mhurhangee/patent-ind-claim-en huggingface dataset:
A flight control method for a host aircraft, the method comprising: receiving position determining data, and a flight plan, FP, from a flight management system, FMS, in the host aircraft; receiving, from a traffic collision advisory system, TCAS, TCAS data ; receiving a TCAS resolution advisory, RA, related to a neighbor aircraft, the TCAS RA being an evasive maneuver ; responsive to receiving the RA, automatically beginning executing the evasive maneuver when both vertical navigation, VNAV, is engaged in the FMS and automatic pilot, AP, is engaged, the evasive maneuver consisting of a vertical speed change, a flight level change, or a vertical path change; and either (i) continuing executing the evasive maneuver by modifying FMS VNAV guidance, responsive to referencing the FMS to determine that a limiting condition does not apply to the evasive maneuver, wherein the limiting condition comprises a nearby parallel runway; or (ii) alerting a pilot to take control for a manual execution of a remainder of the evasive maneuver, responsive to determining that the limiting condition applies to the evasive maneuver. receiving position determining data, and a flight plan, FP, from a flight management system, FMS, in the host aircraft; receiving, from a traffic collision advisory system, TCAS, TCAS data ; receiving a TCAS resolution advisory, RA, related to a neighbor aircraft, the TCAS RA being an evasive maneuver ; responsive to receiving the RA, automatically beginning executing the evasive maneuver when both vertical navigation, VNAV, is engaged in the FMS and automatic pilot, AP, is engaged, the evasive maneuver consisting of a vertical speed change, a flight level change, or a vertical path change; and either (i) continuing executing the evasive maneuver by modifying FMS VNAV guidance, responsive to referencing the FMS to determine that a limiting condition does not apply to the evasive maneuver, wherein the limiting condition comprises a nearby parallel runway; or (ii) alerting a pilot to take control for a manual execution of a remainder of the evasive maneuver, responsive to determining that the limiting condition applies to the evasive maneuver.
Device for dispensing a fluid to a patient, comprising a container having an interior space for receiving the fluid, wherein the container comprises a closure piece arranged in the container , on which closure piece a dispensing opening is formed, via which the fluid from the interior space can be dispensed, wherein the device comprises a conveyor , driven by a conveyor drive , for conveying the fluid out of the interior space of the container , characterized in that the conveyor is arranged fluidically between the interior space and the dispensing opening , such that the fluid can be conveyed by means of the conveyor from the interior space to the dispensing opening , wherein the conveyor is configured as a valveless positive displacement pump.
A concealed antenna node suitable for mounting on a street pole , the concealed antenna node comprising an antenna and an associated radio module which are both housed within a radome of the concealed antenna node ; the antenna comprising a plurality of antenna columns (700A-700D), each antenna column comprising one or more radiator elements, whereby the plurality of antenna columns (700A-700D) are arranged about a central section ; the radio module being located within the central section and inside the radome ; and, the antenna and the radio module being pre-wired together within the radome to form the concealed antenna node suitable for mounting on the street pole , the plurality of antenna columns (700A-700D) being arranged in a spaced-apart formation such that a gap is realised between adjacent antenna columns (700A-700D), characterised in that said concealed antenna node further comprises a cradle , wherein the radio module sits inside the cradle configured to be lowered and installed inside the central section.
A process for operating a multistage compression system for compressing gas feed having a variable flow rate, said multistage compression system comprising at least one centrifugal compressor incorporating a dry gas seal with opposed seal faces, said process comprising: (a) during periods when the flow rate of the gas through the centrifugal compressor(s) is sufficient for normal operation of said multistage compression system , operating said centrifugal compressor(s) in a normal power mode; and (b) during periods when the flow rate of the gas through the centrifugal compressor(s) is not sufficient for normal operation of said multistage compression system , operating the centrifugal compressor or, if more than one, at least one centrifugal compressor in a low power mode at least sufficient to prevent contact of said opposed seal faces of said dry gas seal in said centrifugal compressor(s) . (a) during periods when the flow rate of the gas through the centrifugal compressor(s) is sufficient for normal operation of said multistage compression system , operating said centrifugal compressor(s) in a normal power mode; and (b) during periods when the flow rate of the gas through the centrifugal compressor(s) is not sufficient for normal operation of said multistage compression system , operating the centrifugal compressor or, if more than one, at least one centrifugal compressor in a low power mode at least sufficient to prevent contact of said opposed seal faces of said dry gas seal in said centrifugal compressor(s) .
