressing element is disposed downstream of the first pressing element, so that the first spreaded fiber layer is brought into contact with the coated spreaded fiber layer and pressed into the matrix material by passing over the first pressing element , and so that the coated spreaded fiber layer is pressed into the matrix material by passing over the second pressing element . an extruder configured to supply a sheet or film of the matrix material between the first and second spreaded fiber layers , the extruder being configured to supply the sheet or film of matrix material to an upper surface of the second spreaded fiber layer to form a coated spreaded fiber layer ; a first pressing element disposed downstream of the extruder , the first pressing element having a convex surface configured to press the first spreaded fiber layer into the matrix material; and a second pressing element disposed downstream of the extruder , the second pressing element having a convex surface configured to press the second spreaded fiber layer into the matrix material, wherein the second pressing element is disposed downstream of the first pressing element, so that the first spreaded fiber layer is brought into contact with the coated spreaded fiber layer and pressed into the matrix material by passing over the first pressing element , and so that the coated spreaded fiber layer is pressed into the matrix material by passing over the second pressing element .
Composite material comprising fibres , a matrix and a reflective device which is configured and arranged in a manner such that at least one region of a surface of the composite material is reflective, characterized in that the reflective device has a reflective lamina which is a reflective fabric and/or a reflective felt.
A method for diagnosis of systemic lupus erythematosus (SLE) in a subject wherein, presence or absence of an anti-CXC chemokine receptor (CXCR) antibody is detected in a sample from the subject diagnosed, and wherein the presence of an anti-CXCR antibody is indicative of SLE.
An assembly comprising: a wing , the wing comprising having a gull wing configuration which includes an up angle portion and a flat portion ; a gas turbine engine ; and a mounting structure for mounting said gas turbine engine to a pylon , the gas turbine engine comprising: a propulsor section including a fan having a fan diameter, and a geared architecture driving the fan ; and a generator section including a fan drive turbine that drives the geared architecture , wherein: a turbine to fan diameter ratio is less than 45%; said fan drives air along a bypass flow path (B); the gas turbine engine further comprises a compressor section which draws air along a core flow path (C); the gas turbine engine has a bypass ratio greater than or equal to 10.0: said geared architecture has a gear reduction ratio greater than or equal to 2.3; and said fan has fewer than 26 fan blades. a wing , the wing comprising having a gull wing configuration which includes an up angle portion and a flat portion ; a gas turbine engine ; and a mounting structure for mounting said gas turbine engine to a pylon , the gas turbine engine comprising: a propulsor section including a fan having a fan diameter, and a geared architecture driving the fan ; and a generator section including a fan drive turbine that drives the geared architecture , wherein: a turbine to fan diameter ratio is less than 45%; said fan drives air along a bypass flow path (B); the gas turbine engine further comprises a compressor section which draws air along a core flow path (C); the gas turbine engine has a bypass ratio greater than or equal to 10.0: said geared architecture has a gear reduction ratio greater than or equal to 2.3; and said fan has fewer than 26 fan blades. a propulsor section including a fan having a fan diameter, and a geared architecture driving the fan ; and a generator section including a fan drive turbine that drives the geared architecture , wherein: a turbine to fan diameter ratio is less than 45%; said fan drives air along a bypass flow path (B); the gas turbine engine further comprises a compressor section which draws air along a core flow path (C); the gas turbine engine has a bypass ratio greater than or equal to 10.0: said geared architecture has a gear reduction ratio greater than or equal to 2.3; and said fan has fewer than 26 fan blades. a turbine to fan diameter ratio is less than 45%; said fan drives air along a bypass flow path (B); the gas turbine engine further comprises a compressor section which draws air along a core flow path (C); the gas turbine engine has a bypass ratio greater than or equal to 10.0: said geared architecture has a gear reduction ratio greater than or equal to 2.3; and said fan has fewer than 26 fan blades. said geared architecture has a gear reduction ratio greater than or equal to 2.3; and said fan has fewer than 26 fan blades.
