mhurhangee/ep-ind-claims huggingface dataset:
Use of polymers based on ethylenically unsaturated monomers in carpet coating compositions for the manufacture of carpets, characterized in that the carpet coating compositions are prepared using one or more polymers based on ethylenically unsaturated monomers in the form of water-redispersible powders, wherein the polymers are selected from the group comprising copolymers of one or more vinyl esters with 1 to 50 wt% of ethylene; copolymers of vinyl acetate with 1 to 50 wt% of ethylene and 1 to 50 wt% of one or more further comonomers from the group of vinyl esters having 1 to 13 carbon atoms in the carboxylic acid moiety; copolymers of one or more vinyl esters, 1 to 50 wt% of ethylene and 1 to 60 wt% of (meth)acrylic ester of branched or unbranched alcohols having 1 to 15 carbon atoms; copolymers with 30 to 75 wt% of vinyl acetate, 1 to 35 wt% of vinyl laurate or vinyl ester of an alpha-branched carboxylic acid having 9 to 13 carbon atoms, and also 1 to 30 wt% of (meth)acrylic ester of branched or unbranched alcohols having 1 to 17 carbon atoms which additionally contain 1 to 40 wt% of ethylene; copolymers with one or more vinyl esters, 1 to 50 wt% of ethylene and 1 to 60 wt% of vinyl chloride and also optionally further vinyl esters and/or (meth)acrylic esters; wherein the recitations in wt% add up to 100 wt% in each case.
Chemical compound that imitate the steroid system and contain a sulfamate moiety, the compound defined by the general formula 1: wherein R 1 = H or F or CF 3 or OCF 3; R 2 = H or F or CF 3 or Cl or Br or I or CH 3 or OCH 3 or Et or iPr or NO 2; R 3 = H or F or CF 3 or OCF 3; R 4 = H or F or CF 3 or Cl or Br or I or CH 3 or OCH 3; R 5 = H or F or CF 3.
A test rig for dynamic test assignments on internal combustion engines having a preferably electrical drive and/or loading device which is coupled to a control device for adapting and controlling setpoint values for a speed and a torque characteristic, characterized in that the control device can be adapted in terms of adjusting the weighting of speed control to torque control.
A process for manufacturing a biocide and/or bactericidal material comprising: (i) preparing a solution of at least one arylazide functionalized-photosensitizer which is a porphyrin; (ii) contacting the solution obtained at step (i) and a unmodified support selected from paper, cotton fabrics or polyethylene, thereby resulting in depositing the arylazide functionalized-photosensitizer on the support; and (iii) covalently grafting by an insertion reaction, the arylazide functionalized-photosensitizer deposited on the support at step (ii), said insertion reaction being carried out by a thermal activation and/or a UV irradiation activation; wherein the UV irradiation activation of the insertion reaction is carried out at a wavelength ranging from 300 nm to 380 nm. (i) preparing a solution of at least one arylazide functionalized-photosensitizer which is a porphyrin; (ii) contacting the solution obtained at step (i) and a unmodified support selected from paper, cotton fabrics or polyethylene, thereby resulting in depositing the arylazide functionalized-photosensitizer on the support; and (iii) covalently grafting by an insertion reaction, the arylazide functionalized-photosensitizer deposited on the support at step (ii), said insertion reaction being carried out by a thermal activation and/or a UV irradiation activation; wherein the UV irradiation activation of the insertion reaction is carried out at a wavelength ranging from 300 nm to 380 nm.
An adapter module for attaching to the support plate of a meter panel installation having fastening bars (meter cross support), with a fastening and contacting arrangement, comprising a meter support plate, for an electronic electricity meter, and also with a holding arrangement (9; 10) for additional equipment, wherein means (11 - 15) for coupling the holding arrangement (9; 10) to the fastening and contacting arrangement are provided on the fastening and contacting arrangement and/or the holding arrangement (9; 10), characterised in that the fastening and contacting arrangement comprises a terminal bar for electric cables, for which a covering which can be sealed by sealing the electronic electricity meter is provided, and the coupling means (11 - 15) are arranged on the fastening and contacting arrangement such that they are accessible when the covering is sealed.
