mhurhangee/patent-ind-claim-en huggingface dataset:
Monitoring system for monitoring a kinematic coupling between an actuator and a controlled element of an aircraft, wherein the monitoring system comprises: a first sensor , which is arranged such that it senses an operative movement of the actuator and, on the basis of the sensed operative movement of the actuator, provides a first signal; a second sensor , which is arranged such that it senses a movement of the controlled element and, on the basis of the sensed movement of the controlled element, provides a second signal; a computing unit , which is connected to the first sensor and the second sensor and is designed to receive the first signal and the second signal; wherein the computing unit is designed to determine, on the basis of the first signal, an anticipated movement of the controlled element and to compare the anticipated movement with the sensed movement corresponding to the second signal and to provide a deviation between the anticipated movement and the sensed movement; wherein the computing unit is designed to partially undertake a task which is usually carried out by a dedicated testing apparatus at predefined maintenance intervals on the ground, and to carry out this task during operation of the aircraft in the air; wherein the computing unit is designed to respond to a deviation between the anticipated movement and the sensed movement that exceeds a threshold value by outputting a warning of this deviation, causing the aircraft to be sent for detailed inspection. a first sensor , which is arranged such that it senses an operative movement of the actuator and, on the basis of the sensed operative movement of the actuator, provides a first signal; a second sensor , which is arranged such that it senses a movement of the controlled element and, on the basis of the sensed movement of the controlled element, provides a second signal; a computing unit , which is connected to the first sensor and the second sensor and is designed to receive the first signal and the second signal; wherein the computing unit is designed to determine, on the basis of the first signal, an anticipated movement of the controlled element and to compare the anticipated movement with the sensed movement corresponding to the second signal and to provide a deviation between the anticipated movement and the sensed movement; wherein the computing unit is designed to partially undertake a task which is usually carried out by a dedicated testing apparatus at predefined maintenance intervals on the ground, and to carry out this task during operation of the aircraft in the air; wherein the computing unit is designed to respond to a deviation between the anticipated movement and the sensed movement that exceeds a threshold value by outputting a warning of this deviation, causing the aircraft to be sent for detailed inspection.
A water treatment composition, comprising a unitary structure formed from a blend of: (i) 50 - 99.25 wt.% of a particulate halogen-releasing compound comprising chlorinated isocyanuric acids; and (ii) 0.75 - 2.0 wt.% of particulate fluoropolymer to slow the dissolution rate of the halogen-releasing compound in water, wherein all weight percentages are based on the total weight of said composition. (i) 50 - 99.25 wt.% of a particulate halogen-releasing compound comprising chlorinated isocyanuric acids; and (ii) 0.75 - 2.0 wt.% of particulate fluoropolymer to slow the dissolution rate of the halogen-releasing compound in water,
Stable nanosuspension comprising nanoparticles of methyl {4,6-diamino-2-[5-fluoro-1-(2-fluorobenzyl)-1H-pyrazolo[3,4-b]pyridin-3-yl]pyrimidin-5-yl}carbamate of the formula (I) in crystalline form of modification I, characterized in that the x-ray diffractogram of the compound exhibits peak maxima of the 2 theta angle at 5.9, 6.9, 22.7, and one or more stabilizer(s) in a dispersing agent, wherein the one or more stabilizer is polyvinylpyrrolidone (PVP) in combination with sodium dodecylsulfate (SDS), or selected from the group consisting of vinylpyrrolidone-vinyl acetate copolymer, ethylene oxide-propylene oxide block copolymer, sodium dodecylsulfate (SDS), hydroxypropylmethylcellulose (HPMC), polysorbate, hydroxypropylcellulose (HPC), polyoxyl-35 castor oil, polyoxyl 15 hydroxystearate, Na-desoxycholate, and combinations thereof, the maximum concentration of the one or more stabilizer(s) is the solubility limit of the stabilizer(s) in the suspension, the dispersing agent is selected from the group consisting of water, primary, secondary, and tertiary alcohols, and polyvalent alcohols, the nanoparticles have an average particle size, expressed as d50, of 500 nm or less, and the average particle size, expressed as d50, remains at 500 nm or less at storage for at least one week at a temperature of at least 40°C. in crystalline form of modification I, characterized in that the x-ray diffractogram of the compound exhibits peak maxima of the 2 theta angle at 5.9, 6.9, 22.7, and one or more stabilizer(s) in a dispersing agent, wherein the one or more stabilizer is polyvinylpyrrolidone (PVP) in combination with sodium dodecylsulfate (SDS), or selected from the group consisting of vinylpyrrolidone-vinyl acetate copolymer, ethylene oxide-propylene oxide block copolymer, sodium dodecylsulfate (SDS), hydroxypropylmethylcellulose (HPMC), polysorbate, hydroxypropylcellulose (HPC), polyoxyl-35 castor oil, polyoxyl 15 hydroxystearate, Na-desoxycholate, and combinations thereof, the maximum concentration of the one or more stabilizer(s) is the solubility limit of the stabilizer(s) in the suspension, the dispersing agent is selected from the group consisting of water, primary, secondary, and tertiary alcohols, and polyvalent alcohols, the nanoparticles have an average particle size, expressed as d50, of 500 nm or less, and the average particle size, expressed as d50, remains at 500 nm or less at storage for at least one week at a temperature of at least 40°C.
