mhurhangee/ep-ind-claims huggingface dataset:
Device for adjusting the length of a suspension cord for hanging a tackle under a gantry, which comprises: - an adjustment casing comprising at least one surface (36S, 36I) for pinching a segment of a cord extending generally vertically through the adjustment casing; and - a locking flange -- which comprises means for the fastening thereof at a free end of the cord; -- and which, in the assembled position in the adjustment casing, is movably mounted in relation to adjustment casing between: i) a position for adjusting the position of the adjustment casing along the cord; and ii) a locking position wherein the locking flange clamps a segment of the cord against the pinching surface (36S, 36I). - an adjustment casing comprising at least one surface (36S, 36I) for pinching a segment of a cord extending generally vertically through the adjustment casing; and - a locking flange -- which comprises means for the fastening thereof at a free end of the cord; -- and which, in the assembled position in the adjustment casing, is movably mounted in relation to adjustment casing between: i) a position for adjusting the position of the adjustment casing along the cord; and ii) a locking position wherein the locking flange clamps a segment of the cord against the pinching surface (36S, 36I). -- which comprises means for the fastening thereof at a free end of the cord; -- and which, in the assembled position in the adjustment casing, is movably mounted in relation to adjustment casing between: i) a position for adjusting the position of the adjustment casing along the cord; and ii) a locking position wherein the locking flange clamps a segment of the cord against the pinching surface (36S, 36I). i) a position for adjusting the position of the adjustment casing along the cord; and ii) a locking position wherein the locking flange clamps a segment of the cord against the pinching surface (36S, 36I).
A method of adaptively removing airflow distortions in a turbine engine having an air inlet duct prior to the compressor stage, the distortions being caused at least in part by the interaction of air flow with the air inlet duct, the method comprising the steps of: determining the distortion in the airflow; positioning a plurality of correction vanes based at least upon the determined distortion, each of the plurality of correction vanes being oriented to a respective angle of incidence when at a temperature approximately equal a respective local temperature; and exposing the airflow to the plurality of correction vanes. determining the distortion in the airflow; positioning a plurality of correction vanes based at least upon the determined distortion, each of the plurality of correction vanes being oriented to a respective angle of incidence when at a temperature approximately equal a respective local temperature; and exposing the airflow to the plurality of correction vanes.
A cordless handheld ultrasonic device, comprising: a drive circuit, comprising: a direct current power source; at least one boost converter in series with the power source; a square wave driver in series with the boost converter; a capacitor and an inductor connected in series with the square wave driver for converting a square wave to a sinusoidal wave; and a piezoelectric transducer in series with the capacitor and the inductor, the piezoelectric transducer connectable to a load and having a capacitance, a resonance frequency, and a 3rd harmonic mode of vibration; a phase-locked loop coupled to the drive circuit and configured to synchronize drive voltage to the resonance frequency of the piezoelectric transducer when the piezoelectric transducer is connected to the load; and a frequency limiting circuit coupled to the phase-locked loop and configured to prevent the phase-locked loop from exceeding the resonant frequency of the piezoelectric transducer; wherein the capacitor and the inductor are selected to have a resonance frequency higher than the resonance frequency of the piezoelectric transducer and less than the 3 rd harmonic mode of vibration of the piezoelectric transducer. a drive circuit, comprising: a direct current power source; at least one boost converter in series with the power source; a square wave driver in series with the boost converter; a capacitor and an inductor connected in series with the square wave driver for converting a square wave to a sinusoidal wave; and a piezoelectric transducer in series with the capacitor and the inductor, the piezoelectric transducer connectable to a load and having a capacitance, a resonance frequency, and a 3rd harmonic mode of vibration; a direct current power source; at least one boost converter in series with the power source; a square wave driver in series with the boost converter; a capacitor and an inductor connected in series with the square wave driver for converting a square wave to a sinusoidal wave; and a piezoelectric transducer in series with the capacitor and the inductor, the piezoelectric transducer connectable to a load and having a capacitance, a resonance frequency, and a 3rd harmonic mode of vibration; a phase-locked loop coupled to the drive circuit and configured to synchronize drive voltage to the resonance frequency of the piezoelectric transducer when the piezoelectric transducer is connected to the load; and a frequency limiting circuit coupled to the phase-locked loop and configured to prevent the phase-locked loop from exceeding the resonant frequency of the piezoelectric transducer; wherein the capacitor and the inductor are selected to have a resonance frequency higher than the resonance frequency of the piezoelectric transducer and less than the 3 rd harmonic mode of vibration of the piezoelectric transducer.
A pharmaceutical coating obtained from film-forming coating compositions based on copolymers of N,N-diethylaminoethyl methacrylate and methyl methacrylate in the weight ratio of the monomers of 35:65 to 55:45, where the copolymers are present partially neutralized to 2 to 15 mol% with C 3 -C 10 -dicarboxylic acids.
