mhurhangee/ep-ind-claims huggingface dataset:
A mouse whose genome comprises: (a) an insertion of one or more human VL gene segments and one or more human J L gene segments upstream of a mouse immunoglobulin light chain constant region gene, wherein the one or more human V L gene segments and one or more human J L gene segments are operably linked to the mouse immunoglobulin light chain constant region gene; (b) an insertion of one or more human V L gene segments and one or more human J L gene segments upstream of a mouse immunoglobulin heavy chain constant region gene, wherein the one or more human V L gene segments and one or more human J L gene segments are operably linked to the mouse immunoglobulin heavy chain constant region gene; and (c) an ectopic nucleic acid sequence that encodes a mouse ADAM6a protein or a functional fragment thereof and an ectopic nucleic acid sequence that encodes a mouse ADAM6b protein or a functional fragment thereof, wherein the mouse ADAM6a and ADAM6b proteins or functional fragments thereof are expressed from the ectopic nucleic acid sequences, wherein the mouse expresses an antibody comprising (i) a polypeptide that comprises a human light chain variable domain linked to a mouse heavy chain constant domain; and (ii) a polypeptide that comprises a human light chain variable domain linked to a mouse light chain constant domain. (a) an insertion of one or more human VL gene segments and one or more human J L gene segments upstream of a mouse immunoglobulin light chain constant region gene, wherein the one or more human V L gene segments and one or more human J L gene segments are operably linked to the mouse immunoglobulin light chain constant region gene; (b) an insertion of one or more human V L gene segments and one or more human J L gene segments upstream of a mouse immunoglobulin heavy chain constant region gene, wherein the one or more human V L gene segments and one or more human J L gene segments are operably linked to the mouse immunoglobulin heavy chain constant region gene; and (c) an ectopic nucleic acid sequence that encodes a mouse ADAM6a protein or a functional fragment thereof and an ectopic nucleic acid sequence that encodes a mouse ADAM6b protein or a functional fragment thereof, wherein the mouse ADAM6a and ADAM6b proteins or functional fragments thereof are expressed from the ectopic nucleic acid sequences,
A method for determining the remaining capacity of a lithium-sulfur battery comprising the steps of, a) measuring the initial voltage drop value dV1 at any one point in the range of 0.01 to 0.3 sec after applying a constant current to the battery in an open-circuit state; b) measuring the late voltage drop value dV2 at any one point in the range of 0.5 sec to 20 sec after the application of the constant current; characterised by the following steps: c) computing the additional voltage drop value dV3 by Equation 1 below; d) Computing the value of X by Equation 2 below; and e) determining the remaining capacity (SOC, state of charge) of the battery from the X value: dV3 = dV2 − dV1 X = dV1 − dV3. a) measuring the initial voltage drop value dV1 at any one point in the range of 0.01 to 0.3 sec after applying a constant current to the battery in an open-circuit state; b) measuring the late voltage drop value dV2 at any one point in the range of 0.5 sec to 20 sec after the application of the constant current; c) computing the additional voltage drop value dV3 by Equation 1 below; d) Computing the value of X by Equation 2 below; and e) determining the remaining capacity (SOC, state of charge) of the battery from the X value: dV3 = dV2 − dV1 X = dV1 − dV3.
A power-assisted bicycle comprising a front wheel, a rear wheel, one of the front and rear wheels being a drive wheel, a frame connecting the front and rear wheels, a secondary battery and a motor that are mounted on the frame, a crankshaft to which a manual force is applied, wherein driving force due to manual force applied to the crankshaft and/or the output of the motor can be transmitted to the drive wheel through a sprocket, and wherein reverse input from the drive wheel while the bicycle is not being driven can be transmitted to an output shaft of the motor, and a regenerative mechanism for converting the reverse input applied to the output shaft of the motor to electric power and storing the electric power in the secondary battery; wherein the drive wheel has a hub in which a transmission and a one-way clutch for reverse input are mounted, wherein the transmission is capable of transmitting the driving force from the sprocket to the drive wheel, and wherein the one-way clutch for reverse input is configured to idle while the drive wheel is being driven by manual force applied to the crankshaft and/or the output of the motor and is capable of transmitting reverse input from the drive wheel to the sprocket while the bicycle is not being driven.
