mhurhangee/patent-ind-claim-en huggingface dataset:
Cleaning device suitable for subsea cleaning operations comprising: a frame , wherein a roof plane , a floor plane and connecting frame elements defines an inner space, the connecting frame elements connecting the roof plane and the floor plane a defined distance apart, a first set of thrusters arranged between the inside of the roof plane and the floor plane and mounted to opposite openings in the roof plane and the floor plane respectively to allow thrusters to move water either way through the thrusters orthogonally relative the roof and floor planes , a second set of thrusters comprising one or more thrusters arranged between the inside of the roof plane and the floor plane mounted to allow thrusters to move water either way through the thrusters in the same plane as the roof and floor plane wherein each of the one or more thrusters are arranged close to the outer end of one or more of the most periphery parts of the frame where each thruster has a substantially unobstructed thrust path to both sides of the thruster , a nose cleaning assembly arranged in a corner nozzle housing arranged in one of the corners of the cleaning device , and the nose cleaning assembly comprise jet nozzles connected to a fluid source via a fluid inlet and channels providing cleaning accessibility to difficult to access areas. a frame , wherein a roof plane , a floor plane and connecting frame elements defines an inner space, the connecting frame elements connecting the roof plane and the floor plane a defined distance apart, a first set of thrusters arranged between the inside of the roof plane and the floor plane and mounted to opposite openings in the roof plane and the floor plane respectively to allow thrusters to move water either way through the thrusters orthogonally relative the roof and floor planes , a second set of thrusters comprising one or more thrusters arranged between the inside of the roof plane and the floor plane mounted to allow thrusters to move water either way through the thrusters in the same plane as the roof and floor plane wherein each of the one or more thrusters are arranged close to the outer end of one or more of the most periphery parts of the frame where each thruster has a substantially unobstructed thrust path to both sides of the thruster , a nose cleaning assembly arranged in a corner nozzle housing arranged in one of the corners of the cleaning device , and the nose cleaning assembly comprise jet nozzles connected to a fluid source via a fluid inlet and channels providing cleaning accessibility to difficult to access areas.
Method for axle control of at least one first axle of a rail vehicle, wherein the axle controller has an actuator unit, a passive elastic bearing mechanically functionally connected in parallel therewith and a regulation facility, and the regulation facility is connected at least to the actuator unit for data transfer purposes, wherein the regulation facility exclusively uses an actual actuating force of the actuator unit as control or regulation variable for steering angle γ of the first axle of the rail vehicle.
An in vitro screening method for rapidly testing a subject for a cancerous or precancerous condition, wherein the subject displays no obvious signs or symptoms of a cancerous or precancerous condition, the method comprising the steps of (a) assaying a portion of a biological sample obtained from an individual for the presence therein of glycoprotein containing at least one carbohydrate selected from the group consisting of beta-D-Gal-(1->3)-D-GalNAc, Fuc-alpha-1->2 Gal-Beta(1->4)-Fuc-alpha-1->3-GlcNAc, Fuc-Alpha-1->2Gal-beta-(1->4)-Fuc-alpha-1->3-GlcNAc-beta-(1->3)-Gal-beta-(1>4)-GlcNAc and Fuc-alpha-1->2-Gal-beta-(1->4)-Fuc-alpha-1->3-GlcNAc-beta-(1->3)-Gal-beta-(1->4)-Fuc-alpha-1->3-GlcNAc, by briefly subjecting the sample to oxidizing conditions which are capable of selectively oxidizing only the cyclic sugar moieties of any said marker carbohydrate present in the glycoprotein in the sample at a hydroxy group-bearing ring carbon atom thereof to form an aldehydic sugar moiety and then visualizing any aldehydic saccharide groups thus formed with a Schiff's base dye; (b) also assaying a portion of the biological sample for the presence therein of any glycoprotein by subjecting the sample to the oxidizing action of an oxidizing agent which oxidizes the saccharide moieties of any glycoprotein therein to aldehydic sugar moieties and then visualizing any thus-produced aldehydic sugar moieties, the presence of thereby formed aldehydic sugar moieties confirming the adequacy of the sampling and the absence therein of thereby formed aldehyde sugar moieties establishing that the negative test results were due to sampling error; (c) retesting the individual in the same manner with a fresh biological sample, if the first sample assays negative in steps (a) and (b); and (d) diagnosing the asymptomatic patient as having cancer or a precancerous condition based on visualizing a color change in the Schiff's base dye.
