mhurhangee/patent-ind-claim-en huggingface dataset:
An apparatus comprising: a detector configured to detect electromagnetic radiation emitted by at least one electromagnetic radiation source where the detector comprises a first portion and a second portion ; a deformable substrate configured to support the detector such that the first portion of the detector is moveable relative to the second portion of the detector; and a sensor configured to detect deformation of the substrate and provide information indicative of the detected deformation to image processing circuitry and controlling circuitry , the controlling circuitry being configured to obtain the information indicative of the deformation and, based on this information, to control at least one parameter of the at least one electromagnetic radiation source. a detector configured to detect electromagnetic radiation emitted by at least one electromagnetic radiation source where the detector comprises a first portion and a second portion ; a deformable substrate configured to support the detector such that the first portion of the detector is moveable relative to the second portion of the detector; and a sensor configured to detect deformation of the substrate and provide information indicative of the detected deformation to image processing circuitry and controlling circuitry , the controlling circuitry being configured to obtain the information indicative of the deformation and, based on this information, to control at least one parameter of the at least one electromagnetic radiation source.
An engine bleed system for a gas turbine engine of an aircraft , the engine bleed system comprising: a plurality of engine bleed taps (68, 70, 72A, 72B; 152A-152D) comprising a mid-compressor bleed tap (68; 152B) configured to be located axially between two of a plurality of variable vane assemblies of a compressor section of the gas turbine engine, at least one low stage bleed tap (70; 152A) configured to be located axially upstream from the mid-compressor bleed tap, and at least one high stage bleed tap (72A, 72B; 152C, 152D) configured to be located axially downstream from the mid-compressor bleed tap; a mid-compressor bleed flow path configured to extend between the mid-compressor bleed tap and an aircraft use , the mid-compressor bleed flow path including an external manifold (154; 354; 554; 654) in pneumatic communication with the mid-compressor bleed tap and configured to be located outside of a casing of the gas turbine engine, wherein the external manifold is configured to encase an unison ring and vane arm assembly of at least one of the variable vane assemblies proximate to the mid-compressor bleed tap , and wherein the external manifold is configured such that an actuator of the at least one encased variable vane assembly is outside of the external manifold; and a valve system operable to select one of the engine bleed taps as a bleed air source for the aircraft use. a plurality of engine bleed taps (68, 70, 72A, 72B; 152A-152D) comprising a mid-compressor bleed tap (68; 152B) configured to be located axially between two of a plurality of variable vane assemblies of a compressor section of the gas turbine engine, at least one low stage bleed tap (70; 152A) configured to be located axially upstream from the mid-compressor bleed tap, and at least one high stage bleed tap (72A, 72B; 152C, 152D) configured to be located axially downstream from the mid-compressor bleed tap; a mid-compressor bleed flow path configured to extend between the mid-compressor bleed tap and an aircraft use , the mid-compressor bleed flow path including an external manifold (154; 354; 554; 654) in pneumatic communication with the mid-compressor bleed tap and configured to be located outside of a casing of the gas turbine engine, wherein the external manifold is configured to encase an unison ring and vane arm assembly of at least one of the variable vane assemblies proximate to the mid-compressor bleed tap , and wherein the external manifold is configured such that an actuator of the at least one encased variable vane assembly is outside of the external manifold; and a valve system operable to select one of the engine bleed taps as a bleed air source for the aircraft use.