A boom for an electrical harness, comprising a straight bar extending in a longitudinal direction and having first and second ends (22.1, 22.2) configured so they can be removably attached to at least one support during operation, and several supports distributed along and attached to the bar , to which supports at least one electrical harness (H) is attached in operation, the bar comprising at least two parts configured so as to slide relative to one another in the longitudinal direction, a first part being attached to the first end (22.1) and a second part being attached to the second end (22.2), characterized in that at least one of the first and second parts comprises a tube having an outer surface (S36Ext) provided with longitudinal splines which extend over almost the entire length of the tube and are evenly distributed over its entire circumference.
Floor mat arrangement for riding places, comprising a plurality of mutually interconnected grid elements and a cover layer positioned on the top of the grid elements in which the grid elements each comprise a plurality of through going holes , and the grid elements have a water storage capacity, characterized in that in a number of the openings respective cups are positioned so that the open upper side of the cups face upwards to the cover layer , wherein the combined volume of the cups determines said water storage capacity, and the number of the cups is determined in correspondence with the water supply need of the riding place to ensure the required humidity thereof.
Key cylinder comprising - a cylinder core with a key way for inserting a corresponding key , - a cylinder cam for operating a locking bolt, and - a blocking washer , - wherein the blocking washer is inserted between the cylinder core and the cylinder cam or in a slot of the cylinder core such that the cylinder cam is located on a first side and any core pin is located on a second side of the blocking washer , and - wherein the blocking washer includes at least one cutout or at least one protrusion extending in a direction in which a key has to be inserted into the key cylinder - characterized in that the protrusion and/or the cutout are point symmetric to a central point of the protrusion and/or cutout and comprise a code pattern which is set up by the three letters O S O. - a cylinder core with a key way for inserting a corresponding key , - a cylinder cam for operating a locking bolt, and - a blocking washer , - wherein the blocking washer is inserted between the cylinder core and the cylinder cam or in a slot of the cylinder core such that the cylinder cam is located on a first side and any core pin is located on a second side of the blocking washer , and - wherein the blocking washer includes at least one cutout or at least one protrusion extending in a direction in which a key has to be inserted into the key cylinder - characterized in that the protrusion and/or the cutout are point symmetric to a central point of the protrusion and/or cutout and comprise a code pattern which is set up by the three letters O S O.
A method of operating a terminal device of a wireless communications network, the terminal device being operable in one or more modes, the one or more modes including one or more discontinuous reception, DRX, modes, the method comprising: selecting a duration for an inactivity timer of the DRX mode, wherein the step of selecting the duration for the inactivity timer comprises selecting the duration from a plurality of different durations, wherein durations are defined in RRC signalling from a network node of the wireless communications network to the terminal device; and wherein the step of selecting the duration for the inactivity timer comprises selecting the duration based on a characteristic of wireless traffic received or transmitted by the terminal device; upon receiving or transmitting one or more wireless communications, starting the inactivity timer; and responsive to a determination that the duration for the inactivity timer has expired without the terminal device receiving or transmitting one or more further wireless communications, entering a DRX sleep state. selecting a duration for an inactivity timer of the DRX mode, wherein the step of selecting the duration for the inactivity timer comprises selecting the duration from a plurality of different durations, wherein durations are defined in RRC signalling from a network node of the wireless communications network to the terminal device; and wherein the step of selecting the duration for the inactivity timer comprises selecting the duration based on a characteristic of wireless traffic received or transmitted by the terminal device; upon receiving or transmitting one or more wireless communications, starting the inactivity timer; and responsive to a determination that the duration for the inactivity timer has expired without the terminal device receiving or transmitting one or more further wireless communications, entering a DRX sleep state.
A composite membrane comprising: a first polymer layer comprising a first coating composition comprising polymeric material and no fibres; and a second polymer layer adjacent to the first polymer layer, the second polymer layer comprising a second coating composition comprising polymeric material and fibres; and an additional polymer layer adjacent to the second polymer layer, the additional polymer layer comprising a third coating composition comprising polymer material and no fibres; wherein the composite membrane has fibre-free regions on both membrane faces, wherein the fibres are present in the membrane as a network of randomly orientated individual fibres, and wherein the first, second and additional polymer layers comprise an ion-conducting polymer.
