mhurhangee/patent-ind-claim-en huggingface dataset:
An electronic device comprising: a display ; a wireless communication circuit ; a processor operatively connected to the display and the wireless communication circuit; and a memory operatively connected to the processor and configured to store a first application program having a first priority associated with use of a resource of a wireless communication circuit , wherein the memory stores instructions that cause the processor to: execute the first application program; transmit identification information of the first application program to an external device through the wireless communication circuit; receive a signal for determining whether the first application program has a low latency attribute, through the wireless communication circuit; when the first application program is displayed on the display, determine an attribute of the first application program; and increase a priority of the first application program to be higher than the first priority based at least partly on the determination result, wherein the signal includes information about a value of which the first priority is to be changed. a display ; a wireless communication circuit ; a processor operatively connected to the display and the wireless communication circuit; and a memory operatively connected to the processor and configured to store a first application program having a first priority associated with use of a resource of a wireless communication circuit , wherein the memory stores instructions that cause the processor to: execute the first application program; transmit identification information of the first application program to an external device through the wireless communication circuit; receive a signal for determining whether the first application program has a low latency attribute, through the wireless communication circuit; when the first application program is displayed on the display, determine an attribute of the first application program; and increase a priority of the first application program to be higher than the first priority based at least partly on the determination result, wherein the signal includes information about a value of which the first priority is to be changed. execute the first application program; transmit identification information of the first application program to an external device through the wireless communication circuit; receive a signal for determining whether the first application program has a low latency attribute, through the wireless communication circuit; when the first application program is displayed on the display, determine an attribute of the first application program; and increase a priority of the first application program to be higher than the first priority based at least partly on the determination result, wherein the signal includes information about a value of which the first priority is to be changed.
An aircraft wing , comprising: an outer aircraft skin including an upper skin portion and a lower skin portion defining a chamber therebetween; and a wing spar extending some length of the wing and being positioned within the chamber , said wing spar including an upper spar cap coupled to an inside surface of the upper skin portion , a lower spar cap coupled to an inside surface of the lower skin portion , and a web formed to the upper and lower spar caps , wherein the upper spar cap is configured in a manner that causes it to have built-in tension so that compression forces on the upper skin portion during flight operate to reduce the tension in the upper spar cap , wherein the upper spar cap is configured to have a higher coefficient of thermal expansion, CTE, than the web to provide the built-in tension, wherein both the upper and lower spar caps have a higher CTE than the web to provide built-in tension in both the upper and lower spar caps , wherein the wing spar is made of a graphite composite that is thermally cured, and wherein a different ply lay-up schedule is used for the web than a ply lay-up schedule for the spar caps where a fiber direction of the web plies is configured to have a CTE near zero and the spar cap plies are configured to have a higher CTE. an outer aircraft skin including an upper skin portion and a lower skin portion defining a chamber therebetween; and a wing spar extending some length of the wing and being positioned within the chamber , said wing spar including an upper spar cap coupled to an inside surface of the upper skin portion , a lower spar cap coupled to an inside surface of the lower skin portion , and a web formed to the upper and lower spar caps , wherein the upper spar cap is configured in a manner that causes it to have built-in tension so that compression forces on the upper skin portion during flight operate to reduce the tension in the upper spar cap , wherein the upper spar cap is configured to have a higher coefficient of thermal expansion, CTE, than the web to provide the built-in tension, wherein both the upper and lower spar caps have a higher CTE than the web to provide built-in tension in both the upper and lower spar caps , wherein the wing spar is made of a graphite composite that is thermally cured, and wherein a different ply lay-up schedule is used for the web than a ply lay-up schedule for the spar caps where a fiber direction of the web plies is configured to have a CTE near zero and the spar cap plies are configured to have a higher CTE.
