mhurhangee/patent-ind-claim-en huggingface dataset:
A fixation device for a knife mounting base characterized in that it comprises: a restraint part having a ring shape; an operating part which has a locking section at a base end portion and in which a tip portion enters the inside of the restraint part ; a biasing member which biases the restraint part along an entering direction of the operating part; an engagement section which is provided at one of an inner surface of the restraint part and an outer surface of the operating part ; a helical guide section which is provided in the other of the inner surface of the restraint part and the outer surface of the operating part , is engaged with the engagement section, and can move the restraint part from a first position to a second position against a biasing force of the biasing member by rotating the operating part ; and a blocking section which is provided in the other of the inner surface of the restraint part and the outer surface of the operating part and is configured to block rotation of the operating part in a reverse direction when the restraint part is located at the second position. a restraint part having a ring shape; an operating part which has a locking section at a base end portion and in which a tip portion enters the inside of the restraint part ; a biasing member which biases the restraint part along an entering direction of the operating part; an engagement section which is provided at one of an inner surface of the restraint part and an outer surface of the operating part ; a helical guide section which is provided in the other of the inner surface of the restraint part and the outer surface of the operating part , is engaged with the engagement section, and can move the restraint part from a first position to a second position against a biasing force of the biasing member by rotating the operating part ; and a blocking section which is provided in the other of the inner surface of the restraint part and the outer surface of the operating part and is configured to block rotation of the operating part in a reverse direction when the restraint part is located at the second position.
A method for a wireless communication system that supports operation in a single resource block narrowband region (615-a) of a system bandwidth , the method comprising: identifying (1105; 2705), by a base station (105-c; 105), a location of the narrowband region (615-a) of the system bandwidth as a particular single resource block within a wideband region of the system bandwidth ; and transmitting (1120; 2710), by the base station (105-c; 105) to a user equipment (115-c; 115), UE, an indication of the location of the particular single resource block within the wideband region of the system bandwidth , wherein the indication is transmitted in one or more of a master information block, MIB, or a system information block, SIB including signaling that the narrowband region (615-a) is within the system bandwidth . identifying (1105; 2705), by a base station (105-c; 105), a location of the narrowband region (615-a) of the system bandwidth as a particular single resource block within a wideband region of the system bandwidth ; and transmitting (1120; 2710), by the base station (105-c; 105) to a user equipment (115-c; 115), UE, an indication of the location of the particular single resource block within the wideband region of the system bandwidth , wherein the indication is transmitted in one or more of a master information block, MIB, or a system information block, SIB including signaling that the narrowband region (615-a) is within the system bandwidth .
Method for controlling an ion exchange membrane fuel cell stack, the stack being installed in a system additionally comprising a liquid cooling circuit and a pump for circulating the coolant liquid, the method comprising a phase of starting up the fuel cell stack, this start-up phase comprising the following steps: • the internal temperature of the fuel cell stack is determined while taking account of the heat capacity and the mass of the materials constituting the stack, and the thermal energy dissipated by the stack; • the temperature in the liquid cooling circuit is measured; • a start-up current is applied to the fuel cell stack and, in parallel; o when the internal temperature of the stack is above a first predetermined threshold, and the temperature of the cooling circuit is below a second predetermined threshold, the cooling pump is ordered to operate in pulsed mode; and o when the temperature in the cooling circuit rises above the second predetermined threshold, the cooling pump is ordered to operate in continuous mode. • the internal temperature of the fuel cell stack is determined while taking account of the heat capacity and the mass of the materials constituting the stack, and the thermal energy dissipated by the stack; • the temperature in the liquid cooling circuit is measured; • a start-up current is applied to the fuel cell stack and, in parallel; o when the internal temperature of the stack is above a first predetermined threshold, and the temperature of the cooling circuit is below a second predetermined threshold, the cooling pump is ordered to operate in pulsed mode; and o when the temperature in the cooling circuit rises above the second predetermined threshold, the cooling pump is ordered to operate in continuous mode. o when the internal temperature of the stack is above a first predetermined threshold, and the temperature of the cooling circuit is below a second predetermined threshold, the cooling pump is ordered to operate in pulsed mode; and o when the temperature in the cooling circuit rises above the second predetermined threshold, the cooling pump is ordered to operate in continuous mode.
