mhurhangee/patent-ind-claim-en huggingface dataset:
A turboexpander (1; 201) comprising: a casing (3; 203); a shaft (5; 205) arranged in the casing (3; 203) for rotation therein; mounted on the shaft (3; 203), at least one radial impeller (25; 219) of a radial expansion stage (21; 218); and mounted on said shaft (5; 205), at least one axial expansion wheel (43; 243) of an axial expansion section (23; 217), wherein the axial expansion section is arranged downstream of the radial expansion stage (21; 218); and variable nozzle guide vanes (31; 225) provided at an inlet side of the at least one radial impeller (25; 219); characterized in that the shaft comprises a first shaft portion mounted for rotation in a bearing assembly , and a second shaft portion projecting from the bearing assembly and on which the radial impeller and the axial expansion wheel are mounted; and an auxiliary shaft-supporting bearing is arranged at one end of the second shaft portion , opposite the bearing assembly ; wherein the at least one radial impeller and the axial expansion wheel are arranged between the bearing assembly and the auxiliary shaft-supporting bearing . a casing (3; 203); a shaft (5; 205) arranged in the casing (3; 203) for rotation therein; mounted on the shaft (3; 203), at least one radial impeller (25; 219) of a radial expansion stage (21; 218); and mounted on said shaft (5; 205), at least one axial expansion wheel (43; 243) of an axial expansion section (23; 217), wherein the axial expansion section is arranged downstream of the radial expansion stage (21; 218); and variable nozzle guide vanes (31; 225) provided at an inlet side of the at least one radial impeller (25; 219); characterized in that the shaft comprises a first shaft portion mounted for rotation in a bearing assembly , and a second shaft portion projecting from the bearing assembly and on which the radial impeller and the axial expansion wheel are mounted; and an auxiliary shaft-supporting bearing is arranged at one end of the second shaft portion , opposite the bearing assembly ; wherein the at least one radial impeller and the axial expansion wheel are arranged between the bearing assembly and the auxiliary shaft-supporting bearing .
Apparatus for testing a subject's vision comprising: a polarization arrangement configured to polarize incident light and rotate an angle of polarization applied to the incident light about an axis substantially collinear with a path of the incident light; and an optical component configured to direct light onto the polarization arrangement, wherein the polarization arrangement has a rotating angle of polarization, characterised in that the polarization arrangement is configured to produce light having a selected degree of polarization from multiple selectable degrees of polarization ranging from 0% polarization to 100% polarization, while under observation by the subject. a polarization arrangement configured to polarize incident light and rotate an angle of polarization applied to the incident light about an axis substantially collinear with a path of the incident light; and an optical component configured to direct light onto the polarization arrangement, wherein the polarization arrangement has a rotating angle of polarization, characterised in that the polarization arrangement is configured to produce light having a selected degree of polarization from multiple selectable degrees of polarization ranging from 0% polarization to 100% polarization, while under observation by the subject.
A wireless charging mount comprising: a base portion ; an attachment portion including a post coupled to the base portion and a head coupled to the post , the head configured to engage with a receptacle on a handheld electronic device to support the handheld electronic device on the base portion ; and a wireless charger coupled to the attachment portion to support the wireless charger on the base portion , the wireless charger configured to selectively provide power to the handheld electronic device , wherein the wireless charger is movable along the post between a raised position adjacent to the head and spaced apart from the base portion and a lowered position adjacent to the base portion and spaced apart from the head , characterised in that the post extends through the wireless charger to engage with the head , the lowered position allows connection of the head with the receptacle , and wherein the wireless charger is configured to engage with the receptacle in the raised position to block rotation of the receptacle relative to the attachment portion at the selection of a user. a base portion ; an attachment portion including a post coupled to the base portion and a head coupled to the post , the head configured to engage with a receptacle on a handheld electronic device to support the handheld electronic device on the base portion ; and a wireless charger coupled to the attachment portion to support the wireless charger on the base portion , the wireless charger configured to selectively provide power to the handheld electronic device , wherein the wireless charger is movable along the post between a raised position adjacent to the head and spaced apart from the base portion and a lowered position adjacent to the base portion and spaced apart from the head , characterised in that the post extends through the wireless charger to engage with the head , the lowered position allows connection of the head with the receptacle , and wherein the wireless charger is configured to engage with the receptacle in the raised position to block rotation of the receptacle relative to the attachment portion at the selection of a user.