An incretin-insulin conjugate comprising an incretin peptide; and an insulin agonist peptide, wherein the conjugate has agonist activity at both the insulin receptor and the corresponding incretin receptor and the incretin peptide is linked to the insulin peptide via a linear chain spacer of 5 to 10 atoms, wherein the spacer comprises the general structure of Formula II: wherein R 1, R 2, R 3 and R 4 are independently selected from the group consisting of H and CH 3, n is 0 or 1, and m is 1, 2 or 3, wherein the carboxy terminus of the incretin peptide is linked to the N-terminus of the insulin peptide via the disulfide moiety of Formula II.
A method for determining a local hot gas temperature in a hot gas duct downstream a combustion device, the method comprising extracting at least one flue gas sample at at least one specific cross-sectional location of the hot gas duct downstream the combustion device, characterized in determining at least one flue gas species concentration in the sample, and determining the local flue gas total temperature based upon the at least one flue gas species concentration.
An apparatus for producing reinforcement elements, in particular for shoes, bags or orthopedic applications, comprising a first powder application apparatus having a first powder container for an at least partially meltable powder mixture, for providing a powder mixture on a feeding device and, provided at an outlet of the powder container, a template for defining a basic shape of a reinforcing element to be produced, a first compounding means arranged downstream of the first powder application apparatus for compounding the powder mixture provided in the basic shape on the feeding device, a second powder application apparatus arranged downstream of the first compounding means and having a second powder container for an at least partially meltable powder mixture, for providing a powder mixture at least partially on the basic shape with the aid of a template provided at an outlet of the second powder container for defining a preliminary final shape of a reinforcing element to be produced, and a second compounding means arranged downstream of the second powder application apparatus for compounding the powder mixture provided in the preliminary final shape on the feeding device, characterized in that between the first powder application apparatus and the first compounding means and/or between the first compounding means and the second powder application apparatus, an arrangement apparatus for arranging intermediate elements, such as storage elements, electronic components, fabric, textile fabric, 3D-grids or the like, are provided. a first powder application apparatus having a first powder container for an at least partially meltable powder mixture, for providing a powder mixture on a feeding device and, provided at an outlet of the powder container, a template for defining a basic shape of a reinforcing element to be produced, a first compounding means arranged downstream of the first powder application apparatus for compounding the powder mixture provided in the basic shape on the feeding device, a second powder application apparatus arranged downstream of the first compounding means and having a second powder container for an at least partially meltable powder mixture, for providing a powder mixture at least partially on the basic shape with the aid of a template provided at an outlet of the second powder container for defining a preliminary final shape of a reinforcing element to be produced, and a second compounding means arranged downstream of the second powder application apparatus for compounding the powder mixture provided in the preliminary final shape on the feeding device, characterized in that between the first powder application apparatus and the first compounding means and/or between the first compounding means and the second powder application apparatus, an arrangement apparatus for arranging intermediate elements, such as storage elements, electronic components, fabric, textile fabric, 3D-grids or the like, are provided.
A shaft arrangement for transferring torques acting about a rotation axis, having a variably adjustable torsional rigidity acting about the rotation axis, comprising a first shaft section on which at least one torsion element is fitted in a torsionally and axially fixed manner, which torsion element transfers the torques and is formed and/or mounted so as to be dimensionally stable transverse to the rotation axis, a second shaft section which is axially spaced apart from the first shaft section and on which the at least one torsion element is fitted in a rotationally fixed and axially movable manner, and a means which is or can be brought into an operative connection with the second shaft section and by means of which the second shaft section can be axially moved relative to the first shaft section and to the at least one torsion element, characterized in that the first shaft section is connected to a drive and the second shaft section serves as an inertia that is stationary with respect to the first shaft section, that the first and second shaft sections (1, 2) are arranged within a hollow shaft, and that first shaft section is connected to the hollow shaft in a torsionally and axially fixed manner and the second shaft section is mounted spaced apart from the hollow shaft.
