mhurhangee/patent-ind-claim-en huggingface dataset:
A respiratory treatment device comprising: a housing enclosing a chamber ; an inlet configured to receive air into the chamber ; a first magnet positioned in proximity to the inlet ; an outlet configured to permit air to exit the chamber ; a second magnet positioned in proximity to the outlet ; a shuttle configured to move relative to the first magnet and the second magnet between a closed position where the flow of air through the inlet is blocked by the shuttle , and an open position where the flow of air through the outlet is blocked by the shuttle ; a first one-way inhalation valve configured to permit the flow of air through the chamber into the mouthpiece . a first one-way exhalation valve configured to permit the flow of air from the chamber out of the housing . wherein the shuttle is configured to move from the closed position to the open position when an exhalation pressure at the at the inlet is sufficient to overcome a magnetic attraction force between the shuttle and the first magnet ; and, wherein the shuttle is configured to move from the open position to the closed position when an inhalation pressure in the chamber is sufficient to overcome a magnetic attraction force between the shuttle and the second magnet . a housing enclosing a chamber ; an inlet configured to receive air into the chamber ; a first magnet positioned in proximity to the inlet ; an outlet configured to permit air to exit the chamber ; a second magnet positioned in proximity to the outlet ; a shuttle configured to move relative to the first magnet and the second magnet between a closed position where the flow of air through the inlet is blocked by the shuttle , and an open position where the flow of air through the outlet is blocked by the shuttle ; a first one-way inhalation valve configured to permit the flow of air through the chamber into the mouthpiece . a first one-way exhalation valve configured to permit the flow of air from the chamber out of the housing . wherein the shuttle is configured to move from the closed position to the open position when an exhalation pressure at the at the inlet is sufficient to overcome a magnetic attraction force between the shuttle and the first magnet ; and, wherein the shuttle is configured to move from the open position to the closed position when an inhalation pressure in the chamber is sufficient to overcome a magnetic attraction force between the shuttle and the second magnet .
Lock control device for controlling locking and unlocking of a drive gear of a gear train (GL) having: the drive gear and an idler gear engaged with each other; and a lock gear capable of moving along an axis parallel to axes of the both gears, the gear train being configured so that the drive gear is locked when the lock gear is simultaneously engaged with the both gears and the drive gear is unlocked when the lock gear is disengaged from at least any one of the both gears, the lock control device comprising: a first drive means configured to linearly drive the lock gear in forward and backward directions; the lock control device being characterized in that the lock control device further comprises a second drive means configured to rotationally drive the drive gear or the lock gear in normal and reverse directions; and control means configured to control the both drive means, wherein the control means starts driving the lock gear at a time of unlocking operation, from an engagement position toward a disengagement position through the first drive means and when the drive is started, drives the drive gear or the lock gear toward one of normal and reverse directions and toward the other direction through the second drive means, with a polarity reversal in a predetermined cycle.
