mhurhangee/patent-ind-claim-en huggingface dataset:
A thermal printer comprising: a communication interface configured to receive print data from an external device; a thermal print head configured to thermally print on a sheet (P), line by line according to the received print data; a motor configured to drive a roller to transport the sheet, line by line according to the received print data; and a processor configured to: determine, for a current print line, a target transport speed for transporting the sheet, retrieve one or more intermediate speeds that are defined in advance and are between a current transport speed of transporting the sheet and the target transport speed, retrieve, for each determined intermediate speed, predetermined heating control information for heating the thermal print head, control the motor to transport the sheet at each determined intermediate speed and the target transport speed, sequentially, and control the thermal print head to be heated in accordance with the predetermined heating control information corresponding to the determined intermediate speed closest to the current speed. a communication interface configured to receive print data from an external device; a thermal print head configured to thermally print on a sheet (P), line by line according to the received print data; a motor configured to drive a roller to transport the sheet, line by line according to the received print data; and a processor configured to: determine, for a current print line, a target transport speed for transporting the sheet, retrieve one or more intermediate speeds that are defined in advance and are between a current transport speed of transporting the sheet and the target transport speed, retrieve, for each determined intermediate speed, predetermined heating control information for heating the thermal print head, control the motor to transport the sheet at each determined intermediate speed and the target transport speed, sequentially, and control the thermal print head to be heated in accordance with the predetermined heating control information corresponding to the determined intermediate speed closest to the current speed. determine, for a current print line, a target transport speed for transporting the sheet, retrieve one or more intermediate speeds that are defined in advance and are between a current transport speed of transporting the sheet and the target transport speed, retrieve, for each determined intermediate speed, predetermined heating control information for heating the thermal print head, control the motor to transport the sheet at each determined intermediate speed and the target transport speed, sequentially, and control the thermal print head to be heated in accordance with the predetermined heating control information corresponding to the determined intermediate speed closest to the current speed.
A method comprising: forming, via fusion draw, a laminate structure comprising a core layer comprised of a sodium rich lithium deficient glass composition sandwiched between first and second clad layers comprised of a lithium-rich glass composition; heat treating the laminate structure to diffuse lithium ions from at least one of the first or second clad layers to the core layer, and to diffuse sodium ions from the core layer to at least one of the first or second clad layers; and heat treating the laminate structure a second time, wherein in the second heat treatment the laminate structure is heated sufficiently to nucleate and grow a ceramic phase in the laminate structure. forming, via fusion draw, a laminate structure comprising a core layer comprised of a sodium rich lithium deficient glass composition sandwiched between first and second clad layers comprised of a lithium-rich glass composition; heat treating the laminate structure to diffuse lithium ions from at least one of the first or second clad layers to the core layer, and to diffuse sodium ions from the core layer to at least one of the first or second clad layers; and heat treating the laminate structure a second time, wherein in the second heat treatment the laminate structure is heated sufficiently to nucleate and grow a ceramic phase in the laminate structure.
A pivot pin for an epicyclic gear train sliding bearing, the pivot pin having an axis (X1), about which it can rotate, and a circumference, and further having: - a portion forming a central shank extending around an axial passage of the pivot pin, and - axially opposed circumferential grooves which are open laterally and which radially separate two axially opposed lateral end portions of the central shank from two lateral cantilevered portions of the pivot pin, each circumferential groove having a free lateral end and: -- radially at least one width (I), -- as well as at least one depth (P), in a direction in which the circumferential groove extends inwardly in the pivot pin, from the free lateral end to a bottom end , characterized in that at least one of the circumferential grooves has: - said at least one width (I) and/or said at least one depth (P) which is, or are, more reduced locally than on the rest of the circumference, or, - said at least one width (I) which is equal to zero over part of the circumference, and/or said at least one depth (P) which varies circumferentially. - a portion forming a central shank extending around an axial passage of the pivot pin, and - axially opposed circumferential grooves which are open laterally and which radially separate two axially opposed lateral end portions of the central shank from two lateral cantilevered portions of the pivot pin, each circumferential groove having a free lateral end and: -- radially at least one width (I), -- as well as at least one depth (P), in a direction in which the circumferential groove extends inwardly in the pivot pin, from the free lateral end to a bottom end , -- radially at least one width (I), -- as well as at least one depth (P), in a direction in which the circumferential groove extends inwardly in the pivot pin, from the free lateral end to a bottom end , - said at least one width (I) and/or said at least one depth (P) which is, or are, more reduced locally than on the rest of the circumference, or, - said at least one width (I) which is equal to zero over part of the circumference, and/or said at least one depth (P) which varies circumferentially.
