mhurhangee/ep-ind-claims huggingface dataset:
A process comprising the steps of: a) contacting under emulsion polymerization conditions a first portion of an acrylic monomer with a first portion of a phosphorus acid monomer to form a first stage polymer; and b) contacting the first stage polymer with a second portion of an acrylic monomer and a second portion of a phosphorus acid monomer under emulsion polymerization conditions to form a latex polymer; wherein the amount of the first portion of the phosphorus acid monomer is from 2 to 8 weight percent of the weight of the first stage polymer; the weight of the second portion of the phosphorus acid monomer is from 15 to 40 weight percent of the weight of the first portion of phosphorus acid monomer; the first portion of the acrylic monomer is from 5 to 50 weight percent of the first and second portions of acrylic monomer; with the proviso that the monomers are selected so that the T g of the latex polymer is in the range of -20 to 50 °C. a) contacting under emulsion polymerization conditions a first portion of an acrylic monomer with a first portion of a phosphorus acid monomer to form a first stage polymer; and b) contacting the first stage polymer with a second portion of an acrylic monomer and a second portion of a phosphorus acid monomer under emulsion polymerization conditions to form a latex polymer; wherein the amount of the first portion of the phosphorus acid monomer is from 2 to 8 weight percent of the weight of the first stage polymer; the weight of the second portion of the phosphorus acid monomer is from 15 to 40 weight percent of the weight of the first portion of phosphorus acid monomer; the first portion of the acrylic monomer is from 5 to 50 weight percent of the first and second portions of acrylic monomer; with the proviso that the monomers are selected so that the T g of the latex polymer is in the range of -20 to 50 °C.
A method, comprising: forming a build-up layer on an adhesion layer of a carrier; pressing more than one semiconductor dies into the build-up layer, each of the semiconductor die having been previously functionally tested and having wide pads to facilitate the testing, each pad being at least 40 μm wide, wherein at least some of the wide pads on a same die are spaced apart a minimal distance permitted by said die's manufacturing process; forming a mold over the semiconductor dies; detaching the build-up layer from the carrier; removing the build-up layer over the at least some of the wide pads to form via openings over the at least some of the wide pads; forming a metallization layer on the build-up layer, the metallization layer filling the via openings; and patterning the metallization to form lands over the filled via openings and more than one wiring traces of metallization between respective lands of the at least some of the wide pads. forming a build-up layer on an adhesion layer of a carrier; pressing more than one semiconductor dies into the build-up layer, each of the semiconductor die having been previously functionally tested and having wide pads to facilitate the testing, each pad being at least 40 μm wide, wherein at least some of the wide pads on a same die are spaced apart a minimal distance permitted by said die's manufacturing process; forming a mold over the semiconductor dies; detaching the build-up layer from the carrier; removing the build-up layer over the at least some of the wide pads to form via openings over the at least some of the wide pads; forming a metallization layer on the build-up layer, the metallization layer filling the via openings; and patterning the metallization to form lands over the filled via openings and more than one wiring traces of metallization between respective lands of the at least some of the wide pads.
An aircraft landing gear assembly for an aircraft, comprising: a nose gear and a main landing gear, at least one of the nose gear or the main landing gear comprising: a nonrotational base portion configured to connect to an airframe of the aircraft; a wheel connected to and rotatable with respect to the base portion about a rotational axis; at least one stator connected to the base portion; at least one rotor connected to the wheel and configured to rotate with respect to said at least one stator; wherein each of said stator and said rotor is configured to generate a magnetic flux for causing interaction of the magnetic fluxes of said at least one stator and said at least one rotor; characterized in that the landing gear assembly is configured for, due to said interaction, steering the aircraft by converting electrical energy to rotational torque energy of two or more wheels differentially or in opposite directions; the two or more wheels each having at least one rotor connected to the wheel. a nose gear and a main landing gear, at least one of the nose gear or the main landing gear comprising: a nonrotational base portion configured to connect to an airframe of the aircraft; a wheel connected to and rotatable with respect to the base portion about a rotational axis; at least one stator connected to the base portion; at least one rotor connected to the wheel and configured to rotate with respect to said at least one stator; wherein each of said stator and said rotor is configured to generate a magnetic flux for causing interaction of the magnetic fluxes of said at least one stator and said at least one rotor; characterized in that the landing gear assembly is configured for, due to said interaction, steering the aircraft by converting electrical energy to rotational torque energy of two or more wheels differentially or in opposite directions; the two or more wheels each having at least one rotor connected to the wheel. a nonrotational base portion configured to connect to an airframe of the aircraft; a wheel connected to and rotatable with respect to the base portion about a rotational axis; at least one stator connected to the base portion; at least one rotor connected to the wheel and configured to rotate with respect to said at least one stator; wherein each of said stator and said rotor is configured to generate a magnetic flux for causing interaction of the magnetic fluxes of said at least one stator and said at least one rotor; characterized in that the landing gear assembly is configured for, due to said interaction, steering the aircraft by converting electrical energy to rotational torque energy of two or more wheels differentially or in opposite directions; the two or more wheels each having at least one rotor connected to the wheel.
