mhurhangee/ep-ind-claims huggingface dataset:
Method for shutting down at least one gas turbine, withat least one said gas turbine comprising a gas generator provided with rotary members (14, 15) and with a combustion chamber, with at least one said gas turbine comprising at least one power turbine, with at least one said gas turbine comprising a fuel circuit controlled by a computer, said computer being in communication with a selector, characterised in that the method comprises the following steps for shutting down at least one said gas turbine which is in operation and supplied with fuel by the fuel circuit: - generation of a command to shut down at least one gas turbine by means of the selector, - following said generation of the shutdown command, shutting off of the fuel circuit at the command of the computer, - following said generation of the shutdown command, when at least one said gas turbine is not idling prior to said shutoff or when said at least one gas turbine is idling at the time of said generation of the shutdown command for an operating time below a stored threshold, automatically setting said rotary members (14, 15) into rotation by means of an electric machine for a limited period. - generation of a command to shut down at least one gas turbine by means of the selector, - following said generation of the shutdown command, shutting off of the fuel circuit at the command of the computer, - following said generation of the shutdown command, when at least one said gas turbine is not idling prior to said shutoff or when said at least one gas turbine is idling at the time of said generation of the shutdown command for an operating time below a stored threshold, automatically setting said rotary members (14, 15) into rotation by means of an electric machine for a limited period.
A method of testing the operational status of an infrared sensor system, the system comprising an infrared sensor comprising a thermopile having a plurality of thermocouples connected in series with hot junctions connected to an infrared sensor absorber window, and a heater, located proximate to the infrared sensor, for heating the infrared sensor, wherein said infrared sensor system is located in a vacuum pump and directed to measure the thermal radiation emitted from a vacuum pump rotor surface (105, 105'); said method comprising the steps of: i. directing the infrared sensor at the vacuum pump rotor surface (105, 105'), the vacuum pump rotor surface (105, 105') having an emissivity E; ii. raising the temperature of the heater to heat the infrared sensor without significantly heating the vacuum pump rotor surface (105, 105'); iii. measuring the voltage generated, V G, by heating the infrared sensor; and iv. comparing the voltage generated by the infrared sensor with an expected voltage, V E, and v. if V G does not substantially equal V E, determining that the infrared system requires servicing due to contamination of the window or, if V G substantially equals V E, determining that the infrared sensor system is at ideal operational status. i. directing the infrared sensor at the vacuum pump rotor surface (105, 105'), the vacuum pump rotor surface (105, 105') having an emissivity E; ii. raising the temperature of the heater to heat the infrared sensor without significantly heating the vacuum pump rotor surface (105, 105'); iii. measuring the voltage generated, V G, by heating the infrared sensor; and iv. comparing the voltage generated by the infrared sensor with an expected voltage, V E, and v. if V G does not substantially equal V E, determining that the infrared system requires servicing due to contamination of the window or, if V G substantially equals V E, determining that the infrared sensor system is at ideal operational status.
A radiation curable composition comprising a 10-90 wt% of a cationically polymerizable compound, said polymerizable compound comprising at least an aromatic epoxy-functional and an aliphatic epoxy-functional component b 0.1-10 wt% of a cationic photoinitiator c 1-40 wt% of a radically polymerizable compound d 0.1-10 wt% of a radical photoinitiator and e 5-50 wt% of a filler having a mean average particle size of at least 3 nm and below 50 nm, wherein said composition comprises at least 20 wt.%, relative to the total weight of the composition, of one or more aliphatic epoxies. a 10-90 wt% of a cationically polymerizable compound, said polymerizable compound comprising at least an aromatic epoxy-functional and an aliphatic epoxy-functional component b 0.1-10 wt% of a cationic photoinitiator c 1-40 wt% of a radically polymerizable compound d 0.1-10 wt% of a radical photoinitiator and e 5-50 wt% of a filler having a mean average particle size of at least 3 nm and below 50 nm,
A method for controlling an energy terminal, comprising: determining a metric indicating a future availability of electricity at an energy terminal based on usage data for a user associated to use of electricity by the energy terminal; generating control data to control the distribution of electricity between the energy terminal and an energy infrastructure based on the metric; and communicating the control data to the energy terminal, wherein determining the metric indicating the future availability comprises: receiving geolocation data from a user device associated with a user of an energy terminal; determining, based on the geolocation data, a distance of the user from the energy terminal; and determining a time period of availability of the energy terminal based on the distance of the user from the energy terminal. determining a metric indicating a future availability of electricity at an energy terminal based on usage data for a user associated to use of electricity by the energy terminal; generating control data to control the distribution of electricity between the energy terminal and an energy infrastructure based on the metric; and receiving geolocation data from a user device associated with a user of an energy terminal; determining, based on the geolocation data, a distance of the user from the energy terminal; and determining a time period of availability of the energy terminal based on the distance of the user from the energy terminal.
