mhurhangee/ep-ind-claims huggingface dataset:
A continuous production device for producing a polymer by solution polycondensation, the device comprising: a reactor main body; one or more divider plates configured to divide an interior of the reactor main body into a plurality of reaction vessels; a raw material supply unit configured to supply a raw material; and a reaction mixture recovery unit configured to recover a reaction mixture, wherein each of the one or more divider plates has a rotation center; gas-phase parts of the reaction vessels adjacent to each other are communicating with each other and liquid-phase parts of the reaction vessels adjacent to each other are communicating with each other; and a reaction mixture generated in at least one of the plurality of reaction vessels sequentially moves through the reaction vessels. a reactor main body; one or more divider plates configured to divide an interior of the reactor main body into a plurality of reaction vessels; a raw material supply unit configured to supply a raw material; and a reaction mixture recovery unit configured to recover a reaction mixture, wherein each of the one or more divider plates has a rotation center; gas-phase parts of the reaction vessels adjacent to each other are communicating with each other and liquid-phase parts of the reaction vessels adjacent to each other are communicating with each other; and a reaction mixture generated in at least one of the plurality of reaction vessels sequentially moves through the reaction vessels.
A silicone compound represented by the following Chemical Structure 1: where Y represents a substituted or non-substituted alkyl group having one to ten carbon atoms, X1, X2, and X3 independently represent methyl groups or any of the following Substituents A-1 to A-4, at least one of X1, X2, and X3 is any of the Substituents A-1 to A-4, and l, m, and n are independently zero or an integer of from 1 to 6, where R1 is a hydrogen atom, an alkyl group having one to four carbon atoms, or an alkoxy group having one to four carbon atoms, where R2 represents a single bonding or an alkylene group having one to four carbon atoms and R3 represents a single bonding or an alkyleneoxy group having one to four carbon atoms, where R2 represents a single bonding or an alkylene group having one to four carbon atoms and R3 represents a single bonding or an alkyleneoxy group having one to four carbon atoms, and where R4 and R5 independently represent hydrogen atoms or methyl groups,
Elastic joint with a drive, an elastic mechanism and an output, wherein the elastic mechanism has a cam disc mechanism with a cam disc and a lever mechanism, wherein the torque can be varied non-linearly by rotating the cam disc in conjunction with at least one spring element, and a first lever arm of a lever is rotatably connected to the cam disc outside its centre point, and a second lever arm of the lever is connected to the output, and the pivot of the lever is coupled to an adjustment mechanism for changing the position of the pivot and thus the rigidity, characterised in that the cam disc has two opposing cut-outs, each with a curve with an inwardly pointing edge, and the cam disc is connected to the lever mechanism, and the at least one spring element engages the edge of at least one of the cut-outs of the cam disc via a roller, and the drive is connected to the cam disc via the at least one spring element and the roller. the elastic mechanism has a cam disc mechanism with a cam disc and a lever mechanism, wherein the torque can be varied non-linearly by rotating the cam disc in conjunction with at least one spring element, and a first lever arm of a lever is rotatably connected to the cam disc outside its centre point, and a second lever arm of the lever is connected to the output, and the pivot of the lever is coupled to an adjustment mechanism for changing the position of the pivot and thus the rigidity, characterised in that the cam disc has two opposing cut-outs, each with a curve with an inwardly pointing edge, and the cam disc is connected to the lever mechanism, and the at least one spring element engages the edge of at least one of the cut-outs of the cam disc via a roller, and the drive is connected to the cam disc via the at least one spring element and the roller.
Mechanical workpiece transfer device intended to be positioned between a workpiece support of a machine tool for processing preferably plate-like workpieces, in particular metal sheets, on the one hand and a workpiece deposit for workpieces originating from the workpiece support of the machine tool on the other, wherein the mechanical workpiece transfer device comprises a wiper device, by means of which the workpieces can be transferred on the workpiece deposit side, characterised in that the mechanical workpiece transfer device comprises a workpiece interim deposit provided for the workpieces, located between the workpiece support of the machine tool and the workpiece deposit when viewed in the direction of the material flow, and for which a lifting device is provided, by means of which the workpiece interim deposit can be lifted to a workpiece support side receiving level and lowered to a workpiece deposit side transfer level, • wherein at least one workpiece can be received by the workpiece interim support raised to the receiving level, and • wherein the workpiece interim support lowered to the transfer level together with the received workpiece and the wiper device can be moved relative to each other with a horizontal wiping movement, the workpiece thus being wiped off the workpiece interim support and transferred on the workpiece deposit side. • wherein at least one workpiece can be received by the workpiece interim support raised to the receiving level, and • wherein the workpiece interim support lowered to the transfer level together with the received workpiece and the wiper device can be moved relative to each other with a horizontal wiping movement, the workpiece thus being wiped off the workpiece interim support and transferred on the workpiece deposit side.
