mhurhangee/ep-ind-claims huggingface dataset:
A method of forming a coated article, said method comprising: i) applying the undercoating composition comprising: a) from 20 to 40 wt.% of a vinyl chloride-vinyl acetate copolymer obtained by polymerization of a co-monomer mixture comprising, based on the total weight of the co-monomers, from 85 to 98 wt.% of vinyl chloride, from 2 to 10 wt.% of vinyl acetate and from 0 to 5 % by weight of a co-monomer selected from C 2 to C 8 olefins, vinylidene chloride and styrene; b) at least 2 wt.% of plasticizer selected from epoxidized natural oil(s); and, c) at least 2 wt.% of at least one aliphatic, cycloaliphatic or aromatic compound having a blocked isocyanate group, wherein said isocyanate group is blocked with a blocking agent capable of de-blocking at a temperature in the range of +/- 20°C compared to the de-blocking temperature of the corresponding isocyanate being blocked with nonylphenol. to at least one surface of said article; ii) applying at least one further coating composition onto said undercoating composition; and iii) curing said undercoating and said at least one further coating composition, wherein the undercoating composition is in an uncured state upon application of the coating composition immediately contacting it. i) applying the undercoating composition comprising: a) from 20 to 40 wt.% of a vinyl chloride-vinyl acetate copolymer obtained by polymerization of a co-monomer mixture comprising, based on the total weight of the co-monomers, from 85 to 98 wt.% of vinyl chloride, from 2 to 10 wt.% of vinyl acetate and from 0 to 5 % by weight of a co-monomer selected from C 2 to C 8 olefins, vinylidene chloride and styrene; b) at least 2 wt.% of plasticizer selected from epoxidized natural oil(s); and, c) at least 2 wt.% of at least one aliphatic, cycloaliphatic or aromatic compound having a blocked isocyanate group, wherein said isocyanate group is blocked with a blocking agent capable of de-blocking at a temperature in the range of +/- 20°C compared to the de-blocking temperature of the corresponding isocyanate being blocked with nonylphenol. to at least one surface of said article; a) from 20 to 40 wt.% of a vinyl chloride-vinyl acetate copolymer obtained by polymerization of a co-monomer mixture comprising, based on the total weight of the co-monomers, from 85 to 98 wt.% of vinyl chloride, from 2 to 10 wt.% of vinyl acetate and from 0 to 5 % by weight of a co-monomer selected from C 2 to C 8 olefins, vinylidene chloride and styrene; b) at least 2 wt.% of plasticizer selected from epoxidized natural oil(s); and, c) at least 2 wt.% of at least one aliphatic, cycloaliphatic or aromatic compound having a blocked isocyanate group, wherein said isocyanate group is blocked with a blocking agent capable of de-blocking at a temperature in the range of +/- 20°C compared to the de-blocking temperature of the corresponding isocyanate being blocked with nonylphenol. ii) applying at least one further coating composition onto said undercoating composition; and iii) curing said undercoating and said at least one further coating composition,
Heat exchanger for thermally treating a vehicle cabin, the heat exchanger comprises a core portion made of at least a plurality of tubes and a plurality of fins, the heat exchanger comprises at least one header tank located at one end of the core portion, the header tank comprises at least a collecting plate which have a U-shape, a cover plate connected to the collecting plate and at least one cap plate which is located at one longitudinal end of the header tank, the collecting plate and the cover plate are linked together by an overlapping portion, the collecting plate, the cover plate and the cap plate are defining an internal volume of the header tank that is hydraulically communicating with the core portion, wherein the cap plate is at least partially mounted inside the internal volume and maintained in position by a tongue made in continuation of the overlapping portion and characterized in that the collecting plate comprises at least one lug that extends inside the internal volume defined by the header tank, the cover plate resting at least partially against the lug.
