mhurhangee/ep-ind-claims huggingface dataset:
A method for denying a Multimedia Messaging Service MMS request on a Session Initiation Protocol SIP based network, the method comprising: receiving registration information by an SIP registrar via a transport network from a user and registering the user on the transport network; receiving by an MMS server in communication with the transport network a MMS request for an application service from a Multimedia Messaging Service User Agent, MMS UA, of the user via the SIP registrar; determining, by the MMS Server, to deny the said MMS request; and providing, by the MMS Server, a response corresponding to the denial of the request to the user via the transport network, that response comprising sending a message to the MMS UA containing status parameters indicating that said MMS request has been denied. receiving registration information by an SIP registrar via a transport network from a user and registering the user on the transport network; receiving by an MMS server in communication with the transport network a MMS request for an application service from a Multimedia Messaging Service User Agent, MMS UA, of the user via the SIP registrar; determining, by the MMS Server, to deny the said MMS request; and providing, by the MMS Server, a response corresponding to the denial of the request to the user via the transport network, that response comprising sending a message to the MMS UA containing status parameters indicating that said MMS request has been denied.
A decorative body made of a copper-containing platinum alloy, characterized in that the platinum alloy consists of at least 58.0 wt.% platinum, at least 35.0 wt.% copper and at least 0.06 wt.% manganese. characterized in that the platinum alloy consists of at least 58.0 wt.% platinum, at least 35.0 wt.% copper and at least 0.06 wt.% manganese.
A linkage control device for a blood gas analyser, the linkage control device comprising a rack with the following devices arranged thereon: a power unit, a rotating component provided with bosses (41, 42) and driven by the power unit, and a valve component matched with the bosses of the rotating component in a pushing manner; wherein the linkage control device also comprises a signal control unit for controlling the starting or stopping of the power unit, a sensing switch connected to the signal control unit via signals, and sensing pins (43; 44; 45; 46) arranged in pair with the sensing switch and placed on the rotating component; wherein the valve component comprises a calibration fluid valve, an air valve, a sample valve and a current valve configured for use in the blood gas analyser.
A method to be performed by at least one data processor forming at least part of a computing system, the method comprising: selecting, by the at least one data processor, a first data corresponding to a spatial position of one or more volume elements of a patient; selecting, by the at least one data processor, a second data corresponding to a set-up of a radiation therapy delivery system for delivering one or more radiation fields to the patient; triggering a determination, by the at least one data processor, of an intensity of the one or more radiation fields delivered by the radiation therapy delivery system that intersect with a volume element of the one or more volume elements of the patient; and, generating, by the at least one data processor, a three-dimensional radiation dose matrix for the patient, the three-dimensional radiation dose matrix being generated by applying a predictive model comprising a neural network that is trained, based on historical patient data, to determine a correlation between one or more geometric parameters of patient anatomy and an observed radiation dose distribution, the three-dimensional radiation dose matrix for the patient generated by the predictive model based on the first data and the second data, and the three-dimensional radiation dose matrix determining a radiation exposure for the volume element. selecting, by the at least one data processor, a first data corresponding to a spatial position of one or more volume elements of a patient; selecting, by the at least one data processor, a second data corresponding to a set-up of a radiation therapy delivery system for delivering one or more radiation fields to the patient; triggering a determination, by the at least one data processor, of an intensity of the one or more radiation fields delivered by the radiation therapy delivery system that intersect with a volume element of the one or more volume elements of the patient; and, generating, by the at least one data processor, a three-dimensional radiation dose matrix for the patient, the three-dimensional radiation dose matrix being generated by applying a predictive model comprising a neural network that is trained, based on historical patient data, to determine a correlation between one or more geometric parameters of patient anatomy and an observed radiation dose distribution, the three-dimensional radiation dose matrix for the patient generated by the predictive model based on the first data and the second data, and the three-dimensional radiation dose matrix determining a radiation exposure for the volume element.
