mhurhangee/ep-ind-claims huggingface dataset:
A method for receiving a signal by a user equipment in a wireless communication system, the method comprising: receiving a higher layer signal indicating a subframe in which a detection of downlink control information is performed; receiving the downlink control information comprising scheduling information through a physical downlink control channel within the indicated subframe, wherein the downlink control information further includes information indicating whether the downlink control information is targeted to K subframes, K being greater than 1, or targeted to one subframe, wherein the scheduling information is not applied to at least a subframe configured for a multicast-broadcast single-frequency network, MBSFN and a subframe configured to transmit system information; and when the downlink control information is targeted to the K subframes, receiving a data signal using the scheduling information in M subframes other than the at least one subframe from among the K subframes. receiving a higher layer signal indicating a subframe in which a detection of downlink control information is performed; receiving the downlink control information comprising scheduling information through a physical downlink control channel within the indicated subframe, wherein the downlink control information further includes information indicating whether the downlink control information is targeted to K subframes, K being greater than 1, or targeted to one subframe, wherein the scheduling information is not applied to at least a subframe configured for a multicast-broadcast single-frequency network, MBSFN and a subframe configured to transmit system information; and when the downlink control information is targeted to the K subframes, receiving a data signal using the scheduling information in M subframes other than the at least one subframe from among the K subframes.
Salt substitute comprising between 25% and 96% of sodium chloride by total weight of the salt substitute excluding additives, from 0 to 4% of additive(s) by total weight of the salt substitute, and a remaining composition comprising, by total weight of this remaining composition: - 72% to 87% of potassium chloride, - 10% to 20% of magnesium sulfate, and - 3% to 8% of calcium sulfate. - 72% to 87% of potassium chloride, - 10% to 20% of magnesium sulfate, and - 3% to 8% of calcium sulfate.
A modular load carrying apparatus for a rotary wing aircraft, comprising: a tube that has a first predetermined outer diameter and first and second axial ends (211, 212); a first cap that is located inside the tube at the first axial end and adapted for being connected with the rotary wing aircraft; a second cap that is located inside the tube at the second axial end and comprises a protrusion that protrudes from the second axial end and has a second predetermined outer diameter that is greater than the first predetermined outer diameter; a carrier star that is installed at the second axial end of the tube and comprises a plurality of docking devices, wherein each docking device of the plurality of docking devices is adapted for rotatably receiving at least one of a seat or a carrier beam such that the at least one of a seat or a carrier beam is folded against the tube in a stowed position or unfolded from the tube in a deployed position; and a tension rod that is spanned between the first cap and the second cap and transfers tension loads from the carrier star via the second cap towards the first cap. a tube that has a first predetermined outer diameter and first and second axial ends (211, 212); a first cap that is located inside the tube at the first axial end and adapted for being connected with the rotary wing aircraft; a second cap that is located inside the tube at the second axial end and comprises a protrusion that protrudes from the second axial end and has a second predetermined outer diameter that is greater than the first predetermined outer diameter; a carrier star that is installed at the second axial end of the tube and comprises a plurality of docking devices, wherein each docking device of the plurality of docking devices is adapted for rotatably receiving at least one of a seat or a carrier beam such that the at least one of a seat or a carrier beam is folded against the tube in a stowed position or unfolded from the tube in a deployed position; and a tension rod that is spanned between the first cap and the second cap and transfers tension loads from the carrier star via the second cap towards the first cap.
A dual focal length optical system comprising: a first optical system positioned along an optical axis, the first optical system including an optical structure formed from a solid refractive optical material, the optical structure having an object side surface and an image side surface, the object side surface and the image side surface including a refractive surface portion and a reflective surface portion (225, 235), said first optical system having a first focal length and a first image sensor positioned at a first image plane; and a second optical system positioned on the same optical axis, the second optical system including one or more lenses located within the optical structure and having a second image sensor positioned at a second image plane located within the optical structure, the second optical system having a second focal length, the first focal length being longer than the second focal length wherein the first optical system forms an image on the first image sensor using light incident on an outer region of the object side surface and the second optical system simultaneously forms an image on the second image sensor using light incident on a central region of the object side surface. a first optical system positioned along an optical axis, the first optical system including an optical structure formed from a solid refractive optical material, the optical structure having an object side surface and an image side surface, the object side surface and the image side surface including a refractive surface portion and a reflective surface portion (225, 235), said first optical system having a first focal length and a first image sensor positioned at a first image plane; and a second optical system positioned on the same optical axis, the second optical system including one or more lenses located within the optical structure and having a second image sensor positioned at a second image plane located within the optical structure, the second optical system having a second focal length, the first focal length being longer than the second focal length wherein the first optical system forms an image on the first image sensor using light incident on an outer region of the object side surface and the second optical system simultaneously forms an image on the second image sensor using light incident on a central region of the object side surface.
