mhurhangee/patent-ind-claim-en huggingface dataset:
A GPRS system, wherein the GPRS system characterized by comprising a serving GPRS support node, SGSN, device , and a home location register, HLR/home subscription system, HSS , wherein the SGSN device is configured to: receive a request message from user equipment, UE , acquire an authentication vector from the HLR/HSS , wherein the authentication vector comprises a first ciphering key and a first integrity key, when the request message comprises UE type indication information and the UE type indication information indicates that the UE is UE of a first type, determine that the UE is UE of the first type, select a ciphering algorithm and an integrity algorithm for the UE , send the selected ciphering algorithm and the selected integrity algorithm to the UE , and obtain a second ciphering key and a second integrity key according to the first ciphering key and the first integrity key; and the HLR/HSS is configured to: send the authentication vector to the SGSN device ; wherein the second ciphering key and the ciphering algorithm are used to perform ciphering protection on a message transmitted between the SGSN device and the UE , and the second integrity key and the integrity algorithm are used to perform integrity protection on a message transmitted between the SGSN device and the UE .
Package comprising nutritionally balanced animal food containing a Probiotic, wherein the package comprises an outer layer comprising a barrier having a permeability coefficient of no more than 75 grams/day/m 2 /bar (10 -5 grams/day/cm 2 /mmHg) for water vapor and oxygen permeation, wherein the animal food has a water activity of less than 0.3 when packed, wherein the package is effective at preventing the Probiotic from losing more than two logs after 6 months of packing, wherein the Probiotic is coated on the animal food, wherein the package comprises a desiccant, and wherein the animal food is a kibble.
A method of boring through subterranean formations utilizing a shield boring machine, said method comprising the use of a foamed aqueous composition comprising: (a) from 0.002 to 4.0 % by weight (% wt) of a cationic tamarind gum and (b) from 0.05 to 6.0 % by weight of a surfactant.
1. A cold rolled and heat treated steel sheet having a composition comprising the following elements, expressed in per cent by weight: 0.10% ≤ carbon ≤ 0.6%, 4 % ≤ manganese ≤ 20 %, 5 % ≤ aluminium ≤ 15 %, 0 ≤ silicon ≤ 2 %, aluminium + silicon + nickel ≥ 6.5%, and can possibly contain one or more of the following optional elements 0.01% ≤ niobium ≤ 0.3%, 0.01% ≤ titanium ≤ 0.2% 0.01% ≤ vanadium ≤ 0.6% 0.01% ≤ copper ≤ 2.0% 0.01% ≤ nickel ≤ 2.0% cerium ≤ 0.1% boron ≤ 0.01% magnesium ≤ 0.05% zirconium ≤ 0.05% molybdenum ≤ 2.0% tantalum ≤ 2.0% tungsten ≤ 2.0% the remainder being composed of iron and unavoidable impurities caused by elaboration, wherein the microstructure of said steel sheet comprises in area fraction, 10 to 50 % of austenite, said austenite phase optionally including intragranular kappa carbides, the reminder being regular ferrite and a minimum of 0.1% of ordered ferrite of D03 structure (Fe,Mn,X)3Al, optionally including up to 2% of intragranular kappa carbides (Fe,Mn)3AICx, said steel sheet presenting a ultimate tensile strength higher than or equal to 900 MPa, wherein tensile strength is measured according to ISO standard ISO 6892-1 and the microstructure is measured as defined in the description. 0.10% ≤ carbon ≤ 0.6%, 4 % ≤ manganese ≤ 20 %, 5 % ≤ aluminium ≤ 15 %, 0 ≤ silicon ≤ 2 %, aluminium + silicon + nickel ≥ 6.5%, and can possibly contain one or more of the following optional elements 0.01% ≤ niobium ≤ 0.3%, 0.01% ≤ titanium ≤ 0.2% 0.01% ≤ vanadium ≤ 0.6% 0.01% ≤ copper ≤ 2.0% 0.01% ≤ nickel ≤ 2.0% cerium ≤ 0.1% boron ≤ 0.01% magnesium ≤ 0.05% zirconium ≤ 0.05% molybdenum ≤ 2.0% tantalum ≤ 2.0% tungsten ≤ 2.0%
