mhurhangee/ep-ind-claims huggingface dataset:
A coating composition comprising: an aqueous dispersion of thermoplastic copolymer particles comprising: (i) 0.5-2.0% by weight of the copolymer of phosphorus-containing monomers, in polymerized form; and (ii) at least 20% by weight of the copolymer of one or more monomers, in polymerized form, selected from the group consisting of ethyl acrylate, methyl acrylate, and combinations thereof; and (iii) up to 79.5% by weight of the copolymer of one or more monoethylenically unsaturated monomers, in polymerized form, excluding monomers (i) and (ii); and one or more opacifying colorants. an aqueous dispersion of thermoplastic copolymer particles comprising: (i) 0.5-2.0% by weight of the copolymer of phosphorus-containing monomers, in polymerized form; and (ii) at least 20% by weight of the copolymer of one or more monomers, in polymerized form, selected from the group consisting of ethyl acrylate, methyl acrylate, and combinations thereof; and (iii) up to 79.5% by weight of the copolymer of one or more monoethylenically unsaturated monomers, in polymerized form, excluding monomers (i) and (ii); and (i) 0.5-2.0% by weight of the copolymer of phosphorus-containing monomers, in polymerized form; and (ii) at least 20% by weight of the copolymer of one or more monomers, in polymerized form, selected from the group consisting of ethyl acrylate, methyl acrylate, and combinations thereof; and (iii) up to 79.5% by weight of the copolymer of one or more monoethylenically unsaturated monomers, in polymerized form, excluding monomers (i) and (ii); and one or more opacifying colorants.
Device for displaying and updating a trajectory pattern which describes the trajectory portion which an aircraft must follow in order to perform a drop over a drop zone on the ground, the device displaying the trajectory pattern regarding the representation of a drop zone, the position, the orientation and/or the shape of the trajectory pattern represented being a function of the position and the orientation of the drop zone and trajectory parameters which define the trajectory of the aircraft; the device comprising at least display means (40, 41) in order to display the pattern and the representation of the drop zone and means (43, 45, 46) for calculating and storing the position data of the pattern and the representation of the drop zone; the display device displaying on the display means control points (21, 22) which define the position, the orientation and the length of the representation of the drop zone, these control points being at least a point Po of origin of the drop zone and a point Pdzw which enables the length and the orientation of the drop zone to be modified by means of the movement thereof, and at least one control point (23, 24, 25) linked to the representation of the drop zone, whose position with respect to the drop zone defines the parameter values of the drop trajectory of the aircraft, the at least one control point consisting of a point Pws which enables the value and orientation of the wind speed to be modified by means of the movement thereof, a point Pgs which enables the speed of the aircraft to be modified by means of the movement thereof or a point Pa which enables the drop altitude of the aircraft to be modified by means of the movement thereof, the variation of the parameter values of the drop trajectory being a function of the movement of control points by means of interaction of an operator with the display device.
A method of a communications device configured for wireless communications, the method comprising: determining a retransmission rate associated with retransmissions of one or more packets by the communications device; determining a measurement associated with an antenna gain of at least one antenna of the communications device; and adjusting a transmission power of the communications device based on the retransmission rate and based on the measurement, wherein the adjusting the transmission power of the communications device comprises: increasing the transmission power of the communications device when the retransmission rate satisfies a first threshold and when the measurement satisfies a second threshold; or decreasing the transmission power of the communications device when the retransmission rate fails to satisfy the first threshold or when the measurement fails to satisfy the second threshold. determining a retransmission rate associated with retransmissions of one or more packets by the communications device; determining a measurement associated with an antenna gain of at least one antenna of the communications device; and adjusting a transmission power of the communications device based on the retransmission rate and based on the measurement, wherein the adjusting the transmission power of the communications device comprises: increasing the transmission power of the communications device when the retransmission rate satisfies a first threshold and when the measurement satisfies a second threshold; or decreasing the transmission power of the communications device when the retransmission rate fails to satisfy the first threshold or when the measurement fails to satisfy the second threshold. increasing the transmission power of the communications device when the retransmission rate satisfies a first threshold and when the measurement satisfies a second threshold; or decreasing the transmission power of the communications device when the retransmission rate fails to satisfy the first threshold or when the measurement fails to satisfy the second threshold.
