mhurhangee/ep-ind-claims huggingface dataset:
Tyre comprising a tread having a contact surface for coming into contact with the carriageway when the tyre is rolling, said tread comprising at least one circumferential reinforcing element (8-x), at least a portion of the meridian cross-section of which is in the shape of a triangle, the vertex of which is oriented radially towards the outside, said circumferential reinforcing element (8-x) consisting of a rubber mixture with a dynamic shear modulus G* measured at 60°C at 10 Hz and under an alternating shear stress of 0.7 MPa greater than the dynamic shear modulus G* of the main rubber mixture of the tread, said tread comprising at least two grooves extending at least partially circumferentially, each circumferential groove being delimited by a groove bottom and axially by two side faces, said tread comprising at least one tread block formed between two grooves, said block having an axial width L51 measured at a radial level corresponding substantially to the groove bottom, characterized in that: - at least one of the side faces is undercut, - the circumferential reinforcing element (8-x) is arranged axially relative to said undercut side face at a distance "d" of between 0 and 15% of the axial width L51 of the tread block, at least extending radially from the inside towards the outside from a radial level situated above the wear limit level and to a radial height equal to 5% of the thickness "p" of the tread. - at least one of the side faces is undercut, - the circumferential reinforcing element (8-x) is arranged axially relative to said undercut side face at a distance "d" of between 0 and 15% of the axial width L51 of the tread block, at least extending radially from the inside towards the outside from a radial level situated above the wear limit level and to a radial height equal to 5% of the thickness "p" of the tread.
A method of manufacturing a padded part primarily for use in an item of wear comprising the steps of providing a first sheet of a flexible material; locating at least one fastener (10, 11, 12) on one side of the first sheet; providing a second sheet of flexible material; creating a layered assembly in a mould tool, the layered assembly comprising, in order, the first sheet of material such that said one side of the first sheet is outermost, a piece of mouldable padding, and the second sheet of flexible material, hot melt adhesive layers being provided between the padding and the first and second sheets (3, 4) of flexible material; and moulding the layered assembly in a press after or during heating of the layered assembly to bond the layers of the assembly together and simultaneously to mould the layered assembly into a predetermined shape thereby forming a moulded and pressed laminate; wherein the mould tool is provided with at least one cavity in which said fastener or fasteners (10, 11, 12) located on said one side of the first sheet are inserted whereby the fastener or fasteners (10, 11, 12) are unaffected by the pressure exerted by the press. providing a first sheet of a flexible material; locating at least one fastener (10, 11, 12) on one side of the first sheet; providing a second sheet of flexible material; creating a layered assembly in a mould tool, the layered assembly comprising, in order, the first sheet of material such that said one side of the first sheet is outermost, a piece of mouldable padding, and the second sheet of flexible material, hot melt adhesive layers being provided between the padding and the first and second sheets (3, 4) of flexible material; and moulding the layered assembly in a press after or during heating of the layered assembly to bond the layers of the assembly together and simultaneously to mould the layered assembly into a predetermined shape thereby forming a moulded and pressed laminate; wherein the mould tool is provided with at least one cavity in which said fastener or fasteners (10, 11, 12) located on said one side of the first sheet are inserted whereby the fastener or fasteners (10, 11, 12) are unaffected by the pressure exerted by the press.
Rendering bin handling device comprising a spreader bar 12 of a substantially U-shaped structure that comprises a handling crossbar 13 connecting, substantially at one 14 of their ends 14; 15, two gripping arms 16, 17 which extend on either side of opposite walls 5, 7 of the rendering bin 2 or of a support structure 20 for at least one rendering bin 2 and are rigidly connected respectively to said rendering bin 2 or to said support structure 20 by hinge means 18 about the same horizontal pivot axis 19, said hinge means 18 on the opposite sides 5, 7 of the rendering bin 2 or of the support structure 20 are rigidly connected to the bin so as to be movable along a displacement path C determined with respect to the center of gravity 23 of the rendering bin 2 and/or of said support structure 20, said hinge means 18 being movable between a first position 24 defining a horizontal pivot axis 19 of the rendering bin 2 or, as the case may be, of the support structure 20 of this rendering bin 2, located below the center of gravity 23, as the case may be, of this rendering bin 2 and of the support structure 20 on which it is mounted, and at least one second position 25 in which the pivot axis 19 is located above this center of gravity 23, characterized in that it further comprises means 26 for retaining said hinge means 18 in their first position 24, and control means defined as being for releasing these retaining means 26 during tipping of the rendering bin and/or when the bin is in the overturned position.
