mhurhangee/ep-ind-claims huggingface dataset:
Sliding door system with a sliding door; which sliding door is displaceable along a running rail relative to a stationarily arranged activation member up to a closing position; which sliding door comprises a door leaf; which sliding door comprises at least two carriages, - which each comprise a carriage body and running elements, - which each are connected to the door leaf, and - which each are held in the running rail displaceable in parallel to the longitudinal axis of the running rail; which sliding door is equipped with an activatable sealing device, which comprises an extractable sealing strip and an actuating element; which sliding door is equipped with a transmission device, which comprises a transmission element; and wherein the activation member and the transmission device are arranged such, that, when the sliding door enters into the closing position, a force is transmissible from the activation part via the transmission element to the actuating element in order to eject the sealing strip, characterized in that a stationarily arranged buffer device is provided, which is provided to stop the sliding door in the closed position and which comprises the activation part and, that the buffer device comprises a buffer body and that the activation member is connected or connectable to the buffer body or is an integral part of the buffer body. which sliding door is displaceable along a running rail relative to a stationarily arranged activation member up to a closing position; which sliding door comprises a door leaf; which sliding door comprises at least two carriages, - which each comprise a carriage body and running elements, - which each are connected to the door leaf, and - which each are held in the running rail displaceable in parallel to the longitudinal axis of the running rail; - which each comprise a carriage body and running elements, - which each are connected to the door leaf, and - which each are held in the running rail displaceable in parallel to the longitudinal axis of the running rail; which sliding door is equipped with an activatable sealing device, which comprises an extractable sealing strip and an actuating element; which sliding door is equipped with a transmission device, which comprises a transmission element; and wherein the activation member and the transmission device are arranged such, that, when the sliding door enters into the closing position, a force is transmissible from the activation part via the transmission element to the actuating element in order to eject the sealing strip, characterized in that a stationarily arranged buffer device is provided, which is provided to stop the sliding door in the closed position and which comprises the activation part and, that the buffer device comprises a buffer body and that the activation member is connected or connectable to the buffer body or is an integral part of the buffer body.
A hot-pressed member comprising: a steel chemical composition containing, by mass%, C: 0.28 % or more and less than 0.42 %, Si: 1.5 % or less, Mn: 1.0 % or more and 2.4 % or less, P: 0.05% or less, S: 0.005 % or less, Al: 0.01 % or more and 0.50 % or less, N: 0.005 % or less, Nb: 0.005 % or more and 0.15 % or less, Ti: 0.005 % or more and 0.15 % or less, B: 0.0005 % or more and 0.0050 % or less, and optionally at least one selected from the group consisting of Mo: 0.50 % or less, Cr: 0.50 % or less, Sb: 0.001 % or more and 0.020 % or less, Ca: 0.005 % or less, Mg: 0.005 % or less, REM: 0.005 % or less, V: 0.15 % or less, Cu: 0.50 % or less, Ni: 0.50 % or less, Sn: 0.50 % or less, Zn: 0.10 % or less, Co: 0.10 % or less, Zr: 0.10 % or less, Ta: 0.10 % or less, and W: 0.10 % or less, where among the components of the member, C, Si, Nb, Ti, N, and B satisfy the following Expression, Nb + Ti − 3.4 N + 100 B / C / 8 + Si ≥ 0.25 where each element symbol represents the content by mass% of the corresponding element, with the balance being Fe and inevitable impurities; a microstructure in which a prior austenite average grain size is 7.5 μm or less, a volume fraction of martensite is 95 % or more, and at least 10 Nb-based and Ti-based precipitates having a grain size of 0.005 μm or more and less than 0.10 μm are present on average per 100 μm 2 of a cross section parallel to a thickness direction of the member within a range of 100 μm in the thickness direction from a surface of the member; a B concentration in prior austenite grain boundaries being at least 3.0 times a B concentration at a position 5 nm away from the grain boundaries; and a tensile strength of 1780 MPa or more, wherein the prior austenite average grain size, the volume fraction of martensite, the number of said Nb-based and Ti-based precipitates, the B concentration in prior austenite grain boundaries, the B concentration at a position 5 nm away from the grain boundaries, and the tensile strength are determined by the methods as specified in the description. a microstructure in which a prior austenite average grain size is 7.5 μm or less, a volume fraction of martensite is 95 % or more, and at least 10 Nb-based and Ti-based precipitates having a grain size of 0.005 μm or more and less than 0.10 μm are present on average per 100 μm 2 of a cross section parallel to a thickness direction of the member within a range of 100 μm in the thickness direction from a surface of the member; a B concentration in prior austenite grain boundaries being at least 3.0 times a B concentration at a position 5 nm away from the grain boundaries; and a tensile strength of 1780 MPa or more, wherein the prior austenite average grain size, the volume fraction of martensite, the number of said Nb-based and Ti-based precipitates, the B concentration in prior austenite grain boundaries, the B concentration at a position 5 nm away from the grain boundaries, and the tensile strength are determined by the methods as specified in the description.