A method (500; 1100) of operating a rotorcraft, the method comprising: operating the rotorcraft in a first mode comprising determining an attitude based on a pilot stick signal generated by a pilot stick assembly, determining an actuator command based on the determined attitude, determining the actuator command comprising using a first dynamic controller having an integrator, and providing an output of the first dynamic controller to an actuator, wherein a translational speed or an attitude of the rotorcraft is proportional to an amplitude of the pilot stick signal in the first mode; transitioning from the first mode to a second mode when the translational speed of the rotorcraft exceeds a first velocity threshold, transitioning comprising fading out a gain of the first dynamic controller over a first period of time (502; 1102), and decreasing an output value of the integrator to zero over a second period of time (504; 1104); and operating the rotorcraft in the second mode comprising providing an output of a rate controller to the actuator, wherein the output of the rate controller is proportional to an amplitude of the pilot stick signal. operating the rotorcraft in a first mode comprising determining an attitude based on a pilot stick signal generated by a pilot stick assembly, determining an actuator command based on the determined attitude, determining the actuator command comprising using a first dynamic controller having an integrator, and providing an output of the first dynamic controller to an actuator, wherein a translational speed or an attitude of the rotorcraft is proportional to an amplitude of the pilot stick signal in the first mode; determining an attitude based on a pilot stick signal generated by a pilot stick assembly, determining an actuator command based on the determined attitude, determining the actuator command comprising using a first dynamic controller having an integrator, and providing an output of the first dynamic controller to an actuator, wherein a translational speed or an attitude of the rotorcraft is proportional to an amplitude of the pilot stick signal in the first mode; transitioning from the first mode to a second mode when the translational speed of the rotorcraft exceeds a first velocity threshold, transitioning comprising fading out a gain of the first dynamic controller over a first period of time (502; 1102), and decreasing an output value of the integrator to zero over a second period of time (504; 1104); and fading out a gain of the first dynamic controller over a first period of time (502; 1102), and decreasing an output value of the integrator to zero over a second period of time (504; 1104); and operating the rotorcraft in the second mode comprising providing an output of a rate controller to the actuator, wherein the output of the rate controller is proportional to an amplitude of the pilot stick signal.
An anticorrosion performance degradation detection device for detecting inclusion of a corrosive factor in a solvent to which a corrosion inhibitor for inhibiting corrosion of an anticorrosion target material is added, the anticorrosion performance degradation detection device characterized by comprising: - a detection electrode that is adapted to react with the corrosion inhibitor dissolved in the solvent to form on a surface thereof an electrode surface coating that inhibits corrosion; - a counter electrode disposed to face the detection electrode with a predetermined distance therebetween; - a power supply that is adapted to apply an AC voltage and a DC voltage between the detection electrode and the counter electrode; and - a sensor that is adapted to measure impedance of the detection electrode in at least a low frequency range and a medium frequency range among the low frequency range, the medium frequency range, and a high frequency range, wherein the power supply is adapted to apply the DC voltage when the impedance in the medium frequency range decreases from a first predetermined value, and to release the applied DC voltage when the impedance in the medium frequency range decreases from a second predetermined value, wherein the sensor is adapted to measure whether the impedance of the detection electrode in the low frequency range decreases from a third predetermined value after the release of the applied DC voltage, wherein the medium frequency range is between 1 Hz and 1 kHz, wherein the low frequency range is less than 1 Hz, and wherein the high frequency range is more than 1 kHz. - a detection electrode that is adapted to react with the corrosion inhibitor dissolved in the solvent to form on a surface thereof an electrode surface coating that inhibits corrosion; - a counter electrode disposed to face the detection electrode with a predetermined distance therebetween; - a power supply that is adapted to apply an AC voltage and a DC voltage between the detection electrode and the counter electrode; and - a sensor that is adapted to measure impedance of the detection electrode in at least a low frequency range and a medium frequency range among the low frequency range, the medium frequency range, and a high frequency range, wherein the power supply is adapted to apply the DC voltage when the impedance in the medium frequency range decreases from a first predetermined value, and to release the applied DC voltage when the impedance in the medium frequency range decreases from a second predetermined value, wherein the sensor is adapted to measure whether the impedance of the detection electrode in the low frequency range decreases from a third predetermined value after the release of the applied DC voltage, wherein the medium frequency range is between 1 Hz and 1 kHz, wherein the low frequency range is less than 1 Hz, and wherein the high frequency range is more than 1 kHz.
