mhurhangee/ep-ind-claims huggingface dataset:
A thromboelastometry system for measuring coagulation characteristics of a blood sample, the thromboelastometry system comprising: a control unit housing; a user interface coupled to the control unit housing for displaying coagulation characteristics of a blood sample; and a plurality of individual thromboelastometry measurement modules housed in the control unit housing, each measurement module of the plurality of individual thromboelastometry measurement modules including a shaft configured to receive a probe for testing the blood sample using a probe and cup arrangement, wherein each individual measurement module of the plurality of individual thromboelastometry measurement modules includes a dedicated actuation unit that drives rotation of a respective shaft of the individual measurement module independently from rotation of shafts of all other individual measurement modules of the plurality of individual thromboelastometry measurement modules; and wherein the actuation unit comprises a stepper motor, wherein the stepper motor includes a threaded driveshaft, wherein the actuation unit further comprises a slider unit, and wherein the slider unit comprises a threaded collar that is threadably engaged with the threaded drive shaft such that the stepper motor can drive the slider unit to translate linearly. a control unit housing; a user interface coupled to the control unit housing for displaying coagulation characteristics of a blood sample; and a plurality of individual thromboelastometry measurement modules housed in the control unit housing, each measurement module of the plurality of individual thromboelastometry measurement modules including a shaft configured to receive a probe for testing the blood sample using a probe and cup arrangement, wherein each individual measurement module of the plurality of individual thromboelastometry measurement modules includes a dedicated actuation unit that drives rotation of a respective shaft of the individual measurement module independently from rotation of shafts of all other individual measurement modules of the plurality of individual thromboelastometry measurement modules; and wherein the actuation unit comprises a stepper motor, wherein the stepper motor includes a threaded driveshaft, wherein the actuation unit further comprises a slider unit, and wherein the slider unit comprises a threaded collar that is threadably engaged with the threaded drive shaft such that the stepper motor can drive the slider unit to translate linearly.
An anvil assembly for use with a surgical stapling instrument comprising; an anvil member having a longitudinal axis and a first staple bending pocket and a second staple bending pocket; and a length of reinforcing member extending across the first and second staple bending pockets (56, 58); characterised in that the width of the reinforcing member is less than the width of each of the first and second staple bending pockets (56,58).
A gas turbine combustor which comprises: a main burner to supply a premixed gas, containing a first fuel, to a first combustion region within a combustion chamber and then to combust the premixed gas; and a supplemental burner to supply a premixed gas, containing a second fuel of a composition different from that of the first fuel, to a second combustion region at a location downstream of the first combustion region within the combustion chamber and then to combust the premixed gas; in which the first fuel is of a hydrocarbon system and the second fuel is a gas containing hydrogen in concentration exceeding a stable combustion limiting concentration of the hydrogen, in which the supplemental burner is a premixing burner operable to premix both of the first fuel and the second fuel with an air and supplying it to the second combustion region, characterized in that the supplemental burner comprises a premixing chamber to which the air is introduced, a first nozzle to inject the first fuel into the premixing chamber, a second nozzle to inject the second fuel into the premixing chamber, a first fuel chamber to reserve the first fuel, and a second fuel chamber to reserve the second fuel, and in which the first nozzle is in the form of a plurality of small perforations, which open in the first fuel chamber, and the second nozzle is in the form of a plurality of small perforations which open in the second fuel chamber. a main burner to supply a premixed gas, containing a first fuel, to a first combustion region within a combustion chamber and then to combust the premixed gas; and a supplemental burner to supply a premixed gas, containing a second fuel of a composition different from that of the first fuel, to a second combustion region at a location downstream of the first combustion region within the combustion chamber and then to combust the premixed gas; in which the first fuel is of a hydrocarbon system and the second fuel is a gas containing hydrogen in concentration exceeding a stable combustion limiting concentration of the hydrogen, in which the supplemental burner is a premixing burner operable to premix both of the first fuel and the second fuel with an air and supplying it to the second combustion region, characterized in that the supplemental burner comprises a premixing chamber to which the air is introduced, a first nozzle to inject the first fuel into the premixing chamber, a second nozzle to inject the second fuel into the premixing chamber, a first fuel chamber to reserve the first fuel, and a second fuel chamber to reserve the second fuel, and in which the first nozzle is in the form of a plurality of small perforations, which open in the first fuel chamber, and the second nozzle is in the form of a plurality of small perforations which open in the second fuel chamber.