A radiation curable solder mask inkjet ink comprising a photoinitiator, a polymerizable compound, and a flame retardant, characterized in that the flame retardant has a chemical structure according to Formula II, wherein R6 to R9 independently represent a substituted or unsubstituted aryl group, and L represent a divalent linking group coupled to the phosphate groups via an aromatic carbon atom, and wherein the viscosity of the inkjet ink at 45°C and at a shear rate of 1000 s -1 is less than 15 mPa.s. R6 to R9 independently represent a substituted or unsubstituted aryl group, and L represent a divalent linking group coupled to the phosphate groups via an aromatic carbon atom,
An organic light emitting display device comprising: a hole transport layer ; and a green phosphorescence emission layer on the hole transport layer , the green phosphorescence emission layer including at least one phosphorescent dopant (424G-D), a mixed host including a first host (424G-W) and a hole-type host (424G-H), and an electron-type host (424G-E), wherein the mixed host and the electron-type host (424G-E) form an exciplex, the first host (424G-W) having a triplet energy level between that of the hole-type host (424G-H) and the electron-type host (424G-E) for formation of the exciplex in the emission layer to transfer energy from the exciplex to the at least one dopant (424G-D); characterized in that the organic light emitting display device further comprising: an exciton confinement layer on the emission layer ; wherein when a triplet energy level of the exciton confinement layer is ECL(T1), a triplet energy level of the hole-type host (424G-H) is H(T1), a triplet energy level of the first host (424G-W) is W(T1) and a triplet energy level of the electron-type host (424G-E) is E(T1), ECL(T1)>H(T1)>W(T1)>E(T1) is satisfied. a hole transport layer ; and a green phosphorescence emission layer on the hole transport layer , the green phosphorescence emission layer including at least one phosphorescent dopant (424G-D), a mixed host including a first host (424G-W) and a hole-type host (424G-H), and an electron-type host (424G-E), wherein the mixed host and the electron-type host (424G-E) form an exciplex, the first host (424G-W) having a triplet energy level between that of the hole-type host (424G-H) and the electron-type host (424G-E) for formation of the exciplex in the emission layer to transfer energy from the exciplex to the at least one dopant (424G-D); an exciton confinement layer on the emission layer ; wherein when a triplet energy level of the exciton confinement layer is ECL(T1), a triplet energy level of the hole-type host (424G-H) is H(T1), a triplet energy level of the first host (424G-W) is W(T1) and a triplet energy level of the electron-type host (424G-E) is E(T1), ECL(T1)>H(T1)>W(T1)>E(T1) is satisfied.
A system for deploying a plurality of seismic nodes from a marine vessel , said system comprising: a first overboard wheel (510; 610) configured to at least partially extend off a back deck of said marine vessel , wherein the first overboard wheel (510; 610) is configured to deploy a deployment line coupled to a plurality of autonomous seismic nodes into a body of water, wherein the first overboard wheel is powered to actively change its position during deployment of the plurality of autonomous seismic nodes, and a second overboard cable detection wheel coupled to the first overboard wheel and configured to receive the deployment line, wherein the first overboard wheel (510; 610) is configured to actively change its position during deployment of the plurality of autonomous seismic nodes in response to a change of position of the second overboard cable detection wheel relative to said first overboard wheel (510; 610), due to a change of position of the deployed deployment line. a first overboard wheel (510; 610) configured to at least partially extend off a back deck of said marine vessel , wherein the first overboard wheel (510; 610) is configured to deploy a deployment line coupled to a plurality of autonomous seismic nodes into a body of water, wherein the first overboard wheel is powered to actively change its position during deployment of the plurality of autonomous seismic nodes, and a second overboard cable detection wheel coupled to the first overboard wheel and configured to receive the deployment line, wherein the first overboard wheel (510; 610) is configured to actively change its position during deployment of the plurality of autonomous seismic nodes in response to a change of position of the second overboard cable detection wheel relative to said first overboard wheel (510; 610), due to a change of position of the deployed deployment line.
A method implemented by a baseboard management controller mounted to a motherboard , comprising: receiving a configuration schema that specifies a plurality of devices associated with the motherboard and coupled to the baseboard management controller by a communication bus ; determining that a digital signature associated with the configuration schema is valid and whether the configuration schema is formatted in accordance with a predetermined formatting scheme; responsive to determining that the digital signature is valid and that the configuration schema is formatted in accordance with a predetermined formatting scheme, for each device of the plurality of devices, performing a discovery sequence over the communication bus based on the configuration schema to verify that the device is communicatively coupled to the baseboard management controller and to determine a property of the device; and responsive to verifying that the devices are communicatively coupled to the baseboard management controller, monitoring operation of the devices. receiving a configuration schema that specifies a plurality of devices associated with the motherboard and coupled to the baseboard management controller by a communication bus ; determining that a digital signature associated with the configuration schema is valid and whether the configuration schema is formatted in accordance with a predetermined formatting scheme; responsive to determining that the digital signature is valid and that the configuration schema is formatted in accordance with a predetermined formatting scheme, for each device of the plurality of devices, performing a discovery sequence over the communication bus based on the configuration schema to verify that the device is communicatively coupled to the baseboard management controller and to determine a property of the device; and responsive to verifying that the devices are communicatively coupled to the baseboard management controller, monitoring operation of the devices.