A method of purifying an RNA fraction with < 200 nucleotides in length from a whole blood sample comprising the steps of: (i) providing an absorbent probe comprising a hydrophilic polymeric material in/to which whole blood from the whole blood sample has been absorbed, (ii) contacting the absorbent probe with a fluid comprising a chaotropic agent, and (iii) recovering the fluid comprising a chaotropic agent from step (ii), thereby removing the RNA fraction with ≥ 200 nucleotides in length, and (iv) purifying the RNA fraction with < 200 nucleotides in length from the recovered fluid by one or more separation techniques selected from the group consisting of centrifugation, evaporation/reconstitution, concentration, precipitation, liquid/liquid extraction, and solid phase extraction, wherein the RNA fraction with ≥ 200 nucleotides in length does not enter the fluid and remains absorbed to the hydrophilic polymeric material wherein the hydrophilic polymeric material has a density of ≤ 6 g/cm 3 , and wherein the hydrophilic polymeric material is selected from the group consisting of cotton, a polysaccharide, a polyolefin, and a polyester. (i) providing an absorbent probe comprising a hydrophilic polymeric material in/to which whole blood from the whole blood sample has been absorbed, (ii) contacting the absorbent probe with a fluid comprising a chaotropic agent, and (iii) recovering the fluid comprising a chaotropic agent from step (ii), thereby removing the RNA fraction with ≥ 200 nucleotides in length, and (iv) purifying the RNA fraction with < 200 nucleotides in length from the recovered fluid by one or more separation techniques selected from the group consisting of centrifugation, evaporation/reconstitution, concentration, precipitation, liquid/liquid extraction, and solid phase extraction, wherein the RNA fraction with ≥ 200 nucleotides in length does not enter the fluid and remains absorbed to the hydrophilic polymeric material wherein the hydrophilic polymeric material has a density of ≤ 6 g/cm 3 , and wherein the hydrophilic polymeric material is selected from the group consisting of cotton, a polysaccharide, a polyolefin, and a polyester. wherein the RNA fraction with ≥ 200 nucleotides in length does not enter the fluid and remains absorbed to the hydrophilic polymeric material wherein the hydrophilic polymeric material has a density of ≤ 6 g/cm 3 , and wherein the hydrophilic polymeric material is selected from the group consisting of cotton, a polysaccharide, a polyolefin, and a polyester.
A polymer resin composition for manufacturing an inner liner film, which comprises: a cross-linked polymer comprising polyamide-based segments including repeat units of the following Chemical Formula 1 or Chemical Formula 2 and polyether-based segments including repeat units of the following Chemical Formula 3 and a polyamide-based resin having relative viscosity of 2.5 to 4.0 with respect to 96 % sulfuric acid solution, wherein a content of the polyether-based segments included in the cross-linked polymer is 2 to 40 wt% based on total weight of the polymer resin composition, and the polyamide-based segment is bound to the polyether-based segment via a residue of an aromatic compound including at least one amine group and at least one carboxylic group: in Chemical Formula 1, R 1 is a C1-C20 linear or branched alkylene group, a C6-C20 arylene group, or a C7-C20 linear or branched arylalkylene group; in Chemical Formula 2, R 2 is a C1-C20 linear or branched alkylene group, and R 3 is a C1-C20 linear or branched alkylene group, a C6-C20 arylene group, or a C7-C20 linear or branched arylalkylene group; and in Chemical Formula 3, R 5 is a C1-C10 linear or branched alkylene group, n is an integer of 1 to 100, and R 6 and R 7 may be the same as or different from each other, and are a direct bond, -O-, -NH-, -COO-, or -CONH-, respectively. a cross-linked polymer comprising polyamide-based segments including repeat units of the following Chemical Formula 1 or Chemical Formula 2 and polyether-based segments including repeat units of the following Chemical Formula 3 and a polyamide-based resin having relative viscosity of 2.5 to 4.0 with respect to 96 % sulfuric acid solution, wherein a content of the polyether-based segments included in the cross-linked polymer is 2 to 40 wt% based on total weight of the polymer resin composition, and the polyamide-based segment is bound to the polyether-based segment via a residue of an aromatic compound including at least one amine group and at least one carboxylic group: in Chemical Formula 1, R 1 is a C1-C20 linear or branched alkylene group, a C6-C20 arylene group, or a C7-C20 linear or branched arylalkylene group; in Chemical Formula 2, R 2 is a C1-C20 linear or branched alkylene group, and R 3 is a C1-C20 linear or branched alkylene group, a C6-C20 arylene group, or a C7-C20 linear or branched arylalkylene group; and in Chemical Formula 3, R 5 is a C1-C10 linear or branched alkylene group, n is an integer of 1 to 100, and R 6 and R 7 may be the same as or different from each other, and are a direct bond, -O-, -NH-, -COO-, or -CONH-, respectively.