A method for preparing a compound of formula (A), the method comprising the steps of: (a) contacting a compound of formula , with a compound of formula , in the presence of a Lewis Acid in a solvent to provide a compound of formula , (b) contacting the compound of formula of step (a) with an aqueous base to provide a compound of formula , (c) contacting the compound of formula of step (b) with DMF and a chlorinating agent in an organic solvent, followed by treatment of the resulting acid chloride derivative with aqueous ammonia to provide a compound of formula , (d) contacting the compound of formula of step (c) with an aqueous solution of NaOH and NaOCl to provide a compound of formula , (e) contacting the compound of formula of step (d) with (+)-dibenzoyl-D-tartaric acid monohydrate in a solvent to provide a compound of formula , (f) contacting the compound of formula of step (e) with an aqueous base, followed by treatment of the resulting free base with BoC 2 O in an organic solvent to provide a compound of formula , (g) contacting the compound of formula of step (f) with a mixture of a reducing agent, a chiral auxiliary and a Lewis acid in a solvent, followed by treatment with an oxidant in the presence of a base to provide a compound of formula , and (h) contacting the compound of formula of step (g) with a solution of hydrochloric acid in a solvent to provide the compound of formula (A). (a) contacting a compound of formula , with a compound of formula , in the presence of a Lewis Acid in a solvent to provide a compound of formula , (b) contacting the compound of formula of step (a) with an aqueous base to provide a compound of formula , (c) contacting the compound of formula of step (b) with DMF and a chlorinating agent in an organic solvent, followed by treatment of the resulting acid chloride derivative with aqueous ammonia to provide a compound of formula , (d) contacting the compound of formula of step (c) with an aqueous solution of NaOH and NaOCl to provide a compound of formula , (e) contacting the compound of formula of step (d) with (+)-dibenzoyl-D-tartaric acid monohydrate in a solvent to provide a compound of formula , (f) contacting the compound of formula of step (e) with an aqueous base, followed by treatment of the resulting free base with BoC 2 O in an organic solvent to provide a compound of formula , (g) contacting the compound of formula of step (f) with a mixture of a reducing agent, a chiral auxiliary and a Lewis acid in a solvent, followed by treatment with an oxidant in the presence of a base to provide a compound of formula , and (h) contacting the compound of formula of step (g) with a solution of hydrochloric acid in a solvent to provide the compound of formula (A).
A cartridge for a drug delivery device being at least partially filled with a medicinal product to be dispensed by the drug delivery device, the cartridge comprising - a sidewall of substantially tubular shape, - a proximal end section sealed by an axially displaceable piston , - a distal end section sealed by a seal and being penetrable by a piercing element , wherein the seal is secured to the sidewall by means of a fixing sleeve comprising a centric through opening through which the piercing element is to be guided for piercing and penetrating the seal , wherein the diameter or the surface of a pierceable section of the seal is smaller than 20 % of the diameter or cross section confined by the tubular section of the sidewall , characterized in that the diameter or the surface of the fixing sleeve's through opening is smaller than 30 % of the diameter or cross section of the fixing sleeve . - a sidewall of substantially tubular shape, - a proximal end section sealed by an axially displaceable piston , - a distal end section sealed by a seal and being penetrable by a piercing element , wherein the seal is secured to the sidewall by means of a fixing sleeve comprising a centric through opening through which the piercing element is to be guided for piercing and penetrating the seal , wherein the diameter or the surface of a pierceable section of the seal is smaller than 20 % of the diameter or cross section confined by the tubular section of the sidewall , characterized in that the diameter or the surface of the fixing sleeve's through opening is smaller than 30 % of the diameter or cross section of the fixing sleeve .
A method of manufacturing a color steel sheet having a polished stainless steel texture, characterized by comprising: (a) a step of forming a plating layer on a front surface of a steel sheet material (S10); (b) a step of polishing the plating layer (S20); (c) a step of forming a pretreatment layer on the polished plating layer (S30); (d) a step of forming a top coating layer on the pretreatment layer (S40); and (e) a step of forming a back coating layer on a rear surface of the steel sheet material (S50), wherein the step of polishing the plating layer (S20) includes a first polishing step of primarily polishing the plating layer with a brush roll to form thick and short patterns in the plating layer (S20-1), and a second polishing step of secondarily polishing the plating layer with a belt to form thin and long hairlines in the plating layer (S20-2), the plating layer is polished so that roughness Ra of the plating layer becomes 0.2 to 0.6 after the first polishing step, and a ratio of the 60-degree glossiness in the hairline direction to the 60-degree glossiness