mhurhangee/ep-ind-claims huggingface dataset:
A liquid crystal composition that has a negative dielectric anisotropy and contains at least one compound selected from the group of compounds represented by formula as a first component and at least one compound selected from the group of compounds represented by formula as a second component: wherein R 1, R 2, R 3 and R 4 are independently alkyl having 1 to 12 carbons, alkoxy having 1 to 12 carbons or alkenyl having 2 to 12 carbons; ring A is: X 1, X 2, X 3 and X 4 are independently fluorine or chlorine; Z 1 is a single bond, ethylene or methyleneoxy; and, in formula, at least one of two ring A is: or at least one of two Z 1 is methyleneoxy.
Non-aqueous coating material comprising A) a hydroxy-functional polyacrylate resin and B) tris(alkoxycarbonylamino)triazine as crosslinking agent, characterized in that the polyacrylate resin A) comprises secondary hydroxyl groups and has a hydroxyl number of 100 to 200 mg KOH/g and an acid number of 0 to 35 mg KOH/g, a glass transition temperature of -35 to +70°C and a number-average molecular weight of 1500 to 30 000 g/mol. A) a hydroxy-functional polyacrylate resin and B) tris(alkoxycarbonylamino)triazine as crosslinking agent,
A method for producing a silica aerogel blanket, the method comprising the steps of: 1) preparing a silica sol by mixing a silica precursor, alcohol, and an acidic aqueous solution; 2) producing a silica gel composite by adding a basic catalyst to the silica sol, and then depositing the silica sol added with the basic catalyst in a base material for blanket; 3) producing a hydrophobic silica aerogel by aging, surface modifying, and drying the silica gel composite, wherein the surface modifying of Step 3) is performed by adding one or more kinds of surface modifiers selected from the group consisting of trimethylchlorosilane (TMCS), hexamethyldisilazane (HMDS), methyltrimethoxysilane, trimethylethoxysilane, ethyltriethoxysilane, phenyltriethoxysilane, and polydimethylsiloxane; and 4) heat treating the hydrophobic silica aerogel at a temperature of 500 to 800°C. 1) preparing a silica sol by mixing a silica precursor, alcohol, and an acidic aqueous solution; 2) producing a silica gel composite by adding a basic catalyst to the silica sol, and then depositing the silica sol added with the basic catalyst in a base material for blanket; 3) producing a hydrophobic silica aerogel by aging, surface modifying, and drying the silica gel composite, wherein the surface modifying of Step 3) is performed by adding one or more kinds of surface modifiers selected from the group consisting of trimethylchlorosilane (TMCS), hexamethyldisilazane (HMDS), methyltrimethoxysilane, trimethylethoxysilane, ethyltriethoxysilane, phenyltriethoxysilane, and polydimethylsiloxane; and 4) heat treating the hydrophobic silica aerogel at a temperature of 500 to 800°C.
Method for recovering heat for a drying section of a machine for producing a fibrous web, in particular a paper, cardboard or tissue web, the fibrous web being dried at least by way of a steam-heated drying cylinder and at least one high-temperature drying element with hot air with the production of a waste air stream, the at least one drying cylinder being loaded at least partially with fresh steam, the condensate/steam mixture of the at least one drying cylinder being fed to a condensate separating stage, the steam being fed from the condensate separating stage to the fresh steam or to a fresh steam/high-pressure steam mixture (DF, D1), at least part of the condensate from the condensate separating stage which is connected downstream of the at least one drying cylinder being fed to a heat exchanger in the waste air stream of the high-temperature drying element, and the condensate (K1, K2) being heated there and absorbing energy of the waste air, the at least one part of the condensate from the condensate separating stage which is connected downstream of the at least one drying cylinder being evaporated in the heat exchanger either at least partially with the production of a mixture of steam and condensate, preferably completely, or being heated in the heat exchanger and being expanded with at last partial evaporation after exiting from the heat exchanger, and the steam which is produced being fed into a steam line and/or a steam vessel, characterized in that the steam line and/or the steam vessel can be connected at least indirectly to at least two steam consumers (V1, V2, V3, V4, V5, V6), and the steam line and/or the steam vessel are/is connected selectively to at least one of the steam consumers (V1, V2, V3, V4, V5, V6).