Maraging steel subjected to nitriding treatment, the maraging steel consisting of • 0.008% or less of C, • 0.5% or less of Si, • 0.5% or less of Mn, • 0.5 to 1.5% of Cr, • 16.0 to 22.0% of Ni, • 3.0 to 7.0% of Co, • 3.0 to 7.0% of Mo, • 0.6 to 1.3% of Al, • optionally 0.0001 to 0.0030% of Mg, • optionally 0.0001 to 0.0030% of Ca, • optionally 0.0001 to 0.0030% of B, by mass% and having the shape of a steel strip of a thickness of 0.5 mm or less, wherein the balance consists of Fe and impurities, the impurities are restricted to • 0.01% or less of Ti, • 0.01% or less of Nb, • 0.01% or less of Ta, and • 0.01% or less of W, • 0,05% or less of P, • 0,05% or less of S, • 0,005% or less of N, • 0,003% or less of O, wherein a ratio of Al to Ti satisfies Al/Ti≥250, and a surface hardness of the maraging steel is 800 to 1,050 HV and an internal hardness of the maraging steel is 570 HV or less by Vickers hardness. • 0.008% or less of C, • 0.5% or less of Si, • 0.5% or less of Mn, • 0.5 to 1.5% of Cr, • 16.0 to 22.0% of Ni, • 3.0 to 7.0% of Co, • 3.0 to 7.0% of Mo, • 0.6 to 1.3% of Al, • optionally 0.0001 to 0.0030% of Mg, • optionally 0.0001 to 0.0030% of Ca, • optionally 0.0001 to 0.0030% of B, • 0.01% or less of Ti, • 0.01% or less of Nb, • 0.01% or less of Ta, and • 0.01% or less of W, • 0,05% or less of P, • 0,05% or less of S, • 0,005% or less of N, • 0,003% or less of O,
Filter material for manufacturing a nicotine delivery product, wherein the filter material is hydroentangled and contains at least 50% and at most 100% cellulose fibers, each with respect to the mass of the filter material, wherein the filter material has a basis weight of at least 25 g/m 2 and at most 60 g/m 2, and wherein the filter material has a structure that is characterized in that it provides the filter material with a transparency which, measured in accordance with DIN 53147:1993-01, is at least 45% and at most 70%.
A method of operating a vehicle in a descent profile, the method comprising: obtaining, at a controller module, a mathematical model of performance characteristics for an aircraft; generating an optimal guidance trajectory, for at least a first segment of descent, based on the mathematical model; and operating the aircraft in accordance with the optimal guidance trajectory prior to operating in a position-based guidance during a second segment of descent, which begins at an initial point, wherein operating the aircraft in the position-based guidance comprises operating the aircraft based on an instantaneous position of the aircraft relative to the descent profile; wherein the generating of the optimal guidance trajectory comprises calculating a speed along the optimal guidance trajectory for the mathematical model as a control variable, wherein the generating of the optimal guidance trajectory further comprises performing a cost analysis based on the performance characteristics, and wherein the optimal guidance trajectory is monotonically decreasing and ends at a minimum altitude that is up-track of the initial point of the position-based guidance. obtaining, at a controller module, a mathematical model of performance characteristics for an aircraft; generating an optimal guidance trajectory, for at least a first segment of descent, based on the mathematical model; and operating the aircraft in accordance with the optimal guidance trajectory prior to operating in a position-based guidance during a second segment of descent, which begins at an initial point, wherein operating the aircraft in the position-based guidance comprises operating the aircraft based on an instantaneous position of the aircraft relative to the descent profile; wherein the generating of the optimal guidance trajectory comprises calculating a speed along the optimal guidance trajectory for the mathematical model as a control variable, wherein the generating of the optimal guidance trajectory further comprises performing a cost analysis based on the performance characteristics, and wherein the optimal guidance trajectory is monotonically decreasing and ends at a minimum altitude that is up-track of the initial point of the position-based guidance.
