mhurhangee/ep-ind-claims huggingface dataset:
A central processing unit resource allocation method, wherein the method comprises: adjusting dynamically, according to a change in the number of virtual machines in an advanced resource pool, the number of allocated physical cores in the advanced resource pool; and adjusting, according to the number of the allocated physical cores in the advanced resource pool, the number of allocated physical cores in a default resource pool, wherein the advanced resource pool and the default resource pool are resource pools that are obtained by dividing physical cores of a central processing unit according to service levels of the resource pools, virtual machines in the default resource pool share computing resources of all the physical cores in the default resource pool, and a virtual machine that runs in the advanced resource pool is allowed to occupy a predetermined percentage of one physical core computing resource; wherein the step of adjusting dynamically comprises: when the number of the virtual machines in the advanced resource pool increases, determining, according to the number of increased virtual machines and a service level of the advanced resource pool, a number of physical cores that need to be allocated to the advanced resource pool, and allocating the number of physical cores to the advanced resource pool from the default resource pool; when after the number of the physical cores is allocated to the advanced resource pool from the default resource pool, lower-limit percentage of the physical core computing resources that can be occupied by each virtual machine in the default resource pool cannot be met, the method further comprises: adjusting, a lower limit of physical core computing resources occupied by each default virtual machine in the default resource pool. adjusting dynamically, according to a change in the number of virtual machines in an advanced resource pool, the number of allocated physical cores in the advanced resource pool; and adjusting, according to the number of the allocated physical cores in the advanced resource pool, the number of allocated physical cores in a default resource pool, when the number of the virtual machines in the advanced resource pool increases, determining, according to the number of increased virtual machines and a service level of the advanced resource pool, a number of physical cores that need to be allocated to the advanced resource pool, and allocating the number of physical cores to the advanced resource pool from the default resource pool; when after the number of the physical cores is allocated to the advanced resource pool from the default resource pool, lower-limit percentage of the physical core computing resources that can be occupied by each virtual machine in the default resource pool cannot be met, the method further comprises: adjusting, a lower limit of physical core computing resources occupied by each default virtual machine in the default resource pool. adjusting, a lower limit of physical core computing resources occupied by each default virtual machine in the default resource pool.
A method for wireless communications, comprising: receiving a semi-persistent scheduling, SPS, configuration message from a base station, the SPS configuration message comprising at least one SPS parameter for downlink SPS communications over a shared radio frequency spectrum band; identifying, based at least in part on the SPS configuration, one or more subframes or slots allocated for the downlink SPS communications; and performing the downlink SPS communications during the one or more subframes or slots and according to the SPS configuration, wherein performing the downlink SPS communications is characterised by: determining that a message was not received on a channel of the shared radio frequency spectrum during a first subframe or slot according to the SPS configuration; identifying, based at least in part on the determination, a second subframe or slot that replaces the first subframe or slot for transmission of the message and a configured window within an SPS period; and receiving a grantless transmission of the message on the channel during the second subframe or slot. receiving a semi-persistent scheduling, SPS, configuration message from a base station, the SPS configuration message comprising at least one SPS parameter for downlink SPS communications over a shared radio frequency spectrum band; identifying, based at least in part on the SPS configuration, one or more subframes or slots allocated for the downlink SPS communications; and performing the downlink SPS communications during the one or more subframes or slots and according to the SPS configuration, wherein performing the downlink SPS communications is characterised by: determining that a message was not received on a channel of the shared radio frequency spectrum during a first subframe or slot according to the SPS configuration; identifying, based at least in part on the determination, a second subframe or slot that replaces the first subframe or slot for transmission of the message and a configured window within an SPS period; and receiving a grantless transmission of the message on the channel during the second subframe or slot. determining that a message was not received on a channel of the shared radio frequency spectrum during a first subframe or slot according to the SPS configuration; identifying, based at least in part on the determination, a second subframe or slot that replaces the first subframe or slot for transmission of the message and a configured window within an SPS period; and receiving a grantless transmission of the message on the channel during the second subframe or slot.
An actuator assembly suitable for cryogenic device for controlling an outflow of a cryogenic fluid, wherein said actuator assembly comprises at least one spring leaf and a needle, whereby said spring leaf is configured to bear against a ball of a ball valve of the cryogenic device.