A furniture extension wall, in particular a table furniture extension wall, with a frame , and flat panels arranged on both sides of the frame , wherein at least one flat panel is constituted wholly or partially as a predominantly smooth-surface shaped plastic nonwoven fabric, and wherein the shaped nonwoven fabric is produced from a fibre composite material made of plastic fibres, which are connected to one another mechanically and/or chemically and/or thermally and binder-free, characterised in that the flat panel facing the furniture has a smaller area than the flat panel facing away from the furniture.
A method performed by a base station, the method comprising: receiving a first paging message from a core network, said first paging message being sent to trigger a response including an uplink data transmission having a specific maximum size; sending a second paging message to a user equipment, said second paging message having a dedicated preamble and an indication of said specific maximum size; receiving a response to the second paging message , said response having the dedicated preamble when the user equipment has data available to send, said data being within said specific maximum size; sending a reply to the user equipment, said reply containing a timing advance and an uplink resource allocation corresponding to a size of said available data; and receiving said available data from the user equipment in accordance with said timing advance and said uplink resource allocation. receiving a first paging message from a core network, said first paging message being sent to trigger a response including an uplink data transmission having a specific maximum size; sending a second paging message to a user equipment, said second paging message having a dedicated preamble and an indication of said specific maximum size; receiving a response to the second paging message , said response having the dedicated preamble when the user equipment has data available to send, said data being within said specific maximum size; sending a reply to the user equipment, said reply containing a timing advance and an uplink resource allocation corresponding to a size of said available data; and receiving said available data from the user equipment in accordance with said timing advance and said uplink resource allocation.
A method of detecting at least K. quasipneumoniae or K. variicola within a sample from a subject, comprising: subjecting DNA, RNA, or both from the sample to a PCR amplification reaction using a primer pair selected from the group consisting of: SEQ ID NOs: 7-8, being specific for K. variicola , and SEQ ID NOs: 9-10, being specific for K. quasipneumoniae ; and analyzing amplification products resulting from the PCR amplification reaction to detect species-specific canonical single nucleotide polymorphisms (canSNPs) to detect K . quasipneumoniae , K. variicola , or both in the sample. subjecting DNA, RNA, or both from the sample to a PCR amplification reaction using a primer pair selected from the group consisting of: SEQ ID NOs: 7-8, being specific for K. variicola , and SEQ ID NOs: 9-10, being specific for K. quasipneumoniae ; and analyzing amplification products resulting from the PCR amplification reaction to detect species-specific canonical single nucleotide polymorphisms (canSNPs) to detect K . quasipneumoniae , K. variicola , or both in the sample.
A wing flap system for an aircraft , the wing flap system comprising: a flap movable between a deployed position and a retracted position relative to a fixed trailing edge of a wing of the aircraft; a first actuator to move the flap relative to the fixed trailing edge, the first actuator being actuatable via pressurized hydraulic fluid to be supplied from a hydraulic system of the aircraft to the first actuator via a hydraulic module operatively coupled to the first actuator; a second actuator to move the flap relative to the fixed trailing edge, the second actuator being actuatable via an electric motor of the second actuator connected to a first electrical system of the aircraft; and a shaft operatively coupling the first actuator to the second actuator, the first and second actuators being actuatable via the shaft. a flap movable between a deployed position and a retracted position relative to a fixed trailing edge of a wing of the aircraft; a first actuator to move the flap relative to the fixed trailing edge, the first actuator being actuatable via pressurized hydraulic fluid to be supplied from a hydraulic system of the aircraft to the first actuator via a hydraulic module operatively coupled to the first actuator; a second actuator to move the flap relative to the fixed trailing edge, the second actuator being actuatable via an electric motor of the second actuator connected to a first electrical system of the aircraft; and a shaft operatively coupling the first actuator to the second actuator, the first and second actuators being actuatable via the shaft.
