mhurhangee/patent-ind-claim-en huggingface dataset:
Device for controlling a steering angle in a bicycle handlebar, wherein the device comprises at least - a head tube , - a steering rod which runs through the head tube and is rotatably mounted in the head tube , - at least one spring element situated within the head tube , wherein the at least one spring element is designed, upon a rotational movement of the steering rod , to generate a force opposed to the rotational movement to control the rotational movement in dependence on the steering angle of the bicycle handlebar, wherein the spring element is connected to the steering rod , and the device additionally comprises at least one first stop which is arranged within the head tube , wherein the first stop is designed, upon a rotational movement of the steering rod , to compress the spring element in dependence on the steering angle, characterized in that a component of the first and/or of a second stop is designed to vary the force opposed to the rotational movement. - a head tube , - a steering rod which runs through the head tube and is rotatably mounted in the head tube , - at least one spring element situated within the head tube , wherein the at least one spring element is designed, upon a rotational movement of the steering rod , to generate a force opposed to the rotational movement to control the rotational movement in dependence on the steering angle of the bicycle handlebar,
Cryogenic preservation or vitrification device , comprising: - an accumulator including a first volume of pressurised hydraulic oil (V 1H ); - a control system controlling a valve capable of releasing a second volume of hydraulic oil (V 2H ) from the accumulator toward a cylinder by means of a pipe ; - a cylinder including a piston configured to be driven by the second volume of hydraulic oil (V 2H ) and to drive a first volume of cryogenic fluid (V 1A ) in a cryogenic vessel intended to receive a sample to be cryogenically preserved. - an accumulator including a first volume of pressurised hydraulic oil (V 1H ); - a control system controlling a valve capable of releasing a second volume of hydraulic oil (V 2H ) from the accumulator toward a cylinder by means of a pipe ; - a cylinder including a piston configured to be driven by the second volume of hydraulic oil (V 2H ) and to drive a first volume of cryogenic fluid (V 1A ) in a cryogenic vessel intended to receive a sample to be cryogenically preserved.
A spinning unit comprising: a spinning device adapted to produce a spun yarn by twisting a fiber bundle , a yarn joining device , a suction pipe , a yarn accumulating device comprising a yarn accumulating roller provided downstream of the spinning device in a yarn travelling direction and adapted to accumulate the spun yarn by rotating and winding the spun yarn around an outer peripheral surface thereof, a yarn hooking member arranged downstream of the yarn accumulating roller and adapted to wind the spun yarn around the outer peripheral surface of the yarn accumulating roller by rotating with the yarn accumulating roller while being in contact with the spun yarn , and a yarn removing member adapted to remove the spun yarn from the yarn hooking member , characterized by at least one yarn removal detecting section adapted to detect a removal of the spun yarn from the yarn hooking member . a spinning device adapted to produce a spun yarn by twisting a fiber bundle , a yarn joining device , a suction pipe , a yarn accumulating device comprising a yarn accumulating roller provided downstream of the spinning device in a yarn travelling direction and adapted to accumulate the spun yarn by rotating and winding the spun yarn around an outer peripheral surface thereof, a yarn hooking member arranged downstream of the yarn accumulating roller and adapted to wind the spun yarn around the outer peripheral surface of the yarn accumulating roller by rotating with the yarn accumulating roller while being in contact with the spun yarn , and a yarn removing member adapted to remove the spun yarn from the yarn hooking member , characterized by at least one yarn removal detecting section adapted to detect a removal of the spun yarn from the yarn hooking member .
An aortic arch embolic protection device having an upstream end and a downstream end, comprising: an anchoring structure comprising a first anchoring ring at the upstream end and a second anchoring ring at the downstream end; a first filter element extending from the first anchoring ring to the second anchoring ring and defining a lumen through the aortic arch embolic protection device ; and a second filter element extending transversely across the lumen of the first filter element at a plurality of axial locations along a longitudinal axis of the lumen; wherein the second filter element includes an access port configured to facilitate passage of an interventional catheter through the access port . an anchoring structure comprising a first anchoring ring at the upstream end and a second anchoring ring at the downstream end; a first filter element extending from the first anchoring ring to the second anchoring ring and defining a lumen through the aortic arch embolic protection device ; and a second filter element extending transversely across the lumen of the first filter element at a plurality of axial locations along a longitudinal axis of the lumen; wherein the second filter element includes an access port configured to facilitate passage of an interventional catheter through the access port .