A harvester , comprising: a chassis ; and a header carried by the chassis , the header including: a header frame ; at least one harvesting element carried by the header frame ; and a plurality of dividers pivotably carried by the header frame , each of the plurality of dividers defining a respective divider angle (Dα) relative to a ground plane (GP); and a plurality of actuators carried by the header frame , each of the plurality of actuators coupling to a respective one of the plurality of dividers and being configured to control the respective divider angle (Dα) of the respectively coupled divider characterized in that the harvester further comprising: a controller operatively coupled to the plurality of actuators and configured to activate each of the plurality of actuators independently of the other actuators ; and an adjustable feeder housing carried by the chassis and defining a face angle (Fα) relative to the ground plane (GP) and an angle sensor associated with the feeder housing and operatively coupled to the controller , the controller being configured to detect a change in the face angle (Fα) and activate at least one of the plurality of actuators responsively to detecting the change in the face angle (Fα). a chassis ; and a header carried by the chassis , the header including: a header frame ; at least one harvesting element carried by the header frame ; and a plurality of dividers pivotably carried by the header frame , each of the plurality of dividers defining a respective divider angle (Dα) relative to a ground plane (GP); and a header frame ; at least one harvesting element carried by the header frame ; and a plurality of dividers pivotably carried by the header frame , each of the plurality of dividers defining a respective divider angle (Dα) relative to a ground plane (GP); and a plurality of actuators carried by the header frame , each of the plurality of actuators coupling to a respective one of the plurality of dividers and being configured to control the respective divider angle (Dα) of the respectively coupled divider a controller operatively coupled to the plurality of actuators and configured to activate each of the plurality of actuators independently of the other actuators ; and an adjustable feeder housing carried by the chassis and defining a face angle (Fα) relative to the ground plane (GP) and an angle sensor associated with the feeder housing and operatively coupled to the controller , the controller being configured to detect a change in the face angle (Fα) and activate at least one of the plurality of actuators responsively to detecting the change in the face angle (Fα).
A single-sided, four-way indexable cutting insert having a positive basic shape and comprising: a rake surface ; a base bearing surface located opposite the rake surface ; an insert axis A I extending perpendicular to the base bearing surface and through the center of the insert , the insert axis A I defining: an upward direction D U from the base bearing surface towards the rake surface , a downward direction D D opposite to the upward direction D U , and an outward direction D O perpendicular to the upward and downward directions D U , D D and extending away from the insert axis A I ; a cutting insert height Hi measurable parallel to the insert axis A I , from the base bearing surface to a highest point of the rake surface ; a peripheral surface connecting the rake surface and base bearing surface , the peripheral surface comprising: an unground lower sub-surface which extends upwardly and outwardly from the base bearing surface , the lower sub-surface comprising first, second, third and fourth side abutment surfaces ; and an upper sub-surface connecting the lower sub-surface and the rake surface , the upper sub-surface beginning in the upward direction D U at a minimum upper surface height H U above the base bearing surface ; a cutting edge formed along an intersection of the peripheral surface and rake surface ; a screw hole opening out to the rake and base bearing surfaces , the screw hole having a void volume V s ; wherein: the insert has an imaginary square frustum defined by: a square base containing the base bearing surface ; four isosceles trapezoid side surfaces , each extending upwardly and outwardly from the square base at an abutment surface relief angle θ fulfilling the condition 1° ≤ θ ≤ 15°, and each containing a respective one of the first, second, third and fourth side abutment surfaces ; and a square top connecting the four isosceles trapezoid side surfaces and located a distance equal to the cutting insert height H I from the square base ; the upper sub-surface comprises at least one overhanging portion , which extends outwardly from an adjacent one of the trapezoid side surfaces and has a lowermost point at said minimum upper sub-surface height Hu; characterized in that in a view parallel to the insert axis A I , an inscribed circle diameter Ic of the cutting edges fulfills the condition Ic ≤ 10 mm; and a volume ratio V S /V F of the void volume Vs and a material volume V F of the cutting insert fulfills the condition V S /V F ≥ 0.25.
A method of protecting a fuel level sensor in a fuel tank assembly during transportation, said fuel tank assembly comprising a fuel tank and a fuel level sensor of the type defined for measuring the level of a fuel in the fuel tank; the sensor comprising a wiper and at least one resistive area ; the method comprising: application before the fuel level sensor is assembled to the fuel tank of a temporary barrier layer of material to damp movement between the wiper and the at least one resistive area ; characterized in that : the temporary barrier layer is formed of a material and is applied in a thickness such that it will dissolve when submerged in the fuel on a first filling of the fuel tank . application before the fuel level sensor is assembled to the fuel tank of a temporary barrier layer of material to damp movement between the wiper and the at least one resistive area ; characterized in that : the temporary barrier layer is formed of a material and is applied in a thickness such that it will dissolve when submerged in the fuel on a first filling of the fuel tank .