in the direction perpendicular to the hairline direction is equal or larger than 2 after the second polishing step, and the top coating layer is formed by a paint composition containing 25 to 35 wt% of an A-type resin which is a high-polymer resin, 20 to 30 wt% of a B-type resin which is larger in weight-average molecular weight and higher in glass transition temperature than the A-type resin, 10 to 30 wt% of a solvent, 5 to 15 wt% of an anticorrosive paste, 1 to 10 wt% of a coloring paste, 0.5 to 2 wt% of wax and 0.5 to 1 wt% of acryl beads, on the basis of a total weight of the paint composition, wherein the A-type resin has a weight-average molecular weight of 15,000 to 20,000 and a glass transition temperature of 3 to 8°C, and the B-type resin has a weight-average molecular weight of 20,000 to 25,000 and a glass transition temperature of 60 to 70°C. (a) a step of forming a plating layer on a front surface of a steel sheet material (S10); (b) a step of polishing the plating layer (S20); (c) a step of forming a pretreatment layer on the polished plating layer (S30); (d) a step of forming a top coating layer on the pretreatment layer (S40); and (e) a step of forming a back coating layer on a rear surface of the steel sheet material (S50),
Laying tool for laying cables, in particular in cavities that are difficult to access, for example in suspended ceiling constructions, comprising - an extendable bar with - a fixing means configured as an opening at one end for the detachable fastening of a cable or of a single insulated lead, characterized in that the extendable bar is a folding meter consisting of a multitude of folding members and the opening is an opening, that tapers off in one direction for clamping a cable, that is provided on an end folding member of the folding meter . - an extendable bar with - a fixing means configured as an opening at one end for the detachable fastening of a cable or of a single insulated lead,
A fuel tank (T) having a built-in component with a head portion , a neck portion , and a shoulder portion , and having the built-in component anchored to a tank body (Ta) with a parison (S, SA) wrapped around the neck portion during molding, wherein the fuel tank (T) comprises: a deformation prevention structure configured to prevent a wrapping parison portion wrapped around the neck portion from being deformed due to pressure acting on the tank body, and configured to include at least one convex stepped portion provided on the shoulder portion , characterized in that the shoulder portion is formed, at a position thereof around the neck portion , with two air vent holes such that air in a gap defined between the shoulder portion and the head portion is dischargeable to a back surface of the shoulder portion through the air vent holes . the fuel tank (T) comprises: a deformation prevention structure configured to prevent a wrapping parison portion wrapped around the neck portion from being deformed due to pressure acting on the tank body, and configured to include at least one convex stepped portion provided on the shoulder portion , characterized in that the shoulder portion is formed, at a position thereof around the neck portion , with two air vent holes such that air in a gap defined between the shoulder portion and the head portion is dischargeable to a back surface of the shoulder portion through the air vent holes .
A method of wireless communications, comprising: determining , at a relay node, a first predicted motion of a first vehicle including a first wireless communication device having an established first communication channel (520. 620. 720) with the relay node; determining that the first predicted motion will trigger a communication condition for the first vehicle and a second wireless communication device having an established second communication channel with the relay node , by determining that the first vehicle will travel past the relay node to be closer to the second wireless communication device than the relay node is to the second wireless communication device; reserving radio resources for a third communication channel between the first wireless communication device and the second wireless communication device; and transmitting an indication of the reserved radio resources to the first wireless communication device via the first communication channel and to the second wireless communication device via the second communication channel. determining , at a relay node, a first predicted motion of a first vehicle including a first wireless communication device having an established first communication channel (520. 620. 720) with the relay node; determining that the first predicted motion will trigger a communication condition for the first vehicle and a second wireless communication device having an established second communication channel with the relay node , by determining that the first vehicle will travel past the relay node to be closer to the second wireless communication device than the relay node is to the second wireless communication device; reserving radio resources for a third communication channel between the first wireless communication device and the second wireless communication device; and transmitting an indication of the reserved radio resources to the first wireless communication device via the first communication channel and to the second wireless communication device via the second communication channel.
