mhurhangee/patent-ind-claim-en huggingface dataset:
A strut for a gas turbine engine, the strut comprising: a strut passage extending through the strut along a radial length of the strut ; a tube disposed within the strut passage and spaced from an interior surface of the strut passage ; and a grommet disposed about the tube and in communication with the interior surface of the strut passage , characterized in that the grommet defines a compressible zone comprising a hollow space extending radially through the grommet , the compressible zone disposed between the tube and the interior surface of the strut passage , wherein the grommet comprises a first portion disposed about a perimeter of the tube and at least one second portion extending from the first portion away from the tube , an exterior surface of the first portion and an interior surface of the second portion defining the compressible zone therebetween and wherein an exterior surface of the second portion forms an interface with the interior surface of the strut passage , and wherein the second portion is in communication with the interior surface of the strut passage and the first portion is spaced from the interior surface of the strut passage . a strut passage extending through the strut along a radial length of the strut ; a tube disposed within the strut passage and spaced from an interior surface of the strut passage ; and a grommet disposed about the tube and in communication with the interior surface of the strut passage , characterized in that the grommet defines a compressible zone comprising a hollow space extending radially through the grommet , the compressible zone disposed between the tube and the interior surface of the strut passage , wherein the grommet comprises a first portion disposed about a perimeter of the tube and at least one second portion extending from the first portion away from the tube , an exterior surface of the first portion and an interior surface of the second portion defining the compressible zone therebetween and wherein an exterior surface of the second portion forms an interface with the interior surface of the strut passage , and wherein the second portion is in communication with the interior surface of the strut passage and the first portion is spaced from the interior surface of the strut passage .
An apparatus in communication with and configured to control one or more outdoor devices , wherein the apparatus is configured to activate or deactivate a freeze prevention function of the one or more outdoor devices on the basis of weather information of an area in which the one or more outdoor devices are installed, characterized in that when the freeze prevention function of a corresponding outdoor device is activated, the apparatus is configured to compare a state information and an operation information of the corresponding outdoor device with pre-set operation conditions in order to start the freeze prevention function for the corresponding outdoor device when pre-set operation conditions are matched, and configured to terminate the freeze prevention function of the corresponding outdoor device based on comparing the state information and the operation information with the pre-set operation conditions when pre-set operation conditions are not matched and when freeze prevention is performed. characterized in that when the freeze prevention function of a corresponding outdoor device is activated, the apparatus is configured to compare a state information and an operation information of the corresponding outdoor device with pre-set operation conditions in order to start the freeze prevention function for the corresponding outdoor device when pre-set operation conditions are matched, and configured to terminate the freeze prevention function of the corresponding outdoor device based on comparing the state information and the operation information with the pre-set operation conditions when pre-set operation conditions are not matched and when freeze prevention is performed.
An aircraft power system comprising: i) a hydraulic fluid reservoir , ii) a bi-directional hydraulic pump for pumping hydraulic fluid to and from the reservoir, and iii) an electric motor , wherein: the electric motor is connectable to a first driveable component of the aircraft such that the electric motor is arranged to drive the first driveable component of the aircraft; the hydraulic pump is connectable to the first driveable component of the aircraft such that the hydraulic pump is arranged to act as a hydraulic motor to drive the first driveable component, such that, in a first driveable mode of operation, the first driveable component is driven by both the electric motor and the hydraulic pump; the electric motor and hydraulic pump are connected to each other in parallel such that, in the first driveable mode of operation, both are arranged to supply power to the driveable component independently of the other; characterised in that : the electric motor is connectable to the hydraulic pump such that, during a replenishing mode of operation, the electric motor is arranged to drive the hydraulic pump to pump hydraulic fluid into the reservoir. i) a hydraulic fluid reservoir , ii) a bi-directional hydraulic pump for pumping hydraulic fluid to and from the reservoir, and iii) an electric motor , the electric motor is connectable to a first driveable component of the aircraft such that the electric motor is arranged to drive the first driveable component of the aircraft; the hydraulic pump is connectable to the first driveable component of the aircraft such that the hydraulic pump is arranged to act as a hydraulic motor to drive the first driveable component, such that, in a first driveable mode of operation, the first driveable component is driven by both the electric motor and the hydraulic pump; the electric motor and hydraulic pump are connected to each other in parallel such that, in the first driveable mode of operation, both are arranged to supply power to the driveable component independently of the other; characterised in that : the electric motor is connectable to the hydraulic pump such that, during a replenishing mode of operation, the electric motor is arranged to drive the hydraulic pump to pump hydraulic fluid into the reservoir.