An apparatus, comprising: a sensing component adapted to perform measurement of a parameter and produce an electrical signal based on the measurement; two memristive components (M1, M2) adapted to receive the produced electrical signal from the sensing component, and produce a respective cumulative value of the received electrical signal over time; a switching component (33, 303) adapted to selectively couple the two memristive components to the sensing component; and a processing component adapted to receive the produced cumulative value from the two memristive components and digitize the received cumulative value, wherein the two memristive components are electrically coupled to the processing component in parallel. a sensing component adapted to perform measurement of a parameter and produce an electrical signal based on the measurement; two memristive components (M1, M2) adapted to receive the produced electrical signal from the sensing component, and produce a respective cumulative value of the received electrical signal over time; a switching component (33, 303) adapted to selectively couple the two memristive components to the sensing component; and a processing component adapted to receive the produced cumulative value from the two memristive components and digitize the received cumulative value, wherein the two memristive components are electrically coupled to the processing component in parallel.
A method for using a plurality of renewable sources of energy, comprising: - generating electric energy either being energy having first characteristic frequencies or being DC energy, the electric energy from a renewable form of energy at a plurality of different locations at which reside a pre-existing AC electric power line (401; 501) included in an AC electric power grid carrying electric energy with a second frequency, the first characteristic frequencies being different of the second frequency; and - transferring the electric energy generated at each location to the AC electric power line (401; 501) at each respective location to thereby supply electric energy to the AC electric power grid, wherein the electric energy is transferred via a respective plurality of energy transfer elements being filters (403; 503) for transferring the electric energy generated at each location to the AC electric power line (401; 501), wherein each energy transfer element (403; 503) resides at one of the different locations and wherein the energy transfer elements (403; 503) transfer the generated electric energy with the first frequency to the pre-existing AC electric power line (401; 501) carrying the electric energy with the second frequency via direct electrical current multiplexing of the different types of electrical energies into the same electrical pre-existing power line (401; 501). - generating electric energy either being energy having first characteristic frequencies or being DC energy, the electric energy from a renewable form of energy at a plurality of different locations at which reside a pre-existing AC electric power line (401; 501) included in an AC electric power grid carrying electric energy with a second frequency, the first characteristic frequencies being different of the second frequency; and - transferring the electric energy generated at each location to the AC electric power line (401; 501) at each respective location to thereby supply electric energy to the AC electric power grid, wherein the electric energy is transferred via a respective plurality of energy transfer elements being filters (403; 503) for transferring the electric energy generated at each location to the AC electric power line (401; 501), wherein each energy transfer element (403; 503) resides at one of the different locations and wherein the energy transfer elements (403; 503) transfer the generated electric energy with the first frequency to the pre-existing AC electric power line (401; 501) carrying the electric energy with the second frequency via direct electrical current multiplexing of the different types of electrical energies into the same electrical pre-existing power line (401; 501).
A purified peptide having at least 75% identity to the amino acid sequence RADSRADC (SEQ ID NO: 2), and having an IC 50 of tyrosinase of less than 10mM, such as less than 5mM.
An engine system for an aircraft, the engine system comprising: a first gas turbine engine; a second gas turbine engine; a control system configured to: operate the first gas turbine engine with an idle fuel burn schedule in a taxi mode of the aircraft; dry crank the second gas turbine engine in a first pre-takeoff portion of the taxi mode to cool the second gas turbine engine absent fuel burn by the second gas turbine engine; operate the second gas turbine engine with a sub-idle fuel burn schedule in a second pre-takeoff portion of the taxi mode of the aircraft, the sub-idle fuel burn schedule comprising a reduction of the idle fuel burn schedule; increase a fuel flow of the first gas turbine engine and the second gas turbine engine above the idle fuel burn schedule prior to takeoff of the aircraft; and alternate a designation of the first gas turbine engine and the second gas turbine engine between two or more gas turbine engines of the aircraft. a first gas turbine engine; a second gas turbine engine; a control system configured to: operate the first gas turbine engine with an idle fuel burn schedule in a taxi mode of the aircraft; dry crank the second gas turbine engine in a first pre-takeoff portion of the taxi mode to cool the second gas turbine engine absent fuel burn by the second gas turbine engine; operate the second gas turbine engine with a sub-idle fuel burn schedule in a second pre-takeoff portion of the taxi mode of the aircraft, the sub-idle fuel burn schedule comprising a reduction of the idle fuel burn schedule; increase a fuel flow of the first gas turbine engine and the second gas turbine engine above the idle fuel burn schedule prior to takeoff of the aircraft; and alternate a designation of the first gas turbine engine and the second gas turbine engine between two or more gas turbine engines of the aircraft. operate the first gas turbine engine with an idle fuel burn schedule in a taxi mode of the aircraft; dry crank the second gas turbine engine in a first pre-takeoff portion of the taxi mode to cool the second gas turbine engine absent fuel burn by the second gas turbine engine; operate the second gas turbine engine with a sub-idle fuel burn schedule in a second pre-takeoff portion of the taxi mode of the aircraft, the sub-idle fuel burn schedule comprising a reduction of the idle fuel burn schedule; increase a fuel flow of the first gas turbine engine and the second gas turbine engine above the idle fuel burn schedule prior to takeoff of the aircraft; and alternate a designation of the first gas turbine engine and the second gas turbine engine between two or more gas turbine engines of the aircraft.