Use of an alkoxylated polyethylene glycol of general formula (II) wherein m is an integer in the range of ≥ 1 to ≤ 50, m' is an integer in the range of ≥ 1 to ≤ 50, (m+m') is an integer in the range of ≥ 3 to ≤ 65, n is an integer in the range of ≥ 0 to ≤ 75, n' is an integer in the range of ≥ 0 to ≤ 75, p is an integer in the range of ≥ 0 to ≤ 90, p' is an integer in the range of ≥ 0 to ≤ 90, k is an integer in the range of ≥ 2 to ≤ 50, R 1 denotes an unsubstituted, linear alkyl radical having 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, or 18 carbon atoms, R 2 denotes -CH 2 -CH 3 , and R 3 denotes -CH 3 , whereby the concatenations denoted by k are distributed to form a block polymeric structure and the concatenations denoted by p, p', n, n', m and m' are distributed to form a block polymeric structure or a random polymeric structure, wherein the alkoxylated polyethylene glycol has a weight average molecular weight Mw in the range of 500 to 20000 g/mol determined according to DIN 55672-1 (polystyrene calibration standard), and wherein the ratio of (m+m') to k is in the range of 0.5:1 to 4:1, wherein in case the alkoxylated polyethylene glycol comprises units, wherein R 2 denotes -CH 2 -CH 3 the ratio of (n+n') to k is in the range of 1:1 to 7:1, wherein in case the alkoxylated polyethylene glycol comprises units, wherein R 3 denotes -CH 3 the ratio of (p+p') to k is in the range of 0.8:1 to 5:1, as lubricant, which is capable of reducing friction between surfaces. m is an integer in the range of ≥ 1 to ≤ 50, m' is an integer in the range of ≥ 1 to ≤ 50, (m+m') is an integer in the range of ≥ 3 to ≤ 65, n is an integer in the range of ≥ 0 to ≤ 75, n' is an integer in the range of ≥ 0 to ≤ 75, p is an integer in the range of ≥ 0 to ≤ 90, p' is an integer in the range of ≥ 0 to ≤ 90, k is an integer in the range of ≥ 2 to ≤ 50, R 1 denotes an unsubstituted, linear alkyl radical having 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, or 18 carbon atoms, R 2 denotes -CH 2 -CH 3 , and R 3 denotes -CH 3 ,
An environmental control system of an aircraft, comprising: a ram air circuit including a ram air shell having at least one heat exchanger positioned therein; a dehumidification system arranged in fluid communication with the ram air circuit; and a plurality of compressing devices arranged in fluid communication with the ram air circuit and the dehumidification system, wherein each of the plurality of compressing devices further includes: a turbine comprising a first inlet and a second inlet and configured to provide energy by expanding one or more mediums, the environmental control system being configured such that the first inlet receives a first medium of the one or more mediums and the second inlet receives a second medium of the one or more mediums; and a compressor , the environmental control system being configured such that the compressor receives energy from at least one of the first medium and the second mediums being expanded across the turbine, and compresses the second medium. a ram air circuit including a ram air shell having at least one heat exchanger positioned therein; a dehumidification system arranged in fluid communication with the ram air circuit; and a plurality of compressing devices arranged in fluid communication with the ram air circuit and the dehumidification system, wherein each of the plurality of compressing devices further includes: a turbine comprising a first inlet and a second inlet and configured to provide energy by expanding one or more mediums, the environmental control system being configured such that the first inlet receives a first medium of the one or more mediums and the second inlet receives a second medium of the one or more mediums; and a compressor , the environmental control system being configured such that the compressor receives energy from at least one of the first medium and the second mediums being expanded across the turbine, and compresses the second medium. a turbine comprising a first inlet and a second inlet and configured to provide energy by expanding one or more mediums, the environmental control system being configured such that the first inlet receives a first medium of the one or more mediums and the second inlet receives a second medium of the one or more mediums; and a compressor , the environmental control system being configured such that the compressor receives energy from at least one of the first medium and the second mediums being expanded across the turbine, and compresses the second medium.
