mhurhangee/patent-ind-claim-en huggingface dataset:
An electrosurgical generator for use in fusing or sealing tissue comprising: a controller and an RF amplifier that is arranged to be connected to and to generate an electrical output for an electrosurgical instrument in accordance with signals received from the controller , wherein the controller is arranged to: signal the RF amplifier to, in a first stage, apply RF energy to an area of tissue and to increase the applied voltage in accordance with a dynamic first voltage ramp, determine a peak condition of the area of tissue affected by the applying of the first stage RF energy, wherein the determined peak condition corresponds to a boiling point of fluid in the area of tissue, once the peak condition is determined, signal the RF amplifier to, in a second stage, reduce the voltage of the RF energy being applied to the area of tissue from a first to a second voltage, signal the RF amplifier to, in a third stage, increase the applied voltage in accordance with a second voltage ramp to a third voltage, and wherein the third voltage is between the first voltage and the second voltage, signal the RF amplifier to, in a fourth stage, maintain the applied voltage constant at the third voltage for a predetermined period of time, and signal the RF amplifier to terminate the application of the RF energy to the area of the tissue after the pre-determined period of time has elapsed. signal the RF amplifier to, in a first stage, apply RF energy to an area of tissue and to increase the applied voltage in accordance with a dynamic first voltage ramp, determine a peak condition of the area of tissue affected by the applying of the first stage RF energy, wherein the determined peak condition corresponds to a boiling point of fluid in the area of tissue, once the peak condition is determined, signal the RF amplifier to, in a second stage, reduce the voltage of the RF energy being applied to the area of tissue from a first to a second voltage, signal the RF amplifier to, in a third stage, increase the applied voltage in accordance with a second voltage ramp to a third voltage, and wherein the third voltage is between the first voltage and the second voltage, signal the RF amplifier to, in a fourth stage, maintain the applied voltage constant at the third voltage for a predetermined period of time, and signal the RF amplifier to terminate the application of the RF energy to the area of the tissue after the pre-determined period of time has elapsed.
Timepiece comprising a drive module , a dial comprising a central opening , an hour pipe passing through the central opening of the dial and driven in rotation by the drive module , and a device for attaching the dial, in which said attachment device comprises: - a holding tube arranged around the hour pipe and mechanically connected to the drive module , and - a retaining member arranged between the holding tube and the dial and/or a dial support to which the dial is attached, characterised in that said retaining member is a part fixed thereto. - a holding tube arranged around the hour pipe and mechanically connected to the drive module , and - a retaining member arranged between the holding tube and the dial and/or a dial support to which the dial is attached, characterised in that said retaining member is a part fixed thereto.
An apparatus for controlling the injection pressure of an aqueous polymeric solution in an oil well, the said apparatus being formed by: - At least one pressure modulation valve allowing a maximum pressure loss of 5 bars per valve with practically no mechanical deterioration, the said valve(s) being connected in line with; - A tube , the purpose of the apparatus being that of being able to reduce the pressure to 100 bars with total mechanical deterioration of less than 10%, characterized in that the tube contains vortex modules , each creating a maximum pressure loss of 5 bars, with practically no mechanical deterioration, a vortex module being a section of tube, which is closed at one end thereof by a cap perforated with a hole, and which can be inserted into the tube. - At least one pressure modulation valve allowing a maximum pressure loss of 5 bars per valve with practically no mechanical deterioration, the said valve(s) being connected in line with; - A tube ,
Backrest of a vehicle seat comprising a backrest armature with an upper cross member (17 4 ) and a lower cross member (17 3 ), at least one central upholstery module and two side upholstery modules each arranged on a respective side of the central upholstery module , each of the at least three upholstery modules being fixable to the backrest armature independently of the other two upholstery modules , each of the at least three upholstery modules being preferably fixed to the backrest armature independently of the other two upholstery modules backrest in which the central upholstery module comprises at least one support , fixed to the backrest armature , and one foam block covering in whole or in part the support , wherein the support extends in a longitudinal direction between two longitudinal ends (54 1 , 54 2 ) of the support , the longitudinal ends (54 1 , 54 2 ) of the support being curved, one longitudinal end (54 2 ) of the support resting on the upper cross member (17 4 ) of the backrest armature and the other longitudinal end (54 1 ) of the support accommodating the lower cross member (17 3 ) of the backrest armature , the longitudinal ends (54 1 , 54 2 ) of the support respectively comprising snap fitting reliefs, complementary to snap fitting reliefs on the upper and lower cross members (17 3 , 17 4 ) of the backrest armature for fixing onto the lower (17 3 ) and upper (17 4 ) cross members by snap fitting.