Device for trapping insects, comprising a casing provided with a housing for placing a refill provided with an adhesive surface for trapping insects, said casing comprising a light emitter illuminating at least one part of the refill, characterized in that said refill comprises an outer transparent or translucent frame surrounding the adhesive surface for attracting insects which is illuminated by said light emitter, wherein said refill comprises at least one protective sheet which is removed before a first use.
An uncoated recording medium, comprising: a blend of hardwood fibers and softwood fibers, wherein a total fiber content is at least 80 wt% of a total wt% of the uncoated recording medium; wherein the blend includes a ratio of the hardwood fibers to the softwood fibers ranging from about 70/30 to about 60/40; a filler, chosen from titanium dioxide, precipitated calcium carbonate, ground calcium carbonate, talc, clay, and combinations thereof, present in an amount ranging from about 3 wt% to about 10.2 wt% of the total wt% of the uncoated recording medium; and a salt present in an amount ranging from about 4000 μg per gram of the uncoated recording medium to about 9500 μg per gram of the uncoated recording medium. a blend of hardwood fibers and softwood fibers, wherein a total fiber content is at least 80 wt% of a total wt% of the uncoated recording medium; wherein the blend includes a ratio of the hardwood fibers to the softwood fibers ranging from about 70/30 to about 60/40; a filler, chosen from titanium dioxide, precipitated calcium carbonate, ground calcium carbonate, talc, clay, and combinations thereof, present in an amount ranging from about 3 wt% to about 10.2 wt% of the total wt% of the uncoated recording medium; and a salt present in an amount ranging from about 4000 μg per gram of the uncoated recording medium to about 9500 μg per gram of the uncoated recording medium.
Compositions comprising A) nylon-6 or nylon-6,6, B) at least one quartz powder having a d95 in the range from 5 to 250 μ m determined by laser diffractometry, C) chopped long glass fibres having a starting length in the range from 1 to 50 mm, and D) melamine cyanurate. A) nylon-6 or nylon-6,6, B) at least one quartz powder having a d95 in the range from 5 to 250 μ m determined by laser diffractometry, C) chopped long glass fibres having a starting length in the range from 1 to 50 mm, and D) melamine cyanurate.
A method of fabricating a metallic wire, the method comprising: combining, to form at least a portion of a preform, (i) one or more first metal powders each comprising a plurality of substantially spherical particles, defined by being spherical to within ±10% in any direction, and (ii) one or more second metal powders each comprising a plurality of non-spherical particles, which are either elongated with an aspect ratio of at least 2:1, acicular, having at least one flat surface, having at least one corner or vertex, or polyhedral, the one or more second metal powders being mixed with the one or more first metal powders such that a composition of the preform is substantially homogeneous ±10% along a length of the preform; and reducing a diameter of the preform via one or more mechanical deformation processes, thereby forming a metallic wire, wherein (i) the metallic wire comprises a high-entropy alloy comprising five or more metallic elements selected from Nb, Ta, Mo, W, Ti, Hf, V, Zr, Al, and Cr, each element with a concentration between 5 and 35 atomic % or a multi-principal element alloy comprising four or more metallic elements selected from Nb, Ta, Mo, W, Ti, Hf, V, Zr, Al, and Cr, each element with a concentration between 5 and 35 atomic %, (ii) each first metal powder comprises at least one of the metallic elements, and (iii) each second metal powder comprises at least one of the metallic elements. combining, to form at least a portion of a preform, (i) one or more first metal powders each comprising a plurality of substantially spherical particles, defined by being spherical to within ±10% in any direction, and (ii) one or more second metal powders each comprising a plurality of non-spherical particles, which are either elongated with an aspect ratio of at least 2:1, acicular, having at least one flat surface, having at least one corner or vertex, or polyhedral, the one or more second metal powders being mixed with the one or more first metal powders such that a composition of the preform is substantially homogeneous ±10% along a length of the preform; and reducing a diameter of the preform via one or more mechanical deformation processes, thereby forming a metallic wire, wherein (i) the metallic wire comprises a high-entropy alloy comprising five or more metallic elements selected from Nb, Ta, Mo, W, Ti, Hf, V, Zr, Al, and Cr, each element with a concentration between 5 and 35 atomic % or a multi-principal element alloy comprising four or more metallic elements selected from Nb, Ta, Mo, W, Ti, Hf, V, Zr, Al, and Cr, each element with a concentration between 5 and 35 atomic %, (ii) each first metal powder comprises at least one of the metallic elements, and (iii) each second metal powder comprises at least one of the metallic elements.
