mhurhangee/ep-ind-claims huggingface dataset:
A method for pairing a remote controller with a device, the method comprising, at the device: - receiving, via a voice interface, an activation phrase; - receiving, via a remote controller interface, a command from the remote controller, wherein the command includes a remote controller identifier; - storing the remote controller identifier as an identifier of a paired remote controller; characterized in that the steps of receiving and storing are performed after checking that the activation phrase is received from within an allowable activation angle (12, 22, 32). - receiving, via a voice interface, an activation phrase; - receiving, via a remote controller interface, a command from the remote controller, wherein the command includes a remote controller identifier; - storing the remote controller identifier as an identifier of a paired remote controller;
A discrete half bridge semiconductor device comprising: a first cascode arrangement and a second cascode arrangement; each of the first cascode and second cascode arrangements comprising a high voltage FET device die and a low voltage FET device die, wherein the high voltage FET device of the first cascode arrangement and the high voltage FET device of the second cascode arrangement are having a flipped or inverted orientation; wherein the source of the high voltage FET device die is mounted on and connected to a drain of the low voltage FET device die; the source of the low voltage FET device die of the first cascode arrangement and gate of the high voltage FET device die of the first cascode arrangement are connected to a drain terminal of the high voltage FET device die of the second cascode arrangement at common connection pad; wherein the gate and drain terminals of the high voltage FET device of the first cascode arrangement and the gate and drain terminals of the high voltage FET device of the second cascode arrangement are directly connected to the respective gate and drain pads; and wherein with respect to the second cascode arrangement the gate terminal of the high voltage FET device die and the source terminal of the low voltage FET device die are mounted on respective contact pads, and with respect to the first cascode arrangement the drain terminal of the high voltage FET device die is mounted on a respective contact pad. a first cascode arrangement and a second cascode arrangement; each of the first cascode and second cascode arrangements comprising a high voltage FET device die and a low voltage FET device die, wherein the high voltage FET device of the first cascode arrangement and the high voltage FET device of the second cascode arrangement are having a flipped or inverted orientation; wherein the source of the high voltage FET device die is mounted on and connected to a drain of the low voltage FET device die; the source of the low voltage FET device die of the first cascode arrangement and gate of the high voltage FET device die of the first cascode arrangement are connected to a drain terminal of the high voltage FET device die of the second cascode arrangement at common connection pad; wherein the gate and drain terminals of the high voltage FET device of the first cascode arrangement and the gate and drain terminals of the high voltage FET device of the second cascode arrangement are directly connected to the respective gate and drain pads; and wherein with respect to the second cascode arrangement the gate terminal of the high voltage FET device die and the source terminal of the low voltage FET device die are mounted on respective contact pads, and with respect to the first cascode arrangement the drain terminal of the high voltage FET device die is mounted on a respective contact pad.
A vehicle body structure comprising: a front frame member disposed in a front part of a vehicle body; a rear frame member disposed in a rear part of the vehicle body; and paired left and right middle frame members disposed on outer sides, in a vehicle width direction, of the vehicle body, respectively, and extending in a vehicle front-rear direction between the front frame member and the rear frame member, wherein each of the paired left and right middle frame members includes a first middle frame member (29, 129) disposed on an outer side in the vehicle width direction, and a second middle frame member disposed inward, in the vehicle width direction, of the first middle frame member (29, 129) and coupling the front frame member and the rear frame member to each other, the second middle frame member extends in such a way as to shift farther outward in the vehicle width direction as it gets closer to rear of the vehicle, characterized in that strength of the second middle frame member is set larger than strength of the first middle frame member (29, 129). a front frame member disposed in a front part of a vehicle body; a rear frame member disposed in a rear part of the vehicle body; and paired left and right middle frame members disposed on outer sides, in a vehicle width direction, of the vehicle body, respectively, and extending in a vehicle front-rear direction between the front frame member and the rear frame member, wherein
A device for enhanced delivery of a composition to a body region of a patient utilizing radiofrequency energy, the device comprising: a first longitudinal member with a proximal end and a distal end with at least one lumen extending between the proximal end and the distal end; a composition delivery element located at the distal end of the longitudinal member, the composition delivery element having the composition located on an outside surface thereof; and at least two electrodes (14, 14) located on a second longitudinal member configured to be inserted into the lumen of the first longitudinal member to be located within the composition delivery element, the at least two electrodes coupled to a radiofrequency source to receive radiofrequency energy from the radiofrequency source and insulated such that they can generate an electric field to enhance delivery of the composition to the body region. a first longitudinal member with a proximal end and a distal end with at least one lumen extending between the proximal end and the distal end; a composition delivery element located at the distal end of the longitudinal member, the composition delivery element having the composition located on an outside surface thereof; and at least two electrodes (14, 14) located on a second longitudinal member configured to be inserted into the lumen of the first longitudinal member to be located within the composition delivery element, the at least two electrodes coupled to a radiofrequency source to receive radiofrequency energy from the radiofrequency source and insulated such that they can generate an electric field to enhance delivery of the composition to the body region.