Cage bar pack for installation into a strainer bar cage of a cage screw press, having at least one cage bar set formed from a plurality of cage bars and a set apparatus which fixes the plurality of cage bars of the at least one cage bar set, the set apparatus having, furthermore, at least one base element and one securing means, characterized in that the base element has a hollow semi-cylindrical shape, and in that the cage bar pack is an at least temporary structural unit, in that the base element is coupled temporarily or permanently to at least one strut/rod, and in that the strut/rod dimensionally stabilizes the base element, in that the at least one strut/rod can be used functionally as a handle and/or overhead action region, or in that the cage bar pack has at least one separate holding apparatus, and in that the at least one securing means is formed from at least one tensioning strap which is elastic at least in regions and can be subjected to a tensile load.
A Land Mobile Radio, LMR, comprising: a processor configured to control operations of the LMR; a first communication device (208, 210) coupled to the processor and configured to perform Near Field Communication, NFC, or Radio Frequency Identification, RFID, operations with an external device; and a second communication device coupled to the processor and configured to communicate information over an LMR network to a packet switched LMR infrastructure; and wherein the processor causes the second communication device to send or receive information associated with the NFC or RFID operations via the LMR network; characterized in that the LMR is configured for performing NFC or RFID operations with an external device to obtain access to contents of a safe box, and the LMR is configured for performing NFC or RFID operations with the external device to obtain access to an internal area of a structure that is associated with the incident event, and wherein the LMR is configured for communicating a notification of an access to the safe box's content to a remote computing device via the packet switched LMR infrastructure. a processor configured to control operations of the LMR; a first communication device (208, 210) coupled to the processor and configured to perform Near Field Communication, NFC, or Radio Frequency Identification, RFID, operations with an external device; and a second communication device coupled to the processor and configured to communicate information over an LMR network to a packet switched LMR infrastructure; and wherein the processor causes the second communication device to send or receive information associated with the NFC or RFID operations via the LMR network; characterized in that the LMR is configured for performing NFC or RFID operations with an external device to obtain access to contents of a safe box, and the LMR is configured for performing NFC or RFID operations with the external device to obtain access to an internal area of a structure that is associated with the incident event, and wherein the LMR is configured for communicating a notification of an access to the safe box's content to a remote computing device via the packet switched LMR infrastructure.
Pivoting bearing for a servomotor for a blade for a hub of a rotor of a wind generator, the blade having an axis and the bearing comprising: - a first and a second bearing race (13, 15, 19, 131, 151, 190) extending at two different radial distances away from the axis of the blade, so as to rotate relative to one another about this axis, - at least two series of rolling bodies (11a, 11b, 110a, 110b, 111a, 111b) with convex bearing surfaces collaborating with the concave bearing surfaces of the raceways (60b, 60c, 80a, 80b) that house these rolling bodies, which are stepped at two different levels in a direction parallel to the axis, which rolling bodies of each of the series of rolling bodies being arranged, in a plane radial to the axis of the blade, between the first and second races, - first means of fixing the first race (13, 131) to the rotor hub, - second means of fixing the second race (15, 151) to the blade, - at least one of the races being divided into at least two parts (15a, 15b, 131a, 131b) along a surface transverse to the axis of the blade, so that the rolling bodies can be fitted and/or removed, characterized in that the said at least two series of rolling bodies are series of barrel-shaped rolling bodies (11a, 11b, 110a, 110b, 111a, 111b) and the axes of rotation (112a, 112b) of the at least two series of rolling bodies are concurrent between the stages, which rolling bodies each have: - an axis of rotation (112a, 112b...) permanently oriented at an angle (i) with respect to the axis of the blade, - and, along this axis of rotation, a length between two planar ends of the said rolling body. - a first and a second bearing race (13, 15, 19, 131, 151, 190) extending at two different radial distances away from the axis of the blade, so as to rotate relative to one another about this axis, - at least two series of rolling bodies (11a, 11b, 110a, 110b, 111a, 111b) with convex bearing surfaces collaborating with the concave bearing surfaces of the raceways (60b, 60c, 80a, 80b) that house these rolling bodies, which are stepped at two different levels in a direction parallel to the axis, which rolling bodies of each of the series of rolling bodies being arranged, in a plane radial to the axis of the blade, between the first and second races, - first means of fixing the first race (13, 131) to the rotor hub, - second means of fixing the second race (15, 151) to the blade, - at least one of the races being divided into at least two parts (15a, 15b, 131a, 131b) along a surface transverse to the axis of the blade, so that the rolling bodies can be fitted and/or removed, characterized in that the said at least two series of rolling bodies are series of barrel-shaped rolling bodies (11a, 11b, 110a, 110b, 111a, 111b) and the axes of rotation (112a, 112b) of the at least two series of rolling bodies are concurrent between the stages, which rolling bodies each have: - an axis of rotation (112a, 112b...) permanently oriented at an angle (i) with respect to the axis of the blade, - and, along this axis of rotation, a length between two planar ends of the said rolling body.