A collimator assembly for an X-ray spectrometer device, the collimator assembly comprising a rotatable gear assembly comprising a worm gear assembly and including a collimator plate having a plurality of apertures of different size and/or shape arranged therein; a driving assembly comprising a worm screw for rotating the gear assembly and an electric motor for rotating the worm screw to bring the gear assembly into a rotational position where a selected one of the plurality of apertures is spatially aligned with a predefined axis (B) along which a collimated X-ray beam is to be provided from the X-ray spectrometer device; and a magnet arrangement for generating a magnetic force that is arranged to push or pull the gear assembly into a predefined direction of rotation to prevent rotational movement due to backlash, thereby keeping the selected one of the plurality of apertures spatially aligned with said predefined axis (B). a rotatable gear assembly comprising a worm gear assembly and including a collimator plate having a plurality of apertures of different size and/or shape arranged therein; a driving assembly comprising a worm screw for rotating the gear assembly and an electric motor for rotating the worm screw to bring the gear assembly into a rotational position where a selected one of the plurality of apertures is spatially aligned with a predefined axis (B) along which a collimated X-ray beam is to be provided from the X-ray spectrometer device; and a magnet arrangement for generating a magnetic force that is arranged to push or pull the gear assembly into a predefined direction of rotation to prevent rotational movement due to backlash, thereby keeping the selected one of the plurality of apertures spatially aligned with said predefined axis (B).
A combination of a first compound selected from N-(3,5-dimethoxyphenyl)-N'-(1-methylethyl)-N-[3-(1-methyl-1H-pyrazol-4-yl)quinoxalin-6-yl]ethane-1,2-diamine or a pharmaceutically acceptable salt thereof or a solvate thereof, and N-(2-fluoro-3,5-dimethoxyphenyl)-N-(1H-imidazol-2-ylmethyl)-3-(1-methyl-1H-pyrazol-4-yl)pyrido[2,3-b]pyrazin-6-amine or a pharmaceutically acceptable salt thereof or a solvate thereof; and a second compound which is a cMet inhibitor.
A device for detecting an object conveyed by means of an apparatus for conveying the device through a measuring region of the device, comprising a transmission apparatus for emitting measuring radiation having a frequency in the gigahertz or terahertz range onto the outer contour of the object and a receiving apparatus for receiving the measuring radiation reflected by the object , characterized in that a protective mesh which is transparent to the measuring radiation and permeable to gas is arranged between the transmission apparatus and/or the receiving apparatus, on the one hand, and the measuring region, on the other hand, wherein a flushing apparatus is further provided for flushing the protective mesh with a flushing gas.
A toroidal support structure for a spacecraft comprising: one or more side panels forming a tubular ring extending between a first edge and a second edge ; one or more floor panels forming a planar ring extending between an outer edge and an inner edge , wherein the first edge of the one or more side panels is fixed to the outer edge of the one or more floor panels and the first edge and the outer edge have the same shape and size; a plurality of isolating linear support components connected to the second edge of the one or more side panels at connection points , wherein the connection points are evenly distributed along the second edge and equally spaced from a center axis of the toroidal support structure by a radius; and one or more interior supports connected to the one or more side panels and to the one or more floor panels for maintaining orientation of the one or more side panels relative to the one or more floor panels , the one or more interior supports comprise a plurality of struts connected to the second edge of the one or more side panels at the connection points . one or more side panels forming a tubular ring extending between a first edge and a second edge ; one or more floor panels forming a planar ring extending between an outer edge and an inner edge , wherein the first edge of the one or more side panels is fixed to the outer edge of the one or more floor panels and the first edge and the outer edge have the same shape and size; a plurality of isolating linear support components connected to the second edge of the one or more side panels at connection points , wherein the connection points are evenly distributed along the second edge and equally spaced from a center axis of the toroidal support structure by a radius; and one or more interior supports connected to the one or more side panels and to the one or more floor panels for maintaining orientation of the one or more side panels relative to the one or more floor panels , the one or more interior supports comprise a plurality of struts connected to the second edge of the one or more side panels at the connection points .
An array substrate comprising a substrate having a plurality of sub-pixel regions, wherein the array substrate in each sub-pixel region comprises: a switching element disposed on the substrate , a sintered nanoscale metal material planarizing layer disposed on the switching element , and an ITO pixel electrode disposed directly on the sintered nanoscale metal material planarizing layer , wherein the ITO pixel electrode is electrically connected to an output electrode of the switching element , and wherein the size of the metal material is less than or equal to 1 nm to less than or equal to 200 nm, and wherein more than 80% of the ingredients of the sintered nanoscale metal material planarizing layer is a metal element. a switching element disposed on the substrate , a sintered nanoscale metal material planarizing layer disposed on the switching element , and an ITO pixel electrode disposed directly on the sintered nanoscale metal material planarizing layer , wherein the ITO pixel electrode is electrically connected to an output electrode of the switching element , and wherein the size of the metal material is less than or equal to 1 nm to less than or equal to 200 nm, and wherein more than 80% of the ingredients of the sintered nanoscale metal material planarizing layer is a metal element.