Sand core making machine comprising a core box , a blowing device suitable for introducing a sand-binder mixture in the core box , and a hardening device suitable for introducing pressurized hot air in the core box , conducted through a specific path to said core box , for hardening the mixture present in said core box , the hardening device comprising at least one heating unit (3.1) in said path upstream of the core box for heating said pressurized air before it reaches said core box , characterized in that the machine further comprises a flowmeter for measuring the flow of the pressurized air through said path, a flow regulator for regulating said airflow, the flow regulator being able to be acted on depending on the measurement obtained by the flowmeter , and a control unit which is communicated with the flowmeter and with the flow regulator , and configured for acting on the flow regulator for regulating pressurized airflow depending on the measurement obtained by means of the flowmeter , the core box comprising a cavity (1.3) with the shape of the core to be made, at least one inlet conduit (1.1.1) communicating the outside of the core box with the cavity (1.3) to be able to introduce the mixture and the pressurized air in the cavity (1.3), and at least one outlet conduit (1.2.1) different from the inlet conduit (1.1.1), communicating the outside of the core box with the cavity (1.3) to be able to discharge air present in the cavity (1.3) from said cavity (1.3) as the mixture and the pressurized air are introduced in said cavity (1.3), the machine comprising an outlet pipe fluidically communicated with the outlet conduit (1.2.1) for conducting air discharged through said outlet conduit (1.2.1) where required, and the flow regulator being arranged in said outlet pipe , said flow regulator thereby being configured for directly regulating the flow through the outlet pipe .
An electrical device, comprising: a universal motor having at least one coil ; a first input configured to be coupled to a rechargeable direct current (DC) power source ; a second input configured to be coupled to an alternating current (AC) power source ; a motor control module that is operably connected to the universal motor , to the first input and to the second input , the motor control module configured to deliver power from at least one of the rechargeable DC power source and the AC power source to the universal motor ; and a charge control circuit that is operably connected to the universal motor and to the second input , wherein the charge control circuit is configured to enable charging the rechargeable DC power source using energy from the AC power source and the at least one coil of the universal motor in a buck converter configuration, the charge control circuit being configured to enable charging of the rechargeable DC power source when the universal motor is operating using energy from the AC power source ; wherein the charge control circuit comprises a first switch connected in series between a negative terminal of the rechargeable DC power source and a terminal of the at least one coil and a second switch and a diode connected in series between a positive terminal of the rechargeable DC power source and the terminal of the at least one coil and in parallel to the first switch . a universal motor having at least one coil ; a first input configured to be coupled to a rechargeable direct current (DC) power source ; a second input configured to be coupled to an alternating current (AC) power source ; a motor control module that is operably connected to the universal motor , to the first input and to the second input , the motor control module configured to deliver power from at least one of the rechargeable DC power source and the AC power source to the universal motor ; and a charge control circuit that is operably connected to the universal motor and to the second input , wherein the charge control circuit is configured to enable charging the rechargeable DC power source using energy from the AC power source and the at least one coil of the universal motor in a buck converter configuration, the charge control circuit being configured to enable charging of the rechargeable DC power source when the universal motor is operating using energy from the AC power source ; wherein the charge control circuit comprises a first switch connected in series between a negative terminal of the rechargeable DC power source and a terminal of the at least one coil and a second switch and a diode connected in series between a positive terminal of the rechargeable DC power source and the terminal of the at least one coil and in parallel to the first switch .