A printing apparatus comprising - an emitter arranged within a first fluid and configured to oscillate for generating an acoustic field in said first fluid; - a nozzle with a nozzle tip ; - a second fluid within the nozzle , and - a driving means configured to drive a predetermined volume of the second fluid out of the nozzle , characterized by - a reflector arranged between the emitter and a printing substrate , the reflector has a reflectorless chamber which is a through-hole in a body of the reflector and which is arranged along a printing axis (A) between the nozzle tip and the printing substrate , wherein the nozzle tip is positioned within the reflectorless chamber , and the acoustic field has a force gradient of acoustic forces for detaching the predetermined volume of the second fluid from the nozzle which points into the direction of the printing substrate . - an emitter arranged within a first fluid and configured to oscillate for generating an acoustic field in said first fluid; - a nozzle with a nozzle tip ; - a second fluid within the nozzle , and - a driving means configured to drive a predetermined volume of the second fluid out of the nozzle , - a reflector arranged between the emitter and a printing substrate , the reflector has a reflectorless chamber which is a through-hole in a body of the reflector and which is arranged along a printing axis (A) between the nozzle tip and the printing substrate , wherein
Tyre comprising two beads intended to come into contact with a wheel rim, a crown composed of at least one crown reinforcement and a tread, two sidewalls connecting the crown to the beads, a carcass reinforcement anchored in the two beads, which tyre comprises a rubber component which comprises a rubber composition based on a modified polyisoprene, a vulcanization system and a reinforcing filler, the reinforcing filler comprising a silica, the modified polyisoprene being a polyisoprene which bears pendent imidazole functions, the rubber component being devoid of a filamentary reinforcing element, having no visible face when the tyre is not fitted onto an external wheel rim, and not being intended to come into direct contact with a wheel rim.
A nacelle for a gas turbine engine comprising: at least one hinge axis extending along the nacelle ; and at least one cowl mounted to the nacelle , along the at least one hinge axis , by at least one hinge ; wherein the at least one hinge comprises at least one latch , the at least one latch comprising a clevis and a tang ; wherein the clevis and the tang of the at least one latch are configured to receive a pin , through a pin aperture , when the at least one cowl is in a closed condition; characterised in that : the clevis and the tang are configured to receive the pin along a pin axis substantially perpendicular to the at least one hinge axis . at least one hinge axis extending along the nacelle ; and at least one cowl mounted to the nacelle , along the at least one hinge axis , by at least one hinge ; wherein the at least one hinge comprises at least one latch , the at least one latch comprising a clevis and a tang ; wherein the clevis and the tang of the at least one latch are configured to receive a pin , through a pin aperture , when the at least one cowl is in a closed condition; characterised in that : the clevis and the tang are configured to receive the pin along a pin axis substantially perpendicular to the at least one hinge axis .
Process for coating a substrate with catalytically active material on one or more sides, comprising deposition of material under reduced pressure in a vacuum chamber, with the following steps being carried out (a) loading of the vacuum chamber with at least one substrate, (b) closure and evacuation of the vacuum chamber, (c) cleaning of the substrate by introduction of a gaseous reducing agent into the vacuum chamber, (d) removal of the gaseous reducing agent, (e) application of an intermediate layer, with a material which is identical to the material of which the substrate consists being introduced into the vacuum chamber, (f) setting of the vacuum chamber to a temperature of from 150°C to 400°C, (g) application of a further coating on top of the intermediate layer, with at least one metal selected from the group consisting of ruthenium, iridium, titanium and mixtures thereof being introduced into the vacuum chamber and oxygen being fed in during the entire coating time, (h) in a last step, the vacuum chamber is flooded again and the coated substrate is taken from the chamber, where the abovementioned steps and transitions from one step to the respective next step are carried out under reduced pressure at optionally different pressures which are set by means of a protective gas, characterized in that the application of the intermediate layer in step (e) and the application of the further coating in step (g) on top of the intermediate layer are each carried out by means of vacuum arc deposition, where the further coating on one or more sides is at least 99% free of constituents originally present in the substrate itself and the further coating applied on top of the intermediate layer is at least 99% free of unoxidized metals. (a) loading of the vacuum chamber with at least one substrate, (b) closure and evacuation of the vacuum chamber, (c) cleaning of the substrate by introduction of a gaseous reducing agent into the vacuum chamber, (d) removal of the gaseous reducing agent, (e) application of an intermediate layer, with a material which is identical to the material of which the substrate consists being introduced into the vacuum chamber, (f) setting of the vacuum chamber to a temperature of from 150°C to 400°C, (g) application of a further coating on top of the intermediate layer, with at least one metal selected from the group consisting of ruthenium, iridium, titanium and mixtures thereof being introduced into the vacuum chamber and oxygen being fed in during the entire coating time, (h) in a last step, the vacuum chamber is flooded again and the coated substrate is taken from the chamber,
External casing of an axial turbomachine , notably of an axial turbomachine compressor (4; 6), the casing comprising: - a circular wall comprising an internal annular groove ; - an external sealing shroud arranged at least partially in the groove and intended to provide sealing between the external casing and an annular row of rotor blades of the turbomachine, - connecting elements connecting the external shroud to the wall , the connecting elements being piezoelectric actuators configured to move and/or deform the shroud so as to alter the clearance between the shroud and the rotor blades ; characterized in that the piezoelectric actuators are arranged in two annular rows. - a circular wall comprising an internal annular groove ; - an external sealing shroud arranged at least partially in the groove and intended to provide sealing between the external casing and an annular row of rotor blades of the turbomachine, - connecting elements connecting the external shroud to the wall , the connecting elements being piezoelectric actuators configured to move and/or deform the shroud so as to alter the clearance between the shroud and the rotor blades ; characterized in that the piezoelectric actuators are arranged in two annular rows.