A cable tension control apparatus comprising: a surface vessel; a remotely operated underwater vehicle, the ROV comprising a spool and a cable tension control mechanism with a tension sensor; a cable that includes an optical fiber adapted to transmit signals between a controller on the surface vessel and the ROV; a cable storage device coupled to the surface vessel for storing a first portion of the cable; wherein the spool is configured for storing a second portion of the cable; a release mechanism which controls the removal of the second portion of the cable from the spool; and wherein the tension sensor is configured for detecting the tension in the second portion of the cable; wherein the release mechanism is configured to release the second portion of the cable from the spool when the tension sensor detects that the tension in the cable is greater than a predetermined value. a surface vessel; a remotely operated underwater vehicle, the ROV comprising a spool and a cable tension control mechanism with a tension sensor; a cable that includes an optical fiber adapted to transmit signals between a controller on the surface vessel and the ROV; a cable storage device coupled to the surface vessel for storing a first portion of the cable; a release mechanism which controls the removal of the second portion of the cable from the spool; and wherein the tension sensor is configured for detecting the tension in the second portion of the cable; wherein the release mechanism is configured to release the second portion of the cable from the spool when the tension sensor detects that the tension in the cable is greater than a predetermined value.
An image readout method for scanning a light acquisition section which is movable in a main scanning direction and a sub-scanning direction perpendicular to the main scanning direction and which outputs excitation light onto an image carrier and photoelectrically reads out light received from said image carrier carrying image information so as to obtain image data of an image represented by the image information, wherein the image data is structured such that positions of the light acquisition section in the main and sub-scanning direction are associated with pixel positions of the information carried by the image carrier; the method comprising the steps of: obtaining the number of encoder pulses of an encoder module which reads out a linear scale film of the light acquisition section and positioned along the main scanning direction as a comparative pulse number when the light acquisition section is moved from the scanning start position to the scanning end position in the main scanning direction during image readout; and correcting pixel positions in a direction corresponding to the main scanning direction of the image information carried by the image carrier based on the difference between a reference pulse number which is determined in advance and the comparative pulse number. obtaining the number of encoder pulses of an encoder module which reads out a linear scale film of the light acquisition section and positioned along the main scanning direction as a comparative pulse number when the light acquisition section is moved from the scanning start position to the scanning end position in the main scanning direction during image readout; and correcting pixel positions in a direction corresponding to the main scanning direction of the image information carried by the image carrier based on the difference between a reference pulse number which is determined in advance and the comparative pulse number.
Turbomachine extending along an axis, comprising a high-pressure body with a high-pressure compressor coupled in rotation to a high-pressure turbine, and a low-pressure body including a low-pressure compressor coupled in rotation to a low-pressure turbine, an upstream casing located upstream of the high-pressure compressor, and means of suspension (12, 13) for the turbomachine, intended for attaching the turbomachine to an aircraft pylon, the said means of suspension (12, 13) comprising an upstream suspension system with a beam intended to be attached to the pylon, at least two connecting rods (23, 23', 24) spaced apart circumferentially from each other and each articulated at a first end to the beam and at a second end to the upstream casing, a rudder bar articulated on the beam at the level of a circumferentially central zone of said rudder bar, at least two force-recovery rods to take up the thrust forces of the turbomachine, spaced apart circumferentially from each other and each articulated at a first end on the rudder bar and at a second end on a fixed part of the turbomachine, the said at least two force-recovery rods being located upstream of a radial suspension plane defined by the two connecting rods (23, 23'), the means of suspension (12, 13) also comprising a downstream suspension system capable of connecting the pylon to a fixed downstream casing of the turbomachine.
A method of session handoff between a source access system and a target access system comprising: discovering an address of the target access system by an access terminal, AT, in communication with the source access system; utilizing the address to tunnel a secure channel from the AT to a security gateway of the target access system through the source access system, the tunnelling configured for negotiating an air interface session between the AT and the target access system; and transferring signaling associated with the target access system from the AT to the target access system through the secure channel. discovering an address of the target access system by an access terminal, AT, in communication with the source access system; utilizing the address to tunnel a secure channel from the AT to a security gateway of the target access system through the source access system, the tunnelling configured for negotiating an air interface session between the AT and the target access system; and transferring signaling associated with the target access system from the AT to the target access system through the secure channel.