Cartridge ammunition including: a projectile; a cartridge including: a) a cartridge case having a cylindrical sidewall having an open front end to which the projectile is attached and a base wall extending across the sidewall at a rear end of the cartridge case; b) a primer chamber adjacent the base wall in which an initiating primer is held and into which a firing pin of a firing weapon extends for initiating the primer; c) a high pressure chamber for holding a propellant charge, which is adjacent to and in communication with the primer chamber, the cartridge ammunition being characterised in that the cartridge further includes an intermediate pressure chamber for receiving expanding propellant gases from the high pressure chamber; and a low pressure chamber at an operative rear end of the projectile, for receiving expanding propellant gases from the intermediate pressure chamber, the pressure chambers being delimited by walls within the cartridge case which define at least one high pressure venting hole for expanding propellant gases between the high pressure chamber and the intermediate pressure chamber and at least one intermediate pressure venting hole for expanding propellant gases between the intermediate pressure chamber and the low pressure chamber, said at least one high pressure venting hole being covered by a rupturable burst membrane. a projectile; a cartridge including: a) a cartridge case having a cylindrical sidewall having an open front end to which the projectile is attached and a base wall extending across the sidewall at a rear end of the cartridge case; b) a primer chamber adjacent the base wall in which an initiating primer is held and into which a firing pin of a firing weapon extends for initiating the primer; c) a high pressure chamber for holding a propellant charge, which is adjacent to and in communication with the primer chamber, the cartridge ammunition being characterised in that the cartridge further includes a) a cartridge case having a cylindrical sidewall having an open front end to which the projectile is attached and a base wall extending across the sidewall at a rear end of the cartridge case; b) a primer chamber adjacent the base wall in which an initiating primer is held and into which a firing pin of a firing weapon extends for initiating the primer; c) a high pressure chamber for holding a propellant charge, which is adjacent to and in communication with the primer chamber, the cartridge ammunition being characterised in that the cartridge further includes
A disposable blood processing set for use on a centrifugal blood processing device, said disposable set comprising: a blood separation chamber adapted to be mounted on a rotor of said centrifugal blood processing device; a blood inlet line adapted to be coupled to a blood donor and to an inlet pump on said centrifugal blood processing device; an anti-coagulant line in fluid communication with said inlet line, said anticoagulant line being adapted to be fluidly coupled to a supply of anti-coagulant and being further adapted to be coupled to an anti-coagulant pump on said centrifugal blood processing device; a reservoir adapted to be coupled to at least one sensor for detecting a level of fluid in said reservoir; a return line in fluid communication with said reservoir, said return line being adapted to be coupled to said blood donor and to a return pump on said centrifugal blood processing device; a red blood cell line in fluid communication with said blood separation chamber and said reservoir; a collect line in fluid communication with said blood separation chamber and in selective communication with said reservoir and a collect bag, said collect line being adapted to be coupled to a collect pump; a plasma line in fluid communication with said blood separation chamber and with said reservoir, said plasma line being adapted to be coupled to a plasma pump; and a replacement fluid line in fluid communication with said reservoir and adapted to be placed in fluid communication with a source of replacement fluid such that replacement fluid may selectively flow through said replacement fluid line without mechanical assistance. a blood separation chamber adapted to be mounted on a rotor of said centrifugal blood processing device; a blood inlet line adapted to be coupled to a blood donor and to an inlet pump on said centrifugal blood processing device; an anti-coagulant line in fluid communication with said inlet line, said anticoagulant line being adapted to be fluidly coupled to a supply of anti-coagulant and being further adapted to be coupled to an anti-coagulant pump on said centrifugal blood processing device; a reservoir adapted to be coupled to at least one sensor for detecting a level of fluid in said reservoir; a return line in fluid communication with said reservoir, said return line being adapted to be coupled to said blood donor and to a return pump on said centrifugal blood processing device; a red blood cell line in fluid communication with said blood separation chamber and said reservoir; a collect line in fluid communication with said blood separation chamber and in selective communication with said reservoir and a collect bag, said collect line being adapted to be coupled to a collect pump; a plasma line in fluid communication with said blood separation chamber and with said reservoir, said plasma line being adapted to be coupled to a plasma pump; and a replacement fluid line in fluid communication with said reservoir and adapted to be placed in fluid communication with a source of replacement fluid such that replacement fluid may selectively flow through said replacement fluid line without mechanical assistance.