mhurhangee/ep-ind-claims huggingface dataset:
A paging method, wherein the method comprises: obtaining, by a second device, a discontinuous reception DRX period of a first device and an identifier of the first device; determining, by the second device according to the DRX period of the first device and the identifier of the first device, a paging occasion on which the first device pages the second device, wherein the second device transmits data to a network side device by using the first device as a relay node receiving the data from the second device and forwarding the data to the network side; and transmitting, by the first device, a first paging message on the paging occasion on which the first device pages the second device, wherein the first paging message is used by the first device to page the second device, and wherein the first device and the second device are communications devices. obtaining, by a second device, a discontinuous reception DRX period of a first device and an identifier of the first device; determining, by the second device according to the DRX period of the first device and the identifier of the first device, a paging occasion on which the first device pages the second device, wherein the second device transmits data to a network side device by using the first device as a relay node receiving the data from the second device and forwarding the data to the network side; and transmitting, by the first device, a first paging message on the paging occasion on which the first device pages the second device, wherein the first paging message is used by the first device to page the second device, and wherein the first device and the second device are communications devices.
Method for assisting in the piloting of an aircraft in an approach of the aircraft, with a view to a landing on a landing runway, characterized in that it comprises the following steps implemented iteratively: - a first determination step, implemented by a first determination module, consisting in determining a current state of the aircraft, the current state comprising at least one current position (Pc) of the aircraft; - a second determination step, implemented by a second determination module, consisting in determining a first distance (dstd) between a target state and the current state from a first approach strategy; - a third determination step, implemented by the second determination module, consisting in determining a first ellipse contained in a horizontal plane in which the aircraft is moving, the first ellipse being formed by points determined in such a way that a sum, on the one hand, of a distance between the current position (Pc) of the aircraft and the points of the first ellipse and, on the other hand, of a distance between the points of the first ellipse and a projection onto the horizontal plane of the target position (PFAF) is equal to the first distance (dstd); - a display step, implemented by a display module, comprising the display of at least the first ellipse on a screen of the display module. - a first determination step, implemented by a first determination module, consisting in determining a current state of the aircraft, the current state comprising at least one current position (Pc) of the aircraft; - a second determination step, implemented by a second determination module, consisting in determining a first distance (dstd) between a target state and the current state from a first approach strategy; - a third determination step, implemented by the second determination module, consisting in determining a first ellipse contained in a horizontal plane in which the aircraft is moving, the first ellipse being formed by points determined in such a way that a sum, on the one hand, of a distance between the current position (Pc) of the aircraft and the points of the first ellipse and, on the other hand, of a distance between the points of the first ellipse and a projection onto the horizontal plane of the target position (PFAF) is equal to the first distance (dstd); - a display step, implemented by a display module, comprising the display of at least the first ellipse on a screen of the display module.
A loop type heat pipe comprising: an evaporator that is configured to vaporize a liquid working fluid; a condenser that is configured to condense the vaporized working fluid into the liquid working fluid; a vapor pipe that is provided between the evaporator and the condenser and through which the vaporized working fluid flows; and a liquid pipe that is provided between the evaporator and the condenser and through which the liquid working fluid flows, wherein each of the vapor pipe and the liquid pipe comprises: a lower-side metal layer; an intermediate metal layer that is disposed on the lower-side metal layer; an upper-side metal layer that is disposed on the intermediate metal layer; and a conduit that is formed by the lower-side metal layer, the intermediate metal layer, and the upper-side metal layer, the loop type heat pipe being characterized in that at least one of the upper-side metal layer and the lower-side metal layer warps outward in a first portion of the vapor pipe. an evaporator that is configured to vaporize a liquid working fluid; a condenser that is configured to condense the vaporized working fluid into the liquid working fluid; a vapor pipe that is provided between the evaporator and the condenser and through which the vaporized working fluid flows; and a liquid pipe that is provided between the evaporator and the condenser and through which the liquid working fluid flows, wherein each of the vapor pipe and the liquid pipe comprises: a lower-side metal layer; an intermediate metal layer that is disposed on the lower-side metal layer; an upper-side metal layer that is disposed on the intermediate metal layer; and a conduit that is formed by the lower-side metal layer, the intermediate metal layer, and the upper-side metal layer, the loop type heat pipe being characterized in that at least one of the upper-side metal layer and the lower-side metal layer warps outward in a first portion of the vapor pipe. a lower-side metal layer; an intermediate metal layer that is disposed on the lower-side metal layer; an upper-side metal layer that is disposed on the intermediate metal layer; and a conduit that is formed by the lower-side metal layer, the intermediate metal layer, and the upper-side metal layer, the loop type heat pipe being characterized in that at least one of the upper-side metal layer and the lower-side metal layer warps outward in a first portion of the vapor pipe.