Method for controlling a pressurised white-rice cooker comprising a casing closed by a lid, the casing being equipped with a main heating element , with a vessel placed in the casing , with an element heating the top edge of the vessel , with an element heating the lid , with a controlled depressurisation valve , with a first temperature sensor situated in the vicinity of the bottom of the vessel and with a second temperature sensor placed in the lid , the method being characterised in that it comprises: - a soaking step (A) during which the heating elements are controlled so as to maintain, for a period of between 10 and 40 minutes, a set temperature of between 65 and 85°C inside the vessel ; - a heating step (B) starting at the end of the given soaking period during which the controlled depressurisation valve is in the closed position and the heating elements are controlled so as to achieve a set temperature of between 115 and 120°C inside the vessel ; - a cooking step, comprising a first phase (C) starting as soon as the set temperature is reached, during which the controlled depressurisation valve is maintained in the closed position and the heating elements are controlled so as to maintain the set temperature inside the vessel for a given period of between 2 and 6 minutes. - a soaking step (A) during which the heating elements are controlled so as to maintain, for a period of between 10 and 40 minutes, a set temperature of between 65 and 85°C inside the vessel ; - a heating step (B) starting at the end of the given soaking period during which the controlled depressurisation valve is in the closed position and the heating elements are controlled so as to achieve a set temperature of between 115 and 120°C inside the vessel ; - a cooking step, comprising a first phase (C) starting as soon as the set temperature is reached, during which the controlled depressurisation valve is maintained in the closed position and the heating elements are controlled so as to maintain the set temperature inside the vessel for a given period of between 2 and 6 minutes.
A drug delivery apparatus, comprising : a barrel (B-1100) to contain a substance ; a piston (B-1200) slidable in the barrel along a piston course (L) ; a supply circuit (C-1300) to provide input currents ; an antenna (C-1100) affixed along the barrel (B-1100), characterized in that the antenna comprises : a circuit board with a plurality of layers (C-1110) stacked on top of each other and connected to the supply circuit (C-1300), and a plurality of sets of coils (C-1120) on the layers (C-1110) of said plurality of layers and extending along the piston course (L) to receive the input currents, generate an inductance with the piston, and provide output currents commensurate with the inductance ; and processing circuitry (C-1300) connected to the plurality of sets of coils and configured to receive the output currents ; and determine a quantity of the substance inside the barrel (B-1100) based on the output currents. a barrel (B-1100) to contain a substance ; a piston (B-1200) slidable in the barrel along a piston course (L) ; a supply circuit (C-1300) to provide input currents ; an antenna (C-1100) affixed along the barrel (B-1100), characterized in that the antenna comprises : a circuit board with a plurality of layers (C-1110) stacked on top of each other and connected to the supply circuit (C-1300), and a plurality of sets of coils (C-1120) on the layers (C-1110) of said plurality of layers and extending along the piston course (L) to receive the input currents, generate an inductance with the piston, and provide output currents commensurate with the inductance ; a circuit board with a plurality of layers (C-1110) stacked on top of each other and connected to the supply circuit (C-1300), and a plurality of sets of coils (C-1120) on the layers (C-1110) of said plurality of layers and extending along the piston course (L) to receive the input currents, generate an inductance with the piston, and provide output currents commensurate with the inductance ; receive the input currents, generate an inductance with the piston, and provide output currents commensurate with the inductance ; and processing circuitry (C-1300) connected to the plurality of sets of coils and configured to receive the output currents ; and determine a quantity of the substance inside the barrel (B-1100) based on the output currents.