An ablation method for ablating a surface layer of a wall, said method comprising at least one scanning pass in which shots are fired on to said layer from at least one pulsed laser beam (6 or 6a, 6b, 6c, 6d), a directional control of said shots by optical deflection, characterized in that the beam has a quality M 2 of less than 20 and in that, the simple or composite impact zones of said shots on said layer are separate or substantially contiguous with a minimized overlap, and in that said shot scanning is carried out by means of a stationary deflection head that is located at a distance of between 200 mm and 1 m from said layer to be ablated.
A method for deflating an inflated wall of a device selected from an aerostat balloon, an underwater-balloon, a solar sail, characterized in that said inflated wall is cut by displacing at least one cutting member adapted to cut the inflated wall, on the inflated wall along a score line having the effect of generating an opening for deflating the inflated wall.
A control system for operation of one or more agricultural operations on a field with residue, the control system comprising: at least one camera assembly (74, 78); one or more processor devices in communication with the at least one camera assembly (74, 78); and one or more memory architectures coupled with the one or more processor devices; wherein the one or more processor devices are configured to: identify the execution of a first tillage operation on the field with a tillage implement, the first operation resulting in residue on the field; cause the at least one camera assembly (74, 78) to capture a first image of an area (76, 80) of the field that is one of ahead of and behind the tillage implement; analyze the first image to determine at least one indicator of residue coverage on the field characterized in to identify the execution of a subsequent operation on the field; and control one or more aspects of the subsequent operation on the field based upon, at least in part, the determined indicator of residue coverage, wherein the subsequent operation utilizes a different implement and does not form part of a continuous series of operations with the first operation. at least one camera assembly (74, 78); one or more processor devices in communication with the at least one camera assembly (74, 78); and one or more memory architectures coupled with the one or more processor devices; wherein the one or more processor devices are configured to: identify the execution of a first tillage operation on the field with a tillage implement, the first operation resulting in residue on the field; cause the at least one camera assembly (74, 78) to capture a first image of an area (76, 80) of the field that is one of ahead of and behind the tillage implement; analyze the first image to determine at least one indicator of residue coverage on the field characterized in to identify the execution of a subsequent operation on the field; and control one or more aspects of the subsequent operation on the field based upon, at least in part, the determined indicator of residue coverage, wherein the subsequent operation utilizes a different implement and does not form part of a continuous series of operations with the first operation. identify the execution of a first tillage operation on the field with a tillage implement, the first operation resulting in residue on the field; cause the at least one camera assembly (74, 78) to capture a first image of an area (76, 80) of the field that is one of ahead of and behind the tillage implement; analyze the first image to determine at least one indicator of residue coverage on the field characterized in to identify the execution of a subsequent operation on the field; and control one or more aspects of the subsequent operation on the field based upon, at least in part, the determined indicator of residue coverage, wherein the subsequent operation utilizes a different implement and does not form part of a continuous series of operations with the first operation.
A method of separating a wafer of light emitting devices, the wafer comprising a plurality of light emitting devices disposed in a plurality of rows (72, 74, 76, 86) separated by dicing streets (32, 57, 61, 63, 68, 90, 92, 94, 96) and one or more fiducials (52, 130, 150), wherein the location of the at least one fiducial (52, 130, 150) is programmed into a scribing machine before the wafer is loaded into the machine, the method comprising: scribing a pilot groove, on a dicing street (32, 57, 61, 63, 68, 90, 92, 94, 96) on a surface of the wafer; checking the alignment of the wafer using the distance of the pilot groove relative to the one or more fiducials (52, 130, 150) on the wafer; and after checking the alignment, realigning the wafer position to match a fixed distance, wherein the fixed distance is the distance from the at least one fiducial (52, 130, 150) to the pilot groove; scribing a singulation groove (62, 66) on the dicing street (32, 57, 61, 63, 68, 90, 92, 94, 96) on the surface of the wafer; wherein: the singulation groove (62, 66) is wider and deeper than the pilot groove; the singulation groove (62, 66) is scribed over the pilot groove and the wafer is broken along the singulation groove (62, 66). scribing a pilot groove, on a dicing street (32, 57, 61, 63, 68, 90, 92, 94, 96) on a surface of the wafer; checking the alignment of the wafer using the distance of the pilot groove relative to the one or more fiducials (52, 130, 150) on the wafer; and after checking the alignment, realigning the wafer position to match a fixed distance, wherein the fixed distance is the distance from the at least one fiducial (52, 130, 150) to the pilot groove; scribing a singulation groove (62, 66) on the dicing street (32, 57, 61, 63, 68, 90, 92, 94, 96) on the surface of the wafer; wherein: the singulation groove (62, 66) is wider and deeper than the pilot groove; the singulation groove (62, 66) is scribed over the pilot groove and the wafer is broken along the singulation groove (62, 66). the singulation groove (62, 66) is wider and deeper than the pilot groove; the singulation groove (62, 66) is scribed over the pilot groove and the wafer is broken along the singulation groove (62, 66).