A stator vane assembly comprising: an inner diameter platform; an outer diameter platform defining an air inlet orifice extending radially therethrough; an airfoil extending between the inner diameter platform and the outer diameter platform, the airfoil having a hollow portion therein defining a serpentine cooling airflow path fluidly coupled to the air inlet orifice; characterized by: a collar extending radially outwardly from the outer diameter platform and positioned adjacent the air inlet orifice, the collar extending to a non-uniform radial distance, wherein a radially outer surface of the collar is angled to provide a lower height near the air inlet orifice; and a turn cover operatively coupled to the collar. an inner diameter platform; an outer diameter platform defining an air inlet orifice extending radially therethrough; an airfoil extending between the inner diameter platform and the outer diameter platform, the airfoil having a hollow portion therein defining a serpentine cooling airflow path fluidly coupled to the air inlet orifice; characterized by: a collar extending radially outwardly from the outer diameter platform and positioned adjacent the air inlet orifice, the collar extending to a non-uniform radial distance, wherein a radially outer surface of the collar is angled to provide a lower height near the air inlet orifice; and a turn cover operatively coupled to the collar. a collar extending radially outwardly from the outer diameter platform and positioned adjacent the air inlet orifice, the collar extending to a non-uniform radial distance, wherein a radially outer surface of the collar is angled to provide a lower height near the air inlet orifice; and a turn cover operatively coupled to the collar.
Method for reducing the influence of interference in the evaluation of at least one reception signal of a radar sensor installed in a vehicle, wherein predetermined transmission signals are emitted in predetermined operating situations and partial signals reflected twice or multiple times are received, and the signals received for the predetermined operating situations are stored for the purpose of determining an interference spectrum (r 1, r 2, r 3, r 4) and the influence of interference (7, 9) is reduced by taking into account the interference spectrum (r 1, r 2, r 3, r 4) during the signal evaluation, characterized in that the predetermined operating situations are the standstill of the vehicle in front of traffic lights, wherein, if the predetermined operating situation is detected, the emission of the predetermined transmission signals for sensor calibration is started and the reception signals which are then received and are reflected at stationary or fixed objects are evaluated and a search is made for multiple reflections in the reception signal, which are evaluated in order to determine a correction signal. predetermined transmission signals are emitted in predetermined operating situations and partial signals reflected twice or multiple times are received, and the signals received for the predetermined operating situations are stored for the purpose of determining an interference spectrum (r 1, r 2, r 3, r 4) and the influence of interference (7, 9) is reduced by taking into account the interference spectrum (r 1, r 2, r 3, r 4) during the signal evaluation, characterized in that the predetermined operating situations are the standstill of the vehicle in front of traffic lights, wherein, if the predetermined operating situation is detected, the emission of the predetermined transmission signals for sensor calibration is started and the reception signals which are then received and are reflected at stationary or fixed objects are evaluated and a search is made for multiple reflections in the reception signal, which are evaluated in order to determine a correction signal.