An axial retention assembly for combustor components of a gas turbine engine , the axial retention assembly comprising: a combustor defining an axial centerline extending between a forward end of the combustor and an aft end of the combustor , the combustor further defining a radial direction extending orthogonally outward from the axial centerline , the combustor including a liner and a casing , the casing including a flange spaced apart from the liner along the axial centerline ; a mounting plate including a first end removably coupled to the flange and a second end positioned inward from the casing in the radial direction ; characterized in that the assembly also includes: a clamp removably coupled to the liner ; and a tie rod coupled to the second end of the mounting plate and the clamp to reduce relative movement between the liner and the casing along the axial centerline , wherein the tie rod is positioned between the liner and the casing in the radial direction . a combustor defining an axial centerline extending between a forward end of the combustor and an aft end of the combustor , the combustor further defining a radial direction extending orthogonally outward from the axial centerline , the combustor including a liner and a casing , the casing including a flange spaced apart from the liner along the axial centerline ; a mounting plate including a first end removably coupled to the flange and a second end positioned inward from the casing in the radial direction ; characterized in that the assembly also includes: a clamp removably coupled to the liner ; and a tie rod coupled to the second end of the mounting plate and the clamp to reduce relative movement between the liner and the casing along the axial centerline , wherein the tie rod is positioned between the liner and the casing in the radial direction . a clamp removably coupled to the liner ; and a tie rod coupled to the second end of the mounting plate and the clamp to reduce relative movement between the liner and the casing along the axial centerline , wherein the tie rod is positioned between the liner and the casing in the radial direction .
A waveguide laser comprising: a semiconductor laser emitting laser beams; a solid-state laser element that amplifies the laser beams with a gain achieved by absorption of excitation light; a wavelength conversion element that converts part of fundamental waves of the laser beams output from the solid-state laser element to harmonics; and a wavelength selecting element that selectively reflects laser beams with wavelengths λ = λ 0 , λ 1 , λ 2 , ..., λ n (n ≥ 1) of different laser oscillation modes from among fundamental oscillation wavelengths of the laser beams passing through the wavelength conversion element, and that outputs harmonics resulting from the conversion by the wavelength conversion element, wherein the waveguide laser resonates the fundamental waves through an optical resonator structure including the solid-state laser element, the wavelength conversion element and the wavelength selecting element; and a laser beam is amplified by the solid state laser element during a round-trip between the solid-state laser element and the wavelength selecting element; and the wavelength conversion element converts the laser beams with the wavelengths λ = λ 0 , λ 1 , λ 2 , ..., λ n (n ≥ 1) of the different laser oscillation modes reflected by the wavelength selecting element to harmonics. a semiconductor laser emitting laser beams; a solid-state laser element that amplifies the laser beams with a gain achieved by absorption of excitation light; a wavelength conversion element that converts part of fundamental waves of the laser beams output from the solid-state laser element to harmonics; and a wavelength selecting element that selectively reflects laser beams with wavelengths λ = λ 0 , λ 1 , λ 2 , ..., λ n (n ≥ 1) of different laser oscillation modes from among fundamental oscillation wavelengths of the laser beams passing through the wavelength conversion element, and that outputs harmonics resulting from the conversion by the wavelength conversion element, wherein the waveguide laser resonates the fundamental waves through an optical resonator structure including the solid-state laser element, the wavelength conversion element and the wavelength selecting element; and a laser beam is amplified by the solid state laser element during a round-trip between the solid-state laser element and the wavelength selecting element; and the wavelength conversion element converts the laser beams with the wavelengths λ = λ 0 , λ 1 , λ 2 , ..., λ n (n ≥ 1) of the different laser oscillation modes reflected by the wavelength selecting element to harmonics.
A telescope comprising a fastener plate , a primary mirror carried by a front face of the plate, and a secondary mirror held facing the primary mirror by a support , the telescope being of Cassegrain type and characterized in that the plate has a rear surface including positioning references for positioning the telescope relative to an image capture device arranged facing the rear face, the positioning references being obtained by optical quality machining, and they comprise a face perpendicular to the optical axis of the telescope in order to form a tilt reference, a central bore in order to form a centering reference, and a concave surface in the form of a spherical cap having a center on the optical axis in order to define a distance for the image capture device relative to the secondary mirror .
