mhurhangee/ep-ind-claims huggingface dataset:
A method comprising: presenting to a user a window comprising at least both of: a) one or more controls for editing an object; and b) a modal-less save interface comprising an editable text box; wherein the save interface is configured to permit executing save operations on the object without launching a modal window for the save operations; receiving, via the one or more controls, one or more commands to add to or modify data inside the object, thereby creating a modified object; receiving, via the save interface, textual input in the editable text box that indicates a location at which to save the modified object; wherein the save interface is configured to receive the textual input without requiring the user to navigate menu items; in response to the input that specifies a location at which to save the modified object, storing the modified object at the location; wherein the method is performed by one or more computing devices. presenting to a user a window comprising at least both of: a) one or more controls for editing an object; and b) a modal-less save interface comprising an editable text box; a) one or more controls for editing an object; and b) a modal-less save interface comprising an editable text box; wherein the save interface is configured to permit executing save operations on the object without launching a modal window for the save operations; receiving, via the one or more controls, one or more commands to add to or modify data inside the object, thereby creating a modified object; receiving, via the save interface, textual input in the editable text box that indicates a location at which to save the modified object; wherein the save interface is configured to receive the textual input without requiring the user to navigate menu items; in response to the input that specifies a location at which to save the modified object, storing the modified object at the location; wherein the method is performed by one or more computing devices.
A semiconductor light emitting element, comprising: an insulating substrate having a plurality of convexes on its surface, a plurality of light emitting element components (10a, 10b, 10c, 10d) that have semiconductor laminates that are laminated on the insulating substrate and are separated from one another by a groove that expose the convexes on the surface of the insulating substrate, a connector that connects between the light emitting element components, plurality of the light emitting element components include a first light emitting element component and a second light emitting element component, the first light emitting element component is separated from the second light emitting element component with the groove in between, and has a first protrusion that protrudes toward the second light emitting element component, the connector includes a first connector that has a shape that straddles the groove separating the first protrusion and the second light emitting element component and that follows the convexes on the surface of the insulating substrate, and has a straight section running from the first protrusion toward the second light emitting element component, and an insulating film that covers the groove, side faces of the semiconductor laminate adjacent to the groove, and the semiconductor laminate directly under the connector; wherein the connector is disposed along a side surface of the first light emitting element component, a bottom surface of the groove and a side surface of the second light emitting element component. an insulating substrate having a plurality of convexes on its surface, a plurality of light emitting element components (10a, 10b, 10c, 10d) that have semiconductor laminates that are laminated on the insulating substrate and are separated from one another by a groove that expose the convexes on the surface of the insulating substrate, a connector that connects between the light emitting element components, plurality of the light emitting element components include a first light emitting element component and a second light emitting element component, the first light emitting element component is separated from the second light emitting element component with the groove in between, and has a first protrusion that protrudes toward the second light emitting element component, the connector includes a first connector that has a shape that straddles the groove separating the first protrusion and the second light emitting element component and that follows the convexes on the surface of the insulating substrate, and has a straight section running from the first protrusion toward the second light emitting element component, and an insulating film that covers the groove, side faces of the semiconductor laminate adjacent to the groove, and the semiconductor laminate directly under the connector; wherein the connector is disposed along a side surface of the first light emitting element component, a bottom surface of the groove and a side surface of the second light emitting element component.
A construction element, comprising: a base, made flat and having a rectangular form, sides of which having a length in multiples of «a», and an interlocking joint, created by protrusions (2, 3, 4, 6) on the base, the protrusions (2, 3, 4, 6) forming four groups, wherein a first group has protrusions, positioned at least on one side of the base, with a height greater than «0.5a» but not more than «a», made with a cross-shaped cross-section, where a distance between opposing ends of the cross is equal to «a», a second group has protrusions, positioned at least on one side of the base, with a height equal to «0.5a», made tubular with cross-sections in a form of square having side length in the tubular protrusion channel equal to «a», a third group has protrusions, made in a form of rectangular plates, positioned with its longest midline on ends of the base, flush with these ends, having, along short sides, ledges, with a width equal to «a», protruding not more than «0.5a» from the base ends, angled towards each other with a gap formed between their end parts no greater than «a», a fourth group has protrusions made in a form of corners, having shelves positioned perpendicular to the planes of the base on its adjacent ends, flush with these ends, having a length equal to «a», a width not greater than «0.5a», wherein the protrusions (2, 3, 4, 6) of the first to fourth group are positioned on the base either in accordance with a coordinate grid of mutually perpendicular lines parallel to base edges, wherein a distance between neighboring lines on the coordinate grid is equal to «2a» and a distance between edges and neighboring lines on the coordinate grid is equal to «0.5a, or in accordance with diagonal grid lines which run diagonally to the aforementioned coordinate grid, wherein the protrusions of the first group are positioned at points where coordinate grid lines intersect, the protrusions of the second group arc positioned at points where diagonal grid lines of the coordinate grid intersect, the protrusions of the third group are positioned in a middle between neighboring protrusions of the first group that are positioned flush with the ends of the base, and the protrusions of the fourth group are positioned at the corners of the base.
