mhurhangee/ep-ind-claims huggingface dataset:
A gastric-retention type sustained-release formulation comprising: a sustained-release granulated material, which comprises granules comprising metformin or a pharmaceutically acceptable salt thereof and a swellable polymer, and a coating layer containing a water-insoluble polymer applied on the surface of the granules; and a superdisintegrant, wherein the superdisintegrant is present as an extragranular component mixed with the sustained-release granulated material, wherein the superdisintegrant is at least one selected from the group consisting of croscarmellose sodium and crospovidone, and wherein the superdisintegrant is comprised in the amount from 0.5 wt% to 5 wt% based on the total amount of the formulation. a sustained-release granulated material, which comprises granules comprising metformin or a pharmaceutically acceptable salt thereof and a swellable polymer, and a coating layer containing a water-insoluble polymer applied on the surface of the granules; and a superdisintegrant, wherein the superdisintegrant is present as an extragranular component mixed with the sustained-release granulated material, wherein the superdisintegrant is at least one selected from the group consisting of croscarmellose sodium and crospovidone, and wherein the superdisintegrant is comprised in the amount from 0.5 wt% to 5 wt% based on the total amount of the formulation.
A method for determining a time-domain resource allocation, the method being performed by a system comprising a user equipment, UE, and a base station, the UE being wirelessly connectable to the base station, the method comprising: the UE receiving from the base station a downlink control information, DCI, that schedules a downlink transmission from the base station to the UE; the UE detecting a Radio Network Temporary Identifier, RNTI, used in the base station's scheduling of the downlink transmission; the UE selecting a time-domain resource allocation table from multiple different time-domain resource allocation tables based on the detected RNTI, wherein each of the different time domain resource allocation tables is defined by a plurality of entries that specify different combinations of starting orthogonal frequency division multiplexing, OFDM, symbol and duration in OFDM symbols for a time-domain resource allocation; and the UE determining a time-domain resource allocation for the downlink transmission based on a time-domain resource allocation field in the DCI, the time-domain resource allocation field indicating an entry within the selected time-domain resource allocation table. the UE receiving from the base station a downlink control information, DCI, that schedules a downlink transmission from the base station to the UE; the UE detecting a Radio Network Temporary Identifier, RNTI, used in the base station's scheduling of the downlink transmission; the UE selecting a time-domain resource allocation table from multiple different time-domain resource allocation tables based on the detected RNTI, wherein each of the different time domain resource allocation tables is defined by a plurality of entries that specify different combinations of starting orthogonal frequency division multiplexing, OFDM, symbol and duration in OFDM symbols for a time-domain resource allocation; and the UE determining a time-domain resource allocation for the downlink transmission based on a time-domain resource allocation field in the DCI, the time-domain resource allocation field indicating an entry within the selected time-domain resource allocation table.
A metal anode (1, 4) for use in a metal/air electrochemical cell, said anode being a spatial body bounded by a surface consisting of two opposite parallel bases and four lateral sides lying in planes which are essentially perpendicular to the bases, characterized in that a resilient polymer is applied on said lateral sides of the anode, to protect said lateral sides from being oxidized by an alkaline electrolyte, wherein the resilient polymer is a rubber or an elastomer.
An apparatus, comprising: a charged particle beam generator configured to project simultaneously at least one non-astigmatic charged particle beam and at least one astigmatic charged particle beam onto locations on a surface of a specimen, thereby causing released electrons to be emitted from the locations; an imaging detector configured to receive the released electrons from the locations and to form images of the locations from the released electrons; and an aberrating element which is positioned before the imaging detector and which is configured to produce an aberration in the images; and a processor, coupled to the imaging detector, configured to adjust a focus of the at least one non-astigmatic charged particle beam in response to at least one element of a group of elements comprising the aberration and a subset of the images, the subset being produced by the at least one astigmatic charged particle beam. a charged particle beam generator configured to project simultaneously at least one non-astigmatic charged particle beam and at least one astigmatic charged particle beam onto locations on a surface of a specimen, thereby causing released electrons to be emitted from the locations; an imaging detector configured to receive the released electrons from the locations and to form images of the locations from the released electrons; and an aberrating element which is positioned before the imaging detector and which is configured to produce an aberration in the images; and a processor, coupled to the imaging detector, configured to adjust a focus of the at least one non-astigmatic charged particle beam in response to at least one element of a group of elements comprising the aberration and a subset of the images, the subset being produced by the at least one astigmatic charged particle beam.