A method of separating or extracting a phosphorylated tyrosine,or peptide or protein containing phosphorylated tyrosine wherein the method comprises providing a molecularly imprinted polymer by providing at least one monomer exhibiting selective affinity for phosphorylated tyrosine groups, wherein the monomer is selected from 1,3-disubstituted urea or thiourea, 1,3-diarylsubstituted urea or thiourea, at least one template wherein the template is a single amino acid derivative selected from a N- and/or O-protected phosphotyrosine or a salt thereof, and at least one cross-linker, forming a pre-polymerization mixture, and polymerizing said pre-polymerization mixture; removing said template; contacting said molecularly imprinted polymer with a mixture containing at least one phosphorylated tyrosine, or peptide, protein containing phosphorylyated tyrosine or a mixture thereof, and capturing the at least one phosphorylated tyrosine, or peptide, protein containing phosphorylyated tyrosine or a mixture thereof by the molecularly imprinted polymer; wherein the phosphorylated tyrosine, peptide or protein containing phosphorylated tyrosine is selectively extracted or separated over peptides or proteins with other phosphorylated or non-phosphorylated amino acid side chains.
A computer-implemented method for detecting damage to a gas turbine engine having a fan and a plurality of turbine stages including a low pressure turbine stage, the fan being drivably coupled to the low pressure turbine stage, the method comprising: receiving a first signal indicative of a speed of rotation of the fan; receiving a second signal indicative of a speed of rotation (N1T) of the low pressure turbine stage; determining, based on the first signal and the second signal, a difference metric (ΔN) representative of a difference between the speed of rotation of the fan and the speed of rotation (N1T) of the low pressure turbine stage; and determining whether a damage event has occurred based on whether the difference metric (ΔN) passes a threshold (TH, TH1, TH2); characterised by: determining an approximate impact energy associated with a damage event based on a magnitude of the difference metric (ΔN); and categorising the damage event as one of a plurality of different possible types of damage event based on the determined approximate impact energy. receiving a first signal indicative of a speed of rotation of the fan; receiving a second signal indicative of a speed of rotation (N1T) of the low pressure turbine stage; determining, based on the first signal and the second signal, a difference metric (ΔN) representative of a difference between the speed of rotation of the fan and the speed of rotation (N1T) of the low pressure turbine stage; and determining whether a damage event has occurred based on whether the difference metric (ΔN) passes a threshold (TH, TH1, TH2); determining an approximate impact energy associated with a damage event based on a magnitude of the difference metric (ΔN); and categorising the damage event as one of a plurality of different possible types of damage event based on the determined approximate impact energy.
A battery case shaping apparatus (100, 200, 300) comprising: a punch (110, 210, 310, 410, 510) configured to press a laminate sheet (101, 201, 301) in order to shape a battery case; a die (120, 220, 320) in which an accommodation portion (121, 221, 321) is formed, the accommodation portion (121, 221, 321) having a size corresponding to an electrode assembly receiving portion that is shaped by the punch (110, 210, 310, 410, 510); a holder (130, 230, 330) configured to fix an outer periphery of the laminate sheet; and an elastic separator (140, 240, 340) located under the punch in order to prevent direct contact between the punch (110, 210, 310, 410, 510) and the laminate sheet (101, 201, 301), characterized in that the elastic separator (140, 240, 340) is fixed to the holder (130, 230, 330). a punch (110, 210, 310, 410, 510) configured to press a laminate sheet (101, 201, 301) in order to shape a battery case; a die (120, 220, 320) in which an accommodation portion (121, 221, 321) is formed, the accommodation portion (121, 221, 321) having a size corresponding to an electrode assembly receiving portion that is shaped by the punch (110, 210, 310, 410, 510); a holder (130, 230, 330) configured to fix an outer periphery of the laminate sheet; and an elastic separator (140, 240, 340) located under the punch in order to prevent direct contact between the punch (110, 210, 310, 410, 510) and the laminate sheet (101, 201, 301), characterized in that the elastic separator (140, 240, 340) is fixed to the holder (130, 230, 330).
An unloading device comprising a body having side walls (91, 92), a back wall extending between the side walls and a front opening between the side walls, a rotatable mixer extending between the side walls, one or more rotatable pre-mixers (10, 11, 12) extending between the side walls and located between said rotatable mixer and said front opening, a rotary feeder, a rotatable feeder screw, and a rotatable post-mixer located between said rotatable feeder screw and said rotary feeder, wherein the unloading device is characterized in that it comprises one or more independently controllable motors (71, 72) for rotating said one or more rotatable pre-mixers (10, 11, 12), an independently controllable motor for rotating said rotatable mixer, an independently controllable motor for rotating said post-mixer, and a remote controller configured to control said independently controllable motors (71, 72, 73, 74). a body having side walls (91, 92), a back wall extending between the side walls and a front opening between the side walls, a rotatable mixer extending between the side walls, one or more rotatable pre-mixers (10, 11, 12) extending between the side walls and located between said rotatable mixer and said front opening, a rotary feeder, a rotatable feeder screw, and a rotatable post-mixer located between said rotatable feeder screw and said rotary feeder, one or more independently controllable motors (71, 72) for rotating said one or more rotatable pre-mixers (10, 11, 12), an independently controllable motor for rotating said rotatable mixer, an independently controllable motor for rotating said post-mixer, and a remote controller configured to control said independently controllable motors (71, 72, 73, 74).