A fuel cell system comprising: a fuel cell which generates electric power by using a hydrogen gas and an oxidizing gas; a hydrogen gas supply route through which the hydrogen gas to be supplied to an anode of the fuel cell flows; an anode off-gas discharge route for discharging an anode off-gas discharged from the anode of the fuel cell to outside; an anode off-gas discharge valve provided to the anode off-gas discharge route; an anode off-gas circulation route for sending the anode off-gas from the anode off-gas discharge route to the hydrogen gas supply route; an anode off-gas circulator provided to the anode off-gas circulation route to circulate the anode off-gas; a coolant route through which a coolant to be supplied to the fuel cell flows; a coolant feeder provided to the coolant route to supply the coolant to the fuel cell; a humidifier provided to the coolant route and the hydrogen gas supply route to humidify the hydrogen gas by using the coolant; and a controller configured to cause the anode off-gas discharge valve to be opened when a temperature of any of the hydrogen gas supply route, the anode of the fuel cell, the anode off-gas discharge route, and the anode off-gas discharge valve becomes equal to or lower than a predetermined temperature, wherein the controller is further configured to cause the coolant feeder and the anode off-gas circulator to operate and causes the anode off-gas discharge valve to be opened, when a temperature of the coolant route becomes equal to or lower than a predetermined temperature. a fuel cell which generates electric power by using a hydrogen gas and an oxidizing gas; a hydrogen gas supply route through which the hydrogen gas to be supplied to an anode of the fuel cell flows; an anode off-gas discharge route for discharging an anode off-gas discharged from the anode of the fuel cell to outside; an anode off-gas discharge valve provided to the anode off-gas discharge route; an anode off-gas circulation route for sending the anode off-gas from the anode off-gas discharge route to the hydrogen gas supply route; an anode off-gas circulator provided to the anode off-gas circulation route to circulate the anode off-gas; a coolant route through which a coolant to be supplied to the fuel cell flows; a coolant feeder provided to the coolant route to supply the coolant to the fuel cell; a humidifier provided to the coolant route and the hydrogen gas supply route to humidify the hydrogen gas by using the coolant; and a controller configured to cause the anode off-gas discharge valve to be opened when a temperature of any of the hydrogen gas supply route, the anode of the fuel cell, the anode off-gas discharge route, and the anode off-gas discharge valve becomes equal to or lower than a predetermined temperature, wherein the controller is further configured to cause the coolant feeder and the anode off-gas circulator to operate and causes the anode off-gas discharge valve to be opened, when a temperature of the coolant route becomes equal to or lower than a predetermined temperature.
Method of operating a variable speed wind turbine as a function of wind speed, the wind turbine having a rotor with a plurality of blades and a generator, wherein the generator has a design rotor speed which varies so as to follow a theoretical generator rotor speed curve describing the rotational speed of the rotor as a function of wind speed, and the method comprising determining an erosion risk condition of the blades, and determining erosion damage of one or more of the blades accumulated over time, wherein the method further comprises, changing the rotor rotational speed from the design rotor speed as a function of the determined erosion risk condition and the determined accumulated erosion damage. determining an erosion risk condition of the blades, and determining erosion damage of one or more of the blades accumulated over time,
A method of magnetic crack depth prediction for a magnetisable component of a first geometry comprising: determining a measure of remnant magnetic flux leakage for a section of the component by obtaining at least one signal representative of remnant magnetic flux leakage at multiple sampling points along the section of the component and processing the at least one signal to determine remnant magnetic flux leakage; and, converting the remnant magnetic flux leakage to a predicted crack depth for that section of the component using an empirically determined relationship between remnant magnetic flux leakage and crack depth for a previously tested in service component of the first geometry; characterised in that the magnetisable component is subject to rolling contact fatigue and the processing comprises filtering the at least one signal through a digital high pass filter in opposite directions to remove signal components having a wavelength greater than a first wave length. determining a measure of remnant magnetic flux leakage for a section of the component by obtaining at least one signal representative of remnant magnetic flux leakage at multiple sampling points along the section of the component and processing the at least one signal to determine remnant magnetic flux leakage; and, converting the remnant magnetic flux leakage to a predicted crack depth for that section of the component using an empirically determined relationship between remnant magnetic flux leakage and crack depth for a previously tested in service component of the first geometry;