An apparatus for controlling a power supplied to a fixing unit of an image forming device, the apparatus comprising: at least one heating lamp; a voltage detector for detecting a voltage of an input power supplied to heat the at least one heating lamp ; a synch signal generator for generating a synch signal in response to the detected voltage; a switching unit for switching a supply path of the input power to be applied to the at least one heating lamp ; and a controller having table information of temporal duty level values for the input power that is initially supplied, wherein the switching unit is operable to perform the switching operation corresponding to a control signal, wherein the switching unit comprises at least two self turn-off switching components including a first self turn-off switching component (SW 1 ) and a second self turn-off switching component (SW2), characterised in that the controller is configured to output the control signal for alternately controlling a switching operation of the first self turn-off switching component or the second self turn-off switching component every half-wave period of the input power and for controlling the respective first and second switching components to switch on and off a plurality of times within a half-wave period according to a duty level value associated with the half-wave period using the generated synch signal and the table information. at least one heating lamp; a voltage detector for detecting a voltage of an input power supplied to heat the at least one heating lamp ; a synch signal generator for generating a synch signal in response to the detected voltage; a switching unit for switching a supply path of the input power to be applied to the at least one heating lamp ; and a controller having table information of temporal duty level values for the input power that is initially supplied, wherein the switching unit is operable to perform the switching operation corresponding to a control signal, wherein the switching unit comprises at least two self turn-off switching components including a first self turn-off switching component (SW 1 ) and a second self turn-off switching component (SW2), characterised in that the controller is configured to output the control signal for alternately controlling a switching operation of the first self turn-off switching component or the second self turn-off switching component every half-wave period of the input power and for controlling the respective first and second switching components to switch on and off a plurality of times within a half-wave period according to a duty level value associated with the half-wave period using the generated synch signal and the table information.
An optical device, comprising: a light pipe having a proximal end adapted for optical coupling to a light source to receive a plurality of light rays therefrom and a distal end providing an output surface for the light rays, said light pipe being configured to cause mixing of at least some of the light rays via total internal reflection at one or more lateral surfaces thereof as the light rays pass through the light pipe, said light pipe having an input surface at the proximal end for receiving said light rays from the light source, a lens optically coupled to the output surface of said light pipe to receive light thereofrom and to project the light onto a target surface, characterized in that said output surface comprises surface texturing formed thereon to spread the incident light rays; and wherein said light pipe comprises at least two portions exhibiting different cross-sectional shapes. a light pipe having a proximal end adapted for optical coupling to a light source to receive a plurality of light rays therefrom and a distal end providing an output surface for the light rays, said light pipe being configured to cause mixing of at least some of the light rays via total internal reflection at one or more lateral surfaces thereof as the light rays pass through the light pipe, said light pipe having an input surface at the proximal end for receiving said light rays from the light source, a lens optically coupled to the output surface of said light pipe to receive light thereofrom and to project the light onto a target surface, characterized in that said output surface comprises surface texturing formed thereon to spread the incident light rays; and wherein said light pipe comprises at least two portions exhibiting different cross-sectional shapes.
A wireless transmit/receive unit, WTRU, comprising: a processor configured to: receive configuration information, wherein the configuration information is associated with a transition to a first activity level from a second activity level, and wherein the configuration information indicates conditions associated with determining a secondary cell group, SCG, activation level associated with resumption of the first activity level, wherein the SCG activation level is an activated SCG or a deactivated SCG; transition from the first activity level to the second activity level; transition from the second activity level to the first activity level; determine the SCG activation level based on an evaluation of the conditions in the configuration information, wherein the conditions in the configuration information comprise a WTRU condition and a network condition, wherein the network condition comprises at least whether a bearer type associated with UL data is a first bearer type or a second bearer type; and indicate, to a base station, the determined SCG activation level. transition from the first activity level to the second activity level; transition from the second activity level to the first activity level; determine the SCG activation level based on an evaluation of the conditions in the configuration information, wherein the conditions in the configuration information comprise a WTRU condition and a network condition, wherein the network condition comprises at least whether a bearer type associated with UL data is a first bearer type or a second bearer type; and indicate, to a base station, the determined SCG activation level.