A computer-implemented method for determining magnetic resonance imaging ("MRI") scan parameters for a multi-spectral imaging ("MSI") scan, the steps of the method comprising: (a) providing to a computer system, calibration data acquired with an MRI system from a field -of-view of a subject, wherein the calibration data contains a plurality of different data sets each acquired at a different resonance frequency offset, the data sets corresponding to a plurality of spectral bins, each spectral bin corresponding to a section acquired at a different discrete resonance frequency offset; (b) computing with the computer system, a field map from the calibration data, the field map containing information about off-resonance effects in the field-of-view; (c) determining with the computer system, a spectral range from the computed field map, wherein the spectral range is tailored to the frequency offset distribution within the field of view, and wherein the spectral range defines a range of off-resonance frequency values to be used in the MSI scan of said subject; (d) setting with the computer system, a number of spectral bins based on the determined spectral range; and (e) generating with the computer system, scan parameters based on the number of spectral bins and the determined spectral range, the scan parameters defining the spectral bins at which spins are to be excited and data are to be acquired with an MRI system performing the MSI scan of said subject. (a) providing to a computer system, calibration data acquired with an MRI system from a field -of-view of a subject, wherein the calibration data contains a plurality of different data sets each acquired at a different resonance frequency offset, the data sets corresponding to a plurality of spectral bins, each spectral bin corresponding to a section acquired at a different discrete resonance frequency offset; (b) computing with the computer system, a field map from the calibration data, the field map containing information about off-resonance effects in the field-of-view; (c) determining with the computer system, a spectral range from the computed field map, wherein the spectral range is tailored to the frequency offset distribution within the field of view, and wherein the spectral range defines a range of off-resonance frequency values to be used in the MSI scan of said subject; (d) setting with the computer system, a number of spectral bins based on the determined spectral range; and (e) generating with the computer system, scan parameters based on the number of spectral bins and the determined spectral range, the scan parameters defining the spectral bins at which spins are to be excited and data are to be acquired with an MRI system performing the MSI scan of said subject.
Fan for a motor vehicle, comprising an impeller formed by multiple blades and a base supporting the impeller, said impeller being rotated about an axis of rotation , said base comprising an upstream front wall facing the ventilation air flow and extending externally in a radial plane with reference to said axis, and an outer wall extending axially from said front wall, said front wall having a protrusion bordering the impeller, said protrusion extending axially upstream with respect to the plane of said front wall, and the upstream end of which is situated further upstream than the upstream end of the blades of said impeller, the blades being connected externally to a shroud , and said protrusion having the form of an axisymmetric rib which extends as far as an inner radial end positioned radially inside the outer end of the blades or of the shroud , characterized in that said front wall is positioned axially in the same plane as said upstream end of the blades and/or of the shroud.
An isolated, modified human kynureninase enzyme, said modified enzyme having substitutions relative to native human kynureninase (see SEQ ID NO: 8), wherein the substitutions are at positions: A99, F306, and A436; or A99, G112, F306, V339, 1405, and S408; or A99, 1131, F249, E259, and F306; or A99 and F306; or A99, T138, F306, and A436; or A99, G112, F306, L337, 1405, and S408; or A99, G112, F306, L337, V339, 1405, and S408; or A99, G112, F306, V339, 1405, and S408. A99, F306, and A436; or A99, G112, F306, V339, 1405, and S408; or A99, 1131, F249, E259, and F306; or A99 and F306; or A99, T138, F306, and A436; or A99, G112, F306, L337, 1405, and S408; or A99, G112, F306, L337, V339, 1405, and S408; or A99, G112, F306, V339, 1405, and S408.
An airbag for a vehicle occupant restraint system comprising an airbag panel defining an inflatable airbag volume and including a front panel portion and a rear panel portion , a tether extending in the interior of the airbag across the inflatable airbag volume, a discharge orifice formed in the rear panel portion of the airbag panel , as well as a first closing tab and a second closing tab for closing the discharge orifice , wherein the tether extends from a first tether end tightly connected to the front panel portion in the direction of the discharge orifice to an opposed second tether end , wherein the first closing tab extends from a first tab end tightly connected to the rear panel portion to a second tab end tightly connected to the second tether end , and wherein the second closing tab is fastened adjacent to the discharge orifice on the rear panel portion , characterized in that the two closing tabs are coupled by a connection releasable when a vehicle occupant impacts on the inflated airbag .
