mhurhangee/patent-ind-claim-en huggingface dataset:
A method for autonomous and adaptive data security by processing data, comprising: executing on a processor a cognitive data file, the cognitive data file being a computer file comprising autonomous security means embedded in data for securing the data, wherein the processor is configured to perform steps comprising: establishing an initial dormant state for the data from a plurality of states including dormant, active, and moving; monitoring for a state change event of the data to an active or moving state; logging the state change event and data structure fields into memory along with metadata describing the data state, wherein the metadata contains at least data creator information, current user information, and current data environment information; establishing an indication of degree of trust of a data instantiation based on said state change event and data structure fields, wherein the degree of trust includes at least one of a degree of certainty or level of confidence that the data instantiation is permitted; determining and applying security requirements to permit a user access to contents of the data instantiation based on the degree of trust of the data instantiation; and managing and controlling the computational environment of said data based on the security requirements. establishing an initial dormant state for the data from a plurality of states including dormant, active, and moving; monitoring for a state change event of the data to an active or moving state; logging the state change event and data structure fields into memory along with metadata describing the data state, wherein the metadata contains at least data creator information, current user information, and current data environment information; establishing an indication of degree of trust of a data instantiation based on said state change event and data structure fields, wherein the degree of trust includes at least one of a degree of certainty or level of confidence that the data instantiation is permitted; determining and applying security requirements to permit a user access to contents of the data instantiation based on the degree of trust of the data instantiation; and managing and controlling the computational environment of said data based on the security requirements.
A replaceable tip for a demolition tool , the replaceable tip comprising: a first sidewall having a first contact side ; a second sidewall having a second contact side ; and a centre wall connecting the first sidewall and the second sidewall , the centre wall having a third contact side provided with a recess , the recess having a first and a second abutment surfaces and the third contact side having a third abutment surface adjacent the recess ; and a channel defined by the first, second and third contact sides , the channel being configured to receive an adapter of the demolition tool characterised in that first sidewall , second sidewall and centre wall are formed as a monolithic body, wherein the first abutment surface is substantially perpendicular to the second abutment surface and wherein the abutment surfaces are configured so as to transfer a resultant demolition force to the adapter in a direction perpendicular to the first abutment surface . a first sidewall having a first contact side ; a second sidewall having a second contact side ; and a centre wall connecting the first sidewall and the second sidewall , the centre wall having a third contact side provided with a recess , the recess having a first and a second abutment surfaces and the third contact side having a third abutment surface adjacent the recess ; and a channel defined by the first, second and third contact sides , the channel being configured to receive an adapter of the demolition tool characterised in that first sidewall , second sidewall and centre wall are formed as a monolithic body, wherein the first abutment surface is substantially perpendicular to the second abutment surface and wherein the abutment surfaces are configured so as to transfer a resultant demolition force to the adapter in a direction perpendicular to the first abutment surface .
A turbomachine assembly comprising: • a first rotor module comprising a first blade and a disk centered on a turbomachine longitudinal axis (X-X), the first blade being mounted on the external periphery of the disk from which it extends, and further comprising an airfoil , a platform , a support and a root embedded in a housing of the disk , • a second rotor module , connected to the first rotor module , and comprising a second blade with a length less than the first blade and a ferrule comprising a circumferential extension extending toward the platform of the first blade , and • a damping device extending with at least one component along the turbomachine longitudinal axis (X-X), characterized in that the damping device is annular while extending circumferentially around the turbomachine longitudinal axis (X-X) and in that the damping device comprises a first external surface supported with friction against the first module , as well as a second external surface supported with friction against the second module , so as to couple the modules in order to damp their respective vibrational movements during operation, the first external surface of the damping device being supported with friction on a radially internal surface of the platform of the first blade , the second external surface of the damping device being supported with friction on the ferrule . • a first rotor module comprising a first blade and a disk centered on a turbomachine longitudinal axis (X-X), the first blade being mounted on the external periphery of the disk from which it extends, and further comprising an airfoil , a platform , a support and a root embedded in a housing of the disk , • a second rotor module , connected to the first rotor module , and comprising a second blade with a length less than the first blade and a ferrule comprising a circumferential extension extending toward the platform of the first blade , and • a damping device extending with at least one component along the turbomachine longitudinal axis (X-X),