A method of adaptive modulation in a wireless communication system, the wireless communication system including first and second transceivers operable to transmit and receive signals over a communication channel using a plurality of modulation modes, comprising: receiving a first signal transmitted using OFDM over the communication channel from the first transceiver to the second transceiver; determining, from measurements of the communication channel, a first channel equalisation characteristic being the frequency domain response of an OFDM equaliser for receiving the first signal at the second transceiver; the method being characterised by: determining, from the first channel equalisation characteristic, a second channel equalisation characteristic being the frequency response of a tapped delay line equaliser for Single Carrier; determining a measure of a difference between the second channel equalisation characteristic and the first channel equalisation characteristic; and selecting Single Carrier for transmission over the communication channel from the first transceiver at least in part in dependence on said measure. receiving a first signal transmitted using OFDM over the communication channel from the first transceiver to the second transceiver; determining, from measurements of the communication channel, a first channel equalisation characteristic being the frequency domain response of an OFDM equaliser for receiving the first signal at the second transceiver; the method being characterised by: determining, from the first channel equalisation characteristic, a second channel equalisation characteristic being the frequency response of a tapped delay line equaliser for Single Carrier; determining a measure of a difference between the second channel equalisation characteristic and the first channel equalisation characteristic; and selecting Single Carrier for transmission over the communication channel from the first transceiver at least in part in dependence on said measure. determining, from the first channel equalisation characteristic, a second channel equalisation characteristic being the frequency response of a tapped delay line equaliser for Single Carrier; determining a measure of a difference between the second channel equalisation characteristic and the first channel equalisation characteristic; and selecting Single Carrier for transmission over the communication channel from the first transceiver at least in part in dependence on said measure.
An implantable device, comprising: a flexible cable comprising a lead-in part, a stimulation part and a connection part between the lead-in part and the stimulation part; a circuit chip fixed to a surface of one side of the lead-in part and electrically connected to the lead-in part; characterised by a fluid adhesion layer adhered to an outer side of the circuit chip and an outer side of the lead-in part; and a vapor deposited layer directly deposited on an outer side of the fluid adhesion layer. a flexible cable comprising a lead-in part, a stimulation part and a connection part between the lead-in part and the stimulation part; a circuit chip fixed to a surface of one side of the lead-in part and electrically connected to the lead-in part; characterised by a fluid adhesion layer adhered to an outer side of the circuit chip and an outer side of the lead-in part; and a vapor deposited layer directly deposited on an outer side of the fluid adhesion layer.
A method for measuring a feature of an object, the method comprising: taking a representation of at least the feature on the object comprising multiple data points in a three-dimensional measurement space, acquired via surface measurement of at least the feature; fitting a model substantially replicating at least the feature of the object to the representation, the model comprising parameters defining at least two independently alterable portions (62, 64) that each replicate a different region on the surface of the object and that are linked along a common edge, said fitting comprising changing the form of the model by altering at least one of the at least two independently alterable portions; and obtaining information regarding at least the feature from the fitted model. taking a representation of at least the feature on the object comprising multiple data points in a three-dimensional measurement space, acquired via surface measurement of at least the feature; fitting a model substantially replicating at least the feature of the object to the representation, the model comprising parameters defining at least two independently alterable portions (62, 64) that each replicate a different region on the surface of the object and that are linked along a common edge, said fitting comprising changing the form of the model by altering at least one of the at least two independently alterable portions; and obtaining information regarding at least the feature from the fitted model.
A water-based ink composition containing an extender part and a pigment base part, characterized in that a binder in the extender part is a combination of a lignin, at least one acrylic resin and at least one co-resin, wherein said co-resin is selected from the group consisting of polyamides, polyurethanes, polyurethane-acrylic copolymers, polyvinylalcohol resins, polyvinylacetates, sulfopolyesters resins, styrene-butadiene rubbers, ethylene-acrylic acid copolymers, perfluoropolyethers resins, polyolefins and chlorinated polyolefins.