An information processing method, applied to a User Equipment, UE, and comprising: receiving, by the UE, first Downlink Control Information, DCI, used for scheduling first downlink data transmission, wherein the first DCI is transmitted on a first Control Resource Set, CORESET, in a first CORESET group, and the first CORESET group comprises one or more CORESETs; and detecting, by the UE, second DCI for scheduling second downlink data transmission, wherein the first DCI corresponds to a first Transmission Configuration Indicator, TCI, state group, and, the second DCI corresponds to a second TCI state group; wherein the method further comprises: determining one or more TCI states according to Radio Resource Control, RRC, configuration signaling; and selecting at least part of TCI states in the one or more TCI states as the first TCI state group according to Media Access Control, MAC, Control Element, CE, signaling. receiving, by the UE, first Downlink Control Information, DCI, used for scheduling first downlink data transmission, wherein the first DCI is transmitted on a first Control Resource Set, CORESET, in a first CORESET group, and the first CORESET group comprises one or more CORESETs; and detecting, by the UE, second DCI for scheduling second downlink data transmission, wherein the first DCI corresponds to a first Transmission Configuration Indicator, TCI, state group, and, the second DCI corresponds to a second TCI state group; wherein the method further comprises: determining one or more TCI states according to Radio Resource Control, RRC, configuration signaling; and selecting at least part of TCI states in the one or more TCI states as the first TCI state group according to Media Access Control, MAC, Control Element, CE, signaling. determining one or more TCI states according to Radio Resource Control, RRC, configuration signaling; and selecting at least part of TCI states in the one or more TCI states as the first TCI state group according to Media Access Control, MAC, Control Element, CE, signaling.
A method comprising: receiving , by a computing system of an access management system, from a computing device operated by a user, a validation request to authenticate the access management system, the validation request including user identification information associated with the user; sending , by the computing system, to a destination associated with the user based on the user identification information, first temporary access information for the user to authenticate the access management system; receiving , by the computing system, from the computing device, a first response including second temporary access information; upon determining that the second temporary access information received in the first response matches the first temporary access information, sending , by the computing system, personal information about the user to the computing device; receiving , from the computing device, a second response, wherein the second response indicates a confirmation by the user of the personal information sent to the computing device, wherein the second response includes credential data of the user, wherein the second response is separate from the first response, and wherein the first response does not comprise the credential data; and determining , by the computing system, authentication of the user to access a resource from the computing device, wherein the authentication of the user is determined based on the credential data and the confirmation of the personal information received in the second response. receiving , by a computing system of an access management system, from a computing device operated by a user, a validation request to authenticate the access management system, the validation request including user identification information associated with the user; sending , by the computing system, to a destination associated with the user based on the user identification information, first temporary access information for the user to authenticate the access management system; receiving , by the computing system, from the computing device, a first response including second temporary access information; upon determining that the second temporary access information received in the first response matches the first temporary access information, sending , by the computing system, personal information about the user to the computing device; receiving , from the computing device, a second response, wherein the second response indicates a confirmation by the user of the personal information sent to the computing device, wherein the second response includes credential data of the user, wherein the second response is separate from the first response, and wherein the first response does not comprise the credential data; and determining , by the computing system, authentication of the user to access a resource from the computing device, wherein the authentication of the user is determined based on the credential data and the confirmation of the personal information received in the second response.
A method for determining filter coefficients of an audio precompensation controller for the compensation of an associated sound system , comprising N ≥ 2 loudspeakers, wherein said method comprises the steps of: - estimating (S1), for each one of at least a pair of said loudspeakers, a model transfer function at each of a plurality M of control points distributed in Z ≥ 2 spatially separated listening zones in a listening environment of said sound system; - determining (S2), for each of said M control points, a zone-dependent target transfer function at least based on the zone affiliation of the control point, wherein said target transfer function in each control point is determined based on phase differences between at least a pair of said loudspeakers in said control point, wherein said phase differences are defined by said model transfer function(s) in said control point, and wherein the phase characteristics of said zone-dependent target transfer functions differ between control points affiliated with different listening zones; and - determining (S3) said filter coefficients of said audio precompensation controller at least based on said model transfer functions and said target transfer functions of said M control points. - estimating (S1), for each one of at least a pair of said loudspeakers, a model transfer function at each of a plurality M of control points distributed in Z ≥ 2 spatially separated listening zones in a listening environment of said sound system; - determining (S2), for each of said M control points, a zone-dependent target transfer function at least based on the zone affiliation of the control point, wherein said target transfer function in each control point is determined based on phase differences between at least a pair of said loudspeakers in said control point, wherein said phase differences are defined by said model transfer function(s) in said control point, and wherein the phase characteristics of said zone-dependent target transfer functions differ between control points affiliated with different listening zones; and - determining (S3) said filter coefficients of said audio precompensation controller at least based on said model transfer functions and said target transfer functions of said M control points.