A method for operating an apparatus including a set of interferometers (201-204) located along a surface of a substrate, the substrate having a quantum well operable to trap a 2D charge carrier gas such that the trapped 2D charge carrier gas extends along the surface, each interferometer having a cell and a set of gate electrodes located around the cell, the method comprising: calibrating each one of the interferometers to confine a droplet of the 2D charge carrier gas in a fractional quantum Hall effect state of filling factor 17/5 or 12/5 in an area of the cell thereof while a reentrant phase of integer quantum Hall effect states of the 2D charge carrier gas is located between the area of the droplet of the 2D charge carrier gas in a fractional quantum Hall effect state and the electrodes of the one of the interferometers: wherein the calibrating includes setting a value of a magnetic field across the substrate such that the reentrant phase and the droplet of the 2D charge carrier gas are present in at least one of the interferometers based on interference measurements on the at least one of the interferometers for different values of the magnetic field; and wherein the calibrating comprises using the interference measurements to determine whether a reentrant phase of integer quantum Hall effect states of the 2D charge carrier gas is present in the at least one of the interferometers. calibrating each one of the interferometers to confine a droplet of the 2D charge carrier gas in a fractional quantum Hall effect state of filling factor 17/5 or 12/5 in an area of the cell thereof while a reentrant phase of integer quantum Hall effect states of the 2D charge carrier gas is located between the area of the droplet of the 2D charge carrier gas in a fractional quantum Hall effect state and the electrodes of the one of the interferometers: wherein the calibrating includes setting a value of a magnetic field across the substrate such that the reentrant phase and the droplet of the 2D charge carrier gas are present in at least one of the interferometers based on interference measurements on the at least one of the interferometers for different values of the magnetic field; and wherein the calibrating comprises using the interference measurements to determine whether a reentrant phase of integer quantum Hall effect states of the 2D charge carrier gas is present in the at least one of the interferometers.
A compound of general formula (I), including any stereoisomer and salt thereof: wherein R 1 is selected from C 1 -C 10 alkoxy, aryloxy, benzyloxy or halogen; R 2 is selected from straight or branched C 2 -C 8 alkyl, straight or branched C 2 -C 8 alkenyl; straight or branched C 2 -C 8 alkynyl; wherein said alkyl, alkenyl and alkynyl are each substituted by at least one group selected from -OH, -C(=O)O(C 1 -C 5 alkyl), -C(=O)OH, and -C(=O)NR 3 R 4 ; and R 3 and R 4 are each independently selected from H, straight or branched C 1 -C 10 alkyl and aryl; for use in the reduction of at least one condition selected from oxidative stress, release of NO and release of pro-inflammatory cytokine. R 1 is selected from C 1 -C 10 alkoxy, aryloxy, benzyloxy or halogen; R 2 is selected from straight or branched C 2 -C 8 alkyl, straight or branched C 2 -C 8 alkenyl; straight or branched C 2 -C 8 alkynyl; wherein said alkyl, alkenyl and alkynyl are each substituted by at least one group selected from -OH, -C(=O)O(C 1 -C 5 alkyl), -C(=O)OH, and -C(=O)NR 3 R 4 ; and R 3 and R 4 are each independently selected from H, straight or branched C 1 -C 10 alkyl and aryl; for use in the reduction of at least one condition selected from oxidative stress, release of NO and release of pro-inflammatory cytokine.
Drying device for drying planar textile structures , in particular mats or carpets, wherein the drying device comprises: - a housing which has or forms at least one drying chamber , - a blower and a heating element , which are fluidically coupled to the drying chamber and are configured for the fluidic treatment of a drying air flow , - a conveying device having a continuous conveying section which extends through the at least one drying chamber and along which the planar textile structures can be conveyed through the at least one drying chamber , - wherein the conveying device has at least one first conveying section and a second conveying section , wherein the second conveying section is contiguous to the first conveying section in a conveying direction (F) specified by the conveying section by way of a deflection device within the housing , and wherein the first conveying section as well as the second conveying section are able to be impinged with the drying air flow , characterized in that the drying air flow within the housing is guided counter to the conveying direction (F) of the conveying device , wherein at least one of the first conveying section and the second conveying section has at least a first belt conveyor which has a revolving flexible belt that is guided by at least two rollers mutually spaced apart in the conveying direction (F). - a housing which has or forms at least one drying chamber , - a blower and a heating element , which are fluidically coupled to the drying chamber and are configured for the fluidic treatment of a drying air flow , - a conveying device having a continuous conveying section which extends through the at least one drying chamber and along which the planar textile structures can be conveyed through the at least one drying chamber , - wherein the conveying device has at least one first conveying section and a second conveying section , wherein the second conveying section is contiguous to the first conveying section in a conveying direction (F) specified by the conveying section by way of a deflection device within the housing , and wherein the first conveying section as well as the second conveying section are able to be impinged with the drying air flow , characterized in that the drying air flow within the housing is guided counter to the conveying direction (F) of the conveying device , wherein at least one of the first conveying section and the second conveying section has at least a first belt conveyor which has a revolving flexible belt that is guided by at least two rollers mutually spaced apart in the conveying direction (F).