A light emitting device comprising a plurality of GaN-based light emitting diodes monolithically formed in a two-dimensional pattern having an even number of rows on an insulating substrate, wherein the plurality of light emitting diodes form two groups having an equal number of light emitting diodes, wherein within each of the two groups the light emitting diodes are electrically connected in series to form a light emitting diode array and the two light emitting diode arrays are electrically connected in parallel between two electrodes such that the two light emitting diode arrays are of opposite polarities, characterized in that the light emitting diodes and the two electrodes have a planar shape of triangle, the light emitting diodes, except for the light emitting diodes arranged adjacent to the two electrodes, are arranged two by two opposing to each other at one side of the triangle so that two light emitting diodes form an approximate square and the opposing sides of two light emitting diodes form an common n electrode, and the two electrodes are each arranged opposing to the adjacent light emitting diode at one side of the triangle to each form an approximate square with the adjacent light emitting diode.
A method of operating an aircraft, the method comprising: obtaining, by a processing system, one or more user inputs to initiate an automated action to be performed by a system onboard the aircraft, the automated action comprising an autonomous adjustment by the system to a mechanical or electrical configuration of an onboard component to influence the aircraft's travel; obtaining, by the processing system, current status information for the aircraft; determining, by the processing system, a pilot objective based at least in part on the current status information and the one or more user inputs to initiate the automated action; determining, by the processing system, a projected aircraft behavior based on the current status information and the one or more user inputs to initiate the automated action, wherein determining the projected aircraft behavior comprises determining an anticipated response for the system to the one or more user inputs to initiate the automated action; identifying, by the processing system, a difference between the projected aircraft behavior and the pilot objective; providing, by the processing system via a user interface, guidance information pertaining to the automated action in response to identifying the difference, wherein the guidance information comprises an indication of a remedial action to achieve the pilot objective. obtaining, by a processing system, one or more user inputs to initiate an automated action to be performed by a system onboard the aircraft, the automated action comprising an autonomous adjustment by the system to a mechanical or electrical configuration of an onboard component to influence the aircraft's travel; obtaining, by the processing system, current status information for the aircraft; determining, by the processing system, a pilot objective based at least in part on the current status information and the one or more user inputs to initiate the automated action; determining, by the processing system, a projected aircraft behavior based on the current status information and the one or more user inputs to initiate the automated action, wherein determining the projected aircraft behavior comprises determining an anticipated response for the system to the one or more user inputs to initiate the automated action; identifying, by the processing system, a difference between the projected aircraft behavior and the pilot objective; providing, by the processing system via a user interface, guidance information pertaining to the automated action in response to identifying the difference, wherein the guidance information comprises an indication of a remedial action to achieve the pilot objective.
An aerosol container 1 comprising: an outer casing comprising a body 50 and cone 60; and a composite spout 30 and bag 40 combination within the outer casing; wherein the composite spout 30 has a tubular section 10 adapted to accommodate a valve arrangement 70, 75 and a plastic fishtail section 20, adapted to form a leak-proof seal with the bag 40; characterised in that the bag 40 contains a product and is made from a multilayer film, having a metal foil layer, to provide a barrier against propellant, interspersed between plastic layers, to protect the foil and to form a secure bond with the fishtail section 20, and wherein the tubular section 10 is made from a polymer coated metal and the fishtail section 20 is insert moulded onto the tubular section 10; and wherein a volume defined between the outside of the bag 40 and the inside of the body 50 and cone 60 is pressurised with propellant and sealed by a valve cup 75 and valve 70, such that an outer surface of the tubular section is exposed to propellant. an outer casing comprising a body 50 and cone 60; and a composite spout 30 and bag 40 combination within the outer casing; wherein the composite spout 30 has a tubular section 10 adapted to accommodate a valve arrangement 70, 75 and a plastic fishtail section 20, adapted to form a leak-proof seal with the bag 40; characterised in that the bag 40 contains a product and is made from a multilayer film, having a metal foil layer, to provide a barrier against propellant, interspersed between plastic layers, to protect the foil and to form a secure bond with the fishtail section 20, and wherein the tubular section 10 is made from a polymer coated metal and the fishtail section 20 is insert moulded onto the tubular section 10; and wherein a volume defined between the outside of the bag 40 and the inside of the body 50 and cone 60 is pressurised with propellant and sealed by a valve cup 75 and valve 70, such that an outer surface of the tubular section is exposed to propellant.