A chrome-plated part, comprising: a substrate; a bright nickel plating layer formed over the substrate; a noble potential nickel plating layer formed on the bright nickel plating layer, wherein an electric potential difference between the bright nickel plating layer and the noble potential nickel plating layer is within a range from 60 mV to 150 mV; and a trivalent chrome plating layer formed on the noble potential nickel plating layer and having at least any one of a microporous structure and a microcrack structure, wherein the trivalent chrome plating layer contains 4.0 at% or more of carbon and has 10000/cm 2 or more of fine pores. a substrate; a bright nickel plating layer formed over the substrate; a noble potential nickel plating layer formed on the bright nickel plating layer, wherein an electric potential difference between the bright nickel plating layer and the noble potential nickel plating layer is within a range from 60 mV to 150 mV; and a trivalent chrome plating layer formed on the noble potential nickel plating layer and having at least any one of a microporous structure and a microcrack structure, wherein the trivalent chrome plating layer contains 4.0 at% or more of carbon and has 10000/cm 2 or more of fine pores.
A system (10; 50) for dispensing, to livestock, fodder, concentrate and/or straw or sawdust, intended to form a litter for said livestock, characterized in that it comprises: - at least one tool (12, 13; 60; 70) for dispensing fodder, concentrate and/or straw or sawdust, belonging to the group comprising at least: - mixer; - silo unloader; - bale unroller; - litter distributor; - radial sweeper; - bale clamp, able to be supplied with electrical energy; and - a self-guided electric vehicle (11; 51) having reversible attachment means with said tool (12, 13; 60; 70) comprising means for electrical connection with said tool (12, 13; 60; 70). - at least one tool (12, 13; 60; 70) for dispensing fodder, concentrate and/or straw or sawdust, belonging to the group comprising at least: - mixer; - silo unloader; - bale unroller; - litter distributor; - radial sweeper; - bale clamp, able to be supplied with electrical energy; and - mixer; - silo unloader; - bale unroller; - litter distributor; - radial sweeper; - bale clamp, - a self-guided electric vehicle (11; 51) having reversible attachment means with said tool (12, 13; 60; 70) comprising means for electrical connection with said tool (12, 13; 60; 70).
An endoscope with lateral illumination, having an elongated endoscope shaft with an outer tube, in the distal area of which is arranged an input lens with a viewing direction pivotable in at least one pivot plane, wherein the endoscope shaft accommodates several illumination optical-fiber bundles (20, 22), which terminate at output surfaces at a distal tip of the endoscope shaft, wherein at least a first illumination optical-fiber bundle generates an illumination, at a 0° viewing angle, of an area lying in front of the distal tip of the endoscope shaft, and at least a second illumination optical-fiber bundle generates an illumination of another area with a lateral viewing angle or lateral viewing-angle range of between 0° and 90°, characterized in that one or more light-emitting diodes (24, 26) are arranged in or on the circumference of the endoscope shaft in the area of the distal tip, wherein the light-emitting diode or light-emitting diodes (24, 26) are arranged in the pivot plane and/or around the pivot plane, in order to generate an illumination at a viewing angle or a viewing-angle range about 90°.