A method for transmitting beam information by a user equipment, UE, in a wireless communication system, the method comprising: detecting (S3310, S3410) a beam failure, BF, for one or more secondary cells among a plurality of secondary cells configured for the UE; and transmitting (S3320, S3420), to a base station, BS, the beam information including indication information related to the BF detection for each of the plurality of secondary cells, wherein the indication information is 2 bit information, wherein the indication information includes one indication among a first indication, a second indication, a third indication, and a fourth indication for each of the plurality of secondary cells, and wherein the first indication is for no beam failure, the second indication is for beam failure with new beam identification and reporting, the third indication is for beam failure with new beam identification and no reporting, and the fourth indication is for beam failure with new beam identification failure, wherein the reporting indicated by the second indication indicates that a new beam information for the new beam identification is reported, and wherein the no reporting indicated in the third indication indicates that the new beam information for the new beam identification is not reported due to insufficient resources of a physical uplink shared channel, PUSCH, allocated by the BS. detecting (S3310, S3410) a beam failure, BF, for one or more secondary cells among a plurality of secondary cells configured for the UE; and transmitting (S3320, S3420), to a base station, BS, the beam information including indication information related to the BF detection for each of the plurality of secondary cells, wherein the indication information is 2 bit information, wherein the indication information includes one indication among a first indication, a second indication, a third indication, and a fourth indication for each of the plurality of secondary cells, and wherein the first indication is for no beam failure, the second indication is for beam failure with new beam identification and reporting, the third indication is for beam failure with new beam identification and no reporting, and the fourth indication is for beam failure with new beam identification failure, wherein the reporting indicated by the second indication indicates that a new beam information for the new beam identification is reported, and wherein the no reporting indicated in the third indication indicates that the new beam information for the new beam identification is not reported due to insufficient resources of a physical uplink shared channel, PUSCH, allocated by the BS.
A reduced-pressure treatment system for treating a tissue site on a patient, the reduced-pressure system comprising: a reduced-pressure interface, comprising: a conduit housing having a cavity divided by a dividing wall into a reduced-pressure-application region and a pressure-detection region; a reduced-pressure port disposed within the reduced-pressure-application region; a pressure-detection port disposed within the pressure-detection region; a base connected to the conduit housing, the base having a manifold-contacting surface; wherein the dividing wall includes a surface substantially coplanar with the manifold-contacting surface; and at least one channel disposed in the manifold-contacting surface, the at least one channel adapted to transmit reduced pressure from the reduced-pressure-application region to the pressure-detection region. a reduced-pressure interface, comprising: a conduit housing having a cavity divided by a dividing wall into a reduced-pressure-application region and a pressure-detection region; a reduced-pressure port disposed within the reduced-pressure-application region; a pressure-detection port disposed within the pressure-detection region; a base connected to the conduit housing, the base having a manifold-contacting surface; wherein the dividing wall includes a surface substantially coplanar with the manifold-contacting surface; and at least one channel disposed in the manifold-contacting surface, the at least one channel adapted to transmit reduced pressure from the reduced-pressure-application region to the pressure-detection region. a conduit housing having a cavity divided by a dividing wall into a reduced-pressure-application region and a pressure-detection region; a reduced-pressure port disposed within the reduced-pressure-application region; a pressure-detection port disposed within the pressure-detection region; a base connected to the conduit housing, the base having a manifold-contacting surface; wherein the dividing wall includes a surface substantially coplanar with the manifold-contacting surface; and at least one channel disposed in the manifold-contacting surface, the at least one channel adapted to transmit reduced pressure from the reduced-pressure-application region to the pressure-detection region.
A method of producing transformed cells of a rubber-producing plant, the method comprising the following steps a) to e): a) culturing a tissue fragment from a rubber-producing plant in a medium containing a plant growth hormone to obtain a 5.0 mm or smaller mass of cultured cells; b) dispersing the cultured cells obtained in step a) and a whisker in a liquid and then adhering the whisker to the cultured cells by centrifugation; followed by c) damaging the cultured cells by the whisker under sonication and introducing a foreign gene into the cells; followed by d) restoring the damaged cells without removing the whisker; followed by e) screening transformed cells with an antibiotic, wherein the antibiotic used in step e) is kanamycin at a concentration of 10 mg/L or lower, and wherein the rubber-producing plant is at least one selected from the group consisting of plants of the genera Hevea, Taraxacum, and Parthenium. a) culturing a tissue fragment from a rubber-producing plant in a medium containing a plant growth hormone to obtain a 5.0 mm or smaller mass of cultured cells; b) dispersing the cultured cells obtained in step a) and a whisker in a liquid and then adhering the whisker to the cultured cells by centrifugation; followed by c) damaging the cultured cells by the whisker under sonication and introducing a foreign gene into the cells; followed by d) restoring the damaged cells without removing the whisker; followed by e) screening transformed cells with an antibiotic,