A fuel cell system including a solid oxide fuel cell configured to receive a supply of an anode gas and a cathode gas to generate electric power, the fuel cell system comprising: an anode discharge passage through which an anode off-gas discharged from the fuel cell flows; a cathode discharge passage through which a cathode off-gas discharged from the fuel cell flows; a joining portion where the anode discharge passage and the cathode discharge passage join; a gas supply unit (73A, 28) configured to supply a fuel gas using a fuel stored in a fuel tank into the anode discharge passage during a system stop; and a temperature-sensing unit configured to detect or estimate a temperature of the fuel cell, wherein the gas supply unit (73A, 28) is configured such that a fuel gas is supplied to the anode discharge passage when the temperature of the fuel cell is higher than a reference temperature at which an anode electrode of the fuel cell is not oxidized during the system stop. an anode discharge passage through which an anode off-gas discharged from the fuel cell flows; a cathode discharge passage through which a cathode off-gas discharged from the fuel cell flows; a joining portion where the anode discharge passage and the cathode discharge passage join; a gas supply unit (73A, 28) configured to supply a fuel gas using a fuel stored in a fuel tank into the anode discharge passage during a system stop; and a temperature-sensing unit configured to detect or estimate a temperature of the fuel cell, wherein the gas supply unit (73A, 28) is configured such that a fuel gas is supplied to the anode discharge passage when the temperature of the fuel cell is higher than a reference temperature at which an anode electrode of the fuel cell is not oxidized during the system stop.
A member for a wearable device, comprising: (i) a resin base material; - wherein the resin base material has a concave portion, the electronic component is disposed on the concave portion, and the concave portion and the electronic component are covered with the protecting layer from there above, (ii) an electronic component; and (iii) a protecting layer which protects the electronic component, and which is formed from a curable composition comprising - at least one cross-linking agent selected from organosilicon compounds having, each bonded to Si, at least two -O-R g3 wherein R g3 each independently is H or a monovalent organic group, and organosilicon compounds having two or more H each bonded to Si (Si-H) in one molecule; and - a perfluoropolyether group-containing compound selected from perfluoropolyether group-containing silane compounds and perfluoropolyether group-containing compounds having a carbon-carbon double bond at a molecular end. (i) a resin base material; - wherein the resin base material has a concave portion, the electronic component is disposed on the concave portion, and the concave portion and the electronic component are covered with the protecting layer from there above, - wherein the resin base material has a concave portion, the electronic component is disposed on the concave portion, and the concave portion and the electronic component are covered with the protecting layer from there above, (ii) an electronic component; and (iii) a protecting layer which protects the electronic component, and which is formed from a curable composition comprising - at least one cross-linking agent selected from organosilicon compounds having, each bonded to Si, at least two -O-R g3 wherein R g3 each independently is H or a monovalent organic group, and organosilicon compounds having two or more H each bonded to Si (Si-H) in one molecule; and - a perfluoropolyether group-containing compound selected from perfluoropolyether group-containing silane compounds and perfluoropolyether group-containing compounds having a carbon-carbon double bond at a molecular end. - at least one cross-linking agent selected from organosilicon compounds having, each bonded to Si, at least two -O-R g3 wherein R g3 each independently is H or a monovalent organic group, and organosilicon compounds having two or more H each bonded to Si (Si-H) in one molecule; and - a perfluoropolyether group-containing compound selected from perfluoropolyether group-containing silane compounds and perfluoropolyether group-containing compounds having a carbon-carbon double bond at a molecular end.
A bicycle seat, comprising: a body comprising a support portion and a seat cover, wherein a deformation space is located between the support portion and the seat cover, characterized in that a plurality of filler particles fills the deformation space, wherein the plurality of filler particles is restricted in the deformation space and is arranged such that the particles in the deformation space are sliding and rolling under pressure. a body comprising a support portion and a seat cover, wherein a deformation space is located between the support portion and the seat cover, characterized in that a plurality of filler particles fills the deformation space, wherein the plurality of filler particles is restricted in the deformation space and is arranged such that the particles in the deformation space are sliding and rolling under pressure.
Two-layer road marking or ground coating having a lower layer which is a cured 2-pack (meth)acrylate-based reactive resin formulation containing, prior to curing, in one or both packs, at least 0.3% by weight of crosslinker, at least 4% by weight of (meth)acrylate monomers, at least 2% by weight of prepolymers and optional further additives, characterized in that the second upper layer is a cured reactive resin seal composed of up to 50% by weight of pigments, fillers and/or additives and of at least 50% by weight of a cured (meth)acrylate resin consisting in turn to an extent of at least 50% by weight of repeat units based on (meth)acrylates and having a glass transition temperature T g (DIN EN ISO 11357-1) of at least 60°C.