A light emitting device system comprising power supply terminals and a remote control signal receiver, the power supply terminals being adapted for receiving electrical power from a driver, the remote control signal receiver being adapted for receiving a remote control signal, characterized in - that the power supply terminals being adapted for receiving electrical power from an external driver; and - that the light emitting device system is further adapted for forwarding the received remote control signal as remote control signal information to the external driver, exclusively via the power supply terminals and/or via wireless transmission. - that the power supply terminals being adapted for receiving electrical power from an external driver; and - that the light emitting device system is further adapted for forwarding the received remote control signal as remote control signal information to the external driver, exclusively via the power supply terminals and/or via wireless transmission.
Air inlet device for an air inlet duct to an engine of an aircraft, the air inlet device having: a frame; a centre tube, which extends in an airflow direction; a plurality of air guide arrangements, which extend between the frame and the centre tube; characterized in that an air guide arrangement has an inlet plate, a first pivot plate, a second pivot plate, a third pivot plate and an outlet plate; the inlet plate and the first pivot plate are pivotably connected to each other via a first pivot axis; the first pivot plate and the second pivot plate are pivotably connected to each other via a second pivot axis; the second pivot plate and the third pivot plate are pivotably connected to each other via a third pivot axis; the third pivot plate and the outlet plate are pivotably connected to each other via a fourth pivot axis; the first pivot axis, the second pivot axis, the third pivot axis and the fourth pivot axis run such that they intersect at a common intersection point located on a central axis of the air inlet device. a frame; a centre tube, which extends in an airflow direction; a plurality of air guide arrangements, which extend between the frame and the centre tube; characterized in that an air guide arrangement has an inlet plate, a first pivot plate, a second pivot plate, a third pivot plate and an outlet plate; the inlet plate and the first pivot plate are pivotably connected to each other via a first pivot axis; the first pivot plate and the second pivot plate are pivotably connected to each other via a second pivot axis; the second pivot plate and the third pivot plate are pivotably connected to each other via a third pivot axis; the third pivot plate and the outlet plate are pivotably connected to each other via a fourth pivot axis; the first pivot axis, the second pivot axis, the third pivot axis and the fourth pivot axis run such that they intersect at a common intersection point located on a central axis of the air inlet device.
Plastics line with at least one layer consisting of the following components: 70-94 weight percent of a polyamide selected from the group consisting of: polyamide 516, polyamide 616, polyamide 1016, or mixtures thereof; 4-20 weight percent impact modifier; 2-15 weight percent of plasticiser; 0-5 weight percent of additives different from and, wherein the sum of - is 100 weight percent, and with the proviso that said layer does not contain polyamide 6. 70-94 weight percent of a polyamide selected from the group consisting of: polyamide 516, polyamide 616, polyamide 1016, or mixtures thereof; 4-20 weight percent impact modifier; 2-15 weight percent of plasticiser; 0-5 weight percent of additives different from and,