A computer-implemented method for task execution on a graphics processor , the method comprising: creating a data structure for grouping data resources; populating the data structure with two or more data resources by using an encoding object, wherein the data structure is ordered based on an index associated with each data resource , and wherein the encoding object is configured to reorder the data structure based on one or more characteristics of the graphics processor by encoding the data structure into a graphics processing language; passing the encoded data structure to a first programming interface command, the first programming interface command configured to access the encoded data structure's data resources ; triggering execution of a first function on the graphics processer in response to passing the encoded data structure to the first programming interface command; passing the encoded data structure to a second programming interface command, the second programming interface command configured to access the encoded data structure's data resources ; and triggering execution of a second function on the graphics processer in response to passing the encoded data structure to the second programming interface command. creating a data structure for grouping data resources; populating the data structure with two or more data resources by using an encoding object, wherein the data structure is ordered based on an index associated with each data resource , and wherein the encoding object is configured to reorder the data structure based on one or more characteristics of the graphics processor by encoding the data structure into a graphics processing language; passing the encoded data structure to a first programming interface command, the first programming interface command configured to access the encoded data structure's data resources ; triggering execution of a first function on the graphics processer in response to passing the encoded data structure to the first programming interface command; passing the encoded data structure to a second programming interface command, the second programming interface command configured to access the encoded data structure's data resources ; and triggering execution of a second function on the graphics processer in response to passing the encoded data structure to the second programming interface command.
Use of an aqueous condom-compatible sexual lubricant composition to provide lubrication during sexual activity, wherein the composition comprises a coolant which is a cyclic carboxamide.
An apparatus comprising: a non-volatile storage including a first volume to store a basic input/output system (BIOS) and a second volume to store an operating system (OS) payload portion including an antivirus software stack, wherein the OS payload portion is separate from and is a subset of an OS kernel stored in a different storage and the antivirus software stack is to restore an integrity of the different storage subsequent to corruption of the different storage , wherein the BIOS is to pass control to a boot manager of the OS kernel stored in the different storage , and if the OS kernel does not successfully launch in a predetermined period, the BIOS to cause execution of the antivirus software stack to restore the integrity of the different storage , wherein the different storage comprises a mass storage, wherein the OS payload portion comprises a lightweight kernel that is launched by the antivirus software stack to validate an image of the OS kernel stored in the different storage . a non-volatile storage including a first volume to store a basic input/output system (BIOS) and a second volume to store an operating system (OS) payload portion including an antivirus software stack, wherein the OS payload portion is separate from and is a subset of an OS kernel stored in a different storage and the antivirus software stack is to restore an integrity of the different storage subsequent to corruption of the different storage , wherein the BIOS is to pass control to a boot manager of the OS kernel stored in the different storage , and if the OS kernel does not successfully launch in a predetermined period, the BIOS to cause execution of the antivirus software stack to restore the integrity of the different storage , wherein the different storage comprises a mass storage, wherein the OS payload portion comprises a lightweight kernel that is launched by the antivirus software stack to validate an image of the OS kernel stored in the different storage .
Device for linking seat movement to learning behaviour, whereby this device consists of a number of seating units , wherein these seating units are cube shaped and are each equipped with a digital module that is able to detect movements of the seating unit caused by pupils using them, and wherein each seating unit is configured to communicate these movements wirelessly to a central teaching module , and to wirelessly receive an individual message from the central teaching module afterwards, adapted to the movement that is made with each of the seating units .
Silica-including microcapsule resin particles, comprising: an outer shell constituted of a crosslinked polymer; and a cavity partitioned with said outer shell, wherein said silica-including microcapsule resin particles contain inside said cavity silica particles, and have a volume average particle diameter of 0.5 to 100 μm, the silica-including microcapsule resin particles contain inside said cavity a porous structure in which a part of the plurality of silica particles is mutually connected, and at an unconnected part, gaps as a macropore are formed between the silica particles, and the silica-including microcapsule resin particles are obtainable by the process according any one of claims 6 to 9. an outer shell constituted of a crosslinked polymer; and a cavity partitioned with said outer shell, wherein said silica-including microcapsule resin particles contain inside said cavity silica particles, and have a volume average particle diameter of 0.5 to 100 μm, the silica-including microcapsule resin particles contain inside said cavity a porous structure in which a part of the plurality of silica particles is mutually connected, and at an unconnected part, gaps as a macropore are formed between the silica particles, and the silica-including microcapsule resin particles are obtainable by the process according any one of claims 6 to 9.