An oral care composition comprising: a) a water insoluble and/or slightly soluble calcium source; b) a tubule blockage enhancer selected from calcium dihydrogen phosphate, calcium sulfate hemihydrates or mixtures thereof; c) a phosphate source; and d) a physiologically acceptable carrier; wherein the calcium source is selected from calcium carbonate, calcium aluminate, calcium oxalate, aluminium calcium silicate, calcium hydroxide, calcium glycerophosphate, calcium oxide, calcium sulfate, calcium carboxymethyl cellulose, calcium alginate, calcium salts of citric acid or mixtures thereof; wherein the phosphate source is trisodium phosphate, monosodium dihydrogen phosphate, disodium hydrogen phosphate, ammonium phosphate, diammonium hydrogen phosphate, ammonium dihydrogen phosphate, tripotassium phosphate, monopotassium dihydrogen phosphate, dipotassium hydrogen phosphate or a mixture thereof; and wherein the calcium source and the tubule blockage enhancer are present in a weight ratio from 20:1 to 1:5. a) a water insoluble and/or slightly soluble calcium source; b) a tubule blockage enhancer selected from calcium dihydrogen phosphate, calcium sulfate hemihydrates or mixtures thereof; c) a phosphate source; and d) a physiologically acceptable carrier; wherein the calcium source is selected from calcium carbonate, calcium aluminate, calcium oxalate, aluminium calcium silicate, calcium hydroxide, calcium glycerophosphate, calcium oxide, calcium sulfate, calcium carboxymethyl cellulose, calcium alginate, calcium salts of citric acid or mixtures thereof; wherein the phosphate source is trisodium phosphate, monosodium dihydrogen phosphate, disodium hydrogen phosphate, ammonium phosphate, diammonium hydrogen phosphate, ammonium dihydrogen phosphate, tripotassium phosphate, monopotassium dihydrogen phosphate, dipotassium hydrogen phosphate or a mixture thereof; and wherein the calcium source and the tubule blockage enhancer are present in a weight ratio from 20:1 to 1:5. wherein the calcium source is selected from calcium carbonate, calcium aluminate, calcium oxalate, aluminium calcium silicate, calcium hydroxide, calcium glycerophosphate, calcium oxide, calcium sulfate, calcium carboxymethyl cellulose, calcium alginate, calcium salts of citric acid or mixtures thereof; wherein the phosphate source is trisodium phosphate, monosodium dihydrogen phosphate, disodium hydrogen phosphate, ammonium phosphate, diammonium hydrogen phosphate, ammonium dihydrogen phosphate, tripotassium phosphate, monopotassium dihydrogen phosphate, dipotassium hydrogen phosphate or a mixture thereof; and wherein the calcium source and the tubule blockage enhancer are present in a weight ratio from 20:1 to 1:5.
An apparatus for opening and/or closing and for locking a closed state of a closure device for at least partially closing a room opening, for example a window, a door or the like, the apparatus having a drive and a force transmission means transferring the driving force to the closure device and that can be coupled to a locking device of the closure device, and an end section of the force transmission means facing the closure device being able to be deflected by a deflecting device from a first direction of movement for closing the closure device into a second direction of movement for actuating the locking device of the closure device, and the deflecting device having a control curve, characterised in that the control curve is formed by a control groove made separately from the guide track for the force transmission means, into which groove a control pin disposed on the end section can be brought into contact upon entering into the control groove, and in this way, upon drawing the force transmission means further into the housing of the apparatus the end section can be deflected as regards its direction of movement, and in this way the locking device of the closure device can be actuated.