A leading edge structure for a flow control system of an aircraft , comprising a leading edge panel that surrounds a plenum in a curved manner, the plenum extending in a span direction , wherein the leading edge panel has a first side portion extending from a leading edge point to a first attachment end , wherein the leading edge panel has a second side portion opposite the first side portion , extending from the leading edge point to a second attachment end , wherein the leading edge panel comprises an inner surface facing the plenum and an outer surface in contact with an ambient flow , wherein the leading edge panel comprises a plurality of micro pores forming a fluid connection between the plenum and the ambient flow , and wherein the plenum is separated by a partition wall into a leading edge plenum section in the area of the leading edge point , and a downstream plenum section downstream from the leading edge plenum section , characterized in that the leading edge plenum section is connected to a first air inlet via a first duct , and the downstream plenum section is connected to a second air inlet via a second duct , and wherein the first air inlet is separate from the second air inlet and the first duct is separate from the second duct . a leading edge panel that surrounds a plenum in a curved manner, the plenum extending in a span direction , wherein the leading edge panel has a first side portion extending from a leading edge point to a first attachment end , wherein the leading edge panel has a second side portion opposite the first side portion , extending from the leading edge point to a second attachment end , wherein the leading edge panel comprises an inner surface facing the plenum and an outer surface in contact with an ambient flow , wherein the leading edge panel comprises a plurality of micro pores forming a fluid connection between the plenum and the ambient flow , and wherein the plenum is separated by a partition wall into a leading edge plenum section in the area of the leading edge point , and a downstream plenum section downstream from the leading edge plenum section , characterized in that the leading edge plenum section is connected to a first air inlet via a first duct , and the downstream plenum section is connected to a second air inlet via a second duct , and wherein the first air inlet is separate from the second air inlet and the first duct is separate from the second duct .
A fluid pressure regulation and conditioning module comprising: a manifold including an fluid inlet , fluid outlet and a fluid flow path between the fluid inlet and fluid outlet , and the manifold further including, for heating fluid flowing along the fluid flow path with an externally supplied heat exchange media, a heat exchange media inlet , heat exchange media outlet and a heat exchange media flow path between the heat exchange media inlet and heat exchange media outlet ; a pressure regulator assembled to the manifold and disposed along the fluid flow path for regulating the pressure of the fluid exiting the module; and a high-pressure filter assembly upstream of the pressure regulator , the high-pressure filter assembly including a filter housing characterised by the filter element contained within the filter housing , wherein the filter element comprises a high-pressure coalescing filter element ; and a flow control valve assembled to the manifold for controlling fluid flow from the high-pressure filter assembly to the pressure regulator , wherein the flow control valve is downstream of the high-pressure filter assembly and upstream of the pressure regulator . a manifold including an fluid inlet , fluid outlet and a fluid flow path between the fluid inlet and fluid outlet , and the manifold further including, for heating fluid flowing along the fluid flow path with an externally supplied heat exchange media, a heat exchange media inlet , heat exchange media outlet and a heat exchange media flow path between the heat exchange media inlet and heat exchange media outlet ; a pressure regulator assembled to the manifold and disposed along the fluid flow path for regulating the pressure of the fluid exiting the module; and a high-pressure filter assembly upstream of the pressure regulator , the high-pressure filter assembly including a filter housing characterised by the filter element contained within the filter housing , wherein the filter element comprises a high-pressure coalescing filter element ; and a flow control valve assembled to the manifold for controlling fluid flow from the high-pressure filter assembly to the pressure regulator , wherein the flow control valve is downstream of the high-pressure filter assembly and upstream of the pressure regulator .
A method of receiving system information by a user equipment, UE, in a wireless communication system, the method comprising: receiving from a base station a Physical Downlink Control Channel, PDCCH, including Downlink Control Information, DCI, for scheduling system information; obtaining (S1107) the DCI based on a System Information-Radio Network Temporary Identifier, SI-RNTI; obtaining (S1109) a value for informing a type of the system information from the DCI; receiving from the base station Remaining Minimum System Information, RMSI, based on the value being a first value; and receiving from the base station Other System Information, OSI, based on the value being a second value. receiving from a base station a Physical Downlink Control Channel, PDCCH, including Downlink Control Information, DCI, for scheduling system information; obtaining (S1107) the DCI based on a System Information-Radio Network Temporary Identifier, SI-RNTI; obtaining (S1109) a value for informing a type of the system information from the DCI; receiving from the base station Remaining Minimum System Information, RMSI, based on the value being a first value; and receiving from the base station Other System Information, OSI, based on the value being a second value.
