mhurhangee/patent-ind-claim-en huggingface dataset:
An air conditioning system comprising: a shaft ; a first turbine comprising a plurality of inlet gas flow paths and an exit where the plurality of inlet gas flow paths combine, the plurality of inlet gas flow paths comprising an inner flow path and an outer flow path, the first turbine being located at a first end of the shaft and configured to mix alternative medium flows at the exit of the first turbine during low altitude flight operations, such as ground idle, taxi, take-off, and hold conditions, the alternative medium flows being bleed air sourced from a turbine engine or an auxiliary power unit and fresh air sourced from a scooping mechanism , the inner flow path receiving the bleed air or the fresh air, and the outer flow path receiving a remaining one of the bleed air and the fresh air; a compressor driven by the first turbine from the shaft ; a second turbine connected to the compressor by the shaft and configured to receive cabin discharge air from an aircraft cabin that has been heated by air leaving the compressor ; and a fan driven by the second turbine; wherein the inner flow path is at a first diameter and the outer flow path is at a second diameter. a shaft ; a first turbine comprising a plurality of inlet gas flow paths and an exit where the plurality of inlet gas flow paths combine, the plurality of inlet gas flow paths comprising an inner flow path and an outer flow path, the first turbine being located at a first end of the shaft and configured to mix alternative medium flows at the exit of the first turbine during low altitude flight operations, such as ground idle, taxi, take-off, and hold conditions, the alternative medium flows being bleed air sourced from a turbine engine or an auxiliary power unit and fresh air sourced from a scooping mechanism , the inner flow path receiving the bleed air or the fresh air, and the outer flow path receiving a remaining one of the bleed air and the fresh air; a compressor driven by the first turbine from the shaft ; a second turbine connected to the compressor by the shaft and configured to receive cabin discharge air from an aircraft cabin that has been heated by air leaving the compressor ; and a fan driven by the second turbine; wherein the inner flow path is at a first diameter and the outer flow path is at a second diameter.
A method of providing differentially private database security, comprising: receiving a request from a client to perform a query on data stored in a database; establishing a set of permissions granted to the client with respect to the data in the database, wherein the set of permissions comprises a private compute permission granting permission to perform differentially private operations on specified data in the database; deconstructing the query into query components, wherein the query components comprise at least one relation identifying a dataset in the database and at least one expression specifying an operation to be performed in the identified dataset; identifying permissions necessary to perform the specified operation on the identified dataset, wherein the identified permissions comprise the private compute permission and the identified dataset comprises the specified data; determining whether the established set of permissions granted to the client includes the identified permissions necessary to perform the specified operation on the identified dataset using a set of mutually recursive functions to check whether the established set of permissions granted to the client includes the identified permissions necessary to perform expressions on relations indicated by the deconstructed query components; and selectively executing the query responsive to the determination. receiving a request from a client to perform a query on data stored in a database; establishing a set of permissions granted to the client with respect to the data in the database, wherein the set of permissions comprises a private compute permission granting permission to perform differentially private operations on specified data in the database; deconstructing the query into query components, wherein the query components comprise at least one relation identifying a dataset in the database and at least one expression specifying an operation to be performed in the identified dataset; identifying permissions necessary to perform the specified operation on the identified dataset, wherein the identified permissions comprise the private compute permission and the identified dataset comprises the specified data; determining whether the established set of permissions granted to the client includes the identified permissions necessary to perform the specified operation on the identified dataset using a set of mutually recursive functions to check whether the established set of permissions granted to the client includes the identified permissions necessary to perform expressions on relations indicated by the deconstructed query components; and selectively executing the query responsive to the determination.
Method for dynamically allocating resources in a satellite network comprising at least one satellite configured to form a plurality of satellite beams (401 to 404) and terminals, the method being characterized in that it comprises steps executed by a network supervisor: • a first step of clustering the beams into groups of beams on the basis of an item of information regarding overall loading of each of the beams, • a second step of allocating frequency resources to each of the groups of beams, • a third step of determining, within the beams of one and the same group and beams of different groups sharing common frequency resources, geographical zones in which these frequency resources can be used simultaneously, • a fourth step , carried out for each of the groups of beams on the basis of the overall loading of the beams and the geographical zones determined, of determining a hop frame , the said hop frame comprising first timeslots , in which the frequency resources are allocated to the whole set of terminals of one of the beams of the group of beams, and second timeslots , in which the frequency resources are allotted to a subset of terminals of at least one beam of the group of beams, and steps executed by at least one controller which is associated with at least one of the satellite beams: • a fifth step , carried out for each of the beams, of identifying the said subset of terminals and of allocating to the terminals frequency resources associated with instants of sending in the timeslots of the hop frame, • a sixth step of uploading to the supervisor information relating to the overall loading of each of the beams associated therewith. • a first step of clustering the beams into groups of beams on the basis of an item of information regarding overall loading of each of the beams, • a second step of allocating frequency resources to each of the groups of beams, • a third step of determining, within the beams of one and the same group and beams of different groups sharing common frequency resources, geographical zones in which these frequency resources can be used simultaneously, • a fourth step , carried out for each of the groups of beams on the basis of the overall loading of the beams and the geographical zones determined, of determining a hop frame , the said hop frame comprising first timeslots , in which the frequency resources are allocated to the whole set of terminals of one of the beams of the group of beams, and second timeslots , in which the frequency resources are allotted to a subset of terminals of at least one beam of the group of beams, • a fifth step , carried out for each of the beams, of identifying the said subset of terminals and of allocating to the terminals frequency resources associated with instants of sending in the timeslots of the hop frame, • a sixth step of uploading to the supervisor information relating to the overall loading of each of the beams associated therewith.