A method performed by a tire fitting system for assisting in fitting a tire on a rim of a wheel prior to assembly of the wheel on a vehicle , wherein the method comprises: determining a location of a Radio Frequency Identification, RFID, tag on the tire of the wheel ; determining a location for an air valve on the rim of the wheel ; determining the distance between the location of the RFID tag and the location for the air valve on the rim ; and providing instructions for aligning the tire on the rim based on the determined distance between the location of the RFID tag and the location for the air valve on the rim . determining a location of a Radio Frequency Identification, RFID, tag on the tire of the wheel ; determining a location for an air valve on the rim of the wheel ; determining the distance between the location of the RFID tag and the location for the air valve on the rim ; and providing instructions for aligning the tire on the rim based on the determined distance between the location of the RFID tag and the location for the air valve on the rim .
Connector part for screwing together pipes, which is formed by a metallic main element having an inner channel which on at least one side has an accommodation opening having an inner cone which widens in an outward direction, where a circumferential outer thread is present on the outside of the at least one side of the metallic main element , characterized in that the metallic main element consists of a microalloyed, precipitation-hardened, ferritic-pearlitic steel, where the ferritic-pearlitic steel has the following composition: - from 0.15% by mass to 0.50% by mass of carbon, - from 0.10% by mass to 1.00% by mass of silicon, - from 0.80% by mass to 1.90% by mass of manganese, - from 0.008% by mass to 0.20% by mass of sulfur, - from 0.004% by mass to 0.04% by mass of nitrogen, - from 0.05% by mass to 0.20% by mass of vanadium and/or niobium, - balance iron and melting-related impurities such as phosphorus, where the balance of iron can contain proportions of chromium of less than 0.3% by mass and/or of molybdenum of less than 0.08 per cent by mass or of aluminium in the range from 0.02% by mass to 0.04% by mass and optionally of titanium in the range from 0.01% by mass to 0.02% by mass. - from 0.15% by mass to 0.50% by mass of carbon, - from 0.10% by mass to 1.00% by mass of silicon, - from 0.80% by mass to 1.90% by mass of manganese, - from 0.008% by mass to 0.20% by mass of sulfur, - from 0.004% by mass to 0.04% by mass of nitrogen, - from 0.05% by mass to 0.20% by mass of vanadium and/or niobium, - balance iron and melting-related impurities such as phosphorus, where the balance of iron can contain proportions of chromium of less than 0.3% by mass and/or of molybdenum of less than 0.08 per cent by mass or of aluminium in the range from 0.02% by mass to 0.04% by mass and optionally of titanium in the range from 0.01% by mass to 0.02% by mass.
A system for removing gas from a sealant and transferring gas-less sealant to an applicator, the system comprising: a rotatable chamber including: a first opening for receiving sealant; a hollow conduit arranged such that when gas accumulates in the center of the rotatable chamber when the rotatable chamber is rotating, the gas is ventable from the rotatable chamber ; a second opening for receiving gas-less sealant from the rotatable chamber after the gas is vented from the hollow conduit , wherein the system is configured so that the gas-less sealant can be used on an aircraft; and a motor operatively configured to rotate the rotatable chamber ; and a gas-less sealant applicator in fluid communication with the second opening of the rotatable chamber such that gas-less sealant released by the second opening is flowable into the applicator . a rotatable chamber including: a first opening for receiving sealant; a hollow conduit arranged such that when gas accumulates in the center of the rotatable chamber when the rotatable chamber is rotating, the gas is ventable from the rotatable chamber ; a second opening for receiving gas-less sealant from the rotatable chamber after the gas is vented from the hollow conduit , wherein the system is configured so that the gas-less sealant can be used on an aircraft; and a first opening for receiving sealant; a hollow conduit arranged such that when gas accumulates in the center of the rotatable chamber when the rotatable chamber is rotating, the gas is ventable from the rotatable chamber ; a second opening for receiving gas-less sealant from the rotatable chamber after the gas is vented from the hollow conduit , wherein the system is configured so that the gas-less sealant can be used on an aircraft; and a motor operatively configured to rotate the rotatable chamber ; and a gas-less sealant applicator in fluid communication with the second opening of the rotatable chamber such that gas-less sealant released by the second opening is flowable into the applicator .