Arrangement for operating one or more windows (S1 - S4, SF, SH), which are installed in a vehicle (FZ) and in particular delimit a passenger compartment (FGZ) and whose optical properties can be changed by electrical actuation, wherein the arrangement has the following features: - a position-determining device (ZGA) for determining the position (P1-P3) of an object (IDG1) which is located outside the vehicle (FZ); - a control device (STG, AST) which is configured to actuate the one or more windows (S1 - S4, SF, SH) as a function of the distance (A1, A2, A3) between the vehicle and the object (IDG1), characterized in that the control device is also configured to actuate the one or more windows (S1 - S4, SF, SH) in such way that their translucency is increased with decreasing distance and the translucency is reduced with increasing distance. - a position-determining device (ZGA) for determining the position (P1-P3) of an object (IDG1) which is located outside the vehicle (FZ); - a control device (STG, AST) which is configured to actuate the one or more windows (S1 - S4, SF, SH) as a function of the distance (A1, A2, A3) between the vehicle and the object (IDG1),
Headlamp fastening system for a motor vehicle for fastening and aligning a headlamp structure (S) on two support structures (T) of the motor vehicle, in particular on a vehicle wing fastening structure (TF) and a radiator mounting structure (TK), in respect of three x-, y- and z- spatial directions perpendicular to one another, in particular the x-, y- and z-direction of the vehicle, with a 1-valued alignment element for fastening and aligning the headlamp structure (S) in the z-direction (z) on one of the support structures (T), wherein the headlamp fastening system is designed in such a manner that the structures to be connected (S, TF, TK) are arranged held relatively displaceably to one another via the 1-valued alignment element in an alignment position in respect of the x-, y- and z- spatial directions, in particular the x-, y- and z-direction of the vehicle, wherein the transfer of the alignment element from the alignment position into a fixing position for aligning and fixing the structures (S, TF, TK) in the z-direction (z) simultaneously brings about the fixing thereof in the x-direction (x) and the y-direction (y), wherein the alignment element for alignment in the z-direction (z) in the alignment position aligns the structures to be connected (S, TF, TK) in respect of the xy-plane in such a manner that they remain loose to one another, wherein on the one support structure (T) or the headlamp structure (S) an alignment receiving means is provided and wherein the alignment element engages with the alignment receiving means in the alignment position displaceably in respect of the xy-plane and in a clamp-like manner in respect of the z-direction (z) and is arranged fixed in the fixing position with closure of the clamp-like engagement at the alignment receiving means .
A control method for a hybrid vehicle comprising an electric motor that drives the vehicle to travel, a generator that supplies power to the electric motor , and an engine that drives the generator , the control method comprising: storing timing at which an amount or factor of change in target driving force for the vehicle becomes a predetermined threshold or more; calculating an estimated trajectory of a rotational speed of the engine in accordance with the amount or factor of change in the target driving force; and when a change request for power generation is issued to the engine at different timing than the timing, controlling the rotational speed of the engine on a basis of the calculated estimated trajectory. storing timing at which an amount or factor of change in target driving force for the vehicle becomes a predetermined threshold or more; calculating an estimated trajectory of a rotational speed of the engine in accordance with the amount or factor of change in the target driving force; and when a change request for power generation is issued to the engine at different timing than the timing, controlling the rotational speed of the engine on a basis of the calculated estimated trajectory.