A method of preserving the effectiveness of a membrane in a water process flow, comprising the steps of: adding a halogenated oxidizing biocide to process water in an amount sufficient to effectively reduce the population of microorganisms in the water, further downstream but upstream from the membrane adding a PAA bearing composition to the water, the PAA bearing composition being an oxidant but effectively reducing the halogenated oxidizing biocide so that the harm it causes the membrane is reduced by at least 50%, the method excluding the addition of a reducing agent in an amount capable of substantially neutralizing the halogenated oxidizing biocide so that the harm it causes the membrane is reduced by at least 50%, wherein the addition of the PAA bearing composition neutralizes residual halogenated oxidizing biocide that has been introduced upstream from the addition of the PAA bearing composition. adding a halogenated oxidizing biocide to process water in an amount sufficient to effectively reduce the population of microorganisms in the water, further downstream but upstream from the membrane adding a PAA bearing composition to the water, the PAA bearing composition being an oxidant but effectively reducing the halogenated oxidizing biocide so that the harm it causes the membrane is reduced by at least 50%, the method excluding the addition of a reducing agent in an amount capable of substantially neutralizing the halogenated oxidizing biocide so that the harm it causes the membrane is reduced by at least 50%,
A compound, or a pharmaceutically acceptable salt thereof, of formula I: in which: R 1 is selected from hydrogen, amino and hydroxy-substituted C 1-2 alkyl; R 2 is hydrogen; R 3 is selected from C 1-2 alkyl and halo-substituted-C 1-2 alkyl; R 4 is hydrogen; R 5 is selected from hydrogen and halo; and R 6 is selected from hydrogen and halo. R 1 is selected from hydrogen, amino and hydroxy-substituted C 1-2 alkyl; R 2 is hydrogen; R 3 is selected from C 1-2 alkyl and halo-substituted-C 1-2 alkyl; R 4 is hydrogen; R 5 is selected from hydrogen and halo; and R 6 is selected from hydrogen and halo.
A workpiece conveying wheeled platform , comprising: a slider provided in a vicinity of a loading machine for supplying a workpiece (W) to a working machine , the slider being movable in a predetermined direction between a setup area (SA) for setting up a plurality of workpieces (W) stacked on a pallet (P) and a pickup area (GA) for picking up an uppermost workpiece (W) from among the plurality of workpieces (W) with the loading machine , the slider being recessed to form a placing part for placing the pallet (P); guide mechanisms respectively arranged to both sides of the placing part in a lateral direction orthogonal to the predetermined direction of the slider and configured to support the slider so as to be movable in the predetermined direction; and a drive mechanism arranged to at least one side of the placing part in the lateral direction of the slider and configured to move the slider in the predetermined direction, wherein the placing part of the slider is close to an installation surface (IS) on a floor, characterized in that a notch for allowing a fork (HLa) of a pallet jack (HL) to enter is formed on the placing part of the slider . a slider provided in a vicinity of a loading machine for supplying a workpiece (W) to a working machine , the slider being movable in a predetermined direction between a setup area (SA) for setting up a plurality of workpieces (W) stacked on a pallet (P) and a pickup area (GA) for picking up an uppermost workpiece (W) from among the plurality of workpieces (W) with the loading machine , the slider being recessed to form a placing part for placing the pallet (P); guide mechanisms respectively arranged to both sides of the placing part in a lateral direction orthogonal to the predetermined direction of the slider and configured to support the slider so as to be movable in the predetermined direction; and a drive mechanism arranged to at least one side of the placing part in the lateral direction of the slider and configured to move the slider in the predetermined direction, wherein the placing part of the slider is close to an installation surface (IS) on a floor, characterized in that a notch for allowing a fork (HLa) of a pallet jack (HL) to enter is formed on the placing part of the slider .