An electrolyte for lithium secondary batteries comprising a lithium salt and a non-aqueous solvent, in which the electrolyte comprises 40 wt% to 60 wt% of an ether based solvent, 20 wt% to 30 wt% of ethylpropionata and 20 wt% to 30 wt% of ethylene carbonate with respect to a total weight of the non-aqueous solvent.
An air conditioner comprising: a blow-out port formed in the front surface of a cabinet, a panel covering the front surface; an upper shaft provided in an upper portion of the panel and a lower shaft provided in a lower portion of the panel; the panel being configured to be able to be upwardly and downwardly opened about the upper and lower shafts (22, 23); and an opening and closing mechanism, by which the panel is moved to be opened and closed according to an operating state, characterized in that the opening and closing mechanism includes a regulating section that regulates the opening direction of the panel, and that the regulating section, by holding one of the upper and lower shafts (22, 23), allows one of the upward and downward opening operation, and that the regulating section includes a pair of upper and lower holding sections which holds the upper and lower shafts (22, 23) and a driving section which operates the holding sections, and in that the holding sections includes an upper hook holding the upper shaft of the panel and a lower hook holding the lower shaft of the panel, and in that, when the panel is upwardly opened, the lower hook releases the lower shaft, and the upper hook locks and rotatably holds the upper shaft, and, when the panel is downwardly opened, the upper hook releases the upper shaft and the lower hook locks and rotatably holds the lower shaft.
Reagent vessel insert for a reagent vessel for a centrifuge and/or a pressure varying device with: an insert housing, which is formed such that the reagent vessel insert can be inserted in a reagent vessel for a centrifuge and/or for a pressure varying device; and at least one agitating element, which is arranged in at least one interior volume formed in the insert housing such that a place and/or a position of the at least one agitating element with respect to the insert housing can be changed, at least one subunit of the at least one agitating element being adjustable along an adjusting path such that at least one material that can be filled or has been filled into the at least one interior volume can be agitated; characterized in that during an adjustment along the adjusting path, at least the at least one subunit of the at least one agitating element contacts at least one holding structure, by means of which the at least one agitating element can be held in at least one semi-stable place and/or at least one semi-stable position with respect to the insert housing. an insert housing, which is formed such that the reagent vessel insert can be inserted in a reagent vessel for a centrifuge and/or for a pressure varying device; and at least one agitating element, which is arranged in at least one interior volume formed in the insert housing such that a place and/or a position of the at least one agitating element with respect to the insert housing can be changed, at least one subunit of the at least one agitating element being adjustable along an adjusting path such that at least one material that can be filled or has been filled into the at least one interior volume can be agitated;
An assembly for an aircraft propulsion system, comprising: a first drain tube (32, 32A); a second drain tube; a first container (38, 38A) between and fluidly coupling the first drain tube (32, 32A) and the second drain tube, the first container (38, 38A) configured to receive fluid from the first drain tube (32, 32A); a third drain tube; a second container (38, 38B) fluidly coupling the third drain tube to the second drain tube or a dedicated overboard drain tube, the second container configured to receive a second fluid from the third drain tube; and a gas tube fluidly coupled with the first container (38, 38A), the gas tube configured to direct gas into the first container (38, 38A) for propelling the fluid received within the first container (38, 38A) into the second drain tube; wherein the gas tube or a dedicated pressure fluid tube is further configured to direct gas into the second container for propelling the second fluid received within the second container into the second drain tube or the dedicated overboard drain tube. a first drain tube (32, 32A); a second drain tube; a first container (38, 38A) between and fluidly coupling the first drain tube (32, 32A) and the second drain tube, the first container (38, 38A) configured to receive fluid from the first drain tube (32, 32A); a third drain tube; a second container (38, 38B) fluidly coupling the third drain tube to the second drain tube or a dedicated overboard drain tube, the second container configured to receive a second fluid from the third drain tube; and a gas tube fluidly coupled with the first container (38, 38A), the gas tube configured to direct gas into the first container (38, 38A) for propelling the fluid received within the first container (38, 38A) into the second drain tube; wherein the gas tube or a dedicated pressure fluid tube is further configured to direct gas into the second container for propelling the second fluid received within the second container into the second drain tube or the dedicated overboard drain tube.