A double-sided cutting insert, comprising: a pair of end surfaces facing each other; and a pair of first side surfaces and a pair of second side surfaces connecting the end surfaces and facing each other; wherein a first cutting edge and a second cutting edge are formed by the intersection of each first side surface and second side surface, wherein the first cutting edges and the second cutting edges in the first side surface are diagonally symmetrical with respect to a first imaginary median plane which transverses the middles of both the first side surfaces facing each other, and wherein the first cutting edges and the second cutting edges in the second side surface are diagonally symmetrical with respect to a second imaginary median plane, which transverses the middles of both the second side surfaces facing each other, characterised in that the second cutting edge is offset toward the first median plane from the first cutting edge and obliquely extends from a corner of the cutting insert toward the first median plane, wherein the first cutting edge is offset toward the second median plane from the second cutting edge and obliquely extends from the corner of the cutting insert toward the second median plane. a pair of end surfaces facing each other; and a pair of first side surfaces and a pair of second side surfaces connecting the end surfaces and facing each other; wherein a first cutting edge and a second cutting edge are formed by the intersection of each first side surface and second side surface, wherein the first cutting edges and the second cutting edges in the first side surface are diagonally symmetrical with respect to a first imaginary median plane which transverses the middles of both the first side surfaces facing each other, and wherein the first cutting edges and the second cutting edges in the second side surface are diagonally symmetrical with respect to a second imaginary median plane, which transverses the middles of both the second side surfaces facing each other, characterised in that the second cutting edge is offset toward the first median plane from the first cutting edge and obliquely extends from a corner of the cutting insert toward the first median plane, wherein the first cutting edge is offset toward the second median plane from the second cutting edge and obliquely extends from the corner of the cutting insert toward the second median plane.
An X-ray imaging device comprising: a radiography unit having an X-ray source and an X-ray sensor disposed to face each other with a rotating axis therebetween, wherein the X-ray sensor is configured to obtain X-ray transmission images (St1, St2, St3; Sb11, Sb12, Sb13; Sf11, Sf12, Sf13); a driver configured to rotate the X-ray source and the X-ray sensor about the rotating axis; and characterised by an image processor configured to provide a two-dimensional tomographic image of an image layer disposed between the rotating axis and the X-ray source, by shifting and overlapping the X-ray transmission images after reversing left to right at least some of the X-ray transmission images, wherein the image processor is configured to reverse at least some of the X-ray transmission images left to right, and the reversed X-ray transmission images are shifted in a moving direction of the X-ray sensor and overlapped with each other, whereby the two-dimensional tomographic image (Sb1; f1) of the image layer is provided. a radiography unit having an X-ray source and an X-ray sensor disposed to face each other with a rotating axis therebetween, wherein the X-ray sensor is configured to obtain X-ray transmission images (St1, St2, St3; Sb11, Sb12, Sb13; Sf11, Sf12, Sf13); a driver configured to rotate the X-ray source and the X-ray sensor about the rotating axis; and characterised by an image processor configured to provide a two-dimensional tomographic image of an image layer disposed between the rotating axis and the X-ray source, by shifting and overlapping the X-ray transmission images after reversing left to right at least some of the X-ray transmission images, wherein the image processor is configured to reverse at least some of the X-ray transmission images left to right, and the reversed X-ray transmission images are shifted in a moving direction of the X-ray sensor and overlapped with each other, whereby the two-dimensional tomographic image (Sb1; f1) of the image layer is provided.
A gas turbine engine comprising: a core flow passage; a bypass flow passage; a propulsor arranged at an inlet of said bypass flow passage and said core flow passage, said propulsor including a row of propulsor blades which includes 17 to 20 blades, and having a pressure ratio of between 1.2 and 1.7 across said propulsor blades, wherein said propulsor is coupled to be driven by a turbine through a spool, and a gear assembly is coupled between said propulsor and said spool such that rotation of said turbine drives said propulsor at a different speed than said spool; and a case surrounding said propulsor, wherein said case and said propulsor blades include a carbon-fiber reinforced polymer matrix material, wherein each of said propulsor blades includes an airfoil body and a sheath secured on a leading edge of said airfoil body, and wherein each of said propulsor blades further includes a first distinct region of carbon-fiber reinforced polymer matrix material and a second distinct region of a non-carbon-fiber reinforced polymer matrix material, and characterised in that: said carbon-fiber reinforced polymer matrix material of said propulsor blades is different from said carbon-fiber reinforced polymer matrix material of said case with respect to composition; and said polymer of said carbon-fiber reinforced polymer matrix material of each of said propulsor blades is a thermoplastic polymer and the airfoil body of each of said propulsor blades has a distinct core that supports a skin of said carbon-fiber reinforced polymer matrix material. a core flow passage; a bypass flow passage; a propulsor arranged at an inlet of said bypass flow passage and said core flow passage, said propulsor including a row of propulsor blades which includes 17 to 20 blades, and having a pressure ratio of between 1.2 and 1.7 across said propulsor blades, wherein said propulsor is coupled to be driven by a turbine through a spool, and a gear assembly is coupled between said propulsor and said spool such that rotation of said turbine drives said propulsor at a different speed than said spool; and a case surrounding said propulsor, wherein said case and said propulsor blades include a carbon-fiber reinforced polymer matrix material, wherein each of said propulsor blades includes an airfoil body and a sheath secured on a leading edge of said airfoil body, and wherein each of said propulsor blades further includes a first distinct region of carbon-fiber reinforced polymer matrix material and a second distinct region of a non-carbon-fiber reinforced polymer matrix material, and characterised in that: said carbon-fiber reinforced polymer matrix material of said propulsor blades is different from said carbon-fiber reinforced polymer matrix material of said case with respect to composition; and said polymer of said carbon-fiber reinforced polymer matrix material of each of said propulsor blades is a thermoplastic polymer and the airfoil body of each of said propulsor blades has a distinct core that supports a skin of said carbon-fiber reinforced polymer matrix material.