A gearbox comprising an arrangement, wherein the arrangement comprises a first shaft, a second shaft (3, 11), at least one gear set, which comprises a primary cogwheel arranged on the first shaft and a secondary cogwheel arranged on the second shaft (3, 11), wherein the primary cogwheel and the secondary cogwheel have teeth engaging with each other, and wherein the arrangement comprises a first component (29a-d), which is arranged at a first side of the gear mesh between the primary cogwheel and the secondary cogwheel, said first component (29a-d) is comprised in a unit (19, 20), which is adapted to provide a rotational locking of the secondary cogwheel on the second shaft (3, 11), characterised in that said first component (29a-d) comprises a recess (29a 2 -d 2) in a radial side wall in relation to said shafts (3, 4, 11), which recess has its opening arranged in connection with the gear mesh, so that gearbox oil may be led between the first side of the gear mesh and the recess (29a 2 -d 2).
A method for preparing waste powder from generative production processes, by means of which three-dimensional objects are produced in layers from a powdery base material in that initially a first layer of said base material is applied to a construction platform, which first layer is then irradiated and hardened in accordance with the coordinates of a first plane of the object to be built using a laser, wherein, after completion of processing in said first plane, the construction platform is lowered by the layer thickness of another plane and a new powder layer is applied, and wherein these process steps are repeated in accordance with the number of planes until a three-dimensional object is built, upon completion of which powdery material remains as waste powder outside the areas covered by the laser, wherein said waste powder is subjected to mechanical processing in that it is reduced to small pieces using a grinding mill, characterized in that the waste powder is preferably reduced to a grain size which is smaller than the original grain size of the powder in its new condition.
A method for printing an energy curable ink or coating composition comprising: a) providing an energy curable ink or coating composition, wherein the energy curable ink or coating composition comprises: i) greater than or equal to 20% (w/w) of one or more multifunctional polymerizable monomers, based on the total weight of the ink or coating composition; ii) an aminoacrylate formed by the Michael reaction of polymerisable acrylate monomers or oligomers with alkanolamines; iii) optionally, one or more solvents; and iv) optionally, one or more colorants; b) applying the energy curable ink or coating composition of step a) to a substrate; c) curing the applied energy curable ink or coating composition by electron beam radiation, wherein: i) the accelerating voltage of the electron beam emitter is greater than or equal to 70 keV; and ii) the cure dose is greater than or equal to 30 kGy. a) providing an energy curable ink or coating composition, wherein the energy curable ink or coating composition comprises: i) greater than or equal to 20% (w/w) of one or more multifunctional polymerizable monomers, based on the total weight of the ink or coating composition; ii) an aminoacrylate formed by the Michael reaction of polymerisable acrylate monomers or oligomers with alkanolamines; iii) optionally, one or more solvents; and iv) optionally, one or more colorants; i) greater than or equal to 20% (w/w) of one or more multifunctional polymerizable monomers, based on the total weight of the ink or coating composition; ii) an aminoacrylate formed by the Michael reaction of polymerisable acrylate monomers or oligomers with alkanolamines; iii) optionally, one or more solvents; and iv) optionally, one or more colorants; b) applying the energy curable ink or coating composition of step a) to a substrate; c) curing the applied energy curable ink or coating composition by electron beam radiation, wherein: i) the accelerating voltage of the electron beam emitter is greater than or equal to 70 keV; and ii) the cure dose is greater than or equal to 30 kGy. i) the accelerating voltage of the electron beam emitter is greater than or equal to 70 keV; and ii) the cure dose is greater than or equal to 30 kGy.