A method, performed in a wireless device , for providing a network capability report to a radio network node , the wireless device and the radio network node being comprised in a wireless communications network, the method comprising: - receiving (S0), from the wireless communication network, an enquiry to report network capabilities; - sending (S1) to the network, a network capability report message, wherein the message comprises an indication about conditionally supported features, supported under particular conditions depending on the configuration of wireless device ; - receiving (S2; S2a; S2b), from the wireless communications network , information specifying one or more combinations of features that the wireless communication network supports for the wireless device ; - determining (S3) capabilities of the wireless device with regard to the specified one or more combinations of features by determining one or more conditionally supported combinations of features, supported under particular conditions depending on the configuration of wireless device ; - sending (S4), to the radio network node , a network capability report message defining the determined capabilities comprising the determined one or more conditionally supported combinations of features of the wireless device with respect to the specified one or more combinations of features. - receiving (S0), from the wireless communication network, an enquiry to report network capabilities; - sending (S1) to the network, a network capability report message, wherein the message comprises an indication about conditionally supported features, supported under particular conditions depending on the configuration of wireless device ; - receiving (S2; S2a; S2b), from the wireless communications network , information specifying one or more combinations of features that the wireless communication network supports for the wireless device ; - determining (S3) capabilities of the wireless device with regard to the specified one or more combinations of features by determining one or more conditionally supported combinations of features, supported under particular conditions depending on the configuration of wireless device ; - sending (S4), to the radio network node , a network capability report message defining the determined capabilities comprising the determined one or more conditionally supported combinations of features of the wireless device with respect to the specified one or more combinations of features.
Grouping device for grouping together fuel cells, comprising at least two fuel cells in which at least a first fluid circulates, characterized in that the grouping device comprises a support and at least a portion of a first circuit for the first fluid comprising a first feeder configured to supply the fuel cells with first fluid and a first manifold configured to collect the first fluid from the fuel cells , the support comprising a casing , the first feeder and the first manifold being secured to the casing and positioned between the casing and the fuel cells , each casing comprising at least one outer shoulder extending over at least a part of its periphery.
A method performed by a user equipment, UE, for receiving data in a communication system, the method comprising: acquiring a hybrid automatic repeat request, HARQ, process identifier, ID, using a number of HARQ processes, interval information , and time information , wherein the number of HARQ processes is for periodic resource allocation without corresponding control information on an L1 control channel and the interval information is the periodic resource allocation interval; and wherein the time information is the timing at which the periodic resources are allocated, and receiving data in a first transmission based on the periodic resource allocation and the HARQ process ID. acquiring a hybrid automatic repeat request, HARQ, process identifier, ID, using a number of HARQ processes, interval information , and time information , wherein the number of HARQ processes is for periodic resource allocation without corresponding control information on an L1 control channel and the interval information is the periodic resource allocation interval; and wherein the time information is the timing at which the periodic resources are allocated, and receiving data in a first transmission based on the periodic resource allocation and the HARQ process ID.
A process for the heterologous expression of a protein, which process comprises the step of culturing cells in a cell culture medium, wherein said medium comprises 4-phenyl-3-butenoic acid (PBA) as a peptidylglycine alpha-amidating monooxygenase (PAM) inhibitor, and at least one second step of adding a feed solution comprising PBA as a PAM inhibitor to the cell culture medium, wherein said cells used in said process are Chinese hamster ovary (CHO) cells, wherein the PBA is used in said cell culture medium in a concentration of ≥ 0.01 mmol/kg of cell mass and ≤ 1 mmol/kg of cell mass and serves to inhibit the formation of amidated amino acid residues, and wherein the concentration of PBA in said feed solution is between ≥ 0.1 and ≤ 10 mmol/kg feed solution.