A seal system between a row of buckets supported on a turbine machine rotor and a surrounding stationary casing (118, 218, 318) comprising: a tip shroud secured at radially outer tips of each of the buckets, said tip shroud formed with a radially-projecting rail; a cellular seal structure adapted to be supported in said stationary casing in radial opposition to said tip shroud and said rail, said seal structure having an annular array of axially orientated individual cells (138, 610, 616) formed to provide continuous, substantially axial horizontal flow passages devoid of any radial obstruction along substantially an entire axial length dimension of said cellular seal structure, characterised in that said radially projecting rail is adapted to cut a groove in said cellular seal structure during transient operating conditions of the turbine machine, so that, when the groove is cut into the cellular structure, gas leakage flow, once it crosses over said radially projecting rail, will flow along said substantially axial flow passages and be prevented from turning radially inward into the main gas flow, wherein said annular array of individual cells (610, 616) is formed by plural walls (612, 614) intersecting at substantially 45 degree angles, such that said individual cells are substantially diamond-shaped in cross section, wherein at least some cell wall portions downstream of said bucket are angled radially outwardly to substantially align with a surface of a turbine diffuser extending in a downstream direction, so as to align the gas leakage flow with the angle of the diffuser. a tip shroud secured at radially outer tips of each of the buckets, said tip shroud formed with a radially-projecting rail; a cellular seal structure adapted to be supported in said stationary casing in radial opposition to said tip shroud and said rail, said seal structure having an annular array of axially orientated individual cells (138, 610, 616) formed to provide continuous, substantially axial horizontal flow passages devoid of any radial obstruction along substantially an entire axial length dimension of said cellular seal structure, characterised in that said radially projecting rail is adapted to cut a groove in said cellular seal structure during transient operating conditions of the turbine machine, so that, when the groove is cut into the cellular structure, gas leakage flow, once it crosses over said radially projecting rail, will flow along said substantially axial flow passages and be prevented from turning radially inward into the main gas flow, wherein said annular array of individual cells (610, 616) is formed by plural walls (612, 614) intersecting at substantially 45 degree angles, such that said individual cells are substantially diamond-shaped in cross section, wherein at least some cell wall portions downstream of said bucket are angled radially outwardly to substantially align with a surface of a turbine diffuser extending in a downstream direction, so as to align the gas leakage flow with the angle of the diffuser.
An article having a substrate that is an ester-linked poly(ether-block-amide) polymer, the substrate is coated with a lubricious coating and the coating is a polymerized composition, wherein the composition comprises at least one polyfunctional ethylenically unsaturated monomer, which is a compound having two or more ethylenically unsaturated groups thereon that may be readily polymerized by a radical mechanism to produce a polymer, and a polyvinylpyrrolidone polymer, and said polyvinylpyrrolidone polymer is free of photoinitiator groups thereon.
A ring-shaped or columnar catalyst, which is used at the time of producing a corresponding unsaturated carboxylic acid by causing gas-phase catalytic oxidation of an unsaturated aldehyde and an oxygen-containing gas, wherein an outer peripheral edge part is inclined at an angle from 45 to 85° relative to a center line; a ratio (a/b) of an outside diameter a (mm) to a bottom part diameter b (mm) is 2.35 to 3.5, a ratio (H/b) of a straight body part length H (mm) to the bottom part diameter b (mm) is 1.35 or more and 2.5 or less, the straight body part length H (mm) is from 2 to 11 mm, and the outside diameter a (mm) is from 2 to 7 mm; and wherein the bottom part diameter is the diameter of the bottom part where the inclination is ended, wherein the catalyst contains at least molybdenum and vanadium and is represented by formula Mo a V b Cu c Sb d Si e X f Y g Z h O i X is at least one element selected from the group consisting of Nb and W; Y is at least one element selected from the group consisting of Mg, Ca, Sr, Ba and Zn; Z is at least one element selected from the group consisting of Fe, Co, Ni and Bi, a to h represent a ratio of numbers of atoms of respective elements and when a=12, 0<b≤12, 0<c≤12, 0≤d≤500, 0≤e≤500, 0≤f≤12, 0≤g≤8, and 0≤h≤500; and i is a numerical value satisfying the oxidation state of other elements. a ratio (a/b) of an outside diameter a (mm) to a bottom part diameter b (mm) is 2.35 to 3.5, a ratio (H/b) of a straight body part length H (mm) to the bottom part diameter b (mm) is 1.35 or more and 2.5 or less, the straight body part length H (mm) is from 2 to 11 mm, and the outside diameter a (mm) is from 2 to 7 mm; and wherein the bottom part diameter is the diameter of the bottom part where the inclination is ended, wherein the catalyst contains at least molybdenum and vanadium and is represented by formula Mo a V b Cu c Sb d Si e X f Y g Z h O i X is at least one element selected from the group consisting of Nb and W; Y is at least one element selected from the group consisting of Mg, Ca, Sr, Ba and Zn; Z is at least one element selected from the group consisting of Fe, Co, Ni and Bi, a to h represent a ratio of numbers of atoms of respective elements and when a=12, 0<b≤12, 0<c≤12, 0≤d≤500, 0≤e≤500, 0≤f≤12, 0≤g≤8, and 0≤h≤500; and i is a numerical value satisfying the oxidation state of other elements.