An aircraft , comprising: an airframe with an upper portion and an extending tail ; a counter-rotating, coaxial main rotor assembly disposed at the upper portion of the airframe ; a translational thrust system , including a propeller , disposed at the extending tail of the airframe; a flight control system comprising a flight control computer and a translational thrust interface configured to receive commands from the flight control computer to control one or more actuators for the control of the translational thrust system , the flight control system configured to control at least one of revolutions-per-minute, RPM, and pitch of the propeller of the translational thrust system in response to an input speed or acceleration command, characterised in that the flight control system is configured to allow a pilot of the aircraft to enter a desired velocity or an acceleration, and the flight control computer is configured to generate commands to the translational thrust interface to establish at least one of an RPM and pitch to meet the desired velocity or acceleration. an airframe with an upper portion and an extending tail ; a counter-rotating, coaxial main rotor assembly disposed at the upper portion of the airframe ; a translational thrust system , including a propeller , disposed at the extending tail of the airframe; a flight control system comprising a flight control computer and a translational thrust interface configured to receive commands from the flight control computer to control one or more actuators for the control of the translational thrust system , the flight control system configured to control at least one of revolutions-per-minute, RPM, and pitch of the propeller of the translational thrust system in response to an input speed or acceleration command, characterised in that the flight control system is configured to allow a pilot of the aircraft to enter a desired velocity or an acceleration, and the flight control computer is configured to generate commands to the translational thrust interface to establish at least one of an RPM and pitch to meet the desired velocity or acceleration.
A method for monitoring a parameter of the quality of yarn or a parameter of a sensor in an electronic yarn cleaner having an optical detector with a sensor having one or two rows of individual optical elements having a rectangular shape made by CMOS technology and that produce an analog output signal proportional to irradiation intensity on the respective optical element , wherein a value of intensity of the irradiation is monitored during a measurement cycle, the method comprising: for the parameter of the quality of yarn or the parameter of the sensor that is monitored in each measurement cycle, selecting a number of the optical elements within at least one of the rows of optical elements, for constituting an active zone monitoring the output analog signals of the optical elements of the active zone; evaluating the parameter of the quality of yarn or the parameter of the sensor as a function of the output analog signals from the optical elements within the active zone; wherein for monitored parameter of the quality of yarn, a lowest possible number of the optical elements in the active zone are monitored whose respective output analog signal changes due to a change in the yarn quality parameter; and wherein for monitored parameter of the sensor, a highest possible number of the optical elements in the active zone whose respective output analog signal is not affected by a yam image projection are monitored. for the parameter of the quality of yarn or the parameter of the sensor that is monitored in each measurement cycle, selecting a number of the optical elements within at least one of the rows of optical elements, for constituting an active zone monitoring the output analog signals of the optical elements of the active zone; evaluating the parameter of the quality of yarn or the parameter of the sensor as a function of the output analog signals from the optical elements within the active zone; wherein for monitored parameter of the quality of yarn, a lowest possible number of the optical elements in the active zone are monitored whose respective output analog signal changes due to a change in the yarn quality parameter; and wherein for monitored parameter of the sensor, a highest possible number of the optical elements in the active zone whose respective output analog signal is not affected by a yam image projection are monitored.
A method of regulating fuel flow to a gas turbine engine , the method is characterised by comprising: governing power for the engine using a control structure having an inner control loop and an outer control loop , the outer control loop comprising a feedback controller that outputs a feedback command based on a power error determined as a function of a shaft horsepower, the feedback command used to determine a gas generator speed error, the gas generator speed error used by the inner control loop for outputting a fuel flow command; determining the shaft horsepower from a torque measurement of the engine using a torque pressure transducer; detecting a momentary loss of the torque measurement from the torque pressure transducer; and limiting power fluctuations due to the loss of torque measurement by maintaining the feedback command from the feedback controller constant during the momentary loss of torque measurement. governing power for the engine using a control structure having an inner control loop and an outer control loop , the outer control loop comprising a feedback controller that outputs a feedback command based on a power error determined as a function of a shaft horsepower, the feedback command used to determine a gas generator speed error, the gas generator speed error used by the inner control loop for outputting a fuel flow command; determining the shaft horsepower from a torque measurement of the engine using a torque pressure transducer; detecting a momentary loss of the torque measurement from the torque pressure transducer; and limiting power fluctuations due to the loss of torque measurement by maintaining the feedback command from the feedback controller constant during the momentary loss of torque measurement.