A method for calibrating a machine for the production of rod-shaped articles, the machine comprising a plurality of conveyors , each provided with a plurality of flutes for accommodating the articles, comprising the following steps: - placing a sample product in a first flute (I) of a first conveyor associated with at least one sensor; - performing, with the at least one sensor, at least one measurement on the sample product held in the first flute (I) of the first conveyor while the sample product is moved according to an operating movement of the first conveyor ; - transferring the sample product from the first conveyor to a flute of a second conveyor ; displacing the first conveyor and the second conveyor from each other; - transferring the sample product from the second conveyor to a second flute (II) of the first conveyor , different from the first flute (I); - repeating the step of measuring while the sample product held in the second flute (II) is moved according to an operating movement of the first conveyor ; processing in a control unit the values obtained from the measurements performed by comparing the values measured by the at least one sensor with a theoretical value so as to calibrate the at least one sensor. - placing a sample product in a first flute (I) of a first conveyor associated with at least one sensor; - performing, with the at least one sensor, at least one measurement on the sample product held in the first flute (I) of the first conveyor while the sample product is moved according to an operating movement of the first conveyor ; - transferring the sample product from the first conveyor to a flute of a second conveyor ; - transferring the sample product from the second conveyor to a second flute (II) of the first conveyor , different from the first flute (I); - repeating the step of measuring while the sample product held in the second flute (II) is moved according to an operating movement of the first conveyor ;
A wing airframe for a wing of a tiltrotor aircraft , the tiltrotor aircraft including a pylon assembly subject to aeroelastic movement during forward flight, and the wing subject to deflection in response to the aeroelastic movement of the pylon assembly , comprising: a wing airframe core assembly ; and a wing skin assembly disposed on the wing airframe core assembly , the wing skin assembly including an outer skin and a damping sublayer , the damping sublayer interposed between the outer skin and the wing airframe core assembly; wherein the wing skin assembly further comprises an inner skin interposed between the damping sublayer and the wing airframe core assembly such that the damping sublayer is sandwiched between the inner and outer skins; wherein the damping sublayer , the outer skin and the inner skin have aligned forward and aft edges; wherein the damping sublayer is configured to reduce the deflection of the wing, thereby stabilizing the wing during forward flight; and characterised in that the damping sublayer further comprises an elastomeric material including a rubber compound having a loss tangent greater than natural rubber. a wing airframe core assembly ; and a wing skin assembly disposed on the wing airframe core assembly , the wing skin assembly including an outer skin and a damping sublayer , the damping sublayer interposed between the outer skin and the wing airframe core assembly; wherein the wing skin assembly further comprises an inner skin interposed between the damping sublayer and the wing airframe core assembly such that the damping sublayer is sandwiched between the inner and outer skins; wherein the damping sublayer , the outer skin and the inner skin have aligned forward and aft edges; wherein the damping sublayer is configured to reduce the deflection of the wing, thereby stabilizing the wing during forward flight; and characterised in that the damping sublayer further comprises an elastomeric material including a rubber compound having a loss tangent greater than natural rubber.
Method for determining the colour deviation of at least one print decoration applied to at least one carrier material from a print template Comprising the steps - Recording of at least one NIR spectrum of several reference samples with the print template using at least one NIR measuring head in a wavelength range between 900 nm and 2500 nm, - Applying the at least one printed decoration to the at least one carrier material by means of printing, - recording at least one NIR spectrum of the carrier material printed with the print decoration using the at least one NIR measuring head in a wavelength range between 900 nm and 2500 nm, and - Determining the colour deviation of the print decor from the print template in a wavelength range between 1350 and 1600 nm with a parallel shift of the measured NIR spectra of the print decor from the measured NIR spectra of the print template, or - Determining the colour deviation of the print decor from the print template in different wavelength ranges, where the wavelength range of the print decor is between 1100 and 1200 nm and the wavelength range of the print template is between 1400 and 1600 nm. - Recording of at least one NIR spectrum of several reference samples with the print template using at least one NIR measuring head in a wavelength range between 900 nm and 2500 nm, - Applying the at least one printed decoration to the at least one carrier material by means of printing, - recording at least one NIR spectrum of the carrier material printed with the print decoration using the at least one NIR measuring head in a wavelength range between 900 nm and 2500 nm, and - Determining the colour deviation of the print decor from the print template in a wavelength range between 1350 and 1600 nm with a parallel shift of the measured NIR spectra of the print decor from the measured NIR spectra of the print template, or - Determining the colour deviation of the print decor from the print template in different wavelength ranges, where the wavelength range of the print decor is between 1100 and 1200 nm and the wavelength range of the print template is between 1400 and 1600 nm.
An aerosol-generating device comprising: a first heater configured to heat a first aerosol-generating substrate such that a first aerosol is generated at a first vaporization temperature; a second heater configured to heat a second aerosol-generating substrate such that a second aerosol is generated at a second vaporization temperature; a battery configured to supply power to the first heater and the second heater; and a controller configured to control power supplied to the first heater and the second heater such that the first heater and the second heater are preheated in a preheating section and the first heater is maintained at a preset temperature in a smoking section, wherein the controller starts preheating the second heater after the preheating of the first heater starts and before the preheating of the first heater is completed, in the preheating section. a first heater configured to heat a first aerosol-generating substrate such that a first aerosol is generated at a first vaporization temperature; a second heater configured to heat a second aerosol-generating substrate such that a second aerosol is generated at a second vaporization temperature; a battery configured to supply power to the first heater and the second heater; and a controller configured to control power supplied to the first heater and the second heater such that the first heater and the second heater are preheated in a preheating section and the first heater is maintained at a preset temperature in a smoking section, wherein the controller starts preheating the second heater after the preheating of the first heater starts and before the preheating of the first heater is completed, in the preheating section.
