mhurhangee/patent-ind-claim-en huggingface dataset:
A maneuverable measurement body for determining measurement data during its passage through a fluid, at least comprising two airfoils that are arranged in the central region of the measurement body , multiple controllable rudders that can be adjusted about their axes of rotation , a malfunction module that is automatically activated in the event of a malfunction and has at least a first malfunction system for resetting the rudders into their central zero position, as well as accumulators for the electrical power supply and sensors for determining the measurement data and the position of the measurement body , characterized in that the first malfunction system has a pressure cylinder with an extendable piston per rudder , wherein each piston has a piston head and a piston rod , which is fastened on the piston head and has a guide element that can be moved into a receiving element , wherein each receiving element is rigidly arranged on the respective rudder about its axis of rotation and has a contour channeling into its central zero position, wherein said first malfunction system comprises a common pressure vessel that is connected to the pressure cylinders via fluid lines and has an electromagnetic stop valve , which is automatically opened upon an activation of the malfunction module , and wherein all pistons are extended when the piston heads are acted upon with pressure by the fluid.
A transmitting power determination method, applied to a communication device, characterized by comprising: determining a comprehensive path loss according to a sidelink path loss of a first device, an uplink path loss of the first device, a first adjustment factor corresponding to the sidelink path loss and a second adjustment factor corresponding to the uplink path loss; determining transmitting power of the first device according to a third weight adjustment factor corresponding to the comprehensive path loss and the comprehensive path loss. determining a comprehensive path loss according to a sidelink path loss of a first device, an uplink path loss of the first device, a first adjustment factor corresponding to the sidelink path loss and a second adjustment factor corresponding to the uplink path loss; determining transmitting power of the first device according to a third weight adjustment factor corresponding to the comprehensive path loss and the comprehensive path loss.
An automated welding system comprising: a mounting platform ; a welding tool ; an imaging device configured to acquire data associated with an object ;the automated welding system being characterised by a controller configured to: receive the acquired data; determine an area to be welded in the acquired data; retrieve stored master model data associated with the object ; compare the acquired data to the stored master model data to identify a master model area in the acquired data; mask the master model area in the acquired data, such that the master model area is excluded from the area to be welded ; and generate control instructions for controlling at least one of said mounting platform and said welding tool to weld the area to be welded . a mounting platform ; a welding tool ; an imaging device configured to acquire data associated with an object ;the automated welding system being characterised by a controller configured to: receive the acquired data; determine an area to be welded in the acquired data; retrieve stored master model data associated with the object ; compare the acquired data to the stored master model data to identify a master model area in the acquired data; mask the master model area in the acquired data, such that the master model area is excluded from the area to be welded ; and generate control instructions for controlling at least one of said mounting platform and said welding tool to weld the area to be welded . receive the acquired data; determine an area to be welded in the acquired data; retrieve stored master model data associated with the object ; compare the acquired data to the stored master model data to identify a master model area in the acquired data; mask the master model area in the acquired data, such that the master model area is excluded from the area to be welded ; and generate control instructions for controlling at least one of said mounting platform and said welding tool to weld the area to be welded .
A turbofan engine comprising: a first spool including a first turbine ; a second spool including a second turbine disposed axially forward of the first turbine ; a first tower shaft engaged to the first spool ; a second tower shaft engaged to the second spool ; an accessory gearbox supporting a plurality of accessory components ; a superposition gear system disposed within the accessory gearbox , the superposition gear system including, a plurality of intermediate gears engaged to the sun gear and supported in a carrier and a ring gear circumscribing the intermediate gears , wherein the second tower shaft is engaged to drive the sun gear ; and characterized by a starter selectively coupled to the sun gear through a starter clutch ; a first clutch for selectively coupling the first tower shaft to the ring gear ; and a second clutch for selectively coupling the ring gear to a static structure of the engine . a first spool including a first turbine ; a second spool including a second turbine disposed axially forward of the first turbine ; a first tower shaft engaged to the first spool ; a second tower shaft engaged to the second spool ; an accessory gearbox supporting a plurality of accessory components ; a superposition gear system disposed within the accessory gearbox , the superposition gear system including, a plurality of intermediate gears engaged to the sun gear and supported in a carrier and a ring gear circumscribing the intermediate gears , wherein the second tower shaft is engaged to drive the sun gear ; and characterized by a starter selectively coupled to the sun gear through a starter clutch ; a first clutch for selectively coupling the first tower shaft to the ring gear ; and a second clutch for selectively coupling the ring gear to a static structure of the engine .