Fiber-laser apparatus, comprising: a laser-resonator including a non-polarization maintaining gain-fiber , the laser-resonator terminated at first and second ends thereof by respectively first and second reflectors , the laser-resonator having two orthogonal linear eigen-polarizations; a pump-radiation source arranged to provide pump-radiation to the gain-fiber and cause laser-radiation to circulate in the laser-resonator and laser-radiation to be delivered by the laser-resonator ; a polarizer located between one of the reflectors and the gain-fiber, the polarizer arranged to select one of the two eigen polarizations, the laser radiation circulating in the laser-resonator in only the selected eigen-polarization, thereby causing the laser-radiation delivered from the laser-resonator to be linearly-polarized; and a wavelength-selective device located in the laser-resonator for selecting the wavelength of the delivered radiation from within a gain-bandwidth of the gain-fiber. a laser-resonator including a non-polarization maintaining gain-fiber , the laser-resonator terminated at first and second ends thereof by respectively first and second reflectors , the laser-resonator having two orthogonal linear eigen-polarizations; a pump-radiation source arranged to provide pump-radiation to the gain-fiber and cause laser-radiation to circulate in the laser-resonator and laser-radiation to be delivered by the laser-resonator ; a polarizer located between one of the reflectors and the gain-fiber, the polarizer arranged to select one of the two eigen polarizations, the laser radiation circulating in the laser-resonator in only the selected eigen-polarization, thereby causing the laser-radiation delivered from the laser-resonator to be linearly-polarized; and a wavelength-selective device located in the laser-resonator for selecting the wavelength of the delivered radiation from within a gain-bandwidth of the gain-fiber.
Food composition comprising dairy fat - which food composition is whipped or foamed or which food composition is suitable for whipping or foaming, optionally after reconstitution in water - the food composition having a fat content of at least 15 wt.%, preferably of at least 18 wt. %, more preferably of at least 23 wt.%, in particular of at least 30 wt. %, based on total weight of the food composition, the composition comprising acylglycerides having a carbon number in the range of 24-40 ('CN24-CN40') and acylglycerides having a carbon number in the range of 42-56 ('CN42-CN56'), the molar ratio of acylglycerides having a carbon number in the range of 24-40 to acylglycerides having a carbon number in the range of 42-56 ('CN24-CN40 : CN42-CN56') being in the range of 1.1 - 1.4, and wherein, based on the total weight of the fatty acid residues, calculated as fatty acid methyl ester, the food composition has a C4:0 fatty acid content of at least 3.5 wt. %, preferably of 4.0-5.0 wt. %; a C6:0 fatty acid content of at least 2.0 wt. %, preferably 2.0-3.0 wt. %; a C8:0 fatty acid content of at least. 1.0 wt. %, preferably 1.2-1.5 wt. %, and a C12:0 fatty acid content of less than 6.0 wt. %. a C4:0 fatty acid content of at least 3.5 wt. %, preferably of 4.0-5.0 wt. %; a C6:0 fatty acid content of at least 2.0 wt. %, preferably 2.0-3.0 wt. %; a C8:0 fatty acid content of at least. 1.0 wt. %, preferably 1.2-1.5 wt. %, and a C12:0 fatty acid content of less than 6.0 wt. %.
An additive manufacturing method for depositing a metal paste to produce a metal part, the method comprising: (a1) depositing a metal paste to form a wet film on a metal or ceramic substrate, wherein the metal paste comprises: (i) metal scaffold particles with D50 particle size, measured by volume of particles using static light scattering particle size analyzer, between 1μm and 5μm, the metal scaffold particles having a concentration of between 50-70 wt% of the metal paste; (ii) metal infiltrant particles with D50 particle size, measured by volume of particles using static light scattering particle size analyzer, of less than 1 5 of the D50 particle size of the metal scaffold particles, such that the metal infiltrant particles primarily position in the interstitial spaces formed between the metal scaffold particles, the metal infiltrant particles being in a concentration of 10-30 wt% of the metal paste; (b1) drying the wet film until a solvent is essentially removed from the wet layer by energy input, and some residual components of the wet film optionally decompose, thereby forming a dried film; (c1) performing a laser scribing in which material is selectively removed from the dried film by light excitation with laser power between 1-10W to define a layer shape; (d1) sintering the dried film, wherein energy is applied to the film such that the layer is heated to a temperature of between 500-800°C and metal particles fuse together and with the underlying layer; and (e1) repeating (a1) to (d1) to produce the metal part. (a1) depositing a metal paste to form a wet film on a metal or ceramic substrate, wherein the metal paste comprises: (i) metal scaffold particles with D50 particle size, measured by volume of particles using static light scattering particle size analyzer, between 1μm and 5μm, the metal scaffold particles having a concentration of between 50-70 wt% of the metal paste; (ii) metal infiltrant particles with D50 particle size, measured by volume of particles using static light scattering particle size analyzer, of less than 1 5 of the D50 particle size of the metal scaffold particles, such that the metal infiltrant particles primarily position in the interstitial spaces formed between the metal scaffold particles, the metal infiltrant particles being in a concentration of 10-30 wt% of the metal paste; (b1) drying the wet film until a solvent is essentially removed from the wet layer by energy input, and some residual components of the wet film optionally decompose, thereby forming a dried film; (c1) performing a laser scribing in which material is selectively removed from the dried film by light excitation with laser power between 1-10W to define a layer shape; (d1) sintering the dried film, wherein energy is applied to the film such that the layer is heated to a temperature of between 500-800°C and metal particles fuse together and with the underlying layer; and (e1) repeating (a1) to (d1) to produce the metal part.