A method of processing a plurality of articles through a processing section of a packaging machine, the method comprising: guiding a plurality of articles supported on a support tray blank onto at least one additional conveyor; folding at least one of a leading edge flap and trailing edge flap of the support tray blank with at least one tray folding member provided on the at least one additional conveyor to form a portion of a support tray; and shifting the support tray blank along a conveyor, characterized in that the at least one additional conveyor extends about and rides on the conveyor. guiding a plurality of articles supported on a support tray blank onto at least one additional conveyor; folding at least one of a leading edge flap and trailing edge flap of the support tray blank with at least one tray folding member provided on the at least one additional conveyor to form a portion of a support tray; and shifting the support tray blank along a conveyor, characterized in that the at least one additional conveyor extends about and rides on the conveyor.
Method for producing reinforced core composites, said method comprising the following steps: - incorporating a pin into a foam or filled honeycomb-shaped core material; wherein - the pin and the core material contain a thermoplastic plastics material or a mixture of thermoplastic plastics materials; and - the pin is heated in such a manner that the core material softens or melts at the incorporation location when the pin is being incorporated; and/or - the core material is heated at the incorporation location such that the core material softens or melts; and wherein the core material is particle-reinforced so as to locally heat the core material. - incorporating a pin into a foam or filled honeycomb-shaped core material; - the pin and the core material contain a thermoplastic plastics material or a mixture of thermoplastic plastics materials; and - the pin is heated in such a manner that the core material softens or melts at the incorporation location when the pin is being incorporated; and/or - the core material is heated at the incorporation location such that the core material softens or melts;
A gas jetting apparatus for a film formation apparatus, comprising: a gas supply unit for supplying a gas; a gas dispersion supply unit for accepting the gas supplied from said gas supply unit and dispersing the gas; and a gas jetting cell unit for accepting the gas dispersed in said gas dispersion supply unit, rectifying the gas, and jetting the rectified gas into the film formation apparatus, characterized in that said gas jetting cell unit has a hollow, flat plate fan shape internally formed with a gap (do) serving as a gas route, and the gas in said gas dispersion supply unit enters from a wider-width side of said fan shape into said gap (do), and, due to the fan shape, the gas is rectified, accelerated, and output from a narrower-width side of the fan shape into said film formation apparatus, wherein the gas dispersion supply unit is configured to uniformly supply the gas into said gap (do). a gas supply unit for supplying a gas; a gas dispersion supply unit for accepting the gas supplied from said gas supply unit and dispersing the gas; and a gas jetting cell unit for accepting the gas dispersed in said gas dispersion supply unit, rectifying the gas, and jetting the rectified gas into the film formation apparatus, characterized in that said gas jetting cell unit has a hollow, flat plate fan shape internally formed with a gap (do) serving as a gas route, and the gas in said gas dispersion supply unit enters from a wider-width side of said fan shape into said gap (do), and, due to the fan shape, the gas is rectified, accelerated, and output from a narrower-width side of the fan shape into said film formation apparatus, wherein the gas dispersion supply unit is configured to uniformly supply the gas into said gap (do).
An on-vehicle information terminal, comprising: a traffic information obtaining means for obtaining traffic information including first congestion information for roads and at least either weather information or event information through wireless communication; a control unit, constituted with a microprocessor, for making a decision, based upon at least either the weather information or the event information, as to whether telematics information including second congestion information for roads additional to the first congestion information provided by a server via a mobile communication network is to be downloaded; and a download means for downloading the telematics information via the mobile communication network if the control unit has determined that the telematics information is to be downloaded. a traffic information obtaining means for obtaining traffic information including first congestion information for roads and at least either weather information or event information through wireless communication; a control unit, constituted with a microprocessor, for making a decision, based upon at least either the weather information or the event information, as to whether telematics information including second congestion information for roads additional to the first congestion information provided by a server via a mobile communication network is to be downloaded; and a download means for downloading the telematics information via the mobile communication network if the control unit has determined that the telematics information is to be downloaded.
A gear box, in particular a miniature gear box, comprising a shell, a planetary carrier which is arranged in the shell and attached to an inner end face of an output end of the shell, and an output shaft which penetrates through the output end of the shell and is fixedly positioned on the planetary carrier, characterized in that the output shaft comprises a shaft body and a positioning part coaxially arranged at a tail end of the shaft body, wherein the positioning part and the planetary carrier are in limiting fit along a center axis of the output shaft and towards an outer end of the shaft body, and wherein the outer end of the shaft body and an outer end face of the output end of the shell are in limiting fit along the center axis and towards the tail end of the shaft body.