Method for assisting the piloting of a rotorcraft comprising at least two engines (2, 3) which, in the absence of failure, are capable of transmitting engine torque to at least one main rotor at least providing lift to keep said rotorcraft in the air, said rotorcraft comprising aerodynamic members which allow the piloting of said rotorcraft, said assistance method comprising the following steps: • periodically determining a current position of said rotorcraft, • making a first periodic comparison between said current position and a decision point (TDP, LDP), said first periodic comparison making it possible to determine that said current position of said rotorcraft has a current height which is less than a predetermined height of said decision point (TDP, LDP), • identifying an engine failure in at least one engine (2, 3) of the at least two engines (2, 3); • making a second periodic comparison between said current position of said rotorcraft and a touchdown point, • periodically determining an emergency landing profile, said emergency landing profile being generated at least depending on a result of said second periodic comparison and on a minimum speed of rotation (NRmin) of said at least main rotor to be observed, and • periodically generating control orders to control the aerodynamic members and pilot said rotorcraft according to said emergency landing profile, said periodic generation of control orders being implemented when, on the one hand, said current position of said rotorcraft has a current height which is less than said predetermined height of said decision point (TDP, LDP) and, on the other hand, an engine failure is identified, characterized in that said emergency landing profile is generated depending on the predetermined rate of sink of said rotorcraft to be observed. • periodically determining a current position of said rotorcraft, • making a first periodic comparison between said current position and a decision point (TDP, LDP), said first periodic comparison making it possible to determine that said current position of said rotorcraft has a current height which is less than a predetermined height of said decision point (TDP, LDP), • identifying an engine failure in at least one engine (2, 3) of the at least two engines (2, 3); • making a second periodic comparison between said current position of said rotorcraft and a touchdown point, • periodically determining an emergency landing profile, said emergency landing profile being generated at least depending on a result of said second periodic comparison and on a minimum speed of rotation (NRmin) of said at least main rotor to be observed, and • periodically generating control orders to control the aerodynamic members and pilot said rotorcraft according to said emergency landing profile, said periodic generation of control orders being implemented when, on the one hand, said current position of said rotorcraft has a current height which is less than said predetermined height of said decision point (TDP, LDP) and, on the other hand, an engine failure is identified,
A catalyst system for dewaxing of a hydrocarbon feedstock comprising at least two catalytic sections, the first section comprising a first dewaxing catalyst and a subsequent section comprising a second dewaxing catalyst, wherein the first dewaxing catalyst is a ZSM-12 zeolite based catalyst and the second dewaxing catalyst is a EU-2 and/or ZSM-48 zeolite based catalyst, wherein said ZSM-12 zeolite is present in said first dewaxing catalyst composition in an amount of at least 10 wt. % and at most 70 wt. % and said first dewaxing catalyst composition further comprises a binder in an amount of at least 30 wt. % and no more than 90 wt. %, with such wt. % being based on the dry weight of said composition, and wherein silica is the binder in the first dewaxing catalyst and the second dewaxing catalyst.
A method of making a fuel cell gas diffusion layer comprising the steps: a) providing a carbon fiber construction having an upper surface; b) coating at least said upper surface of said carbon fiber construction with a hydrophobic layer composition which comprises a fluoropolymer; c) exposing said upper surface to at least one plasma so as to generate a hydrophilic surface layer having a thickness of no more than 0.5 micron, wherein said plasma is of species including at least one selected from the group consisting of: oxygen, nitrogen, nitrogen dioxide, nitrous oxide, ammonia and sulfur dioxide, wherein said step c) comprises steps d) and e): d) exposing said upper surface to a first plasma; and subsequently e) exposing said upper surface to a second plasma; wherein said first plasma is of species including at least one selected from the group consisting of: silanes, siloxanes and organometallics, and wherein said second plasma is of species including at least one selected from the group consisting of: oxygen, nitrogen, nitrogen dioxide, nitrous oxide, ammonia and sulfur dioxide. a) providing a carbon fiber construction having an upper surface; b) coating at least said upper surface of said carbon fiber construction with a hydrophobic layer composition which comprises a fluoropolymer; c) exposing said upper surface to at least one plasma so as to generate a hydrophilic surface layer having a thickness of no more than 0.5 micron, wherein said plasma is of species including at least one selected from the group consisting of: oxygen, nitrogen, nitrogen dioxide, nitrous oxide, ammonia and sulfur dioxide, wherein said step c) comprises steps d) and e): d) exposing said upper surface to a first plasma; and subsequently e) exposing said upper surface to a second plasma;