Method (METH) for localizing a beacon (X) by means of a first, second a third transceivers (A, B, C), each of the beacon (X), the first, the second and the third transceivers (A, B, C) comprising a local oscillator theoretically oscillating at a same reference frequency (f ref ) but in practice oscillating at different reference frequencies (f refA , f refB , f refC ) due to frequency drifts, the method (METH) comprising the following steps: - transmission (Etp_Em_FskA), by a first transceiver (A), of a signal, called the initiation signal (FskA), said initiation signal (FskA) being received by second and third transceivers (B, C), - calculation, by means of the initiation signal (FskA), of errors (e AB , e AC ) between the reference frequency (f refA ) of the first transceiver (A) and the reference frequencies (f refB , f refC ) of the second and third transceivers (B, C), - transmission (Et_Em_BpskX), by the beacon (X), of a first pulsed signal (BpskX), said first pulsed signal (BpskX) being received by the first, second and third transceivers (A, B, C), - transmission (Etp_Em_BpskA), by the first transceiver (A), of a second pulsed signal (BpskA), said second pulsed signal (BpskA) being received by the second and third transceivers (B, C), - calculation (Etp_Cal_Δt), by means of frequency reference errors (e AB , e AC ), of at least three differences (Δt 1 , Δt 2 , Δt 3 ) between the times-of-flight of the first and second pulsed signals (BpskX, BpskA), each time-of-flight difference (Δt 1 , Δt 2 , Δt 3 ) being calculated in the base time of the first transceiver (A), and - calculation (Etp_Cal_PosX) of a position of a beacon (X) by means of the time-of-flight differences (Δt 1 , Δt 2 , Δt 3 ). - transmission (Etp_Em_FskA), by a first transceiver (A), of a signal, called the initiation signal (FskA), said initiation signal (FskA) being received by second and third transceivers (B, C), - calculation, by means of the initiation signal (FskA), of errors (e AB , e AC ) between the reference frequency (f refA ) of the first transceiver (A) and the reference frequencies (f refB , f refC ) of the second and third transceivers (B, C), - transmission (Et_Em_BpskX), by the beacon (X), of a first pulsed signal (BpskX), said first pulsed signal (BpskX) being received by the first, second and third transceivers (A, B, C), - transmission (Etp_Em_BpskA), by the first transceiver (A), of a second pulsed signal (BpskA), said second pulsed signal (BpskA) being received by the second and third transceivers (B, C), - calculation (Etp_Cal_Δt), by means of frequency reference errors (e AB , e AC ), of at least three differences (Δt 1 , Δt 2 , Δt 3 ) between the times-of-flight of the first and second pulsed signals (BpskX, BpskA), each time-of-flight difference (Δt 1 , Δt 2 , Δt 3 ) being calculated in the base time of the first transceiver (A), and - calculation (Etp_Cal_PosX) of a position of a beacon (X) by means of the time-of-flight differences (Δt 1 , Δt 2 , Δt 3 ).