A backlight module, comprising: a back plate comprising a bottom plate, side plates surrounding the bottom plate, and bent parts formed by bending the side plates, wherein the bottom plate, the side plates, and the bent parts form a mounting space, each of sides of the bent parts away from the bottom plate is provided with a limiting step, each of the bent parts comprises an upper step surface and a lower step surface connected to the limiting step, and a part of a side of one of the upper step surfaces is recessed with an accommodating groove adjacent to one corresponding lower step surface; a support plate detachably disposed in the accommodating groove, and provided with a hanging ear protruding from a part of the support plate adjacent to the limiting step; a reflective sheet accommodated in the mounting space and disposed on the bottom plate; a light guide plate accommodated in the mounting space and disposed on a side of the reflective sheet away from the bottom plate; and a film accommodated in the mounting space, disposed on a side of the light guide plate away from the reflective sheet, and provided with a positioning portion, wherein the positioning portion comprises a positioning plate extending from a part of a side of the film close to the accommodating groove and perpendicular to the film and a positioning step extending from the positioning plate to the accommodating groove and forming an angle with the positioning plate, the positioning step is provided with a positioning hole, and the positioning step is sleeved on the hanging ear through the positioning hole. a back plate comprising a bottom plate, side plates surrounding the bottom plate, and bent parts formed by bending the side plates, wherein the bottom plate, the side plates, and the bent parts form a mounting space, each of sides of the bent parts away from the bottom plate is provided with a limiting step, each of the bent parts comprises an upper step surface and a lower step surface connected to the limiting step, and a part of a side of one of the upper step surfaces is recessed with an accommodating groove adjacent to one corresponding lower step surface; a support plate detachably disposed in the accommodating groove, and provided with a hanging ear protruding from a part of the support plate adjacent to the limiting step; a reflective sheet accommodated in the mounting space and disposed on the bottom plate; a light guide plate accommodated in the mounting space and disposed on a side of the reflective sheet away from the bottom plate; and a film accommodated in the mounting space, disposed on a side of the light guide plate away from the reflective sheet, and provided with a positioning portion, wherein the positioning portion comprises a positioning plate extending from a part of a side of the film close to the accommodating groove and perpendicular to the film and a positioning step extending from the positioning plate to the accommodating groove and forming an angle with the positioning plate, the positioning step is provided with a positioning hole, and the positioning step is sleeved on the hanging ear through the positioning hole.
A method for verifying a security device comprising an image including a signature, comprising the following steps: - acquiring the image according to a first optical spectrum in order to obtain a first representation, - extracting the signature, and - verifying the signature, characterized in that: - the signature is colorimetric and comprises a particular orientation of a color chart, or - the signature is a frequency signature, the image comprising at least one reference spatial period. - acquiring the image according to a first optical spectrum in order to obtain a first representation, - extracting the signature, and - verifying the signature, - the signature is colorimetric and comprises a particular orientation of a color chart, or - the signature is a frequency signature, the image comprising at least one reference spatial period.
A synchrocyclotron comprising: magnetic yokes (6a, 6b) that define a resonant cavity; a source to provide input voltage to the resonant cavity, the source comprising a voltage controlled oscillator; and feedback circuitry to control the source so that a frequency of the input voltage substantially matches a resonant frequency of the resonant cavity, the feedback circuitry comprising: a phase detector to detect a phase difference between the frequency of the input voltage and the resonant frequency and to output a current pulse; an integrator to receive output current pulses of the phase detector and to sum the output current pulses over time; and a filter to generate a control signal for the VCO based on integrated current pulses, the control signal for causing the VCO to change the frequency of the input voltage when the phase difference deviates from a predetermined value, and circuitry connected to the phase detector and configured to output input signals (f8, f9) to the phase detector, such that frequencies of the input signals (f8, f9) are substantially constant over a frequency range that the resonant cavity is swept. magnetic yokes (6a, 6b) that define a resonant cavity; a source to provide input voltage to the resonant cavity, the source comprising a voltage controlled oscillator; and feedback circuitry to control the source so that a frequency of the input voltage substantially matches a resonant frequency of the resonant cavity, the feedback circuitry comprising: a phase detector to detect a phase difference between the frequency of the input voltage and the resonant frequency and to output a current pulse; an integrator to receive output current pulses of the phase detector and to sum the output current pulses over time; and a filter to generate a control signal for the VCO based on integrated current pulses, the control signal for causing the VCO to change the frequency of the input voltage when the phase difference deviates from a predetermined value, and circuitry connected to the phase detector and configured to output input signals (f8, f9) to the phase detector, such that frequencies of the input signals (f8, f9) are substantially constant over a frequency range that the resonant cavity is swept. a phase detector to detect a phase difference between the frequency of the input voltage and the resonant frequency and to output a current pulse; an integrator to receive output current pulses of the phase detector and to sum the output current pulses over time; and a filter to generate a control signal for the VCO based on integrated current pulses, the control signal for causing the VCO to change the frequency of the input voltage when the phase difference deviates from a predetermined value, and circuitry connected to the phase detector and configured to output input signals (f8, f9) to the phase detector, such that frequencies of the input signals (f8, f9) are substantially constant over a frequency range that the resonant cavity is swept.