A process for the production of a composition comprising (2R,3R,4R,5S)-3,4,5-trihydroxypiperidine-2-carboxylic acid, said process comprising the steps of: (a) providing plant material from a botanical source comprising plants of the genus Cucumis; (b) extracting (2R,3R,4R,5S)-3,4,5-trihydroxypiperidine-2-carboxylic acid from said plant material; and then (c) formulating said (2R,3R,4R,5S)-3,4,5-trihydroxypiperidine-2-carboxylic acid with a cosmetically-, nutraceutically- or pharmaceutically-acceptable excipient or carrier to produce a cosmetic, nutraceutical or pharmaceutical composition. (a) providing plant material from a botanical source comprising plants of the genus Cucumis; (b) extracting (2R,3R,4R,5S)-3,4,5-trihydroxypiperidine-2-carboxylic acid from said plant material; and then (c) formulating said (2R,3R,4R,5S)-3,4,5-trihydroxypiperidine-2-carboxylic acid with a cosmetically-, nutraceutically- or pharmaceutically-acceptable excipient or carrier to produce a cosmetic, nutraceutical or pharmaceutical composition.
A medical device for treating a target site including an atrial septal wall, the medical device comprising: a frame configured to transition from a constricted configuration to an expanded configuration upon deployment thereof at the target site, the frame having proximal and distal ends (126, 122), wherein the frame comprises a proximal disc at the proximal end, a distal disc at the distal end, and a connecting segment extending between the proximal end and the distal end and connecting the proximal and distal discs (124, 120), wherein each of the proximal and distal discs (124, 120) comprises a respective plurality of lobes, wherein each lobe is defined by a peripheral strut; and at least one patch, wherein the at least one patch is coupled to at least one of the proximal and distal discs (124, 120) of the frame characterized in that the proximal disc comprises at least two layers (136, 138), each layer (136, 138) comprising a respective subset of the plurality of lobes of the proximal disc. a frame configured to transition from a constricted configuration to an expanded configuration upon deployment thereof at the target site, the frame having proximal and distal ends (126, 122), wherein the frame comprises a proximal disc at the proximal end, a distal disc at the distal end, and a connecting segment extending between the proximal end and the distal end and connecting the proximal and distal discs (124, 120), wherein each of the proximal and distal discs (124, 120) comprises a respective plurality of lobes, wherein each lobe is defined by a peripheral strut; and at least one patch, wherein the at least one patch is coupled to at least one of the proximal and distal discs (124, 120) of the frame characterized in that the proximal disc comprises at least two layers (136, 138), each layer (136, 138) comprising a respective subset of the plurality of lobes of the proximal disc.