Aircraft including a fuselage, a wing and a tail assembly, further including at least one thruster having the general shape of a ring, and comprising on the one hand a rotor (3, 4) consisting of an annular element (31, 41) from which the blades (30, 40) protrude outwardly, and on the other hand a base also annular, coaxial with said annular element (31, 41), and on which said annular element (31, 41) can rotate under the action of motor means, said base being coaxial with said fuselage and is integrated in the shell which constitutes it, while the blades (30, 40) of said rotor (3, 4) are disposed externally to said shell, characterised in that the motor means consist of brushless-type toric electric motors, with fixed winding and movable peripheral rotor (31, 41), the stator (5, 6) being incorporated in the fixed base integral with the fuselage and includes coils while said rotor (31, 41) carries the blades (30; 40) and includes on the inner side permanent magnets, and in that said motor means consist of toric electric motors powered by an electricity generator.
A function control method using a mobile terminal, the method comprising: detecting at the mobile terminal a connection of an external display device to the mobile terminal; receiving, from the external display device, a resource of the external display device including information on the screen size of the external display device; outputting a window screen from the mobile terminal to the external display device, the window screen having a size determined based on the acquired information on the screen size of the external display device and including at least one icon representing a pre-registered application corresponding to the resource of the external display device; receiving at the mobile terminal a user input corresponding to a selection of an icon displayed in the window screen on the external display device; and controlling at the mobile terminal, in response to the user input, the execution of an application represented by the selected icon so as to cause a corresponding application execution window to be displayed on the window screen output to the external display device. detecting at the mobile terminal a connection of an external display device to the mobile terminal; receiving, from the external display device, a resource of the external display device including information on the screen size of the external display device; outputting a window screen from the mobile terminal to the external display device, the window screen having a size determined based on the acquired information on the screen size of the external display device and including at least one icon representing a pre-registered application corresponding to the resource of the external display device; receiving at the mobile terminal a user input corresponding to a selection of an icon displayed in the window screen on the external display device; and controlling at the mobile terminal, in response to the user input, the execution of an application represented by the selected icon so as to cause a corresponding application execution window to be displayed on the window screen output to the external display device.
Roller changing apparatus for changing a roller of a multitude of rollers of a furnace for a thermal treatment of components, wherein the roller changing apparatus comprises: a sealable housing in which a first protective gas atmosphere is formable; a roller handling device that is at least partially arranged in the housing and designed for removing the roller to be exchanged from the furnace and for installing a replacement roller at the furnace while essentially maintaining a high temperature and a second protective gas atmosphere in the furnace during the roller exchange, wherein the roller handling device is movable at least partially out from the housing through a lock in a wall of the housing in order to handle the roller to be exchanged, wherein the lock in the wall of the housing comprises at the outside of the housing an attachment fitting that is designed for being attachable to the furnace in such a way that a tight connection, in particular a connection that is gas-tight relative to the surroundings, is producable between an interior of the housing and an interior of the furnace. a sealable housing in which a first protective gas atmosphere is formable; a roller handling device that is at least partially arranged in the housing and designed for removing the roller to be exchanged from the furnace and for installing a replacement roller at the furnace while essentially maintaining a high temperature and a second protective gas atmosphere in the furnace during the roller exchange,
A toothbrush head (60, 110) connected to a toothbrush grip handle to thereby define a head - grip handle longitudinal direction (L-L), the head (60, 110) being elongate in the longitudinal direction and having a width direction (W-W) perpendicular to the longitudinal direction (L-L), the toothbrush head (60, 110) having a bristle surface (65, 66, 67, 122) from which plural tufts of bristles extend in a bristle direction, the bristles being arranged in plural tufts each of which contains plural bristles, the bristles comprising plural tapered bristles and plural non-tapered bristles, and the toothbrush head (60, 110) having a construction in the form of three longitudinally elongate sections (62, 63, 64, 111, 112, 113) disposed widthways adjacent across the toothbrush head, each section being flexibly linked to the handle, and being in the form of two widthways oppositely disposed outer sections (62, 64, 111, 113) with one middle section (63, 112) disposed widthways between said outer sections (62, 64, 111, 113), each section independently resiliently moveable relative to a widthways adjacent section, characterised in that the plural bristle tufts are arranged in a pattern on the bristle surface (65, 66, 67, 122) comprising plural outer tufts (68, 117) containing tapered bristles being disposed on the outer sections (62, 64, 111, 113) and being of a first greater length, and plural inner tufts (69, 118) containing non tapering bristles being disposed on the inner section (63, 112) and being of a second lesser length.