An anti-GFRα3 antibody or antigen-binding fragment thereof comprising an HCVR/LCVR pair encoded by a nucleic acid sequence pair selected from the group consisting of: (i) SEQ ID NO: 145 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto, and SEQ ID NO: 153 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto; (ii) SEQ ID NO: 17 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto, and SEQ ID NO: 25 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto; (iii) SEQ ID NO: 49 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto, and SEQ ID NO: 57 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto; (iv) SEQ ID NO: 113 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto, and SEQ ID NO: 121 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto; (v) SEQ ID NO: 209 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto, and SEQ ID NO: 217 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto; and (vi) SEQ ID NO: 289 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto, and SEQ ID NO: 297 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto; wherein the antibody or antigen-binding fragment thereof specifically binds to human GFRα3 and does not bind to mouse GFRα3. (i) SEQ ID NO: 145 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto, and SEQ ID NO: 153 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto; (ii) SEQ ID NO: 17 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto, and SEQ ID NO: 25 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto; (iii) SEQ ID NO: 49 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto, and SEQ ID NO: 57 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto; (iv) SEQ ID NO: 113 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto, and SEQ ID NO: 121 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto; (v) SEQ ID NO: 209 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto, and SEQ ID NO: 217 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto; and (vi) SEQ ID NO: 289 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto, and SEQ ID NO: 297 or a sequence having at least 90%, at least 95%, at least 98%, or at least 99% identity thereto;
A water lubrication air compression system comprising: a compressor comprising an inlet end , an outlet end , a compression chamber , a first bearing chamber , a second bearing chamber , a first air chamber between the first bearing chamber and the compression chamber , and a second air chamber between the second bearing chamber and the compression chamber ; an air channel system connected between the inlet end and the outlet end of the compressor , the air channel system comprising a water vapor isolation device connected to the outlet end of the compressor ; a water channel system connected between an external water source and the inlet end of the compressor ; a lubricant channel system connected to the second bearing chamber where a lubricant in the second bearing chamber is circulated in the lubricant channel system ; and a negative pressure system connected to the first air chamber and the second air chamber and providing a negative pressure for the first air chamber and the second air chamber , characterized in that the negative pressure system comprises: a blower ; and a negative pressure nozzle connected to the blower , the first air chamber , and the second air chamber , the negative pressure nozzle providing the first air chamber and the second air chamber with a negative pressure resulted from an air current fed into the negative pressure nozzle by the blower . a compressor comprising an inlet end , an outlet end , a compression chamber , a first bearing chamber , a second bearing chamber , a first air chamber between the first bearing chamber and the compression chamber , and a second air chamber between the second bearing chamber and the compression chamber ; an air channel system connected between the inlet end and the outlet end of the compressor , the air channel system comprising a water vapor isolation device connected to the outlet end of the compressor ; a water channel system connected between an external water source and the inlet end of the compressor ; a lubricant channel system connected to the second bearing chamber where a lubricant in the second bearing chamber is circulated in the lubricant channel system ; and a negative pressure system connected to the first air chamber and the second air chamber and providing a negative pressure for the first air chamber and the second air chamber , characterized in that the negative pressure system comprises: a blower ; and a negative pressure nozzle connected to the blower , the first air chamber , and the second air chamber , the negative pressure nozzle providing the first air chamber and the second air chamber with a negative pressure resulted from an air current fed into the negative pressure nozzle by the blower . a blower ; and a negative pressure nozzle connected to the blower , the first air chamber , and the second air chamber , the negative pressure nozzle providing the first air chamber and the second air chamber with a negative pressure resulted from an air current fed into the negative pressure nozzle by the blower .