Sensor having a multi-layered ceramic substrate, a metal contact and at least one sensor element which is arranged in the ceramic substrate and which is contacted by means of the metal contact, wherein the individual layers of the ceramic substrate are securely connected to each other by means of sintering, wherein the metal contact is produced by means of a solder connection, which electrically connects the contact to the sensor element and which in this instance produces a secure mechanical connection of the contact with respect to the ceramic substrate, wherein the metal contact is constructed in the form of a pin or stud which is inserted into the ceramic substrate, wherein the sensor element is used for inductive or capacitive path/spacing/position measurement, wherein the contacting is constructed with respect to one or more coils and/or with respect to one or more electrode faces, and wherein the metal contact is inserted in a blind hole of the ceramic substrate.
A stowing system, comprising: a ram air turbine -RAT-; a closed loop hydraulic circuit configured to hold a quantity of a hydraulic fluid to be utilized only by the system; a RAT actuator disposed in fluid communication with the closed loop hydraulic circuit; a pump system comprising a pump connected to the hydraulic circuit to selectively pump the hydraulic fluid to a stow reservoir portion of the RAT actuator to move the RAT actuator from a deployed position to a stowed position; and a control valve connected to the hydraulic circuit between the RAT actuator and the pump to selectively allow the hydraulic fluid to be drained from the stow reservoir portion of the RAT actuator in a drain state and to allow the hydraulic fluid to be pumped into the stow reservoir portion of the RAT actuator in a pump state; wherein the hydraulic fluid is drained from the stow reservoir portion of the RAT actuator through the closed loop hydraulic circuit to a deploy reservoir portion of the RAT actuator. a ram air turbine -RAT-; a closed loop hydraulic circuit configured to hold a quantity of a hydraulic fluid to be utilized only by the system; a RAT actuator disposed in fluid communication with the closed loop hydraulic circuit; a pump system comprising a pump connected to the hydraulic circuit to selectively pump the hydraulic fluid to a stow reservoir portion of the RAT actuator to move the RAT actuator from a deployed position to a stowed position; and a control valve connected to the hydraulic circuit between the RAT actuator and the pump to selectively allow the hydraulic fluid to be drained from the stow reservoir portion of the RAT actuator in a drain state and to allow the hydraulic fluid to be pumped into the stow reservoir portion of the RAT actuator in a pump state; wherein the hydraulic fluid is drained from the stow reservoir portion of the RAT actuator through the closed loop hydraulic circuit to a deploy reservoir portion of the RAT actuator.
An air mixing system for a gas turbine engine comprising a combustor section with a combustion chamber and a diffuser case, the air mixing system comprising: a heat exchanger; a first extraction conduit configured to extract air or other coolant in a mounted state from a location within the diffuser case and fluidly coupled to an inlet of the heat exchanger; a second extraction conduit fluidly coupled to an outlet of the heat exchanger; an injection conduit fluidly coupled to the second extraction conduit; an onboard injector supply chamber configured to be positioned in a mounted state radially inward from the combustion chamber and fluidly coupled to the injection conduit; an onboard injector fluidly coupled to the onboard injector supply chamber; and a third extraction conduit configured to extend from the outer diameter of the combustor section toward the inner diameter of the combustor section and fluidly coupled between the second extraction conduit and the injection conduit, wherein the third extraction conduit has a double walled architecture, and wherein the heat exchanger supplies cooled air to the second extraction conduit; characterized by at least one mixing aperture formed in the third extraction conduit to enable warm air within the plenum of the combustor section and surrounding the third extraction conduit to enter the third extraction conduit and mix with the cooled air. a heat exchanger; a first extraction conduit configured to extract air or other coolant in a mounted state from a location within the diffuser case and fluidly coupled to an inlet of the heat exchanger; a second extraction conduit fluidly coupled to an outlet of the heat exchanger; an injection conduit fluidly coupled to the second extraction conduit; an onboard injector supply chamber configured to be positioned in a mounted state radially inward from the combustion chamber and fluidly coupled to the injection conduit; an onboard injector fluidly coupled to the onboard injector supply chamber; and a third extraction conduit configured to extend from the outer diameter of the combustor section toward the inner diameter of the combustor section and fluidly coupled between the second extraction conduit and the injection conduit, wherein the third extraction conduit has a double walled architecture, and wherein the heat exchanger supplies cooled air to the second extraction conduit; characterized by at least one mixing aperture formed in the third extraction conduit to enable warm air within the plenum of the combustor section and surrounding the third extraction conduit to enter the third extraction conduit and mix with the cooled air.