A gas turbine engine, comprising: a low pressure spool having a low pressure compressor and a low pressure turbine connected by a low pressure shaft; a reduction gear train having a sun gear, a carrier having a plurality of planet gears attached thereto, and a ring gear, wherein the sun gear is connected to the low pressure shaft, and the carrier or the ring gear provides an output drive; a single propulsive fan mounted fore of the gear train and at the front of the engine; a fan shafting arrangement comprising a fan support shaft and a fan shaft, the fan shaft being connected to the output drive of the gear train; the gas turbine engine being characterised in that: the fan support shaft passes freely through the sun gear so as to have no direct contact therewith and as such passes through the centre of the gear train along the axis of rotation of the gearbox and fan; and the fan support shaft is rotatably supported by at least one fore bearing located forward of the gear train, and at least one aft bearing located aft of the gear train. a low pressure spool having a low pressure compressor and a low pressure turbine connected by a low pressure shaft; a reduction gear train having a sun gear, a carrier having a plurality of planet gears attached thereto, and a ring gear, wherein the sun gear is connected to the low pressure shaft, and the carrier or the ring gear provides an output drive; a single propulsive fan mounted fore of the gear train and at the front of the engine; a fan shafting arrangement comprising a fan support shaft and a fan shaft, the fan shaft being connected to the output drive of the gear train; the gas turbine engine being characterised in that: the fan support shaft passes freely through the sun gear so as to have no direct contact therewith and as such passes through the centre of the gear train along the axis of rotation of the gearbox and fan; and the fan support shaft is rotatably supported by at least one fore bearing located forward of the gear train, and at least one aft bearing located aft of the gear train. the fan support shaft passes freely through the sun gear so as to have no direct contact therewith and as such passes through the centre of the gear train along the axis of rotation of the gearbox and fan; and the fan support shaft is rotatably supported by at least one fore bearing located forward of the gear train, and at least one aft bearing located aft of the gear train.
A reversible cold rolling method comprising: a coil building-up step (S0201 to S0608) of sequentially unwinding strips from a plurality of coils to be subjected to a rolling step and joining the strips together by welding to build up a coil; a reversible rolling step (S1101 to S4407) of subjecting a strip unwound from the buildup coil to reversible rolling a predetermined number of times by a cold rolling mill (1, 1a, 1b); and a cutting step (S4103, S4302 to S4304, S4701, S4105, S4307 to S4309, S4702, S4107, S4312 to S4314, and S4703) of cutting the coil in a final pass of the reversible rolling step to desired strip lengths to form a plurality of coils, the steps being performed on a rolling pass line, characterized in that the buildup coil has a coil outside diameter of not more than φ3000 mm, a rolling speed at the cold rolling mill (1, 1a, 1b) in the cutting step (S4103, S4302 to S4304, S4701, S4105, S4307 to S4309, S4702, S4107, S4312 to S4314, and S4703) is more than 0 mpm and not more than 50 mpm, and in the final pass of the reversible rolling step and the cutting step, the buildup coil is wound and the coils after the cutting are carried out, by use of one of the winding/unwinding devices (3, 4) used in the reversible rolling step. '
A fuel pipe for an aircraft, the fuel pipe comprising a wall made of a material including: a matrix composed of an epoxy copolymer obtained through the reaction of a resin of the bisphenol A diglycidyl ether type with an amine hardener, and from 3 to 5 % of an organically modified nanoclay by weight of the epoxy copolymer, the nanoclay including layered magnesium aluminum silicate platelets; and reinforcing fibers embedded in the matrix. a matrix composed of an epoxy copolymer obtained through the reaction of a resin of the bisphenol A diglycidyl ether type with an amine hardener, and from 3 to 5 % of an organically modified nanoclay by weight of the epoxy copolymer, the nanoclay including layered magnesium aluminum silicate platelets; and an epoxy copolymer obtained through the reaction of a resin of the bisphenol A diglycidyl ether type with an amine hardener, and from 3 to 5 % of an organically modified nanoclay by weight of the epoxy copolymer, the nanoclay including layered magnesium aluminum silicate platelets; and reinforcing fibers embedded in the matrix.