A buckle, comprising: a pair of side frame portions; a first crossbar and a second crossbar extending between the pair of side frame portions; and a fastening portion disposed on at least one portion of the buckle for fastening a belt body in case after the belt body is pulled out of a front surface side (Fw) by inserting once the belt body to pass between the pair of side frame portions from a back surface side (Bw) and is wound around the first crossbar, the belt body is pulled out of the back surface side (Bw) again by passing between the first crossbar and the second crossbar, wherein the fastening portion comprises a clamping member rotatably supported in the side frame portions, and clamping the belt body between a free end portion and the first crossbar in a rotating position wherein the free end portion is most closely contacting with the first crossbar from the front surface side (Fw) of the buckle; and a holding device generating an elastic deformation against a rotation of the clamping member relative to the rotation of the clamping member in a direction of separating the free end portion from the first crossbar, characterized in that the holding device is a protruding portion formed in side frame portion, and abutted against one portion of the clamping member at least at a rotation time of the clamping member, two sides clamping a protruding end of the protruding portion are respectively tapered portions. a pair of side frame portions; a first crossbar and a second crossbar extending between the pair of side frame portions; and a fastening portion disposed on at least one portion of the buckle for fastening a belt body in case after the belt body is pulled out of a front surface side (Fw) by inserting once the belt body to pass between the pair of side frame portions from a back surface side (Bw) and is wound around the first crossbar, the belt body is pulled out of the back surface side (Bw) again by passing between the first crossbar and the second crossbar, wherein the fastening portion comprises a clamping member rotatably supported in the side frame portions, and clamping the belt body between a free end portion and the first crossbar in a rotating position wherein the free end portion is most closely contacting with the first crossbar from the front surface side (Fw) of the buckle; and a holding device generating an elastic deformation against a rotation of the clamping member relative to the rotation of the clamping member in a direction of separating the free end portion from the first crossbar, characterized in that the holding device is a protruding portion formed in side frame portion, and abutted against one portion of the clamping member at least at a rotation time of the clamping member, two sides clamping a protruding end of the protruding portion are respectively tapered portions.
A method for determining a presence of a reservoired hydrocarbons having a hydrocarbon seep, the method comprising the steps of: a) locating a hydrocarbon seep (S1, S2, S3, S4, S5) at a seabed location where hydrocarbon is actively flowing out of the seabed; characterised in that the method further comprises: b) determining at least two temporally spaced molecular compositions of the hydrocarbon seep (S1, S2, S3, S4, S5); c) determining a temporal variance between the at least two temporally spaced molecular compositions; d) when the temporal variance falls within a predetermined temporal tolerance, classifying the hydrocarbon seep (S1, S2, S3, S4, S5) as being indicative of the presence of a reservoired hydrocarbons; and e) assigning a unique identifier to the reservoired hydrocarbons. a) locating a hydrocarbon seep (S1, S2, S3, S4, S5) at a seabed location where hydrocarbon is actively flowing out of the seabed; b) determining at least two temporally spaced molecular compositions of the hydrocarbon seep (S1, S2, S3, S4, S5); c) determining a temporal variance between the at least two temporally spaced molecular compositions; d) when the temporal variance falls within a predetermined temporal tolerance, classifying the hydrocarbon seep (S1, S2, S3, S4, S5) as being indicative of the presence of a reservoired hydrocarbons; and e) assigning a unique identifier to the reservoired hydrocarbons.
Spin-stabilized projectile with a guide band, which is comprised of at least two annular sub-guide bands (5, 6) arranged axially one after the other, whereby each of the sub-guide bands (5, 6) is arranged in a separate groove (7, 8) of the projectile, wherein the grooves (7, 8) are dovetail grooves, characterized in that the axial separation of the adjacent grooves (7, 8) and/or the mutually facing regions (9, 10) of the sub-guide bands (5, 6) are selected so that the sub-guide bands (5, 6) are directly joined together.
An aircraft assembly comprising an aircraft base and an aircraft workpiece, and a junction where the base is adjacent the workpiece, the junction defining an outer perimeter, and a perimeter seal, characterised by: the perimeter seal comprising a linear polyurea member formed from a self-curing two-component mix of cured in place polyurea, the perimeter seal contacting the base and the workpiece thereby sealing the junction; wherein the cured polyurea has a hardness in the range of about 40 to 100 Shore A at 25°C; and wherein the linear polyurea member is capable of withstanding in use multiple thermal and pressure cycling between temperatures from about -65C to about 85C and between pressures from about 16.932kPa to about 202.65kPa while maintaining a peel strength of between about 1.751 N/mm to 7N/mm width. wherein the cured polyurea has a hardness in the range of about 40 to 100 Shore A at 25°C; and wherein the linear polyurea member is capable of withstanding in use multiple thermal and pressure cycling between temperatures from about -65C to about 85C and between pressures from about 16.932kPa to about 202.65kPa while maintaining a peel strength of between about 1.751 N/mm to 7N/mm width.