Cooling apparatus comprising: a solar heat collection means; two or more absorption refrigeration modules, each module being arranged to receive heat from the heat collection means and to re-circulate refrigerant through an evaporator; and means for putting air to be cooled into thermal contact with each of the evaporators, wherein each module has: a. a generator containing a solution of refrigerant in a liquid, the generator being arranged to receive heat from the heat collector and to cause evaporation of the refrigerant, b. a bubble pump for pumping the liquid from the generator to an absorber, c. a condenser arranged to receive gaseous refrigerant from the generator and to condense the same, d. an evaporator, e. means for passing liquid refrigerant from the condenser to the evaporator, f. absorbing means for receiving gaseous refrigerant from the evaporator, absorbing it into the liquid from the bubble pump and returning the liquid to the generator, and g. a casing enclosing components (a) to (f) and including means for attaching the modules rigidly together, in which the casing of each module, together with partition walls within the casing, provides an evaporator housing defining a path for the air to be cooled, and includes ports by which the evaporator housings within the casings of adjoining modules are connected together. a. a generator containing a solution of refrigerant in a liquid, the generator being arranged to receive heat from the heat collector and to cause evaporation of the refrigerant, b. a bubble pump for pumping the liquid from the generator to an absorber, c. a condenser arranged to receive gaseous refrigerant from the generator and to condense the same, d. an evaporator, e. means for passing liquid refrigerant from the condenser to the evaporator, f. absorbing means for receiving gaseous refrigerant from the evaporator, absorbing it into the liquid from the bubble pump and returning the liquid to the generator, and g. a casing enclosing components (a) to (f) and including means for attaching the modules rigidly together,
Method for preparing a bone repair material comprising a porous block-shaped scaffold containing a crosslinked polyethylene glycol hydrogel formed by a Michael type addition of at least two precursor molecules, wherein said scaffold is made of a synthetic ceramic material and comprises interconnected macropores having a diameter of at least 100 μm and the scaffold has a total porosity of 60 to less than 80% comprising the steps: a. mixing an aqueous solution comprising a first precursor with an aqueous solution comprising a second precursor, whereby the total concentration of the first and the second precursor in the mixture is less than the equilibrium concentration of the hydrogel b. adding the mixture of step a) to the porous block-shaped scaffold c. removing water from the bone repair material obtained in step b), to allow reaction between the first and the second precursor. a. mixing an aqueous solution comprising a first precursor with an aqueous solution comprising a second precursor, whereby the total concentration of the first and the second precursor in the mixture is less than the equilibrium concentration of the hydrogel b. adding the mixture of step a) to the porous block-shaped scaffold c. removing water from the bone repair material obtained in step b), to allow reaction between the first and the second precursor.
An antisense oligonucleotide for use in treating myotonic dystrophy type in a subject, wherein administration of the antisense oligonucleotide to the subject with myotonic dystrophy inhibits the interaction of MBNL1 with poly exp mRNA, wherein the antisense oligonucleotide is SEQ ID NO: 3, and wherein the antisense oligonucleotide is a morpholino or a peptide nucleic acid.
A computing apparatus, comprising: a camera configured to identify a position of each of a left eye and a right eye of a user; an image sensing device configured to acquire an image of an identification element associated with a user pointing device; an object position estimator configured to calculate first coordinate values based on the identified position of each of a left eye and a right eye of the user and a position of an object point of a 3D object in a displayed 3D image, the first coordinate values representing the position of the object point as recognized by the user; a pointing position estimator configured to calculate second coordinate values based on a position of the identification element, the second coordinate values representing a pointing position of the user; and a pointing determiner configured to determine whether the pointing position of the user corresponds to the object point based on the first coordinate values and second coordinate values; the computing apparatus being characterized in that the pointing position estimator is configured to calculate the second coordinate values by comparing a first shape and a second shape, the first shape being that of the identification element in the acquired image of the identification element, and the second shape being given in advance as a shape of the identification element. a camera configured to identify a position of each of a left eye and a right eye of a user; an image sensing device configured to acquire an image of an identification element associated with a user pointing device; an object position estimator configured to calculate first coordinate values based on the identified position of each of a left eye and a right eye of the user and a position of an object point of a 3D object in a displayed 3D image, the first coordinate values representing the position of the object point as recognized by the user; a pointing position estimator configured to calculate second coordinate values based on a position of the identification element, the second coordinate values representing a pointing position of the user; and a pointing determiner configured to determine whether the pointing position of the user corresponds to the object point based on the first coordinate values and second coordinate values; the computing apparatus being characterized in that the pointing position estimator is configured to calculate the second coordinate values by comparing a first shape and a second shape, the first shape being that of the identification element in the acquired image of the identification element, and the second shape being given in advance as a shape of the identification element.