Method for detecting damage during the operation of a gas turbine, comprising the following steps: - calculation of an average value (T avg,k ) of individual temperature measurement values (T i,k ) over a predetermined sampling period (t k ) of an ensemble of temperature sensors (S i ) in or on the gas turbine, - calculation of the individual temperature differences (ΔT i,k ) between the average value (T avg,k ) and the individual temperature measurement values (T i,k ) over the predetermined sampling period (t k ), - calculation of the individual temperature differences (ΔT i,k ) for chronologically successive sampling periods (t k ) over a predetermined time interval (dt 1 ), - compilation of a first distribution (D 1 ) by dividing the temperature differences (ΔT i,k ) assigned to one temperature sensor (S i ) for the predetermined time interval (dt 1 ) into temperature difference intervals (dT i,j ); - comparison of the first distribution (D 1 ) with a second distribution (D 2 ) of temperature differences (ΔT i,k ) likewise divided into temperature difference intervals (dT i,j ), - generation of an operating signal on the basis of a negative outcome of the comparison, - wherein the second distribution (D 2 ) relates to temperature differences (ΔT i,k ) of the same temperature sensor (S i ), which are divided into the same temperature difference intervals (dT i,j ) but which were calculated for a different time interval (dt 2 ). - calculation of an average value (T avg,k ) of individual temperature measurement values (T i,k ) over a predetermined sampling period (t k ) of an ensemble of temperature sensors (S i ) in or on the gas turbine, - calculation of the individual temperature differences (ΔT i,k ) between the average value (T avg,k ) and the individual temperature measurement values (T i,k ) over the predetermined sampling period (t k ), - calculation of the individual temperature differences (ΔT i,k ) for chronologically successive sampling periods (t k ) over a predetermined time interval (dt 1 ), - compilation of a first distribution (D 1 ) by dividing the temperature differences (ΔT i,k ) assigned to one temperature sensor (S i ) for the predetermined time interval (dt 1 ) into temperature difference intervals (dT i,j ); - comparison of the first distribution (D 1 ) with a second distribution (D 2 ) of temperature differences (ΔT i,k ) likewise divided into temperature difference intervals (dT i,j ), - generation of an operating signal on the basis of a negative outcome of the comparison, - wherein the second distribution (D 2 ) relates to temperature differences (ΔT i,k ) of the same temperature sensor (S i ), which are divided into the same temperature difference intervals (dT i,j ) but which were calculated for a different time interval (dt 2 ).
Flexible cable for use in moving applications including torsional stress, comprising: - one or more insulated cores ; - an extruded polymeric filler layer surrounding the one or more insulated cores , having an external surface defining a filler layer external perimeter substantially forming a closed convex polygonal chain with a plurality of line segments connecting consecutive vertices; and - an outer sheath surrounding the filler layer and directly applied on the filler layer , having an external surface defining a substantially circular outer sheath external perimeter . - one or more insulated cores ; - an extruded polymeric filler layer surrounding the one or more insulated cores , having an external surface defining a filler layer external perimeter substantially forming a closed convex polygonal chain with a plurality of line segments connecting consecutive vertices; and - an outer sheath surrounding the filler layer and directly applied on the filler layer , having an external surface defining a substantially circular outer sheath external perimeter .
A hydratable concentrated surfactant composition comprising: a) from 30 to 50 wt % of anionic surfactant selected from sodium laureth ether sulphate, sodium pareth ether sulphate and mixtures thereof, by weight based on the total weight of the composition; b) from 4 to 12 wt %, of a co-surfactant, which is selected from a betaine, cocamide monoethanolamide and mixtures thereof, based on the total weight of the hydratable concentrated surfactant composition; c) from 0.2 to 3 wt %, by weight of the total composition, of sodium benzoate; d) an additional phase modifier selected from alkyl trimethyl ammonium compounds having an alkyl chain of C8 - C22 carbon atoms and salts thereof;; e) from 0.2 to 3 wt % of a viscosity modifier, by weight of the total composition, which is an inorganic electrolyte; f) from 10 to 60 % by weight water by weight of the total composition; wherein the surfactants are in a lamellar phase; and wherein the hydratable concentrated surfactant composition has a pH of from 3 to 6; and wherein the hydratable concentrated surfactant composition has a viscosity of from 8,000 to 200,000 mPas -1 (cps), when measured at 30°C on a Brookfield DV2T using a Spindle RV-05 at 20 rpm for 60 seconds on a Helipath stand; and wherein the weight ratio of a) the anionic surfactant to b) the co- surfactant is from 3:1 to 10:1. wherein the weight ratio of sodium benzoate (c) to total surfactant (a) + (b) is 1:5 to 1: 75, preferably from 1:10 to 1:65, more preferably 1:15 to 1:50, most preferably 1:15 to 1:35. a) from 30 to 50 wt % of anionic surfactant selected from sodium laureth ether sulphate, sodium pareth ether sulphate and mixtures thereof, by weight based on the total weight of the composition; b) from 4 to 12 wt %, of a co-surfactant, which is selected from a betaine, cocamide monoethanolamide and mixtures thereof, based on the total weight of the hydratable concentrated surfactant composition; c) from 0.2 to 3 wt %, by weight of the total composition, of sodium benzoate; d) an additional phase modifier selected from alkyl trimethyl ammonium compounds having an alkyl chain of C8 - C22 carbon atoms and salts thereof;; e) from 0.2 to 3 wt % of a viscosity modifier, by weight of the total composition, which is an inorganic electrolyte; f) from 10 to 60 % by weight water by weight of the total composition; wherein the surfactants are in a lamellar phase; and wherein the hydratable concentrated surfactant composition has a pH of from 3 to 6; and wherein the hydratable concentrated surfactant composition has a viscosity of from 8,000 to 200,000 mPas -1 (cps), when measured at 30°C on a Brookfield DV2T using a Spindle RV-05 at 20 rpm for 60 seconds on a Helipath stand; and wherein the weight ratio of a) the anionic surfactant to b) the co- surfactant is from 3:1 to 10:1. wherein the weight ratio of sodium benzoate (c) to total surfactant (a) + (b) is 1:5 to 1: 75, preferably from 1:10 to 1:65, more preferably 1:15 to 1:50, most preferably 1:15 to 1:35.