A thrust producing unit for producing thrust in a predetermined direction, comprising a shrouding and at least two rotor assemblies (7d, 8d), wherein the shrouding defines an internal volume and a longitudinal direction along a forward flight direction of the thrust producing unit, and wherein a first rotor assembly of the at least two rotor assemblies (7d, 8d) defines a first rotor axis and a second rotor assembly of the at least two rotor assemblies (7d, 8d) defines a second rotor axis, wherein the first rotor axis is inclined by an associated first inclination angle with respect to the predetermined direction, the first inclination angle being along the longitudinal direction and comprised in a range between +1° and +60°, and the first rotor assembly being arranged outside of the internal volume of the shrouding; and the second rotor axis being inclined by an associated second inclination angle with respect to the predetermined direction, such that the second inclination angle that is along the longitudinal direction amounts to 0°and is inferior to the range of the first inclination angle, and the second rotor assembly is arranged inside of the internal volume of the shrouding. wherein the shrouding defines an internal volume and a longitudinal direction along a forward flight direction of the thrust producing unit, and wherein a first rotor assembly of the at least two rotor assemblies (7d, 8d) defines a first rotor axis and a second rotor assembly of the at least two rotor assemblies (7d, 8d) defines a second rotor axis, wherein the first rotor axis is inclined by an associated first inclination angle with respect to the predetermined direction, the first inclination angle being along the longitudinal direction and comprised in a range between +1° and +60°, and the first rotor assembly being arranged outside of the internal volume of the shrouding; and the second rotor axis being inclined by an associated second inclination angle with respect to the predetermined direction, such that the second inclination angle that is along the longitudinal direction amounts to 0°and is inferior to the range of the first inclination angle, and the second rotor assembly is arranged inside of the internal volume of the shrouding.
An apparatus comprising: means for receiving a signal from a gyroscope sensor (11a, 11b, 22) mounted on a subject, the gyroscope sensor configured to measure rotational movement of the subject's heart, the signal being indicative of a left ventricular twist of the subject's heart; and means for determining a change in the left ventricular twist of the subject's heart caused by occlusion of blood flow by an arterial occlusion device configured to selectively occlude the blood flow of the subject, wherein the arterial occlusion device is a blood pressure cuff. means for receiving a signal from a gyroscope sensor (11a, 11b, 22) mounted on a subject, the gyroscope sensor configured to measure rotational movement of the subject's heart, the signal being indicative of a left ventricular twist of the subject's heart; and means for determining a change in the left ventricular twist of the subject's heart caused by occlusion of blood flow by an arterial occlusion device configured to selectively occlude the blood flow of the subject, wherein the arterial occlusion device is a blood pressure cuff.
A spring support for a coil spring, comprising an annular receiving element having a top side and a bottom side, wherein the top side is provided to receive one end of the coil spring, and comprising an annular damping element, which is in contact with the bottom side of the receiving element, wherein the damping element has a disk-shaped basic form, and furthermore is configured, during mounting of the spring support, by bending from the disk-shaped basic form, to form on its inside a collar which extends from the bottom side of the receiving element in the direction of the coil spring.
Closure device assembly for a piece of luggage, preferably a suitcase, the piece of luggage having a first body portion, a second body portion, and a zipper, said zipper being arranged between said first and second body portions (51,52), the closure device assembly comprising: at least one engagement element adapted for arrangement on said first body portion; at least one buckle element adapted for arrangement on said second body portion, said buckle element being adapted for pivotal motion between an open position and an engagement position such that, in said engagement position, said buckle element is in contact with said engagement element, said pivotal motion being about an axis that extends substantially parallel to said zipper, and at least one zipper slider adapted for operation of said zipper and having at least one engagement section for engagement with said engagement element and/or said buckle element; wherein the closure device assembly further comprises: a locking device for locking said engagement section of said zipper slider when said zipper slider is in a closed position; wherein said buckle element comprises a cover element and is adapted to cover in a closed positon of the closure device assembly with said cover element at least part of the locking device and said engagement section of the zipper slider in said closed position characterized in that the engagement section and the zipper slider are a single-piece element. at least one engagement element adapted for arrangement on said first body portion; at least one buckle element adapted for arrangement on said second body portion, said buckle element being adapted for pivotal motion between an open position and an engagement position such that, in said engagement position, said buckle element is in contact with said engagement element, said pivotal motion being about an axis that extends substantially parallel to said zipper, and at least one zipper slider adapted for operation of said zipper and having at least one engagement section for engagement with said engagement element and/or said buckle element; wherein the closure device assembly further comprises: a locking device for locking said engagement section of said zipper slider when said zipper slider is in a closed position; wherein said buckle element comprises a cover element and is adapted to cover in a closed positon of the closure device assembly with said cover element at least part of the locking device and said engagement section of the zipper slider in said closed position characterized in that the engagement section and the zipper slider are a single-piece element. a locking device for locking said engagement section of said zipper slider when said zipper slider is in a closed position; wherein said buckle element comprises a cover element and is adapted to cover in a closed positon of the closure device assembly with said cover element at least part of the locking device and said engagement section of the zipper slider in said closed position characterized in that the engagement section and the zipper slider are a single-piece element.