A rope having improved cyclic bend over sheave (CBOS) fatigue resistance, said rope comprising high tenacity fibers, said rope and/or said fibers being coated with a composition, characterised by the composition comprising an amino functional silicone resin and a neutralized low molecular weight polyethylene.
Film comprising a carrier substrate, an adhesion layer for applying the film to a target substrate and at least one electrically conductive layer, wherein the at least one electrically conductive layer forms an electrical functional structure in a functional region, wherein the at least one electrically conductive layer forms at least one contacting structure for contacting the electrical functional structure in at least one contacting region, and wherein the adhesion layer does not cover the at least one contacting region at least in certain regions when viewed perpendicularly to a plane spanned by the carrier substrate or wherein the adhesion layer is applied over the entire surface when viewed perpendicularly to a plane spanned by the carrier substrate, wherein the at least one electrically conductive layer is arranged between the carrier substrate and the adhesion layer or the adhesion layer is arranged on the side of the carrier substrate, said side facing away from the at least one electrically conductive layer and wherein the adhesion layer is arranged on the surface of the film, wherein the adhesion layer consists of a material that is highly transparent after application to the target substrate, and the adhesion layer is formed from a hot adhesive or an adhesive that can be cured by radiation. wherein the adhesion layer is arranged on the surface of the film, wherein the adhesion layer consists of a material that is highly transparent after application to the target substrate, and the adhesion layer is formed from a hot adhesive or an adhesive that can be cured by radiation.
A method of controlling a wind turbine comprising a tower supporting a rotor comprising a plurality of pitch-adjustable rotor blades, the method comprising: obtaining a movement signal indicative of a lateral movement of the tower; determining a pitch modulation signal, based on the movement signal, for actuating a rotor blade to produce a desired horizontal force (F x) component to counteract the lateral movement of the tower; characterized in that the method further comprises: determining a radial force component (F radial) acting on a rotor blade; determining a phase offset parameter for the rotor blade based on the radial force component; and, transforming the pitch modulation signal into a pitch reference offset signal (θ 1, θ 2, θ 3) for the rotor blade based on the phase offset parameter. obtaining a movement signal indicative of a lateral movement of the tower; determining a pitch modulation signal, based on the movement signal, for actuating a rotor blade to produce a desired horizontal force (F x) component to counteract the lateral movement of the tower; characterized in that the method further comprises: determining a radial force component (F radial) acting on a rotor blade; determining a phase offset parameter for the rotor blade based on the radial force component; and, transforming the pitch modulation signal into a pitch reference offset signal (θ 1, θ 2, θ 3) for the rotor blade based on the phase offset parameter. determining a radial force component (F radial) acting on a rotor blade; determining a phase offset parameter for the rotor blade based on the radial force component; and, transforming the pitch modulation signal into a pitch reference offset signal (θ 1, θ 2, θ 3) for the rotor blade based on the phase offset parameter.
A process for determining a rig-state of a drill rig during a wellbore drilling operation, the process comprising: a. acquiring surface-derived input data streams from a plurality of sensors associated with a wellbore; b. formatting the acquired data for sample and bandwidth regularization; c. time-correcting the data to provide isochronously sampled data from the plurality of sensors; d. processing the acquired data through a processing graph of networked mathematical operators that apply continuous analytics to the data as rapidly as the data are acquired to determine dynamic conditions of a plurality of rig operations associated with the wellbore; and e. determining a rig-state from the plurality of rig operations conditions; characterized in that step b. includes regularizing sampling to account for variable sample rates from the sensors and regularizing bandwidth to account for variable resolution of the sensors; and step e. comprises a sample-by-sample automated categorization of ongoing rig operations computed from the input data streams to incorporate knowledge of rig state for each data sample. a. acquiring surface-derived input data streams from a plurality of sensors associated with a wellbore; b. formatting the acquired data for sample and bandwidth regularization; c. time-correcting the data to provide isochronously sampled data from the plurality of sensors; d. processing the acquired data through a processing graph of networked mathematical operators that apply continuous analytics to the data as rapidly as the data are acquired to determine dynamic conditions of a plurality of rig operations associated with the wellbore; and e. determining a rig-state from the plurality of rig operations conditions; step b. includes regularizing sampling to account for variable sample rates from the sensors and regularizing bandwidth to account for variable resolution of the sensors; and step e. comprises a sample-by-sample automated categorization of ongoing rig operations computed from the input data streams to incorporate knowledge of rig state for each data sample.