Headlamp for vehicles with a first light module containing at least one LED light source and a first optical unit and with a second light module containing at least one LED light source and a second optical unit , where the first light module is designed in such a way that a low-beam distribution can be generated as a basic light distribution and that the second light module is designed in such a way that an additional light distribution at least partially overlapping the low-beam distribution , characterized in that an LED field of the second light module is designed in such a way and/or interacts with the second optical unit in such a way that a second light bundle with a horizontal aperture angle (α 2 ) of a maximum of 10° and a vertical aperture angle (β 2 ) of a maximum of 0.5° is emitted to form a highway light distribution.
DNA vaccine comprising a polynucleotide sequence which encodes a fusion protein or an expression vector or plasmid comprising said polynucleotide sequence, said fusion protein being SEQ ID NO:32.
A gas turbine engine comprising: a propulsion unit including a fan , and a free turbine connected to drive said fan about a first axis (C); and a plurality of core engines , said core engines each including at least a compressor , a combustion section , and a turbine , said core engine turbine connected to drive said compressor, and said compressor and said core engine turbine rotating about a second axis (X); said plurality of core engines having an output from said core engine turbines passing over said free turbine; and said propulsion unit being positioned forwardly, and toward an inlet of the gas turbine engine relative to said core engines, and said core engines spaced rearwardly of the propulsion unit, and being separate from said propulsion unit; characterised in that said core engines are mounted to rotate about the second axis (X) which is non-parallel to the first axis (C) of said fan. a propulsion unit including a fan , and a free turbine connected to drive said fan about a first axis (C); and a plurality of core engines , said core engines each including at least a compressor , a combustion section , and a turbine , said core engine turbine connected to drive said compressor, and said compressor and said core engine turbine rotating about a second axis (X); said plurality of core engines having an output from said core engine turbines passing over said free turbine; and said propulsion unit being positioned forwardly, and toward an inlet of the gas turbine engine relative to said core engines, and said core engines spaced rearwardly of the propulsion unit, and being separate from said propulsion unit; characterised in that said core engines are mounted to rotate about the second axis (X) which is non-parallel to the first axis (C) of said fan.
A transmission controller which controls a transmission ratio of a toroidal continuously variable transmission which continuously changes the transmission ratio based on a tilt motion angle of a power roller, the transmission controller comprising: an actuator which changes a roller position of the power roller to adjust the tilt motion angle; a tilt motion angle information generation unit which generates information (cpest) of the tilt motion angle (φ); a position estimation unit which derives an estimated value (Xest) of the roller position (X); and a position control unit which derives an operation command value (Iref) of the actuator so that a deviation between a command value (Xref) of the roller position (X) and the estimated value (Xest) of the roller position (X) is cancelled, wherein the position estimation unit is configured to derive the estimated value (Xest)based on the information (cpest) of the tilt motion angle (φ) which is generated by the tilt motion angle information generation unit , and the operation command value (Iref), characterized in that the position estimation unit is configured to compensate the estimated value (Xest) based on environment parameters which affects an operation of the power roller , the environment parameters including a hydraulic oil temperature (T) of the actuator and an input rotation speed (N) of the toroidal continuously variable transmission . an actuator which changes a roller position of the power roller to adjust the tilt motion angle; a tilt motion angle information generation unit which generates information (cpest) of the tilt motion angle (φ); a position estimation unit which derives an estimated value (Xest) of the roller position (X); and a position control unit which derives an operation command value (Iref) of the actuator so that a deviation between a command value (Xref) of the roller position (X) and the estimated value (Xest) of the roller position (X) is cancelled, wherein the position estimation unit is configured to derive the estimated value (Xest)based on the information (cpest) of the tilt motion angle (φ) which is generated by the tilt motion angle information generation unit , and the operation command value (Iref), characterized in that the position estimation unit is configured to compensate the estimated value (Xest) based on environment parameters which affects an operation of the power roller , the environment parameters including a hydraulic oil temperature (T) of the actuator and an input rotation speed (N) of the toroidal continuously variable transmission .