A computer-implemented method of determining a particle size distribution, comprising: obtaining an image of a plurality of particles and one or more calibration marks by using a camera that is positioned to capture an image of the plurality of (x, particles lying on a calibration pattern which includes a background and the calibration marks , wherein the camera includes at least one lens and wherein the plurality of particles and the one or more calibration marks were captured using the same lens ; correcting the image for distortion effects to generate a corrected image, wherein the same correction factor is applied to both the plurality of particles and the one or more calibration marks ; determining a size of the plurality of particles in the image using the corrected image and the dimensions of the one or more calibration marks ; determining a particle size distribution for the plurality of particles; comparing the particle size distribution with a target particle size profile to determine closeness of match; and based on said comparison, indicating to an operator that further grinding would bring the particle size distribution closer to the target particle size profile. obtaining an image of a plurality of particles and one or more calibration marks by using a camera that is positioned to capture an image of the plurality of (x, particles lying on a calibration pattern which includes a background and the calibration marks , wherein the camera includes at least one lens and wherein the plurality of particles and the one or more calibration marks were captured using the same lens ; correcting the image for distortion effects to generate a corrected image, wherein the same correction factor is applied to both the plurality of particles and the one or more calibration marks ; determining a size of the plurality of particles in the image using the corrected image and the dimensions of the one or more calibration marks ; determining a particle size distribution for the plurality of particles; comparing the particle size distribution with a target particle size profile to determine closeness of match; and
A computer-implemented method comprising: (i) receiving first data from a first sensor , the first data comprising values for a first parameter of an aircraft ; (ii) determining whether damage has occurred to the aircraft using the values of the first data; (iii) receiving second data from a second sensor , the second data comprising values for a second parameter of the aircraft ; (iv) determining whether damage has occurred to the aircraft using the values of the second data; (v) determining whether damage has occurred to the aircraft using the determinations of whether damage has occurred at steps (ii) and (iv); (vi) receiving third data from a third sensor , the third data comprising values for a third parameter of the aircraft ; (vii) determining whether damage has occurred to the aircraft using the values of the third data; (viii) determining whether damage has occurred to the aircraft using the determination of whether damage has occurred at steps (v) and (vii); and (ix) controlling output of a signal comprising data indicating the occurrence of damage to the aircraft using the occurrence of damage determined at step (viii), wherein step (ix) is performed subsequent to the determination of damage occurrence at step (v) and at step (viii). (i) receiving first data from a first sensor , the first data comprising values for a first parameter of an aircraft ; (ii) determining whether damage has occurred to the aircraft using the values of the first data; (iii) receiving second data from a second sensor , the second data comprising values for a second parameter of the aircraft ; (iv) determining whether damage has occurred to the aircraft using the values of the second data; (v) determining whether damage has occurred to the aircraft using the determinations of whether damage has occurred at steps (ii) and (iv); (vi) receiving third data from a third sensor , the third data comprising values for a third parameter of the aircraft ; (vii) determining whether damage has occurred to the aircraft using the values of the third data; (viii) determining whether damage has occurred to the aircraft using the determination of whether damage has occurred at steps (v) and (vii); and (ix) controlling output of a signal comprising data indicating the occurrence of damage to the aircraft using the occurrence of damage determined at step (viii), wherein step (ix) is performed subsequent to the determination of damage occurrence at step (v) and at step (viii).
A tool system comprising a pick and a pick holder , wherein the pick has a pick head and a pick shaft , comprising a support element having on its underside a seat surface and a centering projection protruding beyond the seat surface , wherein the centering projection has a centering surface (34.1) which extends at an inclination to the central longitudinal axis (M) of the pick , which transitions directly or indirectly into the seat surface wherein the support element is interrupted along the central longitudinal axis (M) by a receiving bore having an internal diameter D i for receiving the pick shaft , wherein the pick holder receives the pick shaft , wherein the pick holder facing the support element has a wear surface for supporting the seat surface and a centering receptacle for receiving the centering projection of the support element characterised in that a centering height measured in the direction of the central longitudinal axis (M) between one end of the centering receptacle facing away from the wear surface and the wear surface or measured between the end of the centering receptacle and a maximum point of a projection (47.1) protruding beyond the wear surface is designed such that the ratio between the internal diameter D i of the receiving bore of the support element and the centering height is less than 8, such that the support element with its seat surface rests on the wear surface of the pick holder , and such that the projection (47.1) of the pick holder protruding beyond the wear surface is designed corresponding to a recess of the support element moulded in the seat surface and protrudes into this.