A turbine rotor assembly comprising a turbine rotor and a plurality of circumferentially spaced radially outwardly extending turbine rotor blades, the turbine rotor having a hub, a rim and a plurality of circumferentially spaced slots provided in the rim of the turbine rotor, each turbine rotor blade having a root, the root of each turbine rotor blade being arranged in a corresponding one of the slots in the rim of the turbine rotor, each turbine rotor blade being hollow, each turbine rotor blade being provided with at least one internal cooling passage for a coolant, each turbine rotor blade having at least one aperture arranged to supply coolant to the at least one internal cooling passage in the turbine blade, at least one of the slots having a thermally insulating material adjacent the radially inner surface of the slot, at least one of the slots having a chocking device, the at least one chocking device abutting a radially inner surface of the slot, the chocking device abutting a radially inner surface of the root of the corresponding turbine rotor blade, the chocking device comprising said thermally insulating material 54, wherein the thermally insulating material reduces the temperature gradient between a region of the turbine rotor adjacent the at least one slot and the hub of the turbine rotor, characterised in that the chocking device forms a space between the thermally insulating material and the radially inner surface of the root of the corresponding turbine rotor blade r.
Method comprising two modes for generating underground energy using water from a water mass above an underground recipient, comprising the following steps: in a hydroelectric mode: - injecting water into an inlet of a first shaft extending from the water mass to the underground recipient and passing the water through a turbine, where the turbine drives an electrical generator, - measuring back pressure from the recipient, - switching to a thermal mode when the back pressure has built up to a defined back pressure level, in the thermal mode: - injecting water into the first shaft, forcing water in the recipient to exit through a second shaft extending from the recipient; - extracting thermal energy from the water transported via the second shaft, by at least one of the following: i) using the water directly for heating purposes, and ii) generating electrical power in a heat engine. in a hydroelectric mode: - injecting water into an inlet of a first shaft extending from the water mass to the underground recipient and passing the water through a turbine, where the turbine drives an electrical generator, - measuring back pressure from the recipient, - switching to a thermal mode when the back pressure has built up to a defined back pressure level, - injecting water into an inlet of a first shaft extending from the water mass to the underground recipient and passing the water through a turbine, where the turbine drives an electrical generator, - measuring back pressure from the recipient, - switching to a thermal mode when the back pressure has built up to a defined back pressure level, in the thermal mode: - injecting water into the first shaft, forcing water in the recipient to exit through a second shaft extending from the recipient; - extracting thermal energy from the water transported via the second shaft, by at least one of the following: i) using the water directly for heating purposes, and ii) generating electrical power in a heat engine. - injecting water into the first shaft, forcing water in the recipient to exit through a second shaft extending from the recipient; - extracting thermal energy from the water transported via the second shaft, by at least one of the following: i) using the water directly for heating purposes, and ii) generating electrical power in a heat engine.
A cell stack comprising a plurality of single cells (9, 10, 11, 12), wherein each single cell (9, 10, 11, 12) comprises a membrane electrode assembly having a cathode, an anode, and an interposed membrane, as well as an anode gas diffusion layer arranged on the exposed side of the anode having a first thickness gradient in the transverse machine direction (y) or a sintered titanium component and a cathode gas diffusion layer arranged on the exposed side of the cathode having a second thickness gradient in the transverse machine direction (y), wherein a) in a single cell (9, 10, 11, 12), the anode gas diffusion layer and the cathode gas diffusion layer are arranged in relation to one another such that the first thickness gradient of the anode gas diffusion layer and the second thickness gradient of the cathode gas diffusion layer run opposite to one another or b) in two or more single cells (9, 10, 11, 12), the anode gas diffusion layers are arranged in relation to one another such that an overall thickness gradient of these anode gas diffusion layers is minimized and/or wherein in two or more single cells (9, 10, 11, 12), the cathode gas diffusion layers are arranged in relation to one another such that an overall thickness gradient of these cathode gas diffusion layers is minimized. a) in a single cell (9, 10, 11, 12), the anode gas diffusion layer and the cathode gas diffusion layer are arranged in relation to one another such that the first thickness gradient of the anode gas diffusion layer and the second thickness gradient of the cathode gas diffusion layer run opposite to one another or b) in two or more single cells (9, 10, 11, 12), the anode gas diffusion layers are arranged in relation to one another such that an overall thickness gradient of these anode gas diffusion layers is minimized and/or wherein in two or more single cells (9, 10, 11, 12), the cathode gas diffusion layers are arranged in relation to one another such that an overall thickness gradient of these cathode gas diffusion layers is minimized.