An electronic device comprising: a speaker ; a microphone ; at least one processor ; and a memory storing programming instructions, the programming instructions executable by the at least one processor to cause the electronic device to: identify whether registration of a first user is required based on a first voice signal of the first user obtained through the microphone, wherein it is identified that registration of the first user is required if the first voice signal is obtained a designated number of times or more, or over a designated period or longer, or a designated frequency or more over a designated period; when the registration of the first user is required, requesting authentication of the first user by a second user preregistered at the electronic device; and when information authenticating the first user by the second user is received, register the first user based on the received information. a speaker ; a microphone ; at least one processor ; and a memory storing programming instructions, the programming instructions executable by the at least one processor to cause the electronic device to: identify whether registration of a first user is required based on a first voice signal of the first user obtained through the microphone, wherein it is identified that registration of the first user is required if the first voice signal is obtained a designated number of times or more, or over a designated period or longer, or a designated frequency or more over a designated period; when the registration of the first user is required, requesting authentication of the first user by a second user preregistered at the electronic device; and when information authenticating the first user by the second user is received, register the first user based on the received information. identify whether registration of a first user is required based on a first voice signal of the first user obtained through the microphone, wherein it is identified that registration of the first user is required if the first voice signal is obtained a designated number of times or more, or over a designated period or longer, or a designated frequency or more over a designated period; when the registration of the first user is required, requesting authentication of the first user by a second user preregistered at the electronic device; and when information authenticating the first user by the second user is received, register the first user based on the received information.
A method comprising: detecting, by a sensor device of a low-power wide-area network, a sensor event; determining, by a control circuitry of the sensor device and based on the sensor event, a select sensor event message from a plurality of pre-computed sensor event messages, wherein the pre-computed sensor event messages are stored on memory of the sensor device; determining, by a control circuitry of the sensor device, a counter value of a plurality of incremental counter values, wherein the counter value is associated with the select sensor event message; and outputting, via a radio signal output by the sensor device, a packet comprising the select sensor event message and an indication of the counter value. detecting, by a sensor device of a low-power wide-area network, a sensor event; determining, by a control circuitry of the sensor device and based on the sensor event, a select sensor event message from a plurality of pre-computed sensor event messages, wherein the pre-computed sensor event messages are stored on memory of the sensor device; determining, by a control circuitry of the sensor device, a counter value of a plurality of incremental counter values, wherein the counter value is associated with the select sensor event message; and outputting, via a radio signal output by the sensor device, a packet comprising the select sensor event message and an indication of the counter value.
A probe system for an aircraft comprising: a heater comprising a resistive heating element routed through the probe system, wherein an operational voltage is provided to the resistive heating element to provide heating for the probe system, and wherein the resistive heating element has an element capacitance and wherein the resistive heating element is configured to provide an antenna response indicative of dielectric properties of the resistive heating element upon receiving a radio-frequency (RF) signal that comprises a plurality of signal frequencies; and characterised by comprising a control circuit configured to determine the antenna response of the resistive heating element and a resonant frequency from the antenna response and to determine a remaining useful life of the probe system based on the antenna response and resonant frequency over time. a heater comprising a resistive heating element routed through the probe system, wherein an operational voltage is provided to the resistive heating element to provide heating for the probe system, and wherein the resistive heating element has an element capacitance and wherein the resistive heating element is configured to provide an antenna response indicative of dielectric properties of the resistive heating element upon receiving a radio-frequency (RF) signal that comprises a plurality of signal frequencies; and characterised by comprising a control circuit configured to determine the antenna response of the resistive heating element and a resonant frequency from the antenna response and to determine a remaining useful life of the probe system based on the antenna response and resonant frequency over time.
A connecting device allowing a releasable connection between a bracelet strap and a folding clasp comprising at least two articulated arms and two fastening portions capable of reversibly cooperating with each other, the connecting device comprising a first connecting piece capable of being secured to the free end of the bracelet strap and a second connecting piece capable of being mounted on the fastening portion , said first connecting piece and said second connecting piece being configured to reversibly cooperate with each other between a first, open position allowing separation of the first connecting piece and the second connecting piece and a second, closed position in which said first connecting piece and said second connecting piece are locked together, said first connecting piece comprising a fastening portion capable of being mounted on the end of the bracelet strap and a first locking portion capable of cooperating with said second connecting piece , and said second connecting piece comprising a connection portion capable of being mounted on the fastening portion of the folding clasp , said second connecting piece further comprising a second locking portion capable of cooperating with said first locking portion of the first connecting piece, characterized in that said second locking portion of the second connecting piece has a hook form with an opening, capable of allowing the exit of said first locking portion from the first connecting piece in the first, open position and capable of retaining the first locking portion of the first connecting piece in the second, closed position.