Method, in the case of which at least one electrically operated actuator of a vehicle brake system is actuated in a manner which is dependent on a brake request of a vehicle control system, as a result of which a driver-independent build-up of torque takes place at one or more vehicle wheels, a supply voltage of the vehicle on-board electric system being raised, which supply voltage prevails at the electrically operated actuator or actuators, if at least one predefined condition is fulfilled, characterized in that the supply voltage is reset again to the original value as soon as none of the predefined conditions are fulfilled any longer or a standstill of the vehicle is detected, and the supply voltage is reset again to the original value only after no brake request of a vehicle control system has been input for a predefined time period.
A computer-implemented method comprising: receiving input regarding weight of a patient; receiving input regarding hematocrit of blood of the patient; setting a low hematocrit limit (LL Hct ) for the patient; calculating a patient's blood volume (PBV) based on the input regarding the weight of the patient; and calculating a red cell volume (RCV) based on the patient's blood volume and the input regarding the hematocrit of the patient, determining an "on-pump" hematocrit of the patient by dividing a red blood cell volume (RCV) by the sum of the patient's blood volume (PBV), a prime volume of a pump and an intravenous volume, i.e. "on-pump" hematocrit of the patient = RCV/(PBV + pump prime volume + IV volume); and calculating, based on the input regarding the weight of the patient and the input regarding the hematocrit of the blood of the patient, a volume of hematocrit-free fluid that the patient can receive into a blood compartment of the patient until the low hematocrit limit is reached; and displaying the volume of hematocrit-free fluid that the patient can receive until the lower hematocrit level is reached, wherein the volume of hematocrit-free fluid (FVL) is calculated by subtracting the patient's blood volume (PBV), the prime volume of the pump and the intravenous volume from the red blood cell volume (RCV) divided by the set hematocrit low limit (LL Hct ), i.e. FVL = (RCV/LL Hct ) - PBV - pump prime volume - IV volume. receiving input regarding weight of a patient; receiving input regarding hematocrit of blood of the patient; setting a low hematocrit limit (LL Hct ) for the patient; calculating a patient's blood volume (PBV) based on the input regarding the weight of the patient; and calculating a red cell volume (RCV) based on the patient's blood volume and the input regarding the hematocrit of the patient, determining an "on-pump" hematocrit of the patient by dividing a red blood cell volume (RCV) by the sum of the patient's blood volume (PBV), a prime volume of a pump and an intravenous volume, i.e. "on-pump" hematocrit of the patient = RCV/(PBV + pump prime volume + IV volume); and calculating, based on the input regarding the weight of the patient and the input regarding the hematocrit of the blood of the patient, a volume of hematocrit-free fluid that the patient can receive into a blood compartment of the patient until the low hematocrit limit is reached; and displaying the volume of hematocrit-free fluid that the patient can receive until the lower hematocrit level is reached, wherein the volume of hematocrit-free fluid (FVL) is calculated by subtracting the patient's blood volume (PBV), the prime volume of the pump and the intravenous volume from the red blood cell volume (RCV) divided by the set hematocrit low limit (LL Hct ), i.e. FVL = (RCV/LL Hct ) - PBV - pump prime volume - IV volume.
A composite filter having at least one coarse filter fabric and at least one fine filter fabric , characterized in that into the coarse filter fabric hot melt adhesive threads are woven which have a surface that can be melted at least in some areas, and that this surface that can be melted forms itself the adhesive by melting in order to adhere at least in some areas to the threads of the fine filter fabric . that into the coarse filter fabric hot melt adhesive threads are woven which have a surface that can be melted at least in some areas, and that this surface that can be melted forms itself the adhesive by melting in order to adhere at least in some areas to the threads of the fine filter fabric .