An acrylic thermoplastic resin composition comprising a two-layer or more multilayer structure polymer particle and a block copolymer, wherein: the multilayer structure polymer particle is an acrylic multilayer structure polymer particle which has, as an inner layer, at least one rubber component layer consisting of a copolymer consisting of 50 to 99.99% by mass of an acrylic acid ester monomer unit, 49.99 to 0% by mass of an additional monofunctional monomer unit, and 0.01 to 10% by mass of a polyfunctional monomer unit, and has, as an outermost layer, at least one thermoplastic resin component layer consisting of a copolymer consisting of 40 to 100% by mass of a methacrylic acid ester monomer unit and 60 to 0% by mass of an additional monomer unit and having a number-average molecular weight of 30,000 or smaller, the number-average molecular weight of the copolymer constituting the outermost layer of the multilayer structure polymer particle being determined by subjecting the multilayer structure polymer particle to solvent extraction with an organic solvent and measuring the resulting sample by GPC, wherein a mass ratio of the total amount of the rubber component layer to the total amount of the thermoplastic resin component layer (layer /layer) is 30/70 to 90/10, and an average particle size is 150 nm or smaller; the block copolymer is an acrylic block copolymer having a weight-average molecular weight of 32,000 to 300,000 measured by GPC; and a mass ratio of the multilayer structure polymer particle to the block copolymer ( /) is 1/99 to 99/1. the multilayer structure polymer particle is an acrylic multilayer structure polymer particle which has, as an inner layer, at least one rubber component layer consisting of a copolymer consisting of 50 to 99.99% by mass of an acrylic acid ester monomer unit, 49.99 to 0% by mass of an additional monofunctional monomer unit, and 0.01 to 10% by mass of a polyfunctional monomer unit, and has, as an outermost layer, at least one thermoplastic resin component layer consisting of a copolymer consisting of 40 to 100% by mass of a methacrylic acid ester monomer unit and 60 to 0% by mass of an additional monomer unit and having a number-average molecular weight of 30,000 or smaller, the number-average molecular weight of the copolymer constituting the outermost layer of the multilayer structure polymer particle being determined by subjecting the multilayer structure polymer particle to solvent extraction with an organic solvent and measuring the resulting sample by GPC, wherein a mass ratio of the total amount of the rubber component layer to the total amount of the thermoplastic resin component layer (layer /layer) is 30/70 to 90/10, and an average particle size is 150 nm or smaller; the block copolymer is an acrylic block copolymer having a weight-average molecular weight of 32,000 to 300,000 measured by GPC; and a mass ratio of the multilayer structure polymer particle to the block copolymer ( /) is 1/99 to 99/1.
A melt spinning apparatus comprising: a spinning unit comprising a plurality of spinning nozzles that spin filaments; a cooling unit that cools the filaments spun from the spinning nozzles; and a cooling air supply unit that faces the cooling unit and supplies cooling air to the cooling unit through an air-permeable partition, wherein the cooling air supply unit comprises a first cooling air supply unit at a vertically upper side and a second cooling air supply unit at a vertically lower side, divided into two stages in a vertical direction through a partition, there is a gap between an end of the partition facing the air-permeable partition and a face of a side of the air-permeable partition facing the partition, and a distance of the gap (d) is 55 mm or less and the distance of the gap (d) is 5 mm or more. a spinning unit comprising a plurality of spinning nozzles that spin filaments; a cooling unit that cools the filaments spun from the spinning nozzles; and a cooling air supply unit that faces the cooling unit and supplies cooling air to the cooling unit through an air-permeable partition, wherein the cooling air supply unit comprises a first cooling air supply unit at a vertically upper side and a second cooling air supply unit at a vertically lower side, divided into two stages in a vertical direction through a partition, there is a gap between an end of the partition facing the air-permeable partition and a face of a side of the air-permeable partition facing the partition, and a distance of the gap (d) is 55 mm or less and the distance of the gap (d) is 5 mm or more.