A motor car chair for a child, mounted on a motor car seat, comprising a base where clamping catches and a shell bottom seat are positioned, said bottom seat comprising internal belts for a child said belts having two shoulder segments extending within the space of the bottom seat intended for a child and passing to the other side of the bottom seat and there being linked with a tensioning belt that passes through a tensioner, and in the space of the bottom seat intended for a child a connecting crotch element provided with a internal belt clamp, a fastening part of a connecting crotch element is provided with a handle positioned at the opposite side of the bottom seat than a side of the bottom seat intended for a child, characterized in that the tensioner of the belts of the chair is provided with a connector, where the handle of the fastening part of the connecting crotch element and the connector of the tensioner are coupled with clamping catches of the base of the chair upon setting of the bottom seat on the base.
A lighting system with reduced standby power, the lighting system comprising: a lighting device; a main control unit to receive a lighting control signal from an external device and to control the lighting device according to the lighting control signal; a driver connected to the lighting device to supply power to the lighting device; and an AC-DC converting circuit to supply power to the driver, wherein the main control unit comprises: a lighting control unit to control the power supplied to the lighting device; a power control unit; a standby power supply unit to supply standby power to the power control unit in a standby mode; and characterised in that the power control unit is adapted to periodically check a voltage of the standby power supply unit in the standby mode and to charge the standby power supply unit when the voltage of the standby power supply unit is less than a predetermined level. a lighting device; a main control unit to receive a lighting control signal from an external device and to control the lighting device according to the lighting control signal; a driver connected to the lighting device to supply power to the lighting device; and an AC-DC converting circuit to supply power to the driver, wherein the main control unit comprises: a lighting control unit to control the power supplied to the lighting device; a power control unit; a standby power supply unit to supply standby power to the power control unit in a standby mode; and characterised in that the power control unit is adapted to periodically check a voltage of the standby power supply unit in the standby mode and to charge the standby power supply unit when the voltage of the standby power supply unit is less than a predetermined level. a lighting control unit to control the power supplied to the lighting device; a power control unit; a standby power supply unit to supply standby power to the power control unit in a standby mode; and characterised in that the power control unit is adapted to periodically check a voltage of the standby power supply unit in the standby mode and to charge the standby power supply unit when the voltage of the standby power supply unit is less than a predetermined level.
Bolt lock device, comprising a lockable sliding bolt with a first and a second bolt end and a corresponding bolt guide, characterised in that the sliding bolt of the bolt lock device comprises a locking device fixed at the first locking end, wherein the sliding bolt and the locking device are arranged such that they can be actuated in a slidable manner together in the interior of an in particular tubular bolt guide, wherein at least the locking device is encompassed by the bolt guide in each bolt position.
A yarn winding device comprising: a yarn supplying section adapted to supply a yarn; a winding section adapted to wind the yarn into a package, the winding section including a winding drum adapted to make contact with an outer peripheral surface of the package (p) and rotate; and a yarn running speed detecting section adapted to detect a yarn running speed of the yarn running between the yarn supplying section and the winding section; characterized in that the yarn winding device further comprises an error detecting section adapted to calculate a speed ratio by dividing the yarn running speed by a circumferential speed of the winding drum, and to detect presence/absence of a winding error based on the speed ratio. a yarn supplying section adapted to supply a yarn; a winding section adapted to wind the yarn into a package, the winding section including a winding drum adapted to make contact with an outer peripheral surface of the package (p) and rotate; and a yarn running speed detecting section adapted to detect a yarn running speed of the yarn running between the yarn supplying section and the winding section; characterized in that the yarn winding device further comprises an error detecting section adapted to calculate a speed ratio by dividing the yarn running speed by a circumferential speed of the winding drum, and to detect presence/absence of a winding error based on the speed ratio.
Household appliance, comprising a drawer, a user interface element used to select and / or to display a program or parameters of a selected program and a light group comprising a plurality of light elements, said light elements being disposed substantially peripherally with respect to said user interface element, characterized in that said light group is arranged on a side of said user interface element opposite to said drawer, whereby on the side of the user interface element opposite to said light group, only said drawer is visible to a user, and whereby no light elements are arranged between the drawer and the user interface element, whereby the illumination of a respective light element of said light group depends on an operative / positional state of said user interface element.