A method for detecting at least one haemoplasma species within the group of haemoplasmas of the genus Mycoplasma in a biological sample, said method comprising the steps of: i) treating said sample to release haemoplasma nucleic acid in the sample, ii) amplifying a segment of a 16S rRNA gene by real-time PCR (qPCR) using an oligonucleotide primer pair, said oligonucleotide primer pair consisting of a forward primer comprising at least 10 consecutive bases of SEQ ID 1 and a reverse primer comprising at least 10 consecutive bases of SEQ ID 2, thereby producing an amplification product, and iii) detecting the amplification product by means producing a detection signal correlating with the amount of the amplification product which is indicative of a haemoplasma species within the genus Mycoplasma. i) treating said sample to release haemoplasma nucleic acid in the sample, ii) amplifying a segment of a 16S rRNA gene by real-time PCR (qPCR) using an oligonucleotide primer pair, said oligonucleotide primer pair consisting of a forward primer comprising at least 10 consecutive bases of SEQ ID 1 and a reverse primer comprising at least 10 consecutive bases of SEQ ID 2, thereby producing an amplification product, and iii) detecting the amplification product by means producing a detection signal correlating with the amount of the amplification product which is indicative of a haemoplasma species within the genus Mycoplasma.
A pharmaceutical composition comprising atropisomers of the formulae: wherein: ------ represents a carbon-carbon single bond or a carbon-carbon double bond; the bold lines indicate that the bolded atoms, and the groups attached thereto, are sterically restricted so as to exist above the plane defined by the macrocycle ring; X 2, X 4, X 6 and X 8 are fluorine; X 1, X 3, X 5 and X 7 are halogens (F, Cl, Br) or hydrogen; R 1, R 2, R 3 and R 4 are independently -OH, -OR or -SO 2 R", where R" are each independently chosen from -Cl, -OH, -aminoacid, -OR, -NHR or -NR 2, where R are alkyl of 1 to 12 carbon atoms or R 2 represents cycloalkyl with 2 to 12 carbon atoms; R 5, R 6, R 7 and R 8 are independently H, -OH, -OR, -Cl, or -NHR where R are alkyl of 1 to 12 carbon atoms; or pharmaceutically acceptable salts thereof; wherein the relative amount of said atropisomers or their pharmaceutically acceptable salts is more than 70% of the total of atropisomers in the referred pharmaceutical composition. ------ represents a carbon-carbon single bond or a carbon-carbon double bond; the bold lines indicate that the bolded atoms, and the groups attached thereto, are sterically restricted so as to exist above the plane defined by the macrocycle ring; X 2, X 4, X 6 and X 8 are fluorine; X 1, X 3, X 5 and X 7 are halogens (F, Cl, Br) or hydrogen; R 1, R 2, R 3 and R 4 are independently -OH, -OR or -SO 2 R", where R" are each independently chosen from -Cl, -OH, -aminoacid, -OR, -NHR or -NR 2, where R are alkyl of 1 to 12 carbon atoms or R 2 represents cycloalkyl with 2 to 12 carbon atoms; R 5, R 6, R 7 and R 8 are independently H, -OH, -OR, -Cl, or -NHR where R are alkyl of 1 to 12 carbon atoms; or pharmaceutically acceptable salts thereof; wherein the relative amount of said atropisomers or their pharmaceutically acceptable salts is more than 70% of the total of atropisomers in the referred pharmaceutical composition.
A method for location determination in beamformed communication, comprising: transmitting (320; 1505) from a first base station a first beamformed reference signal wherein the first beamformed reference signal and additional beamformed reference signals that are transmitted at different times in accordance to a coordinated time offset schedule by additional base stations are according to beam sweep cycles of neighboring base stations coordinated to minimize collision between the beams using the coordinated time offset schedule; receiving (330; 1510) a first measurement report from a user equipment, UE, the first measurement report indicating a measurement parameter associated with the first beamformed reference signal; receiving (345; 1515) additional measurement reports from the UE for additional base stations, the additional measurement reports each indicating measurement parameters associated with the additional beamformed reference signals; and identifying (350; 1520) a location of the UE based at least in part on the first measurement report and the additional measurement reports. transmitting (320; 1505) from a first base station a first beamformed reference signal wherein the first beamformed reference signal and additional beamformed reference signals that are transmitted at different times in accordance to a coordinated time offset schedule by additional base stations are according to beam sweep cycles of neighboring base stations coordinated to minimize collision between the beams using the coordinated time offset schedule; receiving (330; 1510) a first measurement report from a user equipment, UE, the first measurement report indicating a measurement parameter associated with the first beamformed reference signal; receiving (345; 1515) additional measurement reports from the UE for additional base stations, the additional measurement reports each indicating measurement parameters associated with the additional beamformed reference signals; and identifying (350; 1520) a location of the UE based at least in part on the first measurement report and the additional measurement reports.