A pump including - a stator , - a rotor slidably and rotatably mounted at least partially in the stator, the rotor comprising a first axial extension having a first diameter (D1) and a second axial extension having a second diameter (D2) greater than the first diameter, - a first valve (V1) formed by a first valve seal mounted on the stator around the first axial extension, in conjunction with a first channel in the rotor that is configured to allow liquid communication across the first valve seal when the first valve is in an open position, - a second valve (V2) formed by a second valve seal mounted on the stator around the second axial extension, in conjunction with a second channel in the rotor that is configured to allow liquid communication across the second valve seal when the second valve is in an open position, and - a pump chamber formed between the rotor and stator and between the first valve seal and second valve seal, characterized in that the pump further comprises a priming actuator mounted on a housing of the stator and movable from a priming position to a locked operating position, the priming actuator configured to engage and axially displace the rotor from a priming position in which both first and second valves are open, to an operating position in which at least one of the first and second valves is closed. - a stator , - a rotor slidably and rotatably mounted at least partially in the stator, the rotor comprising a first axial extension having a first diameter (D1) and a second axial extension having a second diameter (D2) greater than the first diameter, - a first valve (V1) formed by a first valve seal mounted on the stator around the first axial extension, in conjunction with a first channel in the rotor that is configured to allow liquid communication across the first valve seal when the first valve is in an open position, - a second valve (V2) formed by a second valve seal mounted on the stator around the second axial extension, in conjunction with a second channel in the rotor that is configured to allow liquid communication across the second valve seal when the second valve is in an open position, and - a pump chamber formed between the rotor and stator and between the first valve seal and second valve seal,
Aircraft air conditioning system with: - a mixer , - a recirculation air line connected to the mixer , and adapted to be flown through with recirculation air taken from an aircraft cabin, in order to supply recirculation air to the mixer, - an ambient air line adapted to be flown through with ambient air and being connected to the mixer , in order to supply ambient air to the mixer , - at least one ambient air compressor arranged in the ambient air line for compressing the ambient air flowing through the ambient air line and - a refrigerating apparatus , which comprises a refrigerant circuit adapted to be flown through with a refrigerant as well as a refrigerant compressor arranged in the refrigerant circuit , wherein the refrigerant circuit is coupled thermally to the ambient air line , in order to transfer heat from the ambient air flowing through the ambient air line to the refrigerant circulating in the refrigerant circuit before the ambient air is supplied to the mixer , characterised by - a cabin exhaust air line , and - a cabin exhaust air turbine , which is connected to the cabin exhaust air line and is coupled to the at least one ambient air compressor arranged in the ambient air line and is configured to expand the cabin exhaust air flowing through the cabin exhaust air line and to drive the at least one ambient air compressor arranged in the ambient air line , wherein the refrigerating apparatus further comprises an evaporator , which thermally couples the refrigerant circuit and the recirculation air line , in order to transfer heat from the recirculation air flowing through the recirculation air line to the refrigerant flowing through the refrigerant circuit . - a mixer , - a recirculation air line connected to the mixer , and adapted to be flown through with recirculation air taken from an aircraft cabin, in order to supply recirculation air to the mixer, - an ambient air line adapted to be flown through with ambient air and being connected to the mixer , in order to supply ambient air to the mixer , - at least one ambient air compressor arranged in the ambient air line for compressing the ambient air flowing through the ambient air line and - a refrigerating apparatus , which comprises a refrigerant circuit adapted to be flown through with a refrigerant as well as a refrigerant compressor arranged in the refrigerant circuit , wherein the refrigerant circuit is coupled thermally to the ambient air line , in order to transfer heat from the ambient air flowing through the ambient air line to the refrigerant circulating in the refrigerant circuit before the ambient air is supplied to the mixer , characterised by - a cabin exhaust air line , and - a cabin exhaust air turbine , which is connected to the cabin exhaust air line and is coupled to the at least one ambient air compressor arranged in the ambient air line and is configured to expand the cabin exhaust air flowing through the cabin exhaust air line and to drive the at least one ambient air compressor arranged in the ambient air line ,
A door for a vehicle for the public transport of passengers comprising at least one leaf , said door comprising selective sealing means placed underneath the lower edge of said leaf and arranged to seal the interior space of said vehicle with respect to the exterior when said door is closed and so as not to obstruct the movement of said leaf during the opening of said door , said selective sealing means comprise an inflatable coil inflatable by means of a pneumatic system, said pneumatic system being the pneumatic opening system of said leaf , characterised in that , when it is inflated the coil occupies the entire gap at the bottom of said leaf to seal the interior of the vehicle, and in that when the body deflates it remains clung to said lower edge of said leaf , extending into said gap so as to avoid any friction with the floor of the vehicle, the coil being realized in polymeric material and being inflated at a pressure lower than 2 bar in order to avoid injures to passengers in said vehicle.