A zoom lens system comprising, in order from an object along an optical axis: a first lens group having a negative refractive power and including a plurality of lenses; a second lens group having a positive refractive power; and a third lens group having a positive refractive power; G is an zooming the distances between the groups are variable; the following conditional expression being satisfied: 0.6 < Ymax × ft / f 1 2 < 1.0 where Ymax denotes the maximum image height of the zoom lens system, ft denotes a focal length of the zoom lens system in a telephoto end state, and fl denotes a focal length of the first lens group; and the following conditional expression being satisfied: 0.51 < N 2 nav − 0.8 ft ⋅ tanωw / TLw < 0.95 where N2nav denotes an average refractive index value at d-line of materials of all the negative lenses included in the second lens group, ωw denotes a half angle of view of the zoom lens system in a wide-angle end state, and TLw denotes a total length of the zoom lens system in the wide-angle end state. a first lens group having a negative refractive power and including a plurality of lenses; a second lens group having a positive refractive power; and a third lens group having a positive refractive power; G is an zooming the distances between the groups are variable; the following conditional expression being satisfied: 0.6 < Ymax × ft / f 1 2 < 1.0 where Ymax denotes the maximum image height of the zoom lens system, ft denotes a focal length of the zoom lens system in a telephoto end state, and fl denotes a focal length of the first lens group; and the following conditional expression being satisfied: 0.51 < N 2 nav − 0.8 ft ⋅ tanωw / TLw < 0.95 where N2nav denotes an average refractive index value at d-line of materials of all the negative lenses included in the second lens group, ωw denotes a half angle of view of the zoom lens system in a wide-angle end state, and TLw denotes a total length of the zoom lens system in the wide-angle end state.
A landing gear (100A, 100B) comprising: an outer cylinder for coupling to a frame of an aircraft; a shock strut assembly movably coupled to the outer cylinder so as to reciprocate along a longitudinal axis of the outer cylinder; and a shrink mechanism (130A, 130B) including a first shrink link member pivotally coupled to the outer cylinder, a second shrink link member coupling the first shrink link member to the shock strut assembly, a crank member (160, 1560) pivotally coupled to the outer cylinder; characterized in that the shrink mechanism (130A, 130B) further includes: a drive member (170, 1570) coupling the crank member (160, 1560) to a walking beam of a landing gear retract mechanism, and a driven member (180, 1580) coupling the crank member (160, 1560) to the first shrink link member. an outer cylinder for coupling to a frame of an aircraft; a shock strut assembly movably coupled to the outer cylinder so as to reciprocate along a longitudinal axis of the outer cylinder; and a shrink mechanism (130A, 130B) including a first shrink link member pivotally coupled to the outer cylinder, a second shrink link member coupling the first shrink link member to the shock strut assembly, a crank member (160, 1560) pivotally coupled to the outer cylinder; a drive member (170, 1570) coupling the crank member (160, 1560) to a walking beam of a landing gear retract mechanism, and a driven member (180, 1580) coupling the crank member (160, 1560) to the first shrink link member.