A method of electromagnetic imaging of a subsurface hydrocarbon reservoir, comprising the steps of: locating a plurality of electromagnetic energy sources in an array over an earth surface above the subsurface hydrocarbon reservoir; emitting high-power pulses of electromagnetic energy signals from the plurality of electromagnetic energy sources to travel through the subsurface hydrocarbon reservoir; recording waveforms of the emitted electromagnetic energy signals received at a plurality of electromagnetic sensors (Rx); forming a measure of the travel time of the signals received at the plurality of electromagnetic sensors (Rx); decomposing the received signals into their frequency components; extracting travel time data of the received signals as a function of frequency; and forming, based on the extracted travel time data as a function of frequency, an inverted velocity image of subsurface features of the subsurface hydrocarbon reservoir. locating a plurality of electromagnetic energy sources in an array over an earth surface above the subsurface hydrocarbon reservoir; emitting high-power pulses of electromagnetic energy signals from the plurality of electromagnetic energy sources to travel through the subsurface hydrocarbon reservoir; recording waveforms of the emitted electromagnetic energy signals received at a plurality of electromagnetic sensors (Rx); forming a measure of the travel time of the signals received at the plurality of electromagnetic sensors (Rx); decomposing the received signals into their frequency components; extracting travel time data of the received signals as a function of frequency; and forming, based on the extracted travel time data as a function of frequency, an inverted velocity image of subsurface features of the subsurface hydrocarbon reservoir.
A lubricating oil composition for internal combustion engines, comprising: a base oil composition containing a GTL base oil as a main component in an amount of 50 mass% or more based on the total amount of the base oil composition and a base oil belonging to Group II of API classification, and having % Cn of 14 to 25% and aniline point of 120 to 126°C wherein the base oil belonging to Group II is present in an amount of 10 mass% or more and 50 mass% or less of the base oil composition; and from 2.0 to 8.0 mass%, based on the total mass of the lubricating oil composition, of a comb-like polymethacrylate based viscosity index improver having a weight average molecular weight (Mw) of 400,000 or more, wherein, a sulfur content is 0.3 mass% or less based on the total weight of the lubricating oil composition. a base oil composition containing a GTL base oil as a main component in an amount of 50 mass% or more based on the total amount of the base oil composition and a base oil belonging to Group II of API classification, and having % Cn of 14 to 25% and aniline point of 120 to 126°C wherein the base oil belonging to Group II is present in an amount of 10 mass% or more and 50 mass% or less of the base oil composition; and from 2.0 to 8.0 mass%, based on the total mass of the lubricating oil composition, of a comb-like polymethacrylate based viscosity index improver having a weight average molecular weight (Mw) of 400,000 or more,
A device comprising: a mechanical resonating structure configured to support Lamb waves and including: an active layer; and a compensating structure configured to provide a desired stiffness variation of the mechanical resonating structure and/or frequency of operation variation of the mechanical resonating structure over a desired temperature range for one or more modes of vibration, the compensating structure being coupled to the active layer and comprising a first layer having a stiffness that increases with increasing temperature over at least the desired temperature range, characterized in that the compensating structure further comprises a third layer having a stiffness that increases with increasing temperature over at least the desired temperature range, and a second layer between the first layer and the third layer, wherein the second layer differs from the first and third layers (210, 214). a mechanical resonating structure configured to support Lamb waves and including: an active layer; and a compensating structure configured to provide a desired stiffness variation of the mechanical resonating structure and/or frequency of operation variation of the mechanical resonating structure over a desired temperature range for one or more modes of vibration, the compensating structure being coupled to the active layer and comprising a first layer having a stiffness that increases with increasing temperature over at least the desired temperature range, an active layer; and a compensating structure configured to provide a desired stiffness variation of the mechanical resonating structure and/or frequency of operation variation of the mechanical resonating structure over a desired temperature range for one or more modes of vibration, the compensating structure being coupled to the active layer and comprising a first layer having a stiffness that increases with increasing temperature over at least the desired temperature range,
A VCSEL array comprising two, three, four or more VCSELs arranged on a common semiconductor substrate, wherein the VCSEL array further comprises one common optical structure integrated on wafer level, wherein the common optical structure is arranged to transform the laser light to transformed laser light such that a continuous illumination pattern can be provided in a reference plane, wherein the common optical structure is arranged to increase a size of the illumination pattern in the reference plane in comparison to an untransformed illumination pattern which can be provided without the common optical structure, and wherein the common optical structure is further arranged such that each VCSEL is arranged to illuminate a sector of the illumination pattern, wherein each sector is smaller than the illumination pattern, wherein the common optical structure comprises steps such that sub-surfaces of the common optical structure with different height above the semiconductor substrate are arranged next to each other, wherein the common optical structure is a prismatic structure or a Fresnel structure, wherein each VCSEL is associated with a sub-surface of the common optical structure, wherein a distance between each VCSEL and a size of the respective sub-surface of the common optical structure is arranged such that each VCSEL illuminates only a part of the respective sub-surface of the common optical structure without illuminating one of the steps, wherein the VCSEL array comprises an array of microlenses, wherein each VCSEL is associated with a microlens, wherein the microlens is arranged to collimate the laser light after traversing the common optical structure.