A closing device for windows and doors adapted to be operatively interposed between a panel and a frame of a window and door to retain or lock the panel in a closing condition of said window and door , said closing device comprising: - a striker adapted to be mounted on the frame and comprising a magnetic abutment system, - a lock comprising a lock body adapted to be mounted on the panel and a latch housed in the lock body and comprising a magnetic closing system, wherein said latch is movable along a direction of motion (X) between a retracted position and at least an extracted position with respect to the lock body , the movement of said latch along a closing direction (X1) from the retracted position to the extracted position being caused by the magnetic interaction between said magnetic abutment system and said magnetic closing system, wherein said lock body comprises a locking system which can be switched between a first configuration, wherein said latch is free to perform said movement along the direction of motion (X), and a second configuration, wherein said latch is locked in the retracted position and creates a magnetic induction closing catch. - a striker adapted to be mounted on the frame and comprising a magnetic abutment system, - a lock comprising a lock body adapted to be mounted on the panel and a latch housed in the lock body and comprising a magnetic closing system, wherein said latch is movable along a direction of motion (X) between a retracted position and at least an extracted position with respect to the lock body , the movement of said latch along a closing direction (X1) from the retracted position to the extracted position being caused by the magnetic interaction between said magnetic abutment system and said magnetic closing system, wherein said lock body comprises a locking system which can be switched between a first configuration, wherein said latch is free to perform said movement along the direction of motion (X), and a second configuration, wherein said latch is locked in the retracted position and creates a magnetic induction closing catch. wherein said latch is movable along a direction of motion (X) between a retracted position and at least an extracted position with respect to the lock body , the movement of said latch along a closing direction (X1) from the retracted position to the extracted position being caused by the magnetic interaction between said magnetic abutment system and said magnetic closing system, wherein said lock body comprises a locking system which can be switched between a first configuration, wherein said latch is free to perform said movement along the direction of motion (X), and a second configuration, wherein said latch is locked in the retracted position and creates a magnetic induction closing catch.
Method for construction of double weaves with an upper fabric and an under fabric on a standard Jacquard loom or on a dobby loom, showing on both sides their separate individuality, for which a) in the first step every surface will get one individuality for the upper fabric and one individuality for the under fabric and will be prepared on a computer with a design program, preferably on a Jacquard design program. b) in a second step both individualities will be treated on the same size or according to the demand of upper- and underwarp. c) in the third step both individualities will be filled with the suitable bindings after the technical treatment floats will be deleted and after that, the individuality of the underfabric will be copied to the individuality of the upper fabric. d) in a fourth step there will be added the warp float, warp upperside and warp underside as well as the tied and the untied points according to the demands of the individualities of face fabic and backside fabric. e) in a fifth step, the computer created data will be sent for the production of the double face fabric to the loom, f) where the kind and/or the density of the yarns from the individuality of the upperside will be different to the kind and/or the density to the individuality of the underside. a) in the first step every surface will get one individuality for the upper fabric and one individuality for the under fabric and will be prepared on a computer with a design program, preferably on a Jacquard design program. b) in a second step both individualities will be treated on the same size or according to the demand of upper- and underwarp. c) in the third step both individualities will be filled with the suitable bindings after the technical treatment floats will be deleted and after that, the individuality of the underfabric will be copied to the individuality of the upper fabric. d) in a fourth step there will be added the warp float, warp upperside and warp underside as well as the tied and the untied points according to the demands of the individualities of face fabic and backside fabric. e) in a fifth step, the computer created data will be sent for the production of the double face fabric to the loom, f) where the kind and/or the density of the yarns from the individuality of the upperside will be different to the kind and/or the density to the individuality of the underside.
A method for image capture, comprising the steps of: determining an exposure range; setting at least one camera parameter of a camera to capture an underexposed image outside the exposure range; processing the underexposed image using a neural network to recover image details, characterized in that the neural network is a neural network trained using a profile of the camera as an input, the profile obtained using mathematical models with an imaging system including the camera being in a controlled lighting environment such that a photo noise floor is known. determining an exposure range; setting at least one camera parameter of a camera to capture an underexposed image outside the exposure range; processing the underexposed image using a neural network to recover image details, characterized in that the neural network is a neural network trained using a profile of the camera as an input, the profile obtained using mathematical models with an imaging system including the camera being in a controlled lighting environment such that a photo noise floor is known.
A method for producing an optical fiber comprising drawing an optical fiber preform in a drawing furnace to produce a silica glass-based optical fiber including a core region containing an alkali metal with an average concentration of 0.5 atomic ppm or more and a cladding region surrounding the core region, characterized in that the drawn optical fiber is passed through a heating furnace whose temperature is 700°C or more, the residence time of the optical fiber in the heating furnace being 0.2 seconds or longer.