An electrolyte for a lithium-sulfur battery, the electrolyte comprising: a lithium salt; and a non-aqueous organic solvent, wherein the non-aqueous organic solvent includes: a first solvent consisting of a conjugated cyclic ether-based compound; a second solvent consisting of dimethoxyethane; and a third solvent consisting of a glyme-based compound represented by Chemical Formula 1: [Chemical Formula 1] R 1 (CH 2 CH 2 O) n R 2 wherein in Chemical Formula 1, R 1 and R 2 are the same as or different from each other, and each independently an alkyl group or alkoxy group having 1 to 10 carbon atoms; and n is an integer of 2 to 4, wherein, based on 100% by volume of the non-aqueous organic solvent including the first solvent, the second solvent and the third solvent, the first solvent is included in an amount of 20% by volume to 49% by volume; the second solvent is included in an amount of 50% by volume to 79% by volume; and the third solvent is included in an amount of greater than or equal to 1% by volume and less than 25% by volume. a lithium salt; and a non-aqueous organic solvent, wherein the non-aqueous organic solvent includes: a first solvent consisting of a conjugated cyclic ether-based compound; a second solvent consisting of dimethoxyethane; and a third solvent consisting of a glyme-based compound represented by Chemical Formula 1: [Chemical Formula 1] R 1 (CH 2 CH 2 O) n R 2 a first solvent consisting of a conjugated cyclic ether-based compound; a second solvent consisting of dimethoxyethane; and a third solvent consisting of a glyme-based compound represented by Chemical Formula 1: [Chemical Formula 1] R 1 (CH 2 CH 2 O) n R 2 wherein in Chemical Formula 1, R 1 and R 2 are the same as or different from each other, and each independently an alkyl group or alkoxy group having 1 to 10 carbon atoms; and n is an integer of 2 to 4, wherein, based on 100% by volume of the non-aqueous organic solvent including the first solvent, the second solvent and the third solvent, the first solvent is included in an amount of 20% by volume to 49% by volume; the second solvent is included in an amount of 50% by volume to 79% by volume; and the third solvent is included in an amount of greater than or equal to 1% by volume and less than 25% by volume.
A method for a propulsion arrangement for providing propulsive power to a marine vessel , comprising: - determining (S1) whether the vessel is running by means of the propulsion arrangement at a constant vessel speed, - storing (S3) a detected value (V1) of the constant vessel speed, - detecting (S4) a value (n1) of a rotational speed of a rotatable part of the propulsion arrangement while the vessel is running at the constant vessel speed, - storing (S5) the detected rotational speed value (n1), - subsequently controlling (S6) the propulsion arrangement so as to change the vessel speed, - subsequently repeating (S7-S11) the steps of determining whether the vessel is running at a constant vessel speed, storing a detected value (V2-V4) of the constant vessel speed, and detecting and storing a value (n2-n4) of the rotational speed of the rotatable part , to obtain a plurality of stored pairs of vessel speed values (V1-V4) and rotational speed values (n1-n4), - creating (S12) based at least partly on the stored pairs of values (V1-V4, n1-n4) a correlation record correlating vessel speed values with rotational speed values, characterized by - receiving (S13) a requested value (Vreq) of the vessel speed, - determining (S14) by means of the correlation record a rotational speed value (ncorr) that is correlated to the requested vessel speed value (Vreq), and - controlling (S15) the rotational speed so as to reach the correlated rotational speed value (ncorr). - determining (S1) whether the vessel is running by means of the propulsion arrangement at a constant vessel speed, - storing (S3) a detected value (V1) of the constant vessel speed, - detecting (S4) a value (n1) of a rotational speed of a rotatable part of the propulsion arrangement while the vessel is running at the constant vessel speed, - storing (S5) the detected rotational speed value (n1), - subsequently controlling (S6) the propulsion arrangement so as to change the vessel speed, - subsequently repeating (S7-S11) the steps of determining whether the vessel is running at a constant vessel speed, storing a detected value (V2-V4) of the constant vessel speed, and detecting and storing a value (n2-n4) of the rotational speed of the rotatable part , to obtain a plurality of stored pairs of vessel speed values (V1-V4) and rotational speed values (n1-n4), - creating (S12) based at least partly on the stored pairs of values (V1-V4, n1-n4) a correlation record correlating vessel speed values with rotational speed values, characterized by - receiving (S13) a requested value (Vreq) of the vessel speed, - determining (S14) by means of the correlation record a rotational speed value (ncorr) that is correlated to the requested vessel speed value (Vreq), and - controlling (S15) the rotational speed so as to reach the correlated rotational speed value (ncorr).