A method in a network node for mitigating disruption during maintenance of an edge gateway node of a communication network , the edge gateway node connecting a plurality of devices to one or more services of the communication network, the plurality of devices comprising one or more first devices which are capable of connecting to a cloud environment of the communication network in the absence of the edge gateway node , and one or more second devices which are incapable of connecting to the cloud environment in the absence of the edge gateway node , the method comprising: establishing respective virtual devices for the one or more second devices , the virtual devices comprising predictive models trained to replicate data output by the respective one or more second devices; and during a time interval in which the maintenance of the edge gateway node is performed: configuring the one or more virtual devices to connect to a virtual edge gateway node established in the cloud environment , wherein the virtual edge gateway node replicates the functionality of the edge gateway node undergoing maintenance; and configuring at least one of the one or more first devices to connect to the virtual edge gateway node . establishing respective virtual devices for the one or more second devices , the virtual devices comprising predictive models trained to replicate data output by the respective one or more second devices; and during a time interval in which the maintenance of the edge gateway node is performed: configuring the one or more virtual devices to connect to a virtual edge gateway node established in the cloud environment , wherein the virtual edge gateway node replicates the functionality of the edge gateway node undergoing maintenance; and configuring at least one of the one or more first devices to connect to the virtual edge gateway node . configuring the one or more virtual devices to connect to a virtual edge gateway node established in the cloud environment , wherein the virtual edge gateway node replicates the functionality of the edge gateway node undergoing maintenance; and configuring at least one of the one or more first devices to connect to the virtual edge gateway node .
A method of operating an air-gas mixture burning appliance that comprises an air-gas mixing unit for mixing of air and gas, in particular hydrogen, to form a combustible air-gas mixture , a burning unit with a burner surface that is arranged downstream of the air-gas mixing unit for burning the combustible air-gas mixture at the burner surface , and a flame detector for sensing presence of a flame at the burner surface on the basis of a predetermined flame detection threshold , the method comprising: adjusting the predetermined flame detection threshold for at least two different operating points of the air-gas mixture burning appliance , characterised in that the predetermined flame detection threshold is configured to avoid indication of a stable flame upon occurrence of a flame in the air-gas mixing unit under a sustained flashback event and/or in the event of a flame stabilising undesirably upstream of the burner surface .
A method for the formation of multi-layer paint films in which an aqueous first colored base paint (A) is coated on an electro-deposition paint cured paint film and a first colored base paint film is formed, then an aqueous second colored base paint (B) is coated on the first colored base paint film without preliminary heating of the first colored base paint film and a second colored base paint film is formed, and then a clear paint (C) is coated on the second colored base paint film after preliminary heating of the first colored base paint film and second colored base paint film and a clear paint film is formed and the three paint films which have been formed are heated and cured at the same time, characterized in that talc pigment is included in each of the aqueous colored first base paint (A) and aqueous colored second base paint (B) in an amount of from 1 to 5 mass% with respect to the total resin solid fraction of each of said aqueous colored first base paint (A) and aqueous colored second base paint (B).
A propeller control system for an aircraft propeller rotatable about a longitudinal axis and having an adjustable blade angle, the control system comprising: a blade angle feedback ring and a sensor , wherein the sensor is couplable to the propeller to rotate with the propeller and to move along the longitudinal axis (A) along with adjustment of the blade angle, said blade angle feedback ring comprising a plurality of position markers spaced around its circumference such that a circumferential distance between at least some adjacent ones of said position markers varies along said longitudinal axis (A); the sensor positioned adjacent said blade angle feedback ring for producing signals indicative of passage of said position markers , such that an interval between ones of said signals is indicative of a circumferential distance between adjacent ones of said position markers ; and a controller in communication with said sensor to measure a longitudinal position of the sensor couplable to the propeller based on an interval between consecutive ones of said signal, said controller configured to produce a warning signal if said longitudinal position is outside a first threshold range, wherein the propeller forms part of a propeller assembly and said first threshold range corresponds to upper and lower dimensional tolerance limits of the propeller assembly. a blade angle feedback ring and a sensor , wherein the sensor is couplable to the propeller to rotate with the propeller and to move along the longitudinal axis (A) along with adjustment of the blade angle, said blade angle feedback ring comprising a plurality of position markers spaced around its circumference such that a circumferential distance between at least some adjacent ones of said position markers varies along said longitudinal axis (A); the sensor positioned adjacent said blade angle feedback ring for producing signals indicative of passage of said position markers , such that an interval between ones of said signals is indicative of a circumferential distance between adjacent ones of said position markers ; and a controller in communication with said sensor to measure a longitudinal position of the sensor couplable to the propeller based on an interval between consecutive ones of said signal, said controller configured to produce a warning signal if said longitudinal position is outside a first threshold range, wherein the propeller forms part of a propeller assembly and said first threshold range corresponds to upper and lower dimensional tolerance limits of the propeller assembly.