A cycloidal marine propulsion unit, comprising: a main rotary body having a central axis; a mounting body for supporting the rotary body on a hull of a marine vessel such that the rotary body is rotatable about said central axis with respect to the hull; at least two blades (3, 3') extending axially from the rotary body away from the hull, when in use, for rotation with the rotary body about the central axis, wherein each blade (3, 3') is mounted for pivotal movement with respect to the rotary body, about respective blade axes generally parallel to the central axis, a drive arrangement comprising at least two electrical blade motors each associated to a respective blade for pivoting thereof, each blade motor being operationally coupled to a respective blade drive for actuating the corresponding blade motor, and a rotary coupling being arranged to provide electrical power transmission between the rotary body and the remaining marine vessel, characterized in that the at least two blade drives each comprise a respective blade drive power converter operationally coupled to a first common intermediate DC-link, and wherein the at least two blade drives are configured to feed power from the first common intermediate DC-link to their respective blade motors, and to feed regenerative power from their respective blade motors to the first common intermediate DC-link. a main rotary body having a central axis; a mounting body for supporting the rotary body on a hull of a marine vessel such that the rotary body is rotatable about said central axis with respect to the hull; at least two blades (3, 3') extending axially from the rotary body away from the hull, when in use, for rotation with the rotary body about the central axis, wherein each blade (3, 3') is mounted for pivotal movement with respect to the rotary body, about respective blade axes generally parallel to the central axis, a drive arrangement comprising at least two electrical blade motors each associated to a respective blade for pivoting thereof, each blade motor being operationally coupled to a respective blade drive for actuating the corresponding blade motor, and a rotary coupling being arranged to provide electrical power transmission between the rotary body and the remaining marine vessel, characterized in that the at least two blade drives each comprise a respective blade drive power converter operationally coupled to a first common intermediate DC-link, and wherein the at least two blade drives are configured to feed power from the first common intermediate DC-link to their respective blade motors, and to feed regenerative power from their respective blade motors to the first common intermediate DC-link.
Use in an electrochemical process of an aqueous solution comprising a methanesulfonic acid and low concentrations of low-valent sulfur compounds and higher-valent sulfur compounds that are susceptible to reduction, wherein the total concentration of reduced sulfur compounds is less than 5 mg/liter, and wherein said low-valent sulfur compounds and higher-valent sulfur compounds are chosen from methylmethanethiosulfonate (MMTS) and trichloromethylsulfone (TCMS).
A turbine engine blade preform, with the preform comprising a strut connecting a plat-form to a blade root portion extending longitudinally in an upstream-downstream direction, an upstream web and a downstream web, which each extend in a direction substantially perpendicular to the longitudinal direction of the blade root and are formed at the upstream and downstream ends of the strut, with such upstream and downstream webs connecting the upstream and downstream ends of the plat-form to the upstream and downstream ends of the blade root, characterized in that the blade root extends in a direction perpendicular to the longitudinal direction of the blade root over a distance smaller than that over which the upstream and downstream webs (26, 28) extend in said direction and in that the upstream and downstream webs each comprise two side edges which are extended by walls that converge at the flanks of the blade root.
A multilayer film comprising: - an adhesive layer A consisting of an extrudable HMPSA composition (a); - a complexable thin layer B consisting of a PolyEthylene composition (b) denoted PE(b); and - a heat-sealable and breakable layer C consisting of a PolyEthylene composition (c) denoted PE(c); layers B and C being bonded together by layer A and said film being characterized in that: (i) the melt flow indices of compositions (b) and (c), measured in g/10 minutes at a temperature of 190°C and a total weight of 2.16 kg, and denoted MFI(b) and MFI(c), respectively, are each between 2.5 and 15 g/10 minutes; and (ii) the melt flow index of the HMPSA composition (a), measured in g/10 minutes at a temperature of 190°C and a total weight of 2.16 kg, and denoted MFI(a), is such that the ratios MFI(a)/MFI(b) and MFI(a)/MFI(c) are each between 1.5 and 10. - an adhesive layer A consisting of an extrudable HMPSA composition (a); - a complexable thin layer B consisting of a PolyEthylene composition (b) denoted PE(b); and - a heat-sealable and breakable layer C consisting of a PolyEthylene composition (c) denoted PE(c); (i) the melt flow indices of compositions (b) and (c), measured in g/10 minutes at a temperature of 190°C and a total weight of 2.16 kg, and denoted MFI(b) and MFI(c), respectively, are each between 2.5 and 15 g/10 minutes; and (ii) the melt flow index of the HMPSA composition (a), measured in g/10 minutes at a temperature of 190°C and a total weight of 2.16 kg, and denoted MFI(a), is such that the ratios MFI(a)/MFI(b) and MFI(a)/MFI(c) are each between 1.5 and 10.