A knife assembly comprising: a flat knife blade of which a front edge is a cutting edge; a holder configured for supporting the knife blade; a clamp (420, 600) arranged for clamping the knife blade onto the holder; and a fastening mechanism (103, 203) cooperating with the holder and clamp for securing and clamping the knife blade between the clamp and the holder with the cutting edge protruding at the front side; wherein the clamp (420, 600) and the holder have complementary shaped portions, with the holder having a slightly curved bearing surface, for tensioning the knife blade and straightening the cutting edge in clamped state, the complementary shaped portion of the clamp (420, 600) comprising a first part defining a clamping line (440, 620) for engaging the knife blade at a complementary contact line on the knife blade rearward from the front edge of the knife blade; wherein the complementary shaped portion of the clamp (420, 600) comprises a second part defining one or more clamping geometrical elements (450, 615, 625) corresponding to complementary contact geometrical elements of the knife blade, the clamping geometrical elements (450, 615, 625) being positioned rearward from said clamping line (440, 620) and being arranged such that in clamped state the clamp (420, 600) engages and tensions the knife blade along the clamping line (440, 620) and at the corresponding contact geometrical elements (450, 615, 625), characterized in that the first part of the clamp defining the clamping line is a frontal tip (440, 620) of the clamp. a flat knife blade of which a front edge is a cutting edge; a holder configured for supporting the knife blade; a clamp (420, 600) arranged for clamping the knife blade onto the holder; and a fastening mechanism (103, 203) cooperating with the holder and clamp for securing and clamping the knife blade between the clamp and the holder with the cutting edge protruding at the front side; wherein the clamp (420, 600) and the holder have complementary shaped portions, with the holder having a slightly curved bearing surface, for tensioning the knife blade and straightening the cutting edge in clamped state, the complementary shaped portion of the clamp (420, 600) comprising a first part defining a clamping line (440, 620) for engaging the knife blade at a complementary contact line on the knife blade rearward from the front edge of the knife blade; wherein the complementary shaped portion of the clamp (420, 600) comprises a second part defining one or more clamping geometrical elements (450, 615, 625) corresponding to complementary contact geometrical elements of the knife blade, the clamping geometrical elements (450, 615, 625) being positioned rearward from said clamping line (440, 620) and being arranged such that in clamped state the clamp (420, 600) engages and tensions the knife blade along the clamping line (440, 620) and at the corresponding contact geometrical elements (450, 615, 625), characterized in that the first part of the clamp defining the clamping line is a frontal tip (440, 620) of the clamp.
Remotely controlled multirotor aircraft for acquiring images, wherein it comprises: - receiving means adapted to receive a direction and/or orientation signal which can be transmitted by an interface device (3, 4), wherein said direction and/or orientation signal defines a direction in which said aircraft must move and/or be oriented, - flight control means adapted to control the attitude of said aircraft, and configured for acquiring said direction and/or orientation signal, calculating, on the basis of said direction and/or orientation signal, the direction in which said aircraft have to move and/or be oriented, generating a control signal adapted to make said aircraft take such an attitude as to make it move and/or be oriented in said defined direction, wherein the direction and/or orientation signal comprises an instruction signal that represents a voice command imparted by the user of said aircraft, and wherein the flight control means are configured for running a sequence of instructions that implements a speech recognition algorithm that converts the voice command represented in the instruction signal into a bit string, and for generating the control signals based on said bit string. - receiving means adapted to receive a direction and/or orientation signal which can be transmitted by an interface device (3, 4), wherein said direction and/or orientation signal defines a direction in which said aircraft must move and/or be oriented, - flight control means adapted to control the attitude of said aircraft, and configured for acquiring said direction and/or orientation signal, calculating, on the basis of said direction and/or orientation signal, the direction in which said aircraft have to move and/or be oriented, generating a control signal adapted to make said aircraft take such an attitude as to make it move and/or be oriented in said defined direction, acquiring said direction and/or orientation signal, calculating, on the basis of said direction and/or orientation signal, the direction in which said aircraft have to move and/or be oriented, generating a control signal adapted to make said aircraft take such an attitude as to make it move and/or be oriented in said defined direction,