A method of manufacturing a body of a fluid control apparatus using additive manufacturing, the method including: forming an inner wall having an outside surface and an inside surface, an area surrounding an inlet, an area surrounding an outlet, and an area surrounding a fluid flow path, wherein the inner wall provides a fluid boundary and connects the inlet and the outlet; forming a portion of the inner wall that receives a valve seat; forming a portion of the inner wall that surrounds a bore and receives a control stem and a control element; forming a three-dimensional lattice structure by depositing a solidifiable material onto the inner wall in a predetermined pattern, wherein the lattice structure includes a plurality of connected lattice members. forming an inner wall having an outside surface and an inside surface, an area surrounding an inlet, an area surrounding an outlet, and an area surrounding a fluid flow path, wherein the inner wall provides a fluid boundary and connects the inlet and the outlet; forming a portion of the inner wall that receives a valve seat; forming a portion of the inner wall that surrounds a bore and receives a control stem and a control element; forming a three-dimensional lattice structure by depositing a solidifiable material onto the inner wall in a predetermined pattern, wherein the lattice structure includes a plurality of connected lattice members.
A helmet comprising a plurality of air vents, and covers (30, 30a) for opening and closing the air vents, wherein the covers (30, 30a) are configured to hinge outwardly from the helmet (10, 95) to open the air vents, characterised in that the covers (30, 30a) are configured to hinge outwardly from the helmet in directions that arc towards a front of the helmet (10, 95).
Fabric with anti-cut characteristics, in particular with a cut resistance level 3 or higher according to EN 388: 2016, comprising: (a) an ultra high molecular weight polyethylene PE-UHMW yarn; (b) a thermal polymer yarn, such as polyester or polypropylene; and (c) a yarn of an elastomer; wherein the three yarns are circular knit with needles arranged radially and fixed horizontally and vertically on the cylinder and plate, with feeds of polyethylene yarn and the same number of thermal polymer yarn feeds, between which the elastomer yarn is inserted internally with a thread guide between the needles creating a double-face fabric with two correct sides and without a wrong side, characterized in that said double-face fabric is a double-face single layer fabric. (a) an ultra high molecular weight polyethylene PE-UHMW yarn; (b) a thermal polymer yarn, such as polyester or polypropylene; and (c) a yarn of an elastomer;
A pharmaceutical composition for use in treating chronic cough, comprising a compound represented by Formula: or a pharmaceutically acceptable salt thereof.
A tobacco smoke filter or filter element comprising an outer wrapper engaged around a single longitudinal extending core of tobacco smoke filtering material, wherein a first end of the outer wrapper is substantially flush with a first end of the core around which it is engaged, and a second end of the outer wrapper extends beyond a second end of the core around which is engaged, to define a cavity at the second end of the filter; the filter or filter element further comprising an additive distanced from the second end of the outer wrapper and/or core.
An aqueous liquid colorant composition having a volatile organic content up to 50g/l and suitable for colouring aqueous or solventborne architectural coatings and base paints comprising based on the total weight of the composition, i) from 1 to 26% of non-volatile organic liquid having a vapour pressure up to 1.3 N/m 2 at 25°C and comprising a mixture of polyethylene glycol and polypropylene glycol ii) from 2 to 13% of stabilising agent iii) from 4 to 77% of colour pigment iv) from 0 to 8% of rheology modifying clay v) from 0 to 20% of extender wherein the ratio of the combined weight of iii)+iv)+v): the combined weight of i)+ii) is from 0.8 to 2.75:1 and the combined weight of the non-volatile organic liquid i) and the stabilising agent ii) is no greater than 28% and the combined weight of the rheology modifying clay iv) and the extender v) is at least 2% when the amount of colour pigment is less than 51 %. i) from 1 to 26% of non-volatile organic liquid having a vapour pressure up to 1.3 N/m 2 at 25°C and comprising a mixture of polyethylene glycol and polypropylene glycol ii) from 2 to 13% of stabilising agent iii) from 4 to 77% of colour pigment iv) from 0 to 8% of rheology modifying clay v) from 0 to 20% of extender
Process for increasing the strength of load-bearing surfaces of shafts, particularly of cylindrical surfaces (2,3) of crankshafts (1,33,36,37) that have been prepared by machining, where the die cylindrical surfaces (2,3) of the main bearing pin (Ji) and crankpin (Pi) and potentially also of the pin of crankshafts (1,33,36,37) have additional oil bores, where at least one load-bearing surface is deep-rolled with at least one cylindrical deep-rolling roll (11,12,25,30) that has a structured surface (19,20,26), characterised by the deep-rolling roll extending over the full width of the load-bearing surface, and the deep-rolled surface subsequently being machined to a low cutting depth.