A printed circuit for integration in a smart card, said printed circuit comprising: - A printed circuit substrate of dielectric material having a first side and a second side; - An antenna having a wiring pattern extending between a first terminal and a second terminal (12a, 12b) and being located on said first side of said printed circuit substrate, said antenna having a resonance frequency; - One or more contact pads located on said second side of said printed circuit substrate and forming an external contact pattern; and - At least a first surface mount capacitor connected to said first terminal and said second terminal (12a, 12b) of said antenna so as to adjust said resonance frequency of said antenna, in order to match a predefined resonance frequency, for instance a resonance frequency comprised within the range defined in ISO 14443 standards, characterized in that: said first surface mount capacitor and said first terminal and said second terminal (12a, 12b) of said antenna are formed on the same side of said printed circuit substrate, and said first terminal of said antenna is connected to a first etched pad of said first capacitor by means of wire bonding. - A printed circuit substrate of dielectric material having a first side and a second side; - An antenna having a wiring pattern extending between a first terminal and a second terminal (12a, 12b) and being located on said first side of said printed circuit substrate, said antenna having a resonance frequency; - One or more contact pads located on said second side of said printed circuit substrate and forming an external contact pattern; and - At least a first surface mount capacitor connected to said first terminal and said second terminal (12a, 12b) of said antenna so as to adjust said resonance frequency of said antenna, in order to match a predefined resonance frequency, for instance a resonance frequency comprised within the range defined in ISO 14443 standards, characterized in that: said first surface mount capacitor and said first terminal and said second terminal (12a, 12b) of said antenna are formed on the same side of said printed circuit substrate, and said first terminal of said antenna is connected to a first etched pad of said first capacitor by means of wire bonding. said first surface mount capacitor and said first terminal and said second terminal (12a, 12b) of said antenna are formed on the same side of said printed circuit substrate, and said first terminal of said antenna is connected to a first etched pad of said first capacitor by means of wire bonding.
Arrangement of at least two actuators (1a; 1b; 1c; 1d) comprising: - a first actuator which includes a first motor which supplies a first torque, which first motor comprises a first rotor and a first stator which are positioned coaxially about a first axis, the first rotor comprising a first rotor body fitted with magnetic elements which are surrounded by the first stator, the first stator being formed by a stator core comprising first polar elements which are distributed over the external periphery of the first stator and project towards the exterior - a second actuator (1b; 1c; 1d) which includes a second motor (4b; 4c; 4d), which second motor (4b; 4c; 4d) comprises a second rotor (30; 42) and a second stator (12; 52), the second rotor (30; 42) and the second stator (12; 52) being positioned coaxially about a second axis, the second motor (4b; 4c; 4d) comprising a central core which is identical to said stator core which forms either the second rotor (30; 42) or the second stator (12; 52) and which comprises second polar elements which are distributed over the external periphery of the second rotor (30; 42) or of the second stator (12; 52) and project towards the exterior, one of the second rotor (30; 42) and stator (12; 52) being different respectively from the first rotor and stator. - a first actuator which includes a first motor which supplies a first torque, which first motor comprises a first rotor and a first stator which are positioned coaxially about a first axis, the first rotor comprising a first rotor body fitted with magnetic elements which are surrounded by the first stator, the first stator being formed by a stator core comprising first polar elements which are distributed over the external periphery of the first stator and project towards the exterior - a second actuator (1b; 1c; 1d) which includes a second motor (4b; 4c; 4d), which second motor (4b; 4c; 4d) comprises a second rotor (30; 42) and a second stator (12; 52), the second rotor (30; 42) and the second stator (12; 52) being positioned coaxially about a second axis, the second motor (4b; 4c; 4d) comprising a central core which is identical to said stator core which forms either the second rotor (30; 42) or the second stator (12; 52) and which comprises second polar elements which are distributed over the external periphery of the second rotor (30; 42) or of the second stator (12; 52) and project towards the exterior, one of the second rotor (30; 42) and stator (12; 52) being different respectively from the first rotor and stator.