Method for lifting a plate-shaped metallic workpiece by means of a holding device , in particular by means of a gripping or suction gripping device, comprising: setting down a plurality of holding elements (8a-c, 10a-c), in particular gripping or suction gripping elements, of the holding device on the workpiece stored in a storage plane (E) and holding the workpiece at a plurality of holding positions (P 1,A , P 1,B , P 1,C ; P 2,A , P 2,B , P 2,C ) associated with the holding elements (8a-c, 10a-c), wherein at least a first and a second holding element are spaced apart from one another along a second direction (Y) at at least one first and one second holding position (P 1,A , P 1,B ), and lifting the workpiece from the storage plane (E) by means of the holding device , elastically deforming the workpiece by lifting the first holding element relative to the second holding element or the second holding element relative to the first holding element in a lifting direction (Z) perpendicular to the storage plane (E), wherein, on elastic deformation, the axial area moment of inertia (I Y ) of the workpiece in the second direction (Y) at a cross-section (Q 1 ) of the workpiece which contains the first and the second holding positions (P 1,A , P 1,BA ) is increased to at least 1.5 times in order to reduce the deflection (D M ) of the lifted workpiece along a first direction (X), which preferably runs perpendicular to the second direction (Y), characterised in that the first and the second holding elements (8a, 8b; 8c, 8a) are attached to a common support structure of the holding device , which is displaceable along the first direction (X). setting down a plurality of holding elements (8a-c, 10a-c), in particular gripping or suction gripping elements, of the holding device on the workpiece stored in a storage plane (E) and holding the workpiece at a plurality of holding positions (P 1,A , P 1,B , P 1,C ; P 2,A , P 2,B , P 2,C ) associated with the holding elements (8a-c, 10a-c), wherein at least a first and a second holding element are spaced apart from one another along a second direction (Y) at at least one first and one second holding position (P 1,A , P 1,B ), and lifting the workpiece from the storage plane (E) by means of the holding device , elastically deforming the workpiece by lifting the first holding element relative to the second holding element or the second holding element relative to the first holding element in a lifting direction (Z) perpendicular to the storage plane (E), wherein, on elastic deformation, the axial area moment of inertia (I Y ) of the workpiece in the second direction (Y) at a cross-section (Q 1 ) of the workpiece which contains the first and the second holding positions (P 1,A , P 1,BA ) is increased to at least 1.5 times in order to reduce the deflection (D M ) of the lifted workpiece along a first direction (X), which preferably runs perpendicular to the second direction (Y), characterised in that the first and the second holding elements (8a, 8b; 8c, 8a) are attached to a common support structure of the holding device , which is displaceable along the first direction (X).
A marine well containment system capable of producing fluids from a marine oil and gas well comprising: a blowout preventer ; a subsea containment assembly connected to the blowout preventer ; a riser assembly , wherein the riser assembly further comprises a vertical pipe riser and a flexible riser and wherein the riser assembly is connected to the subsea containment assembly; a capture vessel connected to the riser assembly; wherein the capture vessel is capable of receiving fluids produced by the blowout preventer , captured by the subsea containment assembly , piped through the riser assembly to the capture vessel or a combination thereof. a blowout preventer ; a subsea containment assembly connected to the blowout preventer ; a riser assembly , wherein the riser assembly further comprises a vertical pipe riser and a flexible riser and wherein the riser assembly is connected to the subsea containment assembly; a capture vessel connected to the riser assembly; wherein the capture vessel is capable of receiving fluids produced by the blowout preventer , captured by the subsea containment assembly , piped through the riser assembly to the capture vessel or a combination thereof.