A rotary winged aircraft , comprising: an airframe ; a main rotor assembly ; an engine disposed at the airframe and operably connected to the main rotor assembly to drive the main rotor assembly ; a firewall through which an inlet duct can extend into an engine compartment of the aircraft ; and an engine inlet assembly comprising: the inlet duct which includes a first inlet duct leg and a second inlet duct leg , the first inlet duct leg and the second inlet duct leg extending toward a common inlet duct outlet disposed at an engine inlet; wherein the first inlet duct leg and the second inlet duct leg are fixedly secured to the airframe of the aircraft at an air inlet, wherein the inlet duct extends through an opening in the firewall into an engine compartment of the aircraft , wherein the inlet duct outlet has a floating interface with the engine inlet and the inlet duct is configured to direct an airflow to the engine inlet, and wherein the firewall has an airtight seal to the engine inlet radially outboard on the inlet duct via a flexible bellows seal to prevent ingestion of an engine compartment airflow into the engine inlet. an airframe ; a main rotor assembly ; an engine disposed at the airframe and operably connected to the main rotor assembly to drive the main rotor assembly ; a firewall through which an inlet duct can extend into an engine compartment of the aircraft ; and an engine inlet assembly comprising: the inlet duct which includes a first inlet duct leg and a second inlet duct leg , the first inlet duct leg and the second inlet duct leg extending toward a common inlet duct outlet disposed at an engine inlet; wherein the first inlet duct leg and the second inlet duct leg are fixedly secured to the airframe of the aircraft at an air inlet, wherein the inlet duct extends through an opening in the firewall into an engine compartment of the aircraft , wherein the inlet duct outlet has a floating interface with the engine inlet and the inlet duct is configured to direct an airflow to the engine inlet, and wherein the firewall has an airtight seal to the engine inlet radially outboard on the inlet duct via a flexible bellows seal to prevent ingestion of an engine compartment airflow into the engine inlet. the inlet duct which includes a first inlet duct leg and a second inlet duct leg , the first inlet duct leg and the second inlet duct leg extending toward a common inlet duct outlet disposed at an engine inlet; wherein the first inlet duct leg and the second inlet duct leg are fixedly secured to the airframe of the aircraft at an air inlet, wherein the inlet duct extends through an opening in the firewall into an engine compartment of the aircraft , wherein the inlet duct outlet has a floating interface with the engine inlet and the inlet duct is configured to direct an airflow to the engine inlet, and wherein the firewall has an airtight seal to the engine inlet radially outboard on the inlet duct via a flexible bellows seal to prevent ingestion of an engine compartment airflow into the engine inlet.
An optical system comprising: an infrared illuminator (126, 237A-237E, 337A-337H, 337I-337U, 537) configured to direct narrow-band infrared illumination light to an eyebox area for eye-tracking; a camera configured to capture eye-tracking images of an eye of a user; a combiner layer configured to receive reflected infrared light of the narrow-band infrared illumination light reflecting off the eye of the user and direct the reflected infrared light to the camera to generate the eye-tracking images; and an anti-reflection, AR, coating disposed on a base curvature , wherein a transmission spectrum of the AR coating is tuned for very-high transmission for visible light over a first angle of incidence, AOI, range and very-high transmission for a narrow-band of infrared light over a second AOI range, the narrow-band of infrared light corresponding to the narrow-band infrared illumination light. an infrared illuminator (126, 237A-237E, 337A-337H, 337I-337U, 537) configured to direct narrow-band infrared illumination light to an eyebox area for eye-tracking; a camera configured to capture eye-tracking images of an eye of a user; a combiner layer configured to receive reflected infrared light of the narrow-band infrared illumination light reflecting off the eye of the user and direct the reflected infrared light to the camera to generate the eye-tracking images; and an anti-reflection, AR, coating disposed on a base curvature , wherein a transmission spectrum of the AR coating is tuned for very-high transmission for visible light over a first angle of incidence, AOI, range and very-high transmission for a narrow-band of infrared light over a second AOI range, the narrow-band of infrared light corresponding to the narrow-band infrared illumination light.
A peristaltic pump comprising a motor , a rotor coupled to the motor , a housing in which the rotor is arranged, an opening and closing mechanism comprising a tube pressuring portion , a slider and a pivotable cover coupled to the housing and the slider , said opening and closing mechanism further comprising an elastic element connected to the slider and the tube pressuring portion so that a tube engaging surface of the tube pressuring portion slides towards and away from the rotor upon closing and opening of the pivotable cover , respectively, characterized in that the housing comprises a first adjustable motion link , the tube pressuring portion comprises a frame that extends into the housing said frame comprising at least two guiding elements and in that the tube pressuring portion's movement towards and away from the rotor is guided by the at least two guiding elements , which interact with the first adjustable motion link and in that the tube pressuring portion comprises an adjustment element to which the elastic element is connected so that the tension in the elastic element can be adjusted, the opening and closing mechanism further comprising a post attached to the slider , the pivotable cover comprising a rotating shaft having an extension extending perpendicular to a longitudinal direction defined by the rotating shaft , said extension being configured to engage the post for moving the slider and via the elastic element also the tube pressuring portion away and towards a top of the housing , when the pivotable cover is opened and closed, respectively.
A mounting apparatus , in particular for mounting insulating material dowels, comprising: a drive train , a transmission element for transmission of a movement of the drive train on a fastening element, and a stop disc , characterized in that the mounting apparatus comprises a guiding sleeve for guiding the fastening element during the arranging of the fastening element at the transmission element , the guiding sleeve being arranged resiliently at the remaining mounting apparatus . a drive train , a transmission element for transmission of a movement of the drive train on a fastening element, and a stop disc , characterized in that the mounting apparatus comprises a guiding sleeve for guiding the fastening element during the arranging of the fastening element at the transmission element , the guiding sleeve being arranged resiliently at the remaining mounting apparatus .