A golf club head comprising: a heel; a toe; a top portion; a sole portion; a striking face extending from the top portion to the sole portion, the striking face providing a contact area for engaging a golf ball; a rear face opposite the striking face, the rear face defining a rear cavity; an interchangeable bridge member (34, 84) extending across the rear cavity, the interchangeable bridge member comprising: a first portion (300, 502) adjacent the heel; a second portion (302, 504) adjacent the toe; and a third portion (304, 506) connected to the first portion and the second portion between the heel and the toe, the interchangeable bridge member varying a center of gravity of the golf club head with respect to the striking face, wherein the third portion is offset from the first portion and the second portion in a direction towards the top portion or the sole portion. a heel; a toe; a top portion; a sole portion; a striking face extending from the top portion to the sole portion, the striking face providing a contact area for engaging a golf ball; a rear face opposite the striking face, the rear face defining a rear cavity; an interchangeable bridge member (34, 84) extending across the rear cavity, the interchangeable bridge member comprising: a first portion (300, 502) adjacent the heel; a second portion (302, 504) adjacent the toe; and a third portion (304, 506) connected to the first portion and the second portion between the heel and the toe, the interchangeable bridge member varying a center of gravity of the golf club head with respect to the striking face, wherein the third portion is offset from the first portion and the second portion in a direction towards the top portion or the sole portion. a first portion (300, 502) adjacent the heel; a second portion (302, 504) adjacent the toe; and a third portion (304, 506) connected to the first portion and the second portion between the heel and the toe, the interchangeable bridge member varying a center of gravity of the golf club head with respect to the striking face, wherein the third portion is offset from the first portion and the second portion in a direction towards the top portion or the sole portion.
A hinge arrangement comprising at least two hinge members (2, 3) connected with each other in a hinged manner, wherein at least one hinge member comprises a sleeve section provided with two radially internal, substantially longitudinal protrusions or recesses extending substantially in the plane passing through the axis of said sleeve section, a pivot pin embedded in said sleeve section and provided with a threaded through adjustment hole substantially perpendicular to the pivot pin axis, two jaw members adjacent to said pivot pin and provided with radially external recesses or protrusions cooperating with said internal protrusions or recesses of said sleeve section, an adjusting screw disposed in said adjustment hole between said jaw members, resting on inner walls of said sleeve section and provided with torque application means accessible from the outside of said sleeve section, a locking screw pressing from the outside one jaw member to the pivot pin after adjusting the hinge arrangement and provided with torque application means accessible from the outside of said sleeve section, wherein radial abutment means are located between said pivot pin and said jaw members, wherein said adjusting screw is inserted into the adjustment hole between edge recesses of said jaw members, and wherein the axes of said adjusting screw and said locking screw are substantially coplanar, characterized in that said radial abutment means are located in the surroundings of the locking screw and are in the form of knurling of the pivot pin, wherein said pivot pin and said jaw members are made of metal, with the hardness of said pivot pin being higher than the hardness of said jaw members, wherein said jaw members are provided with cylindrical, radially ribbed internal surfaces adapted to the external curvature of the pivot pin. said radial abutment means are located in the surroundings of the locking screw and are in the form of knurling of the pivot pin, wherein said pivot pin and said jaw members are made of metal, with the hardness of said pivot pin being higher than the hardness of said jaw members, wherein said jaw members are provided with cylindrical, radially ribbed internal surfaces adapted to the external curvature of the pivot pin.
A composition comprising an ethylene/CO interpolymer, formed from a high pressure, free-radical polymerization, and wherein the ethylene/CO interpolymer has the following properties: a) a CO content from "greater than 0" weight percent to less than, or equal to, 10 weight percent CO (carbon monoxide), based on the weight of the interpolymer; and b) a melting point, Tm, in °C that meets the following relationship: Tm ° C ≤ 601.4 ∗ Density in g / cc − 452.5 ° C. a) a CO content from "greater than 0" weight percent to less than, or equal to, 10 weight percent CO (carbon monoxide), based on the weight of the interpolymer; and b) a melting point, Tm, in °C that meets the following relationship: Tm ° C ≤ 601.4 ∗ Density in g / cc − 452.5 ° C.