A method of producing a nucleator masterbatch in which a nucleator is blended in an olefin polymer, said method being characterized by comprising the step of polymerizing an olefin monomer with incorporation of a nucleator component, which is dissolved in an organoaluminum compound or in an organoaluminum compound and an organic solvent, before or during polymerization of said olefin monomer such that said nucleator component is blended in an amount of 0.05 to 20 parts by mass with respect to 100 parts by mass of said olefin polymer obtained by said polymerization of said olefin monomer, wherein said nucleator is a compound represented by the following Formula or : (wherein, R 1 to R 4 each independently represent a hydrogen atom or an alkyl group having 1 to 9 carbon atoms which is optionally branched; R 5 represents a hydrogen atom or a methyl group; m represents 1 or 2; when m is 1, M 1 represents a hydrogen atom; and, when m is 2, M 1 represents a Group II element, Al(OH) or Zn) (wherein, X 1 represents an alkylene group having 1 to 5 carbon atoms which is optionally branched; R 7 to R 10 each independently represent one selected from the group consisting of a halogen atom, an alkyl group having 1 to 4 carbon atoms which is optionally substituted and/or branched and an alkoxy group having 1 to 4 carbon atoms which is optionally substituted and/or branched; and p, q, r and s each independently represent an integer of 0 to 3 (with a proviso that p and s are not 0).
Linking machine for linking a knitwear and a collar , initially separated, comprising: - a fixed unit comprising a support frame and a feeding device of the knitwear and/or the collar along a longitudinal direction (Y-Y), - and a mobile unit comprising: - a needle equipped with a device for operating said needle along a vertical direction (Z-Z), perpendicular to the longitudinal direction (Y-Y), to perform the linking, wherein the linking machine comprises a guide configured to align a collar seam line with a nape seam line that is at a fixed spacing from a nape edge on a nape of the knitwear and with a neck seam line that is at a fixed spacing from an overlock on a neck of the knitwear , said guide including a plate with at least one stop for the knitwear , arranged in a direction substantially parallel to said longitudinal direction (Y-Y), so as to allow the alignment of the knitwear parallel to the stop itself , and a fold on a corner of the plate and arranged upstream of said at least one stop with respect to a feeding direction of the knitwear , said fold being designed to help unroll the nape edge where the collar is joined, characterized in that the plate includes two stops wherein a first stop is conformed to permit the alignment of the knitwear parallel to the stop itself when linking the nape , and a second stop is conformed to ensure that the overlock of the knitwear maintains the desired seam line when linking the neck . - a fixed unit comprising a support frame and a feeding device of the knitwear and/or the collar along a longitudinal direction (Y-Y), - and a mobile unit comprising: - a needle equipped with a device for operating said needle along a vertical direction (Z-Z), perpendicular to the longitudinal direction (Y-Y), to perform the linking,
Method of compensating for errors in the torque realization of a heat engine belonging to a traction chain of a motor vehicle further comprising: - a gearbox , - the heat engine being coupled to the gearbox via a clutch , and - an electric traction motor disposed downstream of the clutch , - said method comprising, while the clutch is in a closed state: - a comparison step between a target torque corresponding to a desire for acceleration on the part of a driver and an actual torque equal to the sum of a torque (Cme) applied by the electric traction motor and a torque (Cemb) transmitted by the clutch corresponding to the torque (Cmth_r) produced by the heat engine , and - a step of applying an overtorque by the electric traction motor in the case where the actual torque is different from the target torque due to a difference (E) between the torque (Cmth_r) produced by the motor and a setpoint torque (Cmth_cns) of the heat engine , to reach the target torque, characterized in that said method comprises a step of adding a virtual compensatory term (ΔCmth) in the torque (Cemb) transmitted by the clutch . - a gearbox , - the heat engine being coupled to the gearbox via a clutch , and - an electric traction motor disposed downstream of the clutch , - said method comprising, while the clutch is in a closed state: - a comparison step between a target torque corresponding to a desire for acceleration on the part of a driver and an actual torque equal to the sum of a torque (Cme) applied by the electric traction motor and a torque (Cemb) transmitted by the clutch corresponding to the torque (Cmth_r) produced by the heat engine , and - a step of applying an overtorque by the electric traction motor in the case where the actual torque is different from the target torque due to a difference (E) between the torque (Cmth_r) produced by the motor and a setpoint torque (Cmth_cns) of the heat engine , to reach the target torque,