A method of depositing a thin film of a selected material on the surface of a substrate using plasma ion assisted deposition, the method having the steps of: providing a vacuum chamber and within said chamber: providing a substrate on which a coating is to be deposited; providing at a MgF 2 material source and vaporizing said material using an e-beam to provide a coating material vapor flux , said flux passing from said material source through a reversed mask to said substrate; providing a plasma containing oxygen ions from a plasma source ; rotating said substrate at a selected rotation frequency f; and depositing said coating material on said substrate as a coating film and bombarding said substrate and said film with said plasma ions before and during said material depositions; wherein the method forms a smooth, dense uniform composited MgO-MgF 2 coating. providing a substrate on which a coating is to be deposited; providing at a MgF 2 material source and vaporizing said material using an e-beam to provide a coating material vapor flux , said flux passing from said material source through a reversed mask to said substrate; providing a plasma containing oxygen ions from a plasma source ; rotating said substrate at a selected rotation frequency f; and depositing said coating material on said substrate as a coating film and bombarding said substrate and said film with said plasma ions before and during said material depositions; wherein the method forms a smooth, dense uniform composited MgO-MgF 2 coating.
An aircraft cabin light-emitting diode, LED, lighting assembly comprising: a plurality of separately addressable microcontrollers (312; 412); a plurality of multicolor LED lights (304; 404), wherein each respective microcontroller of the plurality of microcontrollers (312; 412) is paired with and controls a respective multicolor LED light of the plurality of multicolored LED lights (304; 404); each multicolor LED light comprising a plurality of LEDs , and the lighting assembly further comprising a printed circuit board, PCB' having first and second surfaces, the plurality of microcontrollers (312; 412) being mounted on the first surface and the plurality of LED lights (304; 404) being mounted on the second surface ; characterized in that each of the plurality of LEDs comprises a shared terminal and a non-shared terminal , wherein the shared terminal is electrically connected to a node that is shared with the other LEDs of the plurality and the non-shared terminal is electrically connected to the microcontroller that is paired with the multicolored LED light; each microcontroller is configured to receive pixel data via a data line and generate a separate pulse wave modulated signal to each of the non-shared terminals of the multicolor LED light in accordance with the received pixel data; and the plurality of microcontrollers (312; 412) and the plurality of LED lights (304; 404) are mounted on the same flexible PCB and the lighting assembly is housed within a flexible housing. a plurality of separately addressable microcontrollers (312; 412); a plurality of multicolor LED lights (304; 404), wherein each respective microcontroller of the plurality of microcontrollers (312; 412) is paired with and controls a respective multicolor LED light of the plurality of multicolored LED lights (304; 404); each multicolor LED light comprising a plurality of LEDs , and the lighting assembly further comprising a printed circuit board, PCB' having first and second surfaces, the plurality of microcontrollers (312; 412) being mounted on the first surface and the plurality of LED lights (304; 404) being mounted on the second surface ; characterized in that each of the plurality of LEDs comprises a shared terminal and a non-shared terminal , wherein the shared terminal is electrically connected to a node that is shared with the other LEDs of the plurality and the non-shared terminal is electrically connected to the microcontroller that is paired with the multicolored LED light; each microcontroller is configured to receive pixel data via a data line and generate a separate pulse wave modulated signal to each of the non-shared terminals of the multicolor LED light in accordance with the received pixel data; and the plurality of microcontrollers (312; 412) and the plurality of LED lights (304; 404) are mounted on the same flexible PCB and the lighting assembly is housed within a flexible housing.
A method for transmitting an emergency call for a motorcycle (M), in which - an emergency-call text message (NTN1) relating to an emergency is sent, wherein - a continuous acoustic signal (AR1) is generated as an acoustic response to the sending of the emergency-call text message (NTN1), - in response to receiving an emergency-call confirmation message (NBN) by means of a communication interface of the motorcycle the continuous acoustic signal (AR1) is terminated dependent on the emergency-call confirmation message (NBN) received, - in which dependent on the emergency-call confirmation message (NBN) a further acoustic signal (AR2) is generated, as acoustic confirmation. - an emergency-call text message (NTN1) relating to an emergency is sent, wherein - a continuous acoustic signal (AR1) is generated as an acoustic response to the sending of the emergency-call text message (NTN1), - in response to receiving an emergency-call confirmation message (NBN) by means of a communication interface of the motorcycle the continuous acoustic signal (AR1) is terminated dependent on the emergency-call confirmation message (NBN) received, - in which dependent on the emergency-call confirmation message (NBN) a further acoustic signal (AR2) is generated, as acoustic confirmation.