A composition, comprising water, a polyurethane polymer and a water-soluble salt of a chelating agent, said polyurethane polymer having a hydrolyzable group, said polyurethane polymer is a reaction product comprising the following reactive components: Component A) an isocyanate, Component B) a compound having an isocyanate-reactive group, wherein said compound comprises at least one group that can be converted to said hydrolyzable group, and wherein said compound has a melting enthalpy of greater than 15 J/g as measured by DSC-7 from Perkin-Elmer using the first heating curve in a temperature range of from 20 to 100 °C according to DIN65467, optionally Component C) an emulsifier, optionally Component D) a solvent, and optionally Component E) a reactive diluent; the composition, after being dried and formed into a film, or said polyurethane polymer has a melting enthalpy of greater than 15 J/g as measured by DSC using the first heating curve in a temperature range of from 20 to 100 °C according to DIN65467; said water-soluble salt of the chelating agent is present in an amount of from 0.04 to 1.8% by weight, relative to 100% by weight of said polyurethane polymer; and said watersoluble salt of the chelating agent comprises a water-soluble monovalent salt of the chelating agent present in an amount of no less than 30% by weight, relative to 100% by weight of said water-soluble salt of the chelating agent. Component A) an isocyanate, Component B) a compound having an isocyanate-reactive group, wherein said compound comprises at least one group that can be converted to said hydrolyzable group, and wherein said compound has a melting enthalpy of greater than 15 J/g as measured by DSC-7 from Perkin-Elmer using the first heating curve in a temperature range of from 20 to 100 °C according to DIN65467, optionally Component C) an emulsifier, optionally Component D) a solvent, and optionally Component E) a reactive diluent; the composition, after being dried and formed into a film, or said polyurethane polymer has a melting enthalpy of greater than 15 J/g as measured by DSC using the first heating curve in a temperature range of from 20 to 100 °C according to DIN65467; said water-soluble salt of the chelating agent is present in an amount of from 0.04 to 1.8% by weight, relative to 100% by weight of said polyurethane polymer; and said watersoluble salt of the chelating agent comprises a water-soluble monovalent salt of the chelating agent present in an amount of no less than 30% by weight, relative to 100% by weight of said water-soluble salt of the chelating agent.
An expression vector comprising a reporter gene operably linked to the 3' end of a DNA and a second reporter gene different from the first reporter gene and operably linked to the 5' end of the DNA, and wherein the DNA is any one of DNAs of the following (a) to (e): (a) the nucleotide sequence consisting of the nucleotide numbers 1 to 9690, the nucleotide numbers 19134 to 19946, and the nucleotide numbers 23030 to 24448 in SEQ ID NO:1, or (b) the nucleotide sequence consisting of the nucleotide numbers 1 to 19946 and the nucleotide numbers 23030 to 24448 in SEQ ID NO:1,or (c) the nucleotide sequence consisting of the nucleotide numbers 1 to 5658 and the nucleotide numbers 23030 to 24448 in SEQ ID NO:1, or (d) the nucleotide sequence consisting of the nucleotide numbers 1 to 2866 and the nucleotide numbers 23030 to 24448 in SEQ ID NO:1, or (e) the nucleotide sequence consisting of the nucleotide numbers 1 to 2866 and the nucleotide numbers 22167 to 24448 in SEQ ID NO:1 (a) the nucleotide sequence consisting of the nucleotide numbers 1 to 9690, the nucleotide numbers 19134 to 19946, and the nucleotide numbers 23030 to 24448 in SEQ ID NO:1, or (b) the nucleotide sequence consisting of the nucleotide numbers 1 to 19946 and the nucleotide numbers 23030 to 24448 in SEQ ID NO:1,or (c) the nucleotide sequence consisting of the nucleotide numbers 1 to 5658 and the nucleotide numbers 23030 to 24448 in SEQ ID NO:1, or (d) the nucleotide sequence consisting of the nucleotide numbers 1 to 2866 and the nucleotide numbers 23030 to 24448 in SEQ ID NO:1, or (e) the nucleotide sequence consisting of the nucleotide numbers 1 to 2866 and the nucleotide numbers 22167 to 24448 in SEQ ID NO:1
1. Use of boronic acids of the general formula for increasing the storage stability of epoxy resin compositions comprising an epoxy resin, a curing agent for curing the epoxy resin and a curing accelerator for accelerating the curing of the epoxy resin, wherein formula represents: wherein residue R 1 means: R 1 = alkyl, hydroxyalkyl or a residue of formula, wherein formula is: wherein R 2, R 3, R 4 independently of one another mean and at least one residue R 2, R 3, R 4 is not hydrogen: R 2, R 3, R 4 = hydrogen, fluorine, chlorine, bromine, iodine, cyano, C 1 to C 5 alkyl, alkoxy, acyl, alkylsulfonyl, aryl, carboxyl or B 2, wherein the epoxy resin composition comprises, as a curing accelerator, a curing accelerator according to formula, wherein formula is: wherein R 6, R 7, R 8 independently of one another mean: R 6, R 7 = independently of one another hydrogen or C 1 to C 5 alkyl, R 8 = hydrogen, C 1 to C 15 alkyl, C 3 to C 15 cycloalkyl, aryl, alkylaryl, C 1 to C 15 alkyl substituted