A catalyst for dehydrogenation of formic acid, comprising: a multinuclear metal complex represented by the following Formula , a tautomer or stereoisomer thereof, or a salt thereof, wherein M 1 and M 2 denote transition metals and may be the same as or different from each other and are each independently selected from the group consisting of iridium, rhodium, ruthenium, cobalt, osmium, nickel, iron, palladium and platinum; Q 1 to Q 6 each denote carbon; R 1 to R 6 each independently denote a hydrogen atom, an alkyl group, a phenyl group, a nitro group, a halogen group, a sulfonate group or sulfo group, a carboxylate group or carboxy group, an alkoxy group, an alkyl amino group, L 1 and L 2 each independently denote a cyclopentadienyl ligand or a benzene ligand, and may be unsubstituted or substituted by one or more substituents; wherein the substituents are selected from an alkyl group, an aromatic group, a hydroxy group, an ester group, an amide group, a halogen atom, an alkoxy group, an alkylthio group, an amino group, a carboxylate group, a nitro group or a sulfonate group, which may be same or different from each other; Y 1 and Y 2 each independently denote a water molecule, a hydrogen atom, a heavy hydrogen atom, an alkoxide ion, a hydroxide ion, a carbonate ion, a trifluoromethanesulfonate ion, a sulfate ion, a nitrate ion, a formate ion, or an acetate ion, or are absent; and m denotes a positive integer, 0, or a negative integer. M 1 and M 2 denote transition metals and may be the same as or different from each other and are each independently selected from the group consisting of iridium, rhodium, ruthenium, cobalt, osmium, nickel, iron, palladium and platinum; Q 1 to Q 6 each denote carbon; R 1 to R 6 each independently denote a hydrogen atom, an alkyl group, a phenyl group, a nitro group, a halogen group, a sulfonate group or sulfo group, a carboxylate group or carboxy group, an alkoxy group, an alkyl amino group, L 1 and L 2 each independently denote a cyclopentadienyl ligand or a benzene ligand, and may be unsubstituted or substituted by one or more substituents; wherein the substituents are selected from an alkyl group, an aromatic group, a hydroxy group, an ester group, an amide group, a halogen atom, an alkoxy group, an alkylthio group, an amino group, a carboxylate group, a nitro group or a sulfonate group, which may be same or different from each other; Y 1 and Y 2 each independently denote a water molecule, a hydrogen atom, a heavy hydrogen atom, an alkoxide ion, a hydroxide ion, a carbonate ion, a trifluoromethanesulfonate ion, a sulfate ion, a nitrate ion, a formate ion, or an acetate ion, or are absent; and m denotes a positive integer, 0, or a negative integer.
A method comprising, performed by at least one apparatus: obtaining a set of radio data comprising signal strength related values for radio signals transmitted by a transmitter with an association of each signal strength related value with a representation of a geographical location; applying a frequency transform to the obtained set of radio data to obtain transform coefficients, each transform coefficient comprising a transform index and an associated transform value; selecting a subset of transform indices having more significant transform values than the remaining transform indices; characterized in that the method further comprises: compressing the selected transform indices by encoding each selected transform index exploiting a probability of occurrence of an index value of a respective transform index. obtaining a set of radio data comprising signal strength related values for radio signals transmitted by a transmitter with an association of each signal strength related value with a representation of a geographical location; applying a frequency transform to the obtained set of radio data to obtain transform coefficients, each transform coefficient comprising a transform index and an associated transform value; selecting a subset of transform indices having more significant transform values than the remaining transform indices;
A curable composite material comprising: at least two layers of reinforcement carbon fibers impregnated with a curable matrix resin; and an interlaminar region formed between adjacent layers of reinforcement carbon fibers, the interlaminar region comprising (i) conductive nano-sized particles dispersed therein, and (ii) a nonwoven carbon veil which is comprised of randomly arranged carbon fibers, wherein each of the conductive nano-sized particles has at least one dimension smaller than 100 nm, and wherein the dimensions of the nano-particles are determined by a Dynamic Light Scattering (DSL) technique. at least two layers of reinforcement carbon fibers impregnated with a curable matrix resin; and an interlaminar region formed between adjacent layers of reinforcement carbon fibers, the interlaminar region comprising (i) conductive nano-sized particles dispersed therein, and (ii) a nonwoven carbon veil which is comprised of randomly arranged carbon fibers, wherein each of the conductive nano-sized particles has at least one dimension smaller than 100 nm, and wherein the dimensions of the nano-particles are determined by a Dynamic Light Scattering (DSL) technique.