A method for determining the life of components of a wind turbine or similar according to its location, comprising the following phases: Phase 1: obtaining an aeroelastic model of the wind turbine according to its design conditions; Phase 2: obtaining an aeroelastic model of the actual wind turbine arranged at its site; Phase 3: determining the specific wind conditions at the site of the wind turbine; Phase 4: determining the specific operating conditions of the wind turbine at its site; Phase 5: determining the design fatigue loads on the components of the wind turbine modeled in phase 1 according to regulatory operating conditions and wind conditions; Phase 6: determining the actual fatigue loads on the components of the wind turbine modeled in phase 2 according to the wind conditions and operating conditions determined in phases 3 and 4; and Phase 7: determining the life of each component of the wind turbine at the site of the wind turbine, reintegrating the actual fatigue loads calculated in phase 6 until the design fatigue loads calculated in phase 5 are reached; characterized in that in phase 4 the degrees of misalignment of the wind turbine with respect to the incident wind are determined, the number of starts, normal stops and emergency stops of the wind turbine are determined, the percentage of the time during which the wind turbine is stopped is determined, and the percentage of the time during which the wind turbine is subjected to ice accretion and/or subjected to accretion conditions on aerodynamic surfaces of the wind turbine due to materials that are suspended in the air is determined. Phase 1: obtaining an aeroelastic model of the wind turbine according to its design conditions; Phase 2: obtaining an aeroelastic model of the actual wind turbine arranged at its site; Phase 3: determining the specific wind conditions at the site of the wind turbine; Phase 4: determining the specific operating conditions of the wind turbine at its site; Phase 5: determining the design fatigue loads on the components of the wind turbine modeled in phase 1 according to regulatory operating conditions and wind conditions; Phase 6: determining the actual fatigue loads on the components of the wind turbine modeled in phase 2 according to the wind conditions and operating conditions determined in phases 3 and 4; and Phase 7: determining the life of each component of the wind turbine at the site of the wind turbine, reintegrating the actual fatigue loads calculated in phase 6 until the design fatigue loads calculated in phase 5 are reached; characterized in that in phase 4 the degrees of misalignment of the wind turbine with respect to the incident wind are determined, the number of starts, normal stops and emergency stops of the wind turbine are determined, the percentage of the time during which the wind turbine is stopped is determined, and the percentage of the time during which the wind turbine is subjected to ice accretion and/or subjected to accretion conditions on aerodynamic surfaces of the wind turbine due to materials that are suspended in the air is determined.
Toilet paper that is three or four-ply toilet paper, wherein a basis weight per ply of the toilet paper is 14.9 g/m 2 or more and 16.2 g/m 2 or less, an overall paper thickness is 297 μm or more and 435 μm or less, a dry tensile strength in a longitudinal direction is 451 cN/25 mm or more and 1001 cN/25 mm or less, and a ratio of a wet tensile strength in a horizontal direction to a dry tensile strength in a horizontal direction is 0.09 or more, wherein the basis weight per ply is measured according to JIS P 8124, the paper thickness is measured by conditioning a test piece according to JIS P 8111 and then measuring the thickness of the test piece using a "PEACOCK G type" dial thickness gauge, the dry tensile strength is measured according to JIS P 8113, and the wet tensile strength is measured according to JIS P 8135. wherein a basis weight per ply of the toilet paper is 14.9 g/m 2 or more and 16.2 g/m 2 or less, an overall paper thickness is 297 μm or more and 435 μm or less, a dry tensile strength in a longitudinal direction is 451 cN/25 mm or more and 1001 cN/25 mm or less, and a ratio of a wet tensile strength in a horizontal direction to a dry tensile strength in a horizontal direction is 0.09 or more, wherein the basis weight per ply is measured according to JIS P 8124, the paper thickness is measured by conditioning a test piece according to JIS P 8111 and then measuring the thickness of the test piece using a "PEACOCK G type" dial thickness gauge, the dry tensile strength is measured according to JIS P 8113, and the wet tensile strength is measured according to JIS P 8135.