A method for measuring distance in a pipeline, comprising: opening the pipeline; disposing a first subsystem of a robotic measuring system into the pipeline at a known location; disposing a second subsystem of the robotic measuring system into the pipeline such that there is a line of sight between the first and second subsystems; actuating a measurement capture process by the robotic measuring system to generate a distance measurement between the first and second subsystems, the measurement capture process including generating a laser beam from one of the first or second subsystems and reflecting it from the other of the first or second subsystems; and characterized in that the method comprises alternately moving the first and second subsystems in the same direction along a length of the pipeline and actuating the measurement capture process after each movement of the first and second subsystems. opening the pipeline; disposing a first subsystem of a robotic measuring system into the pipeline at a known location; disposing a second subsystem of the robotic measuring system into the pipeline such that there is a line of sight between the first and second subsystems; actuating a measurement capture process by the robotic measuring system to generate a distance measurement between the first and second subsystems, the measurement capture process including generating a laser beam from one of the first or second subsystems and reflecting it from the other of the first or second subsystems; and characterized in that the method comprises alternately moving the first and second subsystems in the same direction along a length of the pipeline and actuating the measurement capture process after each movement of the first and second subsystems.
Particulate carbon material from renewable raw materials, which has - a 14 C content corresponding to that of renewable raw materials of greater than 0.20 Bq/g of carbon and less than 0.45 Bq/g of carbon, - an STSA surface area of at least 5 m 2 /g and at most 200 m 2 /g, and - an oil absorption value between 50 ml/100 g and 150 ml/100 g, and which is characterized by - a carbon content, based on the ash-free dry substance, between 60 wt.-% and 80 wt.-%. - a 14 C content corresponding to that of renewable raw materials of greater than 0.20 Bq/g of carbon and less than 0.45 Bq/g of carbon, - an STSA surface area of at least 5 m 2 /g and at most 200 m 2 /g, and - an oil absorption value between 50 ml/100 g and 150 ml/100 g, - a carbon content, based on the ash-free dry substance, between 60 wt.-% and 80 wt.-%.
An automatic ice maker apparatus arranged for use on a refrigerator or freezer door comprising: an elongated mold having a curved bottom wall with a first edge on one side of the mold and a second edge on a second side of the mold; a plurality of transverse partial partition walls within the mold defining a plurality of cavities to contain water to be frozen into ice pieces; a fill trough extending along the second edge above the mold; and at least one opening in the fill trough for water to flow into the mold from the fill trough, characterized in that the fill trough is arranged aside the mold and forms a continuous extension of the curved bottom wall at the second edge and in that it extends along substantially the entire length of the elongated mold. an elongated mold having a curved bottom wall with a first edge on one side of the mold and a second edge on a second side of the mold; a plurality of transverse partial partition walls within the mold defining a plurality of cavities to contain water to be frozen into ice pieces; a fill trough extending along the second edge above the mold; and at least one opening in the fill trough for water to flow into the mold from the fill trough,
A method of making N-(2,4-dinitrophenyl)-4-nitrobenzamide comprising the steps of: a) forming a first mixture comprising 2,4-dinitroaniline and 4-nitrobenzoyl chloride in an organic solvent; b) reacting the first mixture at a temperature of at least 90 °C in the presence of a solid acid catalyst, wherein the solid acid catalyst is not soluble in the organic solvent, to form a second mixture comprising N-(2,4-dinitrophenyl)-4-nitrobenzamide and the organic solvent, wherein the solid acid catalyst is an acidic clay, an ion exchange resin, a beta zeolite, a sulfonated tetrafluoroethylene-based fluoropolymer-copolymer, or some mixture thereof; c) cooling the second mixture to precipitate the N-(2,4-dinitrophenyl)-4-nitrobenzamide as a solid; and d) removing the solid N-(2,4-dinitrophenyl)-4-nitrobenzamide from the second mixture. a) forming a first mixture comprising 2,4-dinitroaniline and 4-nitrobenzoyl chloride in an organic solvent; b) reacting the first mixture at a temperature of at least 90 °C in the presence of a solid acid catalyst, wherein the solid acid catalyst is not soluble in the organic solvent, to form a second mixture comprising N-(2,4-dinitrophenyl)-4-nitrobenzamide and the organic solvent, wherein the solid acid catalyst is an acidic clay, an ion exchange resin, a beta zeolite, a sulfonated tetrafluoroethylene-based fluoropolymer-copolymer, or some mixture thereof; c) cooling the second mixture to precipitate the N-(2,4-dinitrophenyl)-4-nitrobenzamide as a solid; and d) removing the solid N-(2,4-dinitrophenyl)-4-nitrobenzamide from the second mixture.