A repair device for a torn tissue, comprising: a) a tissue attachment unit; b) a clamp unit configured to hold a tissue attachment element; and c) optionally binding means and/or an anchor, characterized in that: - said tissue attachment unit comprises: (i) said tissue attachment element comprising an attachment head configured for securing said repair device to said torn tissue; and (ii) an optional elongation tail; - said clamp unit is separated from said tissue attachment unit, and comprises: (i) a base configured for acting as a positioning platform; (ii) side walls configured for securing the torn tissue in place and determining an attachment area; and (iii) a setter configured for holding the attachment element and optionally setting the angle of its insertion into said tissue; and - said binding means and/or an anchor is associated with said elongation tail, if present. a) a tissue attachment unit; b) a clamp unit configured to hold a tissue attachment element; and c) optionally binding means and/or an anchor, - said tissue attachment unit comprises: (i) said tissue attachment element comprising an attachment head configured for securing said repair device to said torn tissue; and (ii) an optional elongation tail; - said clamp unit is separated from said tissue attachment unit, and comprises: (i) a base configured for acting as a positioning platform; (ii) side walls configured for securing the torn tissue in place and determining an attachment area; and (iii) a setter configured for holding the attachment element and optionally setting the angle of its insertion into said tissue; and - said binding means and/or an anchor is associated with said elongation tail, if present.
An extraction method for extracting hydrocarbons by means of enhanced oil recovery in a subterranean formation including: i. the injection of a composition comprising: a. one or more surfactant(s) selected from among cationic surfactants and/or non-ionic surfactants; and b. one or more polymer(s) selected from among the cationic polymers and/or non-ionic polymers; and ii. the displacement of hydrocarbons by the injected composition; and iii. the production of hydrocarbons. i. the injection of a composition comprising: a. one or more surfactant(s) selected from among cationic surfactants and/or non-ionic surfactants; and b. one or more polymer(s) selected from among the cationic polymers and/or non-ionic polymers; and a. one or more surfactant(s) selected from among cationic surfactants and/or non-ionic surfactants; and b. one or more polymer(s) selected from among the cationic polymers and/or non-ionic polymers; and ii. the displacement of hydrocarbons by the injected composition; and iii. the production of hydrocarbons.
An agent for use in a method of inhibiting metastasis of a cancer in a subject, comprising administering to a subject in need thereof a composition comprising the agent, wherein the agent selectively inhibits the binding of p68 RNA helicase to calmodulin (CaM) in cancer cells and wherein the agent is a peptide or peptidomimetic containing the IQ motif of p68; or a variant thereof that binds human CaM, wherein the variant is a peptide comprising the amino acid sequence FVSAGIQTSFRTGNPTG (SEQ ID NO:7) or the amino acid sequence FVSAGIQTSFRTGNPTGAYG (SEQ ID NO:4); or an antibody that selectively binds the IQ motif of p68 RNA helicase.
Dishwasher, in particular a household dishwasher, comprising a washing container that provides a washing chamber and is used to receive washware to be cleaned, and comprising a water storage tank arranged next to the washing container, and comprising a corrugated pipeline that is guided through the water storage tank at least in portions and is fluidically connected to the washing container, characterised in that the water storage tank is arranged on the washing container, with an air duct being arranged therebetween that extends in the height direction of the washing container and is connected on the inlet side to an air outlet duct of a fresh air blower, the air duct being delimited on the water storage tank side by a deep groove provided by the water storage tank.
An adhesive composition comprising: a main agent containing at least one epoxy resin selected from a bisphenol A epoxy resin, a bisphenol F epoxy resin, and a phenol novolac epoxy resin, and an acrylic rubber; a curing agent containing xylylene diamine; a filler containing silica; and an organic ion exchanger containing at least one compound selected from the group consisting of styrene, divinyl benzene, and derivatives thereof. a main agent containing at least one epoxy resin selected from a bisphenol A epoxy resin, a bisphenol F epoxy resin, and a phenol novolac epoxy resin, and an acrylic rubber; a curing agent containing xylylene diamine; a filler containing silica; and an organic ion exchanger containing at least one compound selected from the group consisting of styrene, divinyl benzene, and derivatives thereof.
An aluminosilicate molecular sieve composition comprising at least one intergrown phase comprising an ERI framework type molecular sieve and an LEV framework type molecular sieve, wherein the molecular sieve composition has a SiO 2 /Al 2 O 3 mole ratio of from 10 to 25, and wherein the ERI framework type molecular sieve is present in the at least one intergrown phase in a proportion to the LEV framework type molecular sieve of from 5% to 95%, as determined by DIFFaX analysis.