An endotracheal tube insertion device comprising: an insertion member ; an optical assembly including an optical housing and an elongated flexible member disposed within the optical housing , the elongated flexible member having a first end which is a distal end and a second end which is a proximal end, the elongated flexible member movably mounted to the insertion member ; an intubation assembly including a rod having a first end which is a distal end and a second end which is a proximal end; and an endotracheal tube carried by the rod ; characterised in that the rod has a guide system formed at said first end thereof, the guide system including a guide rail having an elongated guide member portion laterally retained in a channel formed in the optical assembly and configured for releasable attachment to the first end of the elongated flexible member of the optical assembly ; wherein the first end of the rod has a substantially cone-shaped surface defining a tapered leading end . an insertion member ; an optical assembly including an optical housing and an elongated flexible member disposed within the optical housing , the elongated flexible member having a first end which is a distal end and a second end which is a proximal end, the elongated flexible member movably mounted to the insertion member ; an intubation assembly including a rod having a first end which is a distal end and a second end which is a proximal end; and an endotracheal tube carried by the rod ; characterised in that the rod has a guide system formed at said first end thereof, the guide system including a guide rail having an elongated guide member portion laterally retained in a channel formed in the optical assembly and configured for releasable attachment to the first end of the elongated flexible member of the optical assembly ; wherein the first end of the rod has a substantially cone-shaped surface defining a tapered leading end .
A granule made of biocompatible metallic material, in particular made of titanium or titanium alloys, for vertebroplasty operations, characterized in that it has a spherical shape and comprises a central core with a solid structure, also spherical, having an outer surface from which a first diametrical rib and a second diametrical rib also having a solid structure, protrude, arranged according to two diameters orthogonal to each other, and in that it comprises a portion having a trabeculated structure which extends between the outer surface of said central core and the outer surface of the granule itself.
An array substrate, comprising: a substrate ; a detection circuit and at least one metal layer not overlapping with the detection circuit in a direction perpendicular to the substrate , both located on the substrate ; and a protective layer covering the metal layer, wherein the array substrate further comprises a plurality of input and output terminals formed on the substrate and the protective layer exposes the plurality of input and output terminals , the detection circuit is further arranged between the plurality of input terminals and the plurality of output terminals in a plane view, , characterized in that : the detection circuit and the plurality of input and output terminals form a bonding area for bonding a driver chip, the detection circuit contains a plurality of transistors connected with one another, connected to a display area of the substrate via fan-out wire, and configured for detecting a circuit of the array substrate before bonding the driver chip, and an area exposed by the protective layer is equal to the bonding area or greater than the bonding area. a substrate ; a detection circuit and at least one metal layer not overlapping with the detection circuit in a direction perpendicular to the substrate , both located on the substrate ; and a protective layer covering the metal layer, wherein the array substrate further comprises a plurality of input and output terminals formed on the substrate and the protective layer exposes the plurality of input and output terminals , the detection circuit is further arranged between the plurality of input terminals and the plurality of output terminals in a plane view, , characterized in that : the detection circuit and the plurality of input and output terminals form a bonding area for bonding a driver chip, the detection circuit contains a plurality of transistors connected with one another, connected to a display area of the substrate via fan-out wire, and configured for detecting a circuit of the array substrate before bonding the driver chip, and an area exposed by the protective layer is equal to the bonding area or greater than the bonding area.