A gas turbine engine comprising: a first spool comprising a first compressor and a first turbine mounted to a first shaft; a second spool comprising a second compressor and a second turbine mounted to a second shaft; a third spool comprising a third compressor and a third turbine mounted to a third shaft; a primary combustor disposed between and fluidly communicating with the first compressor and the first turbine; a diffuser disposed between and fluidly communicating with the first compressor and the primary combustor; a secondary combustor disposed between and fluidly communicating with the second compressor and the second turbine; and an outlet duct assembly fluidly connecting the second turbine to the diffuser and the primary combustor, the outlet duct assembly comprising: a main duct extending from and communicating with the second turbine; a plurality of first branch ducts extending from and communicating between the main duct to the diffuser; and a second branch duct extending from and communicating between the main duct to the primary combustor. a first spool comprising a first compressor and a first turbine mounted to a first shaft; a second spool comprising a second compressor and a second turbine mounted to a second shaft; a third spool comprising a third compressor and a third turbine mounted to a third shaft; a primary combustor disposed between and fluidly communicating with the first compressor and the first turbine; a diffuser disposed between and fluidly communicating with the first compressor and the primary combustor; a secondary combustor disposed between and fluidly communicating with the second compressor and the second turbine; and an outlet duct assembly fluidly connecting the second turbine to the diffuser and the primary combustor, the outlet duct assembly comprising: a main duct extending from and communicating with the second turbine; a plurality of first branch ducts extending from and communicating between the main duct to the diffuser; and a second branch duct extending from and communicating between the main duct to the primary combustor. a main duct extending from and communicating with the second turbine; a plurality of first branch ducts extending from and communicating between the main duct to the diffuser; and a second branch duct extending from and communicating between the main duct to the primary combustor.
A rectangular secondary battery comprising: a flat wound group which is obtained by winding an electrode (32, 34) and has a metal foil-exposed portion (32b, 34b); a battery can which stores the wound group; a battery lid which seals the battery can; an external terminal (12, 14) which is provided on the battery lid; and a current collecting plate (24, 44) which electrically connects the external terminal (12, 14) and the wound group, the current collecting plate (24, 44) including a fixed portion (24a, 44a) fixed on the battery lid, a welded portion (24c, 44c) welded on the metal foil-exposed portion (32b, 34b) of the wound group, and a joint connecting the fixed portion (24a, 44a) and the welded portion (24c, 44c), wherein in the current collecting plate (24, 44), the joint has a width portion equal to or less than widths of the fixed portion (24a, 44a) and the welded portion (24c, 44c) and a thickness portion thicker than the fixed portion (24a, 44a) or the welded portion (24c, 44c), wherein the welded portion (24c, 44c) has a thickness portion thicker than the fixed portion (24a, 44a), and characterized in that a minimum cross-sectional area portion of the joint in a direction perpendicular to a current path is larger than at least one of minimum cross-sectional area portions of the fixed portion (24a, 44a) and the welded portion (24c, 44c) in the direction perpendicular to the current path. a flat wound group which is obtained by winding an electrode (32, 34) and has a metal foil-exposed portion (32b, 34b); a battery can which stores the wound group; a battery lid which seals the battery can; an external terminal (12, 14) which is provided on the battery lid; and a current collecting plate (24, 44) which electrically connects the external terminal (12, 14) and the wound group, the current collecting plate (24, 44) including a fixed portion (24a, 44a) fixed on the battery lid, a welded portion (24c, 44c) welded on the metal foil-exposed portion (32b, 34b) of the wound group, and a joint connecting the fixed portion (24a, 44a) and the welded portion (24c, 44c), wherein in the current collecting plate (24, 44), the joint has a width portion equal to or less than widths of the fixed portion (24a, 44a) and the welded portion (24c, 44c) and a thickness portion thicker than the fixed portion (24a, 44a) or the welded portion (24c, 44c), wherein the welded portion (24c, 44c) has a thickness portion thicker than the fixed portion (24a, 44a), and characterized in that a minimum cross-sectional area portion of the joint in a direction perpendicular to a current path is larger than at least one of minimum cross-sectional area portions of the fixed portion (24a, 44a) and the welded portion (24c, 44c) in the direction perpendicular to the current path.