A glazed panel device for a building, comprising: - at least one outer glazed wall, - at least one inner glazed wall, - a frame for attaching said outer glazed wall and said inner glazed wall to a structure of said building, said attachment frame forming a cavity between said outer glazed wall and said inner glazed wall, - at least said outer glazed wall being inclined relative to a longitudinal median plane of said device, - said cavity converging toward an edge of said device, - at least one cell communicating with said cavity at said edge and leading to an opening toward the outer wall, said cell being provided with at least one acoustic insulation, characterized in that it comprises: - at least one sound and/or thermal shield (8, 9), - said at least one shield (8, 9) being installed at the upper and/or lower part of said frame, - said at least one shield (8, 9) being oriented toward the center of said device, according to a slope that flares out relative to said longitudinal median plane of said device. - at least one outer glazed wall, - at least one inner glazed wall, - a frame for attaching said outer glazed wall and said inner glazed wall to a structure of said building, said attachment frame forming a cavity between said outer glazed wall and said inner glazed wall, - at least said outer glazed wall being inclined relative to a longitudinal median plane of said device, - said cavity converging toward an edge of said device, - at least one cell communicating with said cavity at said edge and leading to an opening toward the outer wall, said cell being provided with at least one acoustic insulation, - at least one sound and/or thermal shield (8, 9), - said at least one shield (8, 9) being installed at the upper and/or lower part of said frame, - said at least one shield (8, 9) being oriented toward the center of said device, according to a slope that flares out relative to said longitudinal median plane of said device.
A rotor mechanism of a rotating electrical machine that includes a core obtained by stacking a plurality of disc-shaped magnetic steel plates on an outer circumference of a rotor shaft and disc-shaped end plates (2, 3) arranged on both sides of the core in an axial direction, wherein the rotor shaft includes a crimp groove that is formed in an outer circumferential portion of the rotor shaft in a circumferential direction, the crimp groove being on an outside in the axial direction than any one of the end plates (2, 3), the outside being away from a support region of the core, and the inside being the opposite side of the outside, the one end plate is located in the axial direction by an inside end of a crimp retainer in the axial direction that is ring-shaped, that covers the crimp groove of the rotor shaft to fit to the rotor shaft, that is fitted into the crimp groove of the rotor shaft by crimping an outside portion of the crimp retainer in the axial direction from an outer circumferential side and that engages with a wall surface of the crimp groove on the outside in the axial direction, and characterised in that the crimp retainer includes, in the outside portion of the crimp retainer in the axial direction, slits that extend from an outside end portion of the crimp retainer in the axial direction to an inside in the axial direction.
A robotic surgical instrument comprising: a shaft; an articulated section extending from the shaft and terminating at its distal end in a tip (601, 801), the tip (601, 801) having an attachment (602, 802) for an end effector, where the attachment (602, 802) is connected to the tip (601, 801) by a roll joint; and a drive mechanism configured to drive the articulated section via flexible driving elements (611, 612, 613, 811, 812, 813) thereby altering the angular orientation of the tip (601, 801) relative to the shaft, wherein the drive mechanism is configured to be controlled so as to always fully compress the articulated section along at least one extent at an exterior edge of the articulated section by which the articulated section connects the tip (601, 801) and the shaft such that the articulated section always has its shortest length along said at least one extent whilst driving the articulated section from any one configuration to any other configuration, wherein the drive mechanism constrains movement of the articulated section so as to permit the tip (601, 801) to move with two degrees of rotational freedom and no degrees of translational freedom relative to the shaft. a shaft; an articulated section extending from the shaft and terminating at its distal end in a tip (601, 801), the tip (601, 801) having an attachment (602, 802) for an end effector, where the attachment (602, 802) is connected to the tip (601, 801) by a roll joint; and a drive mechanism configured to drive the articulated section via flexible driving elements (611, 612, 613, 811, 812, 813) thereby altering the angular orientation of the tip (601, 801) relative to the shaft, wherein the drive mechanism is configured to be controlled so as to always fully compress the articulated section along at least one extent at an exterior edge of the articulated section by which the articulated section connects the tip (601, 801) and the shaft such that the articulated section always has its shortest length along said at least one extent whilst driving the articulated section from any one configuration to any other configuration, wherein the drive mechanism constrains movement of the articulated section so as to permit the tip (601, 801) to move with two degrees of rotational freedom and no degrees of translational freedom relative to the shaft.