A propeller blade root airflow system for an aircraft propulsion system, the airflow system comprising: a spinner for shrouding a propeller hub and a plurality of propeller roots; a plurality of root holes disposed about a circumference of the spinner for receiving propeller roots; and a plurality of airflow ducts disposed about a circumference of the spinner for drawing air into the spinner and away from the root holes; wherein the airflow ducts of the plurality of airflow ducts are interspersed between root holes of the plurality of root holes; characterised by an air intake inlet positioned at a nose of the spinner; and wherein each airflow duct of the plurality of airflow ducts comprises a NACA air intake duct. a spinner for shrouding a propeller hub and a plurality of propeller roots; a plurality of root holes disposed about a circumference of the spinner for receiving propeller roots; and a plurality of airflow ducts disposed about a circumference of the spinner for drawing air into the spinner and away from the root holes; wherein the airflow ducts of the plurality of airflow ducts are interspersed between root holes of the plurality of root holes; characterised by an air intake inlet positioned at a nose of the spinner; and wherein each airflow duct of the plurality of airflow ducts comprises a NACA air intake duct.
Method of removing built up scale in a conduit of a geothermal plant, in which conduit a fluid comprising mineralized water is flowing and in which conduit the built up scale to be removed comprises an aluminosilicate scale, the method comprising treating the fluid in the conduit by alternately injecting into the conduit upstream of the location where it is desired to remove the scale an acid composition and a caustic composition, wherein treating is carried out without stopping the fluid flow in the conduit, and wherein the caustic composition comprises 1-40 wt.% alkali, 0.5-30 wt.% chelator, and 0.0-20 wt.% surfactant.
A humidifying device (10, 20) for humidifying a gas, with the water vapour contained in air, comprising: a hollow fiber bundle (14, 24) formed by bundling a plurality of hollow fibers (14a, 24a) permeable by water vapour, the hollow fibers being orientated in a direction of a predetermined axis; a housing (12, 22) having a space for accommodating the hollow fiber bundle (14, 24) therein, and having an introduction port (12a, 22a) for the gas to be humidified, communicating to bores of the hollow fibers (14a, 24a), a discharging port (12b, 22b) for the gas to be humidified, communicating to the bores of the hollow fibers (14a, 24a), an air inlet (12c, 22c) communicating to a space in the housing (12, 22) external of the hollow fibers (14a, 24a) to introduce the outside air, and an air exit (12d, 22d) communicating to the space in the housing (12, 22) external of the hollow fibers (14a, 24a); and characterized in that a fan (16, 26) is arranged at the air inlet of the housing (12, 22) for introducing the outside air into the housing (12, 22), and a ratio between a sum of the cross-sectional areas of the hollow fibers (14a, 24a) taken along a plane perpendicular to the axis, and the cross-sectional area of an air passage, is set within a range from 0.1 to 0.7, the cross-sectional area of the air passage being obtained by subtracting the sum (ΣS hy) of the cross-sectional areas of the hollow fibers (14a, 24a) from the cross-sectional area (S ap) of the space of the housing (12, 22) taken along a plane perpendicular to the axis. a hollow fiber bundle (14, 24) formed by bundling a plurality of hollow fibers (14a, 24a) permeable by water vapour, the hollow fibers being orientated in a direction of a predetermined axis; a housing (12, 22) having a space for accommodating the hollow fiber bundle (14, 24) therein, and having an introduction port (12a, 22a) for the gas to be humidified, communicating to bores of the hollow fibers (14a, 24a), a discharging port (12b, 22b) for the gas to be humidified, communicating to the bores of the hollow fibers (14a, 24a), an air inlet (12c, 22c) communicating to a space in the housing (12, 22) external of the hollow fibers (14a, 24a) to introduce the outside air, and an air exit (12d, 22d) communicating to the space in the housing (12, 22) external of the hollow fibers (14a, 24a); and characterized in that a fan (16, 26) is arranged at the air inlet of the housing (12, 22) for introducing the outside air into the housing (12, 22), and a ratio between a sum of the cross-sectional areas of the hollow fibers (14a, 24a) taken along a plane perpendicular to the axis, and the cross-sectional area of an air passage, is set within a range from 0.1 to 0.7, the cross-sectional area of the air passage being obtained by subtracting the sum (ΣS hy) of the cross-sectional areas of the hollow fibers (14a, 24a) from the cross-sectional area (S ap) of the space of the housing (12, 22) taken along a plane perpendicular to the axis.