Wind turbine blade comprising at least two hollow blade sectors (1,2) that are joined together by means of a first insert to obtain the wind turbine blade, - wherein first and second sides of the said blade sectors (1,2) comprises at least two external access holes (7, 7) aligned in a direction which is generally perpendicular to the length of the blade; - wherein such first insert is arranged as a double-T beam each one of which horizontal extensions, generally plate-shaped, has a pair of holes (40, 40) on each side with floating nuts (5, 5) embedded therein; - wherein the external access holes (7, 7) in the blade segments (1, 2) are axially aligned with the floating nuts (5, 5); - wherein threaded positioning rods (8, 8), extend through the floating nuts (5, 5); - wherein each of said positioning rods (8, 8) is configured to be rotated from one of said external access holes (7, 7) wherein a rotation of such a rod in a first direction reduces a cross-sectional area of said insert to allow the introduction of said insert into one of said blade sectors (1, 2), while a subsequent rotation of said rod in the opposite direction returns the insert towards its previous position; - wherein inner surfaces in the blade sectors (1, 2) comprise toothed profiles (10, 20) being engaged with tooth-shaped surfaces arranged in the horizontal extensions of the first insert. - wherein first and second sides of the said blade sectors (1,2) comprises at least two external access holes (7, 7) aligned in a direction which is generally perpendicular to the length of the blade; - wherein such first insert is arranged as a double-T beam each one of which horizontal extensions, generally plate-shaped, has a pair of holes (40, 40) on each side with floating nuts (5, 5) embedded therein; - wherein the external access holes (7, 7) in the blade segments (1, 2) are axially aligned with the floating nuts (5, 5); - wherein threaded positioning rods (8, 8), extend through the floating nuts (5, 5); - wherein each of said positioning rods (8, 8) is configured to be rotated from one of said external access holes (7, 7) wherein a rotation of such a rod in a first direction reduces a cross-sectional area of said insert to allow the introduction of said insert into one of said blade sectors (1, 2), while a subsequent rotation of said rod in the opposite direction returns the insert towards its previous position; - wherein inner surfaces in the blade sectors (1, 2) comprise toothed profiles (10, 20) being engaged with tooth-shaped surfaces arranged in the horizontal extensions of the first insert.
A magnetic roll having a rotation axis, the magnetic roll comprising: (a) an axial series of segmented rings, each of said rings' segments comprising a permanent magnet (20, 34) having an outer end (22, 36), an inner end (24, 38), an axial end (26, 40), an oppositely axial end (28, 42), a circumferential end (30, 44), a counter-circumferential end (32, 46), a north pole positioned at the inner (24, 38) or outer end (22, 36), and a south pole positioned oppositely from the north pole; (b) a bonding matrix rigidly interconnecting the rings and segments; and (c) a magnetic armature operatively spanning between the permanent magnets' inner ends (24, 38); wherein a first plurality of magnets among the segmented rings' permanent magnets has outer end north poles having axial and oppositely axial ends, wherein a second plurality of the magnets among the segmented rings' permanent magnets has outer end south poles having axial and oppositely axial ends, characterised in that each outer end north pole circumferentially abuts an outer end south pole, wherein the axial end of said each outer end north pole abuts the oppositely axial end of one of the outer end south poles a and wherein said axial end of said each outer end north pole further abuts the oppositely axial end of another outer end north pole. (a) an axial series of segmented rings, each of said rings' segments comprising a permanent magnet (20, 34) having an outer end (22, 36), an inner end (24, 38), an axial end (26, 40), an oppositely axial end (28, 42), a circumferential end (30, 44), a counter-circumferential end (32, 46), a north pole positioned at the inner (24, 38) or outer end (22, 36), and a south pole positioned oppositely from the north pole; (b) a bonding matrix rigidly interconnecting the rings and segments; and (c) a magnetic armature operatively spanning between the permanent magnets' inner ends (24, 38); wherein a first plurality of magnets among the segmented rings' permanent magnets has outer end north poles having axial and oppositely axial ends, wherein a second plurality of the magnets among the segmented rings' permanent magnets has outer end south poles having axial and oppositely axial ends, characterised in that each outer end north pole circumferentially abuts an outer end south pole, wherein the axial end of said each outer end north pole abuts the oppositely axial end of one of the outer end south poles a and wherein said axial end of said each outer end north pole further abuts the oppositely axial end of another outer end north pole.