A fitting for a fluidic coupling, comprising: a tube assembly comprising: an inner tube having an inner tube endface and a first fluid channel; an intermediate tube formed of a polymeric material and disposed over at least a portion of a length of the inner tube , the intermediate tube including an extruded portion having a length and an intermediate tube endface ; and an outer tube formed of a metal and disposed over the intermediate tube , the outer tube having an outer tube endface and an outer surface, a first radial crimp on the outer surface at a first distance from the outer tube endface and extending for a first axial length, and a second radial crimp on the outer surface at a second distance from the outer tube endface and extending for a second axial length, the outer tube endface being co-planar with the inner tube endface , the intermediate tube endface being separated from the inner tube endface and the outer tube endface by the length of the extruded portion, wherein an outer diameter of the inner tube endface does not exceed an inner diameter of the intermediate tube endface and wherein an outer diameter of the intermediate tube endface does not exceed an inner diameter of the outer tube endface . an inner tube having an inner tube endface and a first fluid channel; an intermediate tube formed of a polymeric material and disposed over at least a portion of a length of the inner tube , the intermediate tube including an extruded portion having a length and an intermediate tube endface ; and an outer tube formed of a metal and disposed over the intermediate tube , the outer tube having an outer tube endface and an outer surface, a first radial crimp on the outer surface at a first distance from the outer tube endface and extending for a first axial length, and a second radial crimp on the outer surface at a second distance from the outer tube endface and extending for a second axial length, the outer tube endface being co-planar with the inner tube endface , the intermediate tube endface being separated from the inner tube endface and the outer tube endface by the length of the extruded portion, wherein an outer diameter of the inner tube endface does not exceed an inner diameter of the intermediate tube endface and wherein an outer diameter of the intermediate tube endface does not exceed an inner diameter of the outer tube endface .
A container production method of producing a container (C) that contains a content liquid (L) by liquid blow molding a synthetic resin preform (PF), the method comprising: a preform setup step of disposing the preform (PF) in a blow molding mold that is releasable by being separated into a plurality of separated mold pieces (11a1, 11a2) and engaging a filling nozzle connected to a liquid supply path with a mouth of the preform (PFa); a blow molding step of liquid blow molding the preform (PF) into a shape conforming to a cavity of the blow molding mold by supplying a pressurized liquid supplied to the liquid supply path from the filling nozzle into the preform (PF); a liquid discharge step of releasing the blow molding mold and pressing a trunk (Cb) of a container (C) after molding with a pressing portion that is inserted from a clearance between the separated mold pieces (11a1, 11a2) adjacent to each other to discharge a liquid in the container (C) to outside of the container (C) by a predetermined amount; and a headspace forming step of forming a headspace (HS) in the container (C) by separating the filling nozzle from a mouth of the container (Ca) after a predetermined amount of liquid is discharged to outside. a preform setup step of disposing the preform (PF) in a blow molding mold that is releasable by being separated into a plurality of separated mold pieces (11a1, 11a2) and engaging a filling nozzle connected to a liquid supply path with a mouth of the preform (PFa); a blow molding step of liquid blow molding the preform (PF) into a shape conforming to a cavity of the blow molding mold by supplying a pressurized liquid supplied to the liquid supply path from the filling nozzle into the preform (PF); a liquid discharge step of releasing the blow molding mold and pressing a trunk (Cb) of a container (C) after molding with a pressing portion that is inserted from a clearance between the separated mold pieces (11a1, 11a2) adjacent to each other to discharge a liquid in the container (C) to outside of the container (C) by a predetermined amount; and a headspace forming step of forming a headspace (HS) in the container (C) by separating the filling nozzle from a mouth of the container (Ca) after a predetermined amount of liquid is discharged to outside.