An engine assembly for an aircraft, the engine assembly comprising: an internal combustion engine having a liquid coolant system; a heat exchanger having coolant passages in fluid communication with the liquid coolant system and air passages in heat exchange relationship with the coolant passages ; an exhaust duct in fluid communication with the air passages of the heat exchanger , the exhaust duct having an outlet configured to be in fluid communication with an environment of the aircraft; and an intermediate duct in fluid communication with an exhaust of the internal combustion engine ; and a fan in fluid communication with the exhaust duct for driving a cooling air flow through the air passages of the heat exchanger and into the exhaust duct , wherein the intermediate duct has an outlet positioned within the exhaust duct downstream of the fan and upstream of the outlet of the exhaust duct , the outlet of the intermediate duct spaced inwardly from a peripheral wall of the exhaust duct so that, in use, the flow of cooling air through the exhaust duct surrounds a flow of exhaust gases out of the intermediate duct ; characterised in that : the internal combustion engine is a Wankel rotary engine. an internal combustion engine having a liquid coolant system; a heat exchanger having coolant passages in fluid communication with the liquid coolant system and air passages in heat exchange relationship with the coolant passages ; an exhaust duct in fluid communication with the air passages of the heat exchanger , the exhaust duct having an outlet configured to be in fluid communication with an environment of the aircraft; and an intermediate duct in fluid communication with an exhaust of the internal combustion engine ; and a fan in fluid communication with the exhaust duct for driving a cooling air flow through the air passages of the heat exchanger and into the exhaust duct , wherein the intermediate duct has an outlet positioned within the exhaust duct downstream of the fan and upstream of the outlet of the exhaust duct , the outlet of the intermediate duct spaced inwardly from a peripheral wall of the exhaust duct so that, in use, the flow of cooling air through the exhaust duct surrounds a flow of exhaust gases out of the intermediate duct ;
A clothes lifting device for a washing machine having an imperforated inner drum, the clothes lifting device comprising: a body being configured to be internally provided with an accommodating chamber; water inlets being arranged in the body and being configured to communicate with the accommodating chamber; a centrifugal drainage assembly being arranged in the accommodating chamber, said centrifugal drainage assembly being configured in an initial state of the centrifugal drainage assembly to be closed, and to open for drainage under an action of centrifugal force; and a filtering assembly being arranged on the water inlets of the body for filtering water entering the accommodating chamber, wherein the body comprises a lifting shell , which is internally provided with an open cavity; and a lifting base body , which is detachably installed at an open end of the open cavity of the lifting shell to form the accommodating chamber with the lifting shell ; the centrifugal drainage assembly is installed on the lifting base body ; the water inlets are arranged in the lifting shell , and the filtering assemblies are arranged on the water inlets of the lifting shell wherein a plurality of spraying openings are arranged in the lifting shell and characterised in that the water inlet filtering portion includes a base body water inlet filtering portion arranged on the lifting base body , and the base body water inlet filtering portion includes a plurality of base body water filtering holes which are arranged in the lifting base body and communicating with the accommodating chamber. a body being configured to be internally provided with an accommodating chamber; water inlets being arranged in the body and being configured to communicate with the accommodating chamber; a centrifugal drainage assembly being arranged in the accommodating chamber, said centrifugal drainage assembly being configured in an initial state of the centrifugal drainage assembly to be closed, and to open for drainage under an action of centrifugal force; and a filtering assembly being arranged on the water inlets of the body for filtering water entering the accommodating chamber, wherein the body comprises a lifting shell , which is internally provided with an open cavity; and a lifting base body , which is detachably installed at an open end of the open cavity of the lifting shell to form the accommodating chamber with the lifting shell ; the centrifugal drainage assembly is installed on the lifting base body ; the water inlets are arranged in the lifting shell , and the filtering assemblies are arranged on the water inlets of the lifting shell wherein a plurality of spraying openings are arranged in the lifting shell and characterised in that the water inlet filtering portion includes a base body water inlet filtering portion arranged on the lifting base body , and the base body water inlet filtering portion includes a plurality of base body water filtering holes which are arranged in the lifting base body and communicating with the accommodating chamber.