A converging drum for a crop mowing implement , the converging drum comprising: a body having an exterior surface and extending along a central longitudinal axis between a first end and a second end , wherein the body is configured to rotate about the central longitudinal axis in a defined rotational direction; at least one ramp feature attached to and extending radially outward from the exterior surface of the body relative to the central longitudinal axis , and disposed between the first end and the second end of the body ; and wherein the at least one ramp feature is arranged to form an acute angle relative to a reference plane disposed orthogonal to the central longitudinal axis , characterized in that the body includes a planar wall portion extending parallel to the central longitudinal axis , and in that the at least one ramp feature includes a plate having a straight inner edge disposed against the planar wall portion of the body , and in that the plate extends outward away from the planar wall surface of the body to a curved distal edge . a body having an exterior surface and extending along a central longitudinal axis between a first end and a second end , wherein the body is configured to rotate about the central longitudinal axis in a defined rotational direction; at least one ramp feature attached to and extending radially outward from the exterior surface of the body relative to the central longitudinal axis , and disposed between the first end and the second end of the body ; and wherein the at least one ramp feature is arranged to form an acute angle relative to a reference plane disposed orthogonal to the central longitudinal axis , characterized in that the body includes a planar wall portion extending parallel to the central longitudinal axis , and in that the at least one ramp feature includes a plate having a straight inner edge disposed against the planar wall portion of the body , and in that the plate extends outward away from the planar wall surface of the body to a curved distal edge . the body includes a planar wall portion extending parallel to the central longitudinal axis , and in that the at least one ramp feature includes a plate having a straight inner edge disposed against the planar wall portion of the body , and in that the plate extends outward away from the planar wall surface of the body to a curved distal edge .
A method of controlling a wind turbine , the method comprising: determining a target fatigue life consumption for each of one or more components of the wind turbine; comparing the target fatigue life consumption with a measure of fatigue life consumption for each of the one or more turbine components; and controlling the turbine power output based upon the comparison; characterised in that the target fatigue life consumption is determined by combining data indicative of a target rate of accumulation of fatigue damage over at least a portion of the operating life of the wind turbine and data indicative of an expected rate of accumulation of fatigue damage caused by seasonal variations in turbine operating conditions; wherein the data indicative of an expected rate of accumulation of fatigue damage is obtained from a seasonal schedule defining the expected seasonal rates of accumulation of fatigue damage, the seasonal schedule derived: i) from environmental data for the site on which the wind turbine is located and/or the site on which a wind power plant that includes the wind turbine is located and/or the sites on which one or more nearby wind power plants are located; and ii) using values from the output of one or more lifetime usage estimator algorithms. determining a target fatigue life consumption for each of one or more components of the wind turbine; comparing the target fatigue life consumption with a measure of fatigue life consumption for each of the one or more turbine components; and controlling the turbine power output based upon the comparison; characterised in that the target fatigue life consumption is determined by combining data indicative of a target rate of accumulation of fatigue damage over at least a portion of the operating life of the wind turbine and data indicative of an expected rate of accumulation of fatigue damage caused by seasonal variations in turbine operating conditions; wherein the data indicative of an expected rate of accumulation of fatigue damage is obtained from a seasonal schedule defining the expected seasonal rates of accumulation of fatigue damage, the seasonal schedule derived: i) from environmental data for the site on which the wind turbine is located and/or the site on which a wind power plant that includes the wind turbine is located and/or the sites on which one or more nearby wind power plants are located; and ii) using values from the output of one or more lifetime usage estimator algorithms. i) from environmental data for the site on which the wind turbine is located and/or the site on which a wind power plant that includes the wind turbine is located and/or the sites on which one or more nearby wind power plants are located; and ii) using values from the output of one or more lifetime usage estimator algorithms.