A method of forming a wind turbine blade shear web flange section by resin transfer moulding, the method comprising: providing a matched mould assembly comprising first and second mould parts , the matched mould assembly further comprising a mould surface defining a mould cavity ; arranging a plurality of elongate flange elements with the mould surface in an array such that the flange elements are positioned one on top of another with first and second longitudinal ends of each flange element longitudinally offset from respective first and second longitudinal ends of a neighbouring flange element so as to form a tapered portion at each of a first and second longitudinal end of the flange section ; clamping or pressing together the first and second mould parts to close the mould; injecting resin to the closed mould cavity ; and thereafter curing the array of flange elements in a resin matrix to form a cured flange section having a laminate construction. providing a matched mould assembly comprising first and second mould parts , the matched mould assembly further comprising a mould surface defining a mould cavity ; arranging a plurality of elongate flange elements with the mould surface in an array such that the flange elements are positioned one on top of another with first and second longitudinal ends of each flange element longitudinally offset from respective first and second longitudinal ends of a neighbouring flange element so as to form a tapered portion at each of a first and second longitudinal end of the flange section ; clamping or pressing together the first and second mould parts to close the mould; injecting resin to the closed mould cavity ; and thereafter curing the array of flange elements in a resin matrix to form a cured flange section having a laminate construction.
A process for the production of acid whey having a lactose content of 1.0 to 2.0% by weight and preferably of 1.5 to 1.8% by weight, comprising or consisting of the following steps: (a) providing a skimmed milk; (b) ultrafiltration of the skim milk to obtain a lactose-rich fraction as first permeate P1 and a milk protein concentrate as first retentate R1; (c) reverse osmotic treatment of the permeate P1 from step (b) to obtain diawater as second permeate P2 and a milk protein concentrate as second retentate R2; (d) first standardizing the milk protein concentrate R1 from step (b) by addition of skim milk; (e) second standardizing the mixture from step (d) by addition of diawater P2 from step (c); (f) fermentation of the second mixture from step (e) in a manner known per se; and (g) separation of the fermentation product from step (f) into cream cheese and acid whey. (a) providing a skimmed milk; (b) ultrafiltration of the skim milk to obtain a lactose-rich fraction as first permeate P1 and a milk protein concentrate as first retentate R1; (c) reverse osmotic treatment of the permeate P1 from step (b) to obtain diawater as second permeate P2 and a milk protein concentrate as second retentate R2; (d) first standardizing the milk protein concentrate R1 from step (b) by addition of skim milk; (e) second standardizing the mixture from step (d) by addition of diawater P2 from step (c); (f) fermentation of the second mixture from step (e) in a manner known per se; and (g) separation of the fermentation product from step (f) into cream cheese and acid whey.
An unmanned remote-controlled aircraft comprising at least two engines , configured to allow flight of the aircraft , and a main structure supporting said engines , the main structure being flexible and inflatable so as to allow folding of the main structure between a storage position and a use position, the main structure comprising: - a support chassis longitudinally extending between an upstream end and a downstream end along a longitudinal axis (X), and - inflatable arms connected to the support chassis respectively at the upstream end and the downstream end , each inflatable arm orthogonally extending to the support chassis , so as to form an H-shaped main structure , the aircraft being characterised in that the main structure comprises only two inflatable arms , each inflatable arm comprising two side portions each comprising an engine support end . - a support chassis longitudinally extending between an upstream end and a downstream end along a longitudinal axis (X), and - inflatable arms connected to the support chassis respectively at the upstream end and the downstream end , each inflatable arm orthogonally extending to the support chassis , so as to form an H-shaped main structure , the aircraft being characterised in that the main structure comprises only two inflatable arms , each inflatable arm comprising two side portions each comprising an engine support end .
Fluid line having a tube , which has an input-side end section with a first connector and an output-side end section with a second connector , wherein a cavity is configured in the tube , delimited radially inwardly by at least one auxiliary element , wherein the auxiliary element is configured as a heating rod and in the cavity at least one volume reduction element is arranged in the region of the output-side end section , characterised in that the fluid line has a pump and an injection assembly , wherein the first connector has a nozzle onto which the tube is pushed and a connection geometry which is connected to the pump , wherein the pump has a switchable feeding direction, and wherein the second connector has a nozzle onto which the tube is pushed, and a connection geometry which is connected to the injection assembly .