A device for opening a spout of metallurgical vessels such as pouring ladles or the like, whereby the pouring channel on the lined bottom of the vessel, with a slide valve closure having at least two slide plates (5, 7), wherein the slide valve closure has a stationary slide plate connected to the vessel and at least one displaceable slide plate in operative contact therewith, wherein all slide plates (5, 7) have at least one pouring opening (6, 8) and are displaceable relative to one another in such a way that the pouring openings (6, 8) are brought into alignment in order to open the slide valve and allow the melt flowing out, wherein a plug is arranged above the slide valve closure, the size of which plug exceeds the diameter of the discharge channel and which is connected to the lining of the vessel, wherein the slide closure has a gas supply line and wherein the gas supply line can be acted upon by a pressurised gas in such a way that the plug can be pneumatically released from its closed position to release the discharge channel, characterised in that the gas supply line is arranged in the displaceable slide plate in such a way that during the opening process before the release of the outlet of the gas supply line is connected to the opening of the stationary slide plate and that the gas supply line is connected to a gas reservoir acting as a storage container and the gas reservoir can be charged with gas via a capillary line.
A method for prediction of fatigue life properties of an additive manufactured element, specimen or material structure, in an industrial product design or manufacturing, with a data collection step (1a, 1b) in which several data points for maximum stress vs. cycles to failure for different given processing steps, surface and volume conditions of the element, specimen or material structure are collected, with a training step in which a machine learning system is trained with the collected data, and with an evaluation step (5, 6) in which the trained machine learning system is confronted with new actual processing conditions and used to predict the fatigue life properties of the element, specimen or material structure, and with an application step in which the predicted fatigue life properties are used to design the product or to parametrize an manufacturing process, characterized in that for the evaluation step (5, 6), a definition of topologic properties of the element and a definition of different zones, each with own properties and conditions, are provided, and the evaluation calculates separate fatigue life properties for the different zones. with a data collection step (1a, 1b) in which several data points for maximum stress vs. cycles to failure for different given processing steps, surface and volume conditions of the element, specimen or material structure are collected, with a training step in which a machine learning system is trained with the collected data, and with an evaluation step (5, 6) in which the trained machine learning system is confronted with new actual processing conditions and used to predict the fatigue life properties of the element, specimen or material structure, and with an application step in which the predicted fatigue life properties are used to design the product or to parametrize an manufacturing process, characterized in that for the evaluation step (5, 6), a definition of topologic properties of the element and a definition of different zones, each with own properties and conditions, are provided, and the evaluation calculates separate fatigue life properties for the different zones.
Transparent hot-melt single component sealant composition, characterized in that it comprises from 70 % to 99 weight % of polyisobutylene, preferably from 73 % to 99 %, based on the total weight of the composition.
A method for handling wind turbine sub-assemblies, comprising: coupling a connecting device to a connector of a hoisting device at a first connection interface of the connecting device; coupling a first wind turbine sub-assembly comprising a nacelle to the connecting device at a second connection interface of the connecting device; moving the first wind turbine sub-assembly with the hoisting device; coupling a second wind turbine sub-assembly different than the first wind turbine sub-assembly to the connection device at a third connection interface of the connecting device; and moving the second wind turbine sub-assembly with the hoisting device, wherein the third connection interface includes a movable element movable between a first position and a second position, the connecting device being coupled to the second sub-assembly when the movable element is in the first position and the connecting device being uncoupled from the second sub-assembly when the movable element is in the second position; and wherein the connecting device includes trunnions at spaced-apart locations thereon, and wherein the step of coupling the first wind turbine sub-assembly to the connecting device at the second connection interface further comprises: extending cables from trunnions of the connecting device to connectors on the nacelle; and limiting movement of the cables along the trunnions. coupling a connecting device to a connector of a hoisting device at a first connection interface of the connecting device; coupling a first wind turbine sub-assembly comprising a nacelle to the connecting device at a second connection interface of the connecting device; moving the first wind turbine sub-assembly with the hoisting device; coupling a second wind turbine sub-assembly different than the first wind turbine sub-assembly to the connection device at a third connection interface of the connecting device; and moving the second wind turbine sub-assembly with the hoisting device, wherein the third connection interface includes a movable element movable between a first position and a second position, the connecting device being coupled to the second sub-assembly when the movable element is in the first position and the connecting device being uncoupled from the second sub-assembly when the movable element is in the second position; and wherein the connecting device includes trunnions at spaced-apart locations thereon, and wherein the step of coupling the first wind turbine sub-assembly to the connecting device at the second connection interface further comprises: extending cables from trunnions of the connecting device to connectors on the nacelle; and limiting movement of the cables along the trunnions. extending cables from trunnions of the connecting device to connectors on the nacelle; and limiting movement of the cables along the trunnions.