A method of applying a fastening means to a backsheet of an absorbent product, said backsheet facing away from the user during use, and being opposite to a body facing side of the absorbent product, wherein said method comprises the step of applying an adhesive layer on the backsheet of the absorbent product, characterized in that it further comprises the step of applying by printing an expandable ink, which can be activated by heat or UV radiation, on said adhesive layer, wherein 5-95 % of the backsheet is covered by the expandable ink.
Compound based on hexabenzocoronene having the following formula I: in which: - R 1, R 3, R 4 and R 6 are chosen, independently of each other, from a carboxylic group (-COOH), a cyano group (-C=N), an isocyanate group; (-N+≡C-), a cyanate group (-O-C=N) and a group (CF 3), and - R 2 and R 5 have the following formula: X -ZP46 Formula in which: ∘ X is a spacer group selected from a group -COO- and a group -CONH-, ∘ n 1 = 0 or 1, and ∘ ZP46 has the following formula: in which R is methyl or C6H13. - R 1, R 3, R 4 and R 6 are chosen, independently of each other, from a carboxylic group (-COOH), a cyano group (-C=N), an isocyanate group; (-N+≡C-), a cyanate group (-O-C=N) and a group (CF 3), and - R 2 and R 5 have the following formula: X -ZP46 Formula in which: ∘ X is a spacer group selected from a group -COO- and a group -CONH-, ∘ n 1 = 0 or 1, and ∘ ZP46 has the following formula: in which R is methyl or C6H13. ∘ X is a spacer group selected from a group -COO- and a group -CONH-, ∘ n 1 = 0 or 1, and ∘ ZP46 has the following formula:
A method for managing an embedded secure element, eSE, in a host device, the embedded secure element only being accessible as a slave of at least one resident application (Appl, App2, App3) of the host device in a master-slave relationship, and the embedded secure element including a root security domain, ISD, with which a set of keys is associated to implement security mechanisms, the method being characterised by the following steps: sending (440, 450) a message including an identifier of the embedded secure element eSE, from an application agent embedded in an operating system of the host device to a first entity external to the host device and specified in the application agent; determining a second entity external to the host device and holding the set of keys associated with the root security domain. sending (440, 450) a message including an identifier of the embedded secure element eSE, from an application agent embedded in an operating system of the host device to a first entity external to the host device and specified in the application agent; determining a second entity external to the host device and holding the set of keys associated with the root security domain.
An aerial vehicle having a reduced noise signature, the aerial vehicle comprising: an airframe; a first electric motor configured to drive a first propeller (2, 132) wherein the first propeller (2, 132) is oriented to provide lift to the airframe; and a second electric motor configured to drive a second propeller (2, 132), wherein the second propeller (2, 132) is oriented to provide lift to the airframe, wherein the first propeller (2, 132) employs a first propeller (2, 132) geometry and the second propeller (2, 132) employs a second propeller (2, 132) geometry that is different from the first propeller (2, 132) geometry, and wherein the first propeller (2, 132) and the second propeller (2, 132) are configured to deliver substantially the same amount of thrust when driven at a predetermined revolutions per minute "RPM". an airframe; a first electric motor configured to drive a first propeller (2, 132) wherein the first propeller (2, 132) is oriented to provide lift to the airframe; and a second electric motor configured to drive a second propeller (2, 132), wherein the second propeller (2, 132) is oriented to provide lift to the airframe, wherein the first propeller (2, 132) employs a first propeller (2, 132) geometry and the second propeller (2, 132) employs a second propeller (2, 132) geometry that is different from the first propeller (2, 132) geometry, and wherein the first propeller (2, 132) and the second propeller (2, 132) are configured to deliver substantially the same amount of thrust when driven at a predetermined revolutions per minute "RPM".