A control method for an air conditioner comprising: determining (S12) a user set temperature and performing an air cooling operation or an air heating operation in an indoor space ; determining (S13) whether a user is present in the indoor space ; when it is determined that a user is absent, counting (S15) an elapsed time; and when the elapsed time reaches a set time, performing (S17) a comfort power saving mode, wherein the comfort power saving mode includes an operation controlled according to a set comfort temperature determined such that a predicted mean vote, PMV, determined based on temperature, humidity, air speed, mean radiant temperature, clothing insulation, and metabolic rate is maintained in a preset range, characterised in that in the step of performing a comfort power saving mode, in a case where the air conditioner performs an air cooling operation, when the user set temperature is lower than a first temperature value (A), the set comfort temperature is determined (S20) to be the first temperature value (A), when the user set temperature is higher than the first temperature value (A) and is lower than a second temperature value (B), the set comfort temperature is determined (S31) to be the second temperature value (B), and when the user set temperature is higher than the second temperature value (B), the air conditioner is turned off (S36, S37). determining (S12) a user set temperature and performing an air cooling operation or an air heating operation in an indoor space ; determining (S13) whether a user is present in the indoor space ; when it is determined that a user is absent, counting (S15) an elapsed time; and when the elapsed time reaches a set time, performing (S17) a comfort power saving mode, wherein the comfort power saving mode includes an operation controlled according to a set comfort temperature determined such that a predicted mean vote, PMV, determined based on temperature, humidity, air speed, mean radiant temperature, clothing insulation, and metabolic rate is maintained in a preset range, characterised in that in the step of performing a comfort power saving mode, in a case where the air conditioner performs an air cooling operation, when the user set temperature is lower than a first temperature value (A), the set comfort temperature is determined (S20) to be the first temperature value (A), when the user set temperature is higher than the first temperature value (A) and is lower than a second temperature value (B), the set comfort temperature is determined (S31) to be the second temperature value (B), and when the user set temperature is higher than the second temperature value (B), the air conditioner is turned off (S36, S37).
Mould for producing footwear by means of direct injection onto the upper of a sole comprising a tread and a midsole , wherein the midsole is composed of a first layer and a second layer ; the mould comprising a base , a pair of first half-rings , a pair of second half-rings , a first cover , a second cover and a mould last , wherein the first half-rings are designed to be arranged close together so as to abut against the base and against the first cover , so as to form a first mould cavity for moulding the tread , and/or to abut against the base and against the second cover, so to form a second mould cavity for moulding the first layer of the midsole ; and wherein, with the first half-rings abutting against the base , the second half-rings are designed to be arranged close together, so as to be superimposed on the first half-rings and to abut against the upper , fitted onto the mould last , so as form a third mould cavity for moulding the second layer of the midsole ; wherein the mould comprises gripping means designed to fix selectively the first half-rings to the base or to the second half-rings , the gripping means comprising first coupling means , provided between the base and the first half-rings , and second coupling means , provided between the first half-rings and the second half-rings .
An enclosure , comprising: a plurality of panel sections rotatably coupled together, at least one panel section of the plurality of panel sections including a first frame component extending along a top of the at least one panel section and being directly coupled to a second frame component of an adjacent panel section ; and a bottom frame component extending along a bottom of the at least one panel section , parallel to the said first frame component , a razor wire panel extending across each of the plurality of panel sections , between the first frame component and the bottom frame component , wherein the razor wire panel is arranged as a mesh in which a first plurality of razor wire strands is positioned across a second plurality of razor wire strands. a plurality of panel sections rotatably coupled together, at least one panel section of the plurality of panel sections including a first frame component extending along a top of the at least one panel section and being directly coupled to a second frame component of an adjacent panel section ; and a bottom frame component extending along a bottom of the at least one panel section , parallel to the said first frame component , a razor wire panel extending across each of the plurality of panel sections , between the first frame component and the bottom frame component , wherein the razor wire panel is arranged as a mesh in which a first plurality of razor wire strands is positioned across a second plurality of razor wire strands.