A satellite or a spacecraft comprising: a chassis; and a superconducting magnet control system mounted to or within at least a portion of said chassis for position control of said satellite or said spacecraft, wherein, said superconducting magnet control system comprises: at least one superconducting electromagnet comprising at least one coil, and further comprising or mounted to at least one cooling element that is in thermal contact with said at least one coil; and at least one cryocooler; wherein, said at least one cryocooler is thermally coupled to said at least one cooling element to cool at least said at least one coil through said at least one cooling element by conduction cooling alone. a chassis; and a superconducting magnet control system mounted to or within at least a portion of said chassis for position control of said satellite or said spacecraft, wherein, said superconducting magnet control system comprises: at least one superconducting electromagnet comprising at least one coil, and further comprising or mounted to at least one cooling element that is in thermal contact with said at least one coil; and at least one cryocooler; wherein, said at least one cryocooler is thermally coupled to said at least one cooling element to cool at least said at least one coil through said at least one cooling element by conduction cooling alone. at least one superconducting electromagnet comprising at least one coil, and further comprising or mounted to at least one cooling element that is in thermal contact with said at least one coil; and at least one cryocooler; wherein, said at least one cryocooler is thermally coupled to said at least one cooling element to cool at least said at least one coil through said at least one cooling element by conduction cooling alone.
A flow measurement probe, comprising: an elongate probe comprising an averaging pitot tube element having a plurality of upstream and downstream openings arranged along a length of the elongate probe; and at least one cavity extending through the elongate probe allowing fluid flow therethrough, the at least one cavity positioned between at least two of the plurality of upstream and downstream openings; and a thermal flow measurement sensor disposed in the at least one cavity and within the elongate probe. an elongate probe comprising an averaging pitot tube element having a plurality of upstream and downstream openings arranged along a length of the elongate probe; and at least one cavity extending through the elongate probe allowing fluid flow therethrough, the at least one cavity positioned between at least two of the plurality of upstream and downstream openings; and a thermal flow measurement sensor disposed in the at least one cavity and within the elongate probe.
A method for forcing the commutating of a bypass silicon controlled rectifier - SCR - of an uninterruptible power supply - UPS - system comprising a sequence of the following steps: a) detecting an outage of a mains supply of the UPS system, b) turning on an inverter of the UPS system with a normal output polarity, wherein the inverter is capable to switch into an output current limitation mode in which its output current is limited and to generate a signal when switched into the output current limitation mode, c) switching off the bypass SCR and thereafter determining if and how long the inverter is operated in the output current limitation mode, and if it is determined that the inverter operation in the output current limitation mode exceeds a predetermined time span then performing the following steps: d) turning off the inverter, and e) turning on the inverter with a reverse output polarity for a predetermined time interval so that a reverse current is drawn via the bypass SCR. a) detecting an outage of a mains supply of the UPS system, b) turning on an inverter of the UPS system with a normal output polarity, wherein the inverter is capable to switch into an output current limitation mode in which its output current is limited and to generate a signal when switched into the output current limitation mode, c) switching off the bypass SCR and thereafter determining if and how long the inverter is operated in the output current limitation mode, and if it is determined that the inverter operation in the output current limitation mode exceeds a predetermined time span then performing the following steps: d) turning off the inverter, and e) turning on the inverter with a reverse output polarity for a predetermined time interval so that a reverse current is drawn via the bypass SCR.
A method of manufacturing an iron-based powder, comprising: providing an iron-based molten steel manufactured through an iron making process and a steelmaking process to a tundish; water atomizing the molten steel discharged through a nozzle connected to the tundish; and adding a sulfer-containing material to the molten steel so that a content of sulfur included in the molten steel before provided to the tundish is 0.1 wt% to 0.2 wt%. providing an iron-based molten steel manufactured through an iron making process and a steelmaking process to a tundish; water atomizing the molten steel discharged through a nozzle connected to the tundish; and adding a sulfer-containing material to the molten steel so that a content of sulfur included in the molten steel before provided to the tundish is 0.1 wt% to 0.2 wt%.
A speech encoding apparatus configured to encode a wide band signal in a first layer and to encode an extended band signal, whose frequency band is located in higher frequency than the wide band signal, in an extended band layer, the apparatus comprising: a band-selecting unit that selects, as a frequency band to which a limiting is applied, a frequency band to be removed from an encoding target in the extended band layeras being wider, the higher is a pitch frequency of an input signal; and a band-limiting unit that applies the limiting to the selected frequency band of the input signal by removing the selected frequency band from the encoding target. a band-selecting unit that selects, as a frequency band to which a limiting is applied, a frequency band to be removed from an encoding target in the extended band layeras being wider, the higher is a pitch frequency of an input signal; and a band-limiting unit that applies the limiting to the selected frequency band of the input signal by removing the selected frequency band from the encoding target.