A folding wing hinge for a wing having a fixed wing portion and a folding wing portion , the folding wing hinge comprising: a hinge pin including a hinge pin spline and having a first longitudinal axis ; an input fitting coupled to one of the fixed wing portion and the folding wing portion , the input fitting including an input fitting spline and a second longitudinal axis ; a spline coupling member having a coupling spline configured to couple with the hinge pin spline and the input fitting spline so that the first longitudinal axis is moveable relative to the second longitudinal axis by a first predetermined amount of movement ; and at least one hinge pin bushing coupled to at least one of the fixed wing portion and the folding wing portion , the at least one hinge pin bushing having a third longitudinal axis ; wherein the hinge pin extends through the at least one hinge pin bushing ; and wherein the first longitudinal axis is movable relative to the third longitudinal axis by a second predetermined amount of movement , the second predetermined amount of movement being less than the first predetermined amount of movement so that flight loads between the fixed wing portion and the folding wing portion are substantially isolated to a load path that passes through the at least one hinge pin bushing . a hinge pin including a hinge pin spline and having a first longitudinal axis ; an input fitting coupled to one of the fixed wing portion and the folding wing portion , the input fitting including an input fitting spline and a second longitudinal axis ; a spline coupling member having a coupling spline configured to couple with the hinge pin spline and the input fitting spline so that the first longitudinal axis is moveable relative to the second longitudinal axis by a first predetermined amount of movement ; and at least one hinge pin bushing coupled to at least one of the fixed wing portion and the folding wing portion , the at least one hinge pin bushing having a third longitudinal axis ; wherein the hinge pin extends through the at least one hinge pin bushing ; and wherein the first longitudinal axis is movable relative to the third longitudinal axis by a second predetermined amount of movement , the second predetermined amount of movement being less than the first predetermined amount of movement so that flight loads between the fixed wing portion and the folding wing portion are substantially isolated to a load path that passes through the at least one hinge pin bushing .
A method, comprising: - illuminating a sample with a light source , wherein the sample includes a plurality of fluorescent species, and wherein illuminating the sample with the light source excites at least two of the plurality of fluorescent species; - measuring at least two fluorescence signals from the sample, wherein the at least two fluorescence signals include component signals from the at least two of the plurality of fluorescent species; further comprising, by an assaying device, determining a correlation between each pair of derivatives of the at least two fluorescence signals , calculating a crosstalk metric based on these pair wise correlations, characterized in that : the correlation is the pointwise product of the respective time derivatives of the pair and wherein the crosstalk metric is defined as one of the integral of the absolute value of the point-wise product, the integral of the square of the values of the point-wise product, the RMS average of the point-wise product, the sum of absolute values of the point-wise product. - illuminating a sample with a light source , wherein the sample includes a plurality of fluorescent species, and wherein illuminating the sample with the light source excites at least two of the plurality of fluorescent species; - measuring at least two fluorescence signals from the sample, wherein the at least two fluorescence signals include component signals from the at least two of the plurality of fluorescent species;
A liquid reservoir for a refrigeration system, comprising: a drum body , a gas-liquid separation chamber being defined therein; and an air intake pipe , configured to be connected to an evaporating pipe of an evaporator of the refrigeration system, and extending into the gas-liquid separation chamber from one end of the drum body , the end of the air intake pipe extending into the gas-liquid separation chamber being provided with a baffle opposite to a mouth of the air intake pipe , so that a mixture discharged from the air intake pipe hits the baffle and then is discharged into the gas-liquid separation chamber from an interval between the baffle and the air intake pipe , characterised in that the pipe diameter of the part of the air intake pipe extending into the gas-liquid separation chamber gradually shrinks with the increase of an extending length. a drum body , a gas-liquid separation chamber being defined therein; and an air intake pipe , configured to be connected to an evaporating pipe of an evaporator of the refrigeration system, and extending into the gas-liquid separation chamber from one end of the drum body , the end of the air intake pipe extending into the gas-liquid separation chamber being provided with a baffle opposite to a mouth of the air intake pipe , so that a mixture discharged from the air intake pipe hits the baffle and then is discharged into the gas-liquid separation chamber from an interval between the baffle and the air intake pipe , characterised in that the pipe diameter of the part of the air intake pipe extending into the gas-liquid separation chamber gradually shrinks with the increase of an extending length.