An assembly for an aircraft propulsion system , comprising: a fixed structure ; an inner cowl door extending circumferentially between an inner cowl door first end and an inner cowl door second end , the inner cowl door pivotally connected to the fixed structure at the inner cowl door first end ; an outer cowl door pivotally connected to the fixed structure , the outer cowl door radially outboard of and overlapping the inner cowl door ; and a linkage extending between and movably connected to the inner cowl door and the outer cowl door , the linkage pivotally connected to the inner cowl door and pivotally connected to the outer cowl door , wherein the linkage is arranged proximate the fixed structure , characterized in that : the linkage has a fixed length and is arranged closer to the fixed structure than to the inner cowl door second end , and the linkage is configured to pull against and thereby open the inner cowl door as the outer cowl door is opened. a fixed structure ; an inner cowl door extending circumferentially between an inner cowl door first end and an inner cowl door second end , the inner cowl door pivotally connected to the fixed structure at the inner cowl door first end ; an outer cowl door pivotally connected to the fixed structure , the outer cowl door radially outboard of and overlapping the inner cowl door ; and a linkage extending between and movably connected to the inner cowl door and the outer cowl door , the linkage pivotally connected to the inner cowl door and pivotally connected to the outer cowl door , wherein the linkage is arranged proximate the fixed structure ,
A method for mesh network performance optimization performed by a Cloud-Server, the method comprising: receiving data from a plurality of client steering daemons, CSDs, each operating on an 802.11 access point, AP; performing processing on the received data, wherein the processing includes performing machine learning on the received data to determine a pair of steering profiles for each CSD of the plurality of CSDs, wherein the pair of steering profiles include a steering decision profile, SDP, and a steering mechanism profile, SMP, wherein the SDP is a set of parameters used for computing the cost of keeping a station, STA, at an AP/interface, and wherein the SMP is a set of actions for steering the STA based on the SDP of the pair of steering profiles; generating a pool of steering profiles comprising a set of pairs of SDPs and SMPs based on the processing; and sending a subset of steering profiles of the generated pool of steering profiles to each of the plurality of CSDs to enable steering of a STA based on a single pair of steering profiles from the subset of steering profiles. receiving data from a plurality of client steering daemons, CSDs, each operating on an 802.11 access point, AP; performing processing on the received data, wherein the processing includes performing machine learning on the received data to determine a pair of steering profiles for each CSD of the plurality of CSDs, wherein the pair of steering profiles include a steering decision profile, SDP, and a steering mechanism profile, SMP, wherein the SDP is a set of parameters used for computing the cost of keeping a station, STA, at an AP/interface, and wherein the SMP is a set of actions for steering the STA based on the SDP of the pair of steering profiles; generating a pool of steering profiles comprising a set of pairs of SDPs and SMPs based on the processing; and sending a subset of steering profiles of the generated pool of steering profiles to each of the plurality of CSDs to enable steering of a STA based on a single pair of steering profiles from the subset of steering profiles.
Mechanical oscillator for a timepiece comprising an inertial mass arranged to oscillate about a neutral position under the effect of a restoring force provided by at least one elastic element , wherein said mechanical oscillator further comprises a compensation spring pivotably linked to said inertial mass by means of a substantially rigid first connecting bar , said compensation spring and said first connecting bar being arranged so as to apply a compensating force to said inertial mass which varies in function of displacement of said inertial mass from its neutral position, characterised in that said compensation spring is attached to a slider arranged to translate along a respective axis, said slider being pivotally linked to said substantially rigid first connecting bar . wherein said mechanical oscillator further comprises a compensation spring pivotably linked to said inertial mass by means of a substantially rigid first connecting bar , said compensation spring and said first connecting bar being arranged so as to apply a compensating force to said inertial mass which varies in function of displacement of said inertial mass from its neutral position, characterised in that said compensation spring is attached to a slider arranged to translate along a respective axis, said slider being pivotally linked to said substantially rigid first connecting bar .
A TCR-anti-CD3 fusion molecule comprising a soluble TCR and an anti-CD3 antibody, or functional fragment thereof, which is covalently linked to the C- or N-terminus of the alpha or beta chain of the TCR, wherein the TCR has the property of binding to a SLLQHLIGL (SEQ ID NO: 1) HLA-A*02 complex and comprises a TCR alpha chain variable domain and a TCR beta chain variable domain, each of which comprises FR1-CDR1-FR2-CDR2-FR3-CDR3-FR4 where FR is a framework region and CDR is a complementarity determining region, wherein (a) the alpha chain CDRs have the following sequences: CDR1 - TISGTDY (SEQ ID NO: 39) CDR2 - GLTSN (SEQ ID NO: 40) CDR3 - CILILGHSRLGNYIATF (SEQ ID NO: 46) and (b) the beta chain CDRs have the following sequences: CDR1 - LNHDA (SEQ ID NO: 42) CDR2 - SQIMGDE (SEQ ID NO: 48) CDR3 - CASSWWTGGASPIRF (SEQ ID NO: 58). (a) the alpha chain CDRs have the following sequences: CDR1 - TISGTDY (SEQ ID NO: 39) CDR2 - GLTSN (SEQ ID NO: 40) CDR3 - CILILGHSRLGNYIATF (SEQ ID NO: 46) and CDR1 - TISGTDY (SEQ ID NO: 39) CDR2 - GLTSN (SEQ ID NO: 40) CDR3 - CILILGHSRLGNYIATF (SEQ ID NO: 46) and (b) the beta chain CDRs have the following sequences: CDR1 - LNHDA (SEQ ID NO: 42) CDR2 - SQIMGDE (SEQ ID NO: 48) CDR3 - CASSWWTGGASPIRF (SEQ ID NO: 58). CDR1 - LNHDA (SEQ ID NO: 42) CDR2 - SQIMGDE (SEQ ID NO: 48) CDR3 - CASSWWTGGASPIRF (SEQ ID NO: 58).