A tool for assaying microarrays that reduces the likelihood of air bubbles being trapped by the microarrays, comprising: two clamps, each of the two clamps comprising: a tool mount portion, the tool mount portion configured to engage a lifting mechanism of a plate handling robot for moving a pillar plate comprising microarrays, and a grasping portion, and characterized in that the grasping portion is configured to freely suspend the pillar plate at an inclination of a non-zero tilt angle relative to a plane normal to the tool mount portion. a tool mount portion, the tool mount portion configured to engage a lifting mechanism of a plate handling robot for moving a pillar plate comprising microarrays, and a grasping portion, and characterized in that the grasping portion is configured to freely suspend the pillar plate at an inclination of a non-zero tilt angle relative to a plane normal to the tool mount portion.
Polyester comprising ethylene-2,5-furandicarboxylate units, which polyester has an IV of at least 0.75 dl/g,an acetaldehyde content of less than 0.5 mg/kg and an amount of carboxylic acid end groups in the range of 5 to 30 meq/kg, all measured as described in the description.
A data-collecting implant having a sensor capable of generating output data in response to said implant receiving an interrogation signal, said implant comprising: a housing used to contain said sensor, said housing including a transparent window; electrical components located within said housing and selectively creating an RF communication link between said implant and a remote controller, said implant using said RF communication link to selectively transmit said output data of said sensor to said remote controller; and electrical components that selectively create an optical communication link between said remote controller and said sensor so that calibration data may be transmitted from said remote controller to said sensor optically through said transparent window of said housing. a housing used to contain said sensor, said housing including a transparent window; electrical components located within said housing and selectively creating an RF communication link between said implant and a remote controller, said implant using said RF communication link to selectively transmit said output data of said sensor to said remote controller; and electrical components that selectively create an optical communication link between said remote controller and said sensor so that calibration data may be transmitted from said remote controller to said sensor optically through said transparent window of said housing.
Water abrasive suspension cutting device, comprising at least one pressure generating device for generating a desired water pressure of a high-pressure cutting jet, at least one water inlet for supplying pure water, at least one abrasive agent container with abrasive agent, at least one cutting nozzle for discharging the high-pressure cutting jet for water abrasive suspension cutting and at least one valve device for selectively switching on or off the high-pressure cutting jet emerging from the cutting nozzle of the water abrasive suspension cutting device, the valve device having at least one first feed connection for the abrasive-containing cutting medium, at least one second feed connection for clean water and an outlet connection for discharging media supplied via the first and/or the second feed connection (31, 32) to the cutting nozzle, the first feed connection being connected to the abrasive medium container or a feed line for the abrasive-containing cutting medium, the second feed connection is connected to the water inlet and the outlet connection is connected to the cutting nozzle, characterized in that the valve device has at least one seat valve and/or at least one slide valve and/or at least one ball valve, with which the high-pressure cutting jet can be selectively switched on or off.
A method comprising: operating a diesel opposed piston engine with a first compression ratio to supply engine power in response to a first engine load, the diesel opposed piston engine comprising a combustion chamber defined at least in part by crowns of two pistons (302, 304) each individually coupled to one of two crankshafts, and changing the first compression ratio to a second compression ratio to supply engine power in response to a second engine load, the second engine load being larger than the first engine load, the second compression ratio being smaller than the first compression ratio, characterized in that each of the two pistons (302, 304) has a respective piston crown comprising one or more swirl canceling features (202, 204). operating a diesel opposed piston engine with a first compression ratio to supply engine power in response to a first engine load, the diesel opposed piston engine comprising a combustion chamber defined at least in part by crowns of two pistons (302, 304) each individually coupled to one of two crankshafts, and changing the first compression ratio to a second compression ratio to supply engine power in response to a second engine load, the second engine load being larger than the first engine load, the second compression ratio being smaller than the first compression ratio, characterized in that each of the two pistons (302, 304) has a respective piston crown comprising one or more swirl canceling features (202, 204).