with -NHC NR 6 R 7, Cato C 15 cycloalkyl substituted with -NHC NR 6 R 7, aryl substituted with -NHC NR 6 R 7 or alkylaryl substituted with -NHC NR 6 R 7. R 1 = alkyl, hydroxyalkyl or a residue of formula, wherein formula is: wherein R 2, R 3, R 4 independently of one another mean and at least one residue R 2, R 3, R 4 is not hydrogen: R 2, R 3, R 4 = hydrogen, fluorine, chlorine, bromine, iodine, cyano, C 1 to C 5 alkyl, alkoxy, acyl, alkylsulfonyl, aryl, carboxyl or B 2, wherein the epoxy resin composition comprises, as a curing accelerator, a curing accelerator according to formula, wherein formula is: wherein R 6, R 7, R 8 independently of one another mean: R 6, R 7 = independently of one another hydrogen or C 1 to C 5 alkyl, R 8 = hydrogen, C 1 to C 15 alkyl, C 3 to C 15 cycloalkyl, aryl, alkylaryl, C 1 to C 15 alkyl substituted with -NHC NR 6 R 7, Cato C 15 cycloalkyl substituted with -NHC NR 6 R 7, aryl substituted with -NHC NR 6 R 7 or alkylaryl substituted with -NHC NR 6 R 7. C 1 to C 15 alkyl substituted with -NHC NR 6 R 7, Cato C 15 cycloalkyl substituted with -NHC NR 6 R 7, aryl substituted with -NHC NR 6 R 7 or alkylaryl substituted with -NHC NR 6 R 7.
An ionization gauge comprising an anode, a cathode, and an electromagnetic wave source, wherein the cathode comprises a first cathode plate, said cathode plate including a first through hole through which the anode passes, a storage portion configured to store the electromagnetic wave source, and a passage (50, 70, 80) arranged between the storage portion and the first through hole, characterised in that the passage (50, 70, 80) is a groove or a slit exposed to a space or a through hole arranged such that the electromagnetic wave generated by the electromagnetic wave source passes through the passage (50, 70, 80) to the first through hole. the cathode comprises a first cathode plate, said cathode plate including a first through hole through which the anode passes, a storage portion configured to store the electromagnetic wave source, and a passage (50, 70, 80) arranged between the storage portion and the first through hole, characterised in that the passage (50, 70, 80) is a groove or a slit exposed to a space or a through hole arranged such that the electromagnetic wave generated by the electromagnetic wave source passes through the passage (50, 70, 80) to the first through hole.
A turbine system comprising: a shaft configured to rotate about a rotational axis; a plurality of blades coupled to the shaft, wherein the blades are oriented with the width (chord) axis of the blades aligned in a radial direction away from the axis, and wherein the blades are configured to provide lift according to the Bernoulli principle resulting from lower pressure on the convex first external surface of the blades than on the non-convex second external surface of the blades, when fluid passes on both sides of the blades, the lift provided in the direction of rotation through portions of the rotation of the blades about the rotational axis on both the windward and leeward sides of the rotational axis; mounting formations which attach the blades to the shaft and suspend the blades away from the shaft, with air flow passages defined between the shaft and the blades; and an air flow director configured to expose the blades to air flow through a first part of rotation of the blades about the rotational axis, and to block air flow to the blades through a second part of the rotation of the blades about the rotational axis; wherein the air flow director is configured and oriented to direct the air flow in part through the air flow passages defined between the shaft and the blades; and characterised in that the air flow director has a convex outer surface located on the leeward side of the blades, with the convex outer surface exposed to the air flow. a shaft configured to rotate about a rotational axis; a plurality of blades coupled to the shaft, wherein the blades are oriented with the width (chord) axis of the blades aligned in a radial direction away from the axis, and wherein the blades are configured to provide lift according to the Bernoulli principle resulting from lower pressure on the convex first external surface of the blades than on the non-convex second external surface of the blades, when fluid passes on both sides of the blades, the lift provided in the direction of rotation through portions of the rotation of the blades about the rotational axis on both the windward and leeward sides of the rotational axis; mounting formations which attach the blades to the shaft and suspend the blades away from the shaft, with air flow passages defined between the shaft and the blades; and an air flow director configured to expose the blades to air flow through a first part of rotation of the blades about the rotational axis, and to block air flow to the blades through a second part of the rotation of the blades about the rotational axis; wherein the air flow director is configured and oriented to direct the air flow in part through the air flow passages defined between the shaft and the blades; and characterised in that the air flow director has a convex outer surface located on the leeward side of the blades, with the convex outer surface exposed to the air flow.