A process for the preparation of a cyanoacetate, steps of which comprise: (a) reacting an ester of cyanoacetic acid and an alcohol, in the presence of ytterbium trifluoromethane sulfonate [Yb(OTf) 3 ] catalyst and nitromethane, at 105 °C, for six hours to yield a cyanoacetate, wherein said ester of cyanoacetic acid is ethyl cyanoacetate and said alcohol is one of n-butanol, 2-pentanol and phenyl ethanol; (b) optionally, separating the so formed cyanoacetate substantially free from the ester of cyanoacetic acid, the alcohol and/or the catalyst, and by-products. (a) reacting an ester of cyanoacetic acid and an alcohol, in the presence of ytterbium trifluoromethane sulfonate [Yb(OTf) 3 ] catalyst and nitromethane, at 105 °C, for six hours to yield a cyanoacetate, wherein said ester of cyanoacetic acid is ethyl cyanoacetate and said alcohol is one of n-butanol, 2-pentanol and phenyl ethanol; (b) optionally, separating the so formed cyanoacetate substantially free from the ester of cyanoacetic acid, the alcohol and/or the catalyst, and by-products.
A system , comprising: a restraining system for a ride vehicle of an amusement park ; and an audio system comprising a speaker and a microphone , wherein the audio system is positioned inside of the restraining system and configured to produce an audio output via the speaker in response to an audio activation signal, wherein the restraining system is configured to generate the audio activation signal when the restraining system is moved from an unlocked configuration to a locked configuration, and wherein the audio system is configured to change the produced audio output from a first sound to a second sound when the audio activation signal is received. a restraining system for a ride vehicle of an amusement park ; and an audio system comprising a speaker and a microphone , wherein the audio system is positioned inside of the restraining system and configured to produce an audio output via the speaker in response to an audio activation signal, wherein the restraining system is configured to generate the audio activation signal when the restraining system is moved from an unlocked configuration to a locked configuration, and wherein the audio system is configured to change the produced audio output from a first sound to a second sound when the audio activation signal is received.
A storage device , comprising a body enclosing an accommodation cavity , a pair of guiding mechanisms and a first partition frame for dividing the accommodation cavity , the body comprising a bottom wall, a pair of first side walls and a pair of second side walls , wherein the pair of guiding mechanisms is arranged at the pair of second side walls respectively, the guiding mechanism comprises a guiding element which slides in a front-rear direction with respect to the body , the guiding element comprises a mounting hole extending in the front-rear direction and a limiting portion ; the first partition frame comprises a partition element, a pair of fixing portions and a pair of limited portions , the partition element extends in a left-right direction, for dividing the accommodation cavity , the pair of fixing portions are provided to be long rods extending in the front-rear direction and are formed at two ends of the first partition frame ; characterized in that the fixing portion is inserted into the mounting hole in a forward horizontal direction, such that the first partition frame is slidably connected onto the guiding element synchronously, and at this point, the fixing portion and the mounting hole are limited mutually in the left-right direction, so that the fixing portion cannot move left and right with respect to the guiding element , and the limiting portion is fitted and connected with the limited portion to limit the front-rear direction movement of the first partition frame with respect to the guiding element .
Electromechanical actuator for electrical flight controls of an aircraft, comprising: - a transmission shaft provided with an axis of rotation , - at least three electromechanical conversion members each provided with a stator and a rotor that is rigidly connected to said transmission shaft and rotates about said axis of rotation , said stator being provided with teeth and windings , each winding surrounding at least one tooth , said rotor being provided with permanent magnets each having a north magnetic pole and a south magnetic pole , - at least three flight control chains , each flight control chain supplying power to and controlling an electromechanical conversion member , a flight control chain being connected to a single electromechanical conversion member and supplying said conversion member with an alternating electric current, characterised in that said teeth are dimensioned so that each electromechanical conversion member operates at the saturation bend of a curve of variation of the magnetic induction of the ferromagnetic material constituting said teeth , thus allowing at least two of said electromechanical conversion members to mitigate a short-circuit-type failure of another electromechanical conversion member , one of said two electromechanical conversion members compensating for the majority, or even all, of the short-circuit torque of said failed electromechanical conversion member , while the other of said two electromechanical conversion members delivers the nominal torque necessary for the operation of said electromechanical actuator . - a transmission shaft provided with an axis of rotation , - at least three electromechanical conversion members each provided with a stator and a rotor that is rigidly connected to said transmission shaft and rotates about said axis of rotation , said stator being provided with teeth and windings , each winding surrounding at least one tooth , said rotor being provided with permanent magnets each having a north magnetic pole and a south magnetic pole , - at least three flight control chains , each flight control chain supplying power to and controlling an electromechanical conversion member , a flight control chain being connected to a single electromechanical conversion member and supplying said conversion member with an alternating electric current,