Isolated or purified heparan sulphate HS9, wherein following digestion with heparin lyases I, II and III and then subjecting the resulting disaccharide fragments to capillary electrophoresis analysis the heparan sulphate HS9 has a disaccharide composition comprising: Disaccharide Normalised weight percentage ΔUA,2S-GlcNS,6S 26.0±3.0 ΔUA,2S-GlcNS 10.0±2.0 ΔUA-GlcNS,6S 30.6±3.0 ΔUA,2S-GlcNAc,6S 1.75±2.0 or 1.7±2.0 ΔUA-GlcNS 18.0±3.0 ΔUA,2S-GlcNAc 1.2±0.5 ΔUA-GlcNAc,6S 12.5±3.0
Assembly for machining running surfaces and the edges on skis and snowboards, comprising a machine frame for securing the machining tools and the holding elements for the skis or snowboards during the machining of their running surfaces and edges, wherein the skis or snowboards during the machining are held stationary by the holding elements and the machining tools are movable in the machine frame on a carriage in the longitudinal direction of the skis, wherein a motor-driven sliding surface- and structure-grinding wheel is arranged on the carriage and designed to machine the bottom, and wherein two grinding wheels designed to machine the outer surfaces of the edges are arranged on the carriage, of which at least one is axially displaceable relative to the other one, characterized in that the grinding wheels designed to machine the outer surfaces of the edges are cup grinding wheels, two tuning grinding wheels designed to machine the edge underside are arranged on the carriage, of which at least one is axially displaceable relative to the other one, and means for determining the distance of the at least one tuning grinding wheel and the at least one cup grinding wheel to the ski and for controlling their axial feed are provided.
A Raschel machine, comprising: a plurality of first guide needles arranged along a first direction for guiding warp threads; a plurality of second guide needles arranged along the first direction for guiding weft threads; a plurality of needles arranged along the first direction for creating interlocked loops formed by threads, whereby wales are created, wherein the first guide needles are held by a first needle bar, the second guide needles are held by a second needle bar and the second needle bar can be moved back and forth between in each case two adjacent first guide needles, characterized in that the distance (d) between adjacent first guide needles is 50.8 mm. a plurality of first guide needles arranged along a first direction for guiding warp threads; a plurality of second guide needles arranged along the first direction for guiding weft threads; a plurality of needles arranged along the first direction for creating interlocked loops formed by threads, whereby wales are created, wherein the first guide needles are held by a first needle bar, the second guide needles are held by a second needle bar and the second needle bar can be moved back and forth between in each case two adjacent first guide needles, characterized in that the distance (d) between adjacent first guide needles is 50.8 mm.
A composition comprising a pattern-triggered immunity inductor and a systemic resistance inductor wherein the pattern-triggered immunity inductor is chitooligosaccharides and the systemic resistance inductor is sodium saccharin.
Frequency drift tracking receiver designed to receive packets of symbols modulating an RF signal, said receiver comprising an RF stage to translate the RF signal received at an intermediate frequency by means of a quadrature mixer and to digitise the signal thus obtained, characterised in that it also comprises: a digital mixer using a CORDIC to bring the frequency translated signal thus digitised into the base band, the CORDIC making a phase rotation (Δ φ) of each sample as a function of an estimate of the intermediate frequency; a base band digital processing module designed to be synchronised with packets of symbols and to estimate data transmitted in said packets, and to determine the sign ( ε n) of the variation in the frequency drift for each symbol from the data thus estimated, the intermediate frequency being estimated by integration of corrections of elementary frequency steps by a predetermined value ( δf) modified by the signs thus determined. a digital mixer using a CORDIC to bring the frequency translated signal thus digitised into the base band, the CORDIC making a phase rotation (Δ φ) of each sample as a function of an estimate of the intermediate frequency; a base band digital processing module designed to be synchronised with packets of symbols and to estimate data transmitted in said packets, and to determine the sign ( ε n) of the variation in the frequency drift for each symbol from the data thus estimated, the intermediate frequency being estimated by integration of corrections of elementary frequency steps by a predetermined value ( δf) modified by the signs thus determined.
Multi-layer loudspeaker cover for covering a loudspeaker, having at least a first layer, a second layer and a third layer, wherein the first layer is an air-permeable layer, the second layer is a layer with through-holes for the reduction of dynamic pressure, and the third layer is a dimensionally stable foam layer.