A method comprising: receiving a plurality of measurements of electric current amplitude in a primary winding of an engine ignition system comprising the primary winding and a spark plug ; identifying an ignition start time; identifying an inflection point based on the plurality of measurements; determining an inflection point time representative of a time at which the identified inflection point occurred; determining a spark start time based on an amount of time between the ignition start time and the inflection point time; and providing a signal indicative of the spark start time; characterized by identifying a second inflection point based on the plurality of measurements; determining that a spark developed by the spark plug has been extinguished based on the second inflection point; and, providing an extinguishment signal indicative of a condition in which the spark plug spark has been extinguished. receiving a plurality of measurements of electric current amplitude in a primary winding of an engine ignition system comprising the primary winding and a spark plug ; identifying an ignition start time; identifying an inflection point based on the plurality of measurements; determining an inflection point time representative of a time at which the identified inflection point occurred; determining a spark start time based on an amount of time between the ignition start time and the inflection point time; and providing a signal indicative of the spark start time; characterized by identifying a second inflection point based on the plurality of measurements; determining that a spark developed by the spark plug has been extinguished based on the second inflection point; and, providing an extinguishment signal indicative of a condition in which the spark plug spark has been extinguished.
A humidification system comprising a respiratory circuit for delivering a volume of gas to a patient and a humidifier portion (130; 200; 300; 400) for delivering a humidifying agent, more in particular comprising water, to the volume of gas flowing through the respiratory circuit , comprising: a flow controller for pulsing, via the humidifier portion (130; 200; 300; 400), a delivery of humidifying agent to the volume of gas; a controller configured to actuate the flow controller such that a pulsed interval commences immediately after patient exhalation or during patient inhalation, and a non-pulsed interval commences immediately after patient inhalation or during patient exhalation; a heating element for heating the volume of gas upstream of a discharge line of the respiratory circuit ; and wherein the controller is configured to actuate the flow controller such that a dry volume of gas is delivered to the discharge line of the respiratory circuit during the non-pulsed interval, said dry volume of gas being capable of vaporizing condensed humidifying agent present in the respiratory circuit to reduce the condensed humidifying agent present in the humidification system . a flow controller for pulsing, via the humidifier portion (130; 200; 300; 400), a delivery of humidifying agent to the volume of gas; a controller configured to actuate the flow controller such that a pulsed interval commences immediately after patient exhalation or during patient inhalation, and a non-pulsed interval commences immediately after patient inhalation or during patient exhalation; a heating element for heating the volume of gas upstream of a discharge line of the respiratory circuit ; and wherein the controller is configured to actuate the flow controller such that a dry volume of gas is delivered to the discharge line of the respiratory circuit during the non-pulsed interval, said dry volume of gas being capable of vaporizing condensed humidifying agent present in the respiratory circuit to reduce the condensed humidifying agent present in the humidification system .
An automated floor cleaning apparatus, comprising an automatic cleaning robot and a washing base , wherein the rear end of the robot body of the automatic cleaning robot is provided with a mop mechanism , the mop mechanism comprises a rotation component rotatably connected to the robot body and a crawler-type wiping cloth sleeving outside and rotating along with the rotation component; the washing base comprises: an outer container having an opening at its front side for the crawler-type wiping cloth to stretch in, a water supply mechanism, with its water outlet facing the side of the crawler-type wiping cloth that stretches inside the opening, and a cleaning brush , arranged inside the outer container and abuts against the side of the crawler-type wiping cloth that stretches inside the opening so as to remove dirt attached to the crawler-type wiping cloth through friction, characterized in that the mop mechanism further comprises a mount support in the robot body , the rotation component is rotatably arranged in the mount support , a drive motor for driving the rotation component to rotate is further arranged on the mount support , and the robot body is internally provided with a lifting mechanism for driving the mount support to ascend and descend. an outer container having an opening at its front side for the crawler-type wiping cloth to stretch in, a water supply mechanism, with its water outlet facing the side of the crawler-type wiping cloth that stretches inside the opening, and a cleaning brush , arranged inside the outer container and abuts against the side of the crawler-type wiping cloth that stretches inside the opening so as to remove dirt attached to the crawler-type wiping cloth through friction, characterized in that the mop mechanism further comprises a mount support in the robot body , the rotation component is rotatably arranged in the mount support , a drive motor for driving the rotation component to rotate is further arranged on the mount support , and the robot body is internally provided with a lifting mechanism for driving the mount support to ascend and descend.