A method for identifying an application scenario of a terminal device, comprising: analyzing an application program running on a terminal device by means of compilation to obtain characteristic data of the application program, wherein the application program includes one or more functions, the one or more functions are compiled, and the characteristic data of an application program refers to the one or more functions that are included in the application program; and determining, from a scenario characteristic data set according to the characteristic data of the application program, application scenario information corresponding to the characteristic data of the application program, wherein the scenario characteristic data set is determined in advance, stored in a file or a database, and comprises a correspondence between multiple types of application scenario information and characteristic data of multiple application programs, and the application scenario information corresponding to the characteristic data of the application program is used to indicate an application scenario currently used for the terminal device. analyzing an application program running on a terminal device by means of compilation to obtain characteristic data of the application program, wherein the application program includes one or more functions, the one or more functions are compiled, and the characteristic data of an application program refers to the one or more functions that are included in the application program; and determining, from a scenario characteristic data set according to the characteristic data of the application program, application scenario information corresponding to the characteristic data of the application program, wherein the scenario characteristic data set is determined in advance, stored in a file or a database, and comprises a correspondence between multiple types of application scenario information and characteristic data of multiple application programs, and the application scenario information corresponding to the characteristic data of the application program is used to indicate an application scenario currently used for the terminal device.
Computer-implemented method for detecting the position of at least one sought notable point (VL, VP, CO) of an ophthalmic lens provided with temporary markings (11, 12, 13, 14, 15) that indicate notable points (VL, VP, CO) of this lens, characterized in that it comprises: - a step of acquiring an image of the temporary markings (11, 12, 13, 14, 15) of the ophthalmic lens, - a step of reading a register each record of which comprises data representative of the arrangement of the temporary markings (31, 32, 33, 34, 35) of a referenced type of ophthalmic lenses, to find a corresponding record the arrangement of the temporary markings (31, 32, 33, 34, 35) of which corresponds, with a certain level of correspondence, to the arrangement of some at least of the temporary markings (11, 12, 13, 14, 15) of the ophthalmic lens the image of which was acquired; and - a step of determining the position of said at least one sought notable point (VL, VP, CO) depending on the match between the temporary markings (11, 12, 13, 14, 15) of the ophthalmic lens and the data representative of the arrangement of the temporary markings (31, 32, 33, 34, 35) of the referenced type of ophthalmic lenses of the corresponding record, and in that, to find the corresponding record, for each read record of the register, a level of correspondence between the arrangement of the temporary markings (31, 32, 33, 34, 35) of this read record and the arrangement of all the temporary markings (11, 12, 13, 14, 15) of the ophthalmic lens the image of which was acquired is determined. - a step of acquiring an image of the temporary markings (11, 12, 13, 14, 15) of the ophthalmic lens, - a step of reading a register each record of which comprises data representative of the arrangement of the temporary markings (31, 32, 33, 34, 35) of a referenced type of ophthalmic lenses, to find a corresponding record the arrangement of the temporary markings (31, 32, 33, 34, 35) of which corresponds, with a certain level of correspondence, to the arrangement of some at least of the temporary markings (11, 12, 13, 14, 15) of the ophthalmic lens the image of which was acquired; and - a step of determining the position of said at least one sought notable point (VL, VP, CO) depending on the match between the temporary markings (11, 12, 13, 14, 15) of the ophthalmic lens and the data representative of the arrangement of the temporary markings (31, 32, 33, 34, 35) of the referenced type of ophthalmic lenses of the corresponding record, and
A disc for use in industrial applications comprising two annular plates connected to one another at an angle around corresponding outer peripheral edges such that corresponding inner peripheral edges of the plates are spaced apart from one another, characterised in that each plate comprises one or more integral ribs extending substantially radially between its inner edge and outer edge formed from folds in the annular plate.