An apparatus comprising: a support structure; a positioning system associated with the support structure and configured to position the support structure with respect to a number of linear axes; and a retention system associated with the support structure and configured to retain a portion of an object and move the portion of the object towards a platform such that the portion of the object substantially conforms to a shape of the platform, characterised in that the apparatus comprises: an attachment system configured for use in attaching a tool to the support structure, wherein the attachment system comprises a number of rails usable to hold the tool and to allow the tool to move along the support structure. a support structure; a positioning system associated with the support structure and configured to position the support structure with respect to a number of linear axes; and a retention system associated with the support structure and configured to retain a portion of an object and move the portion of the object towards a platform such that the portion of the object substantially conforms to a shape of the platform, characterised in that the apparatus comprises: an attachment system configured for use in attaching a tool to the support structure, wherein the attachment system comprises a number of rails usable to hold the tool and to allow the tool to move along the support structure.
A cooking attachment for a heatable vessel of a food processor, wherein said cooking attachment features one or more bottom openings, through which steam exiting the vessel can enter the cooking attachment and condensate can flow from the cooking attachment into the vessel, characterized in that the cooking attachment features a heating device, which provides heating irrespective of the steam exiting the vessel.
A gas turbine engine, comprising: a first engine component and a second engine component, the first engine component having a mate face adjacent a mate face of the second engine component; and a seal between the mate face of the first engine component and the mate face of the second engine component, wherein the seal includes a central curved portion near a centerline of the seal, and curved ends distal from the central curved portion, the curved ends connected to the central curved portion by sloped walls extending from opposed sides of the central curved portion, the central curved portion including a curvature substantially corresponding to a first radius (R 1), and the curved ends including a curvature substantially corresponding to a second radius (R 2) smaller than the first radius (R 1); wherein the seal establishes three points of contact (P 1, P 2, P 3) with each mate face in at least one condition; in the at least one condition, each sloped wall contacts a respective one of the mate faces (74, 76) to provide a first point of contact (P 1) between the seal and the respective mate face (74, 76), and each curved end contacts a respective one of the mate faces (74, 76) at two distinct points to provide second and third points of contact (P 2, P 3) between the seal and the respective mate face (74, 76); and the first radius (R 1) has an origin radially spaced from the seal and characterised in that the first radius origin is on a high pressure side (P HIGH) of the seal and on the same side of the seal as origins of the second radii (R 2). a first engine component and a second engine component, the first engine component having a mate face adjacent a mate face of the second engine component; and a seal between the mate face of the first engine component and the mate face of the second engine component, wherein the seal includes a central curved portion near a centerline of the seal, and curved ends distal from the central curved portion, the curved ends connected to the central curved portion by sloped walls extending from opposed sides of the central curved portion, the central curved portion including a curvature substantially corresponding to a first radius (R 1), and the curved ends including a curvature substantially corresponding to a second radius (R 2) smaller than the first radius (R 1); wherein the seal establishes three points of contact (P 1, P 2, P 3) with each mate face in at least one condition; in the at least one condition, each sloped wall contacts a respective one of the mate faces (74, 76) to provide a first point of contact (P 1) between the seal and the respective mate face (74, 76), and each curved end contacts a respective one of the mate faces (74, 76) at two distinct points to provide second and third points of contact (P 2, P 3) between the seal and the respective mate face (74, 76); and the first radius (R 1) has an origin radially spaced from the seal and characterised in that the first radius origin is on a high pressure side (P HIGH) of the seal and on the same side of the seal as origins of the second radii (R 2).
A reciprocating compressor comprising a crank mechanism, said crank mechanism being of the type suitable for fixedly connecting to a rod (24, 24A, 24B) of a piston (22, 22A, 22B) of the compressor and to a crank shaft, said crank mechanism comprising at least one cross head arranged to be operatively connected to said crank shaft through a connecting rod and to said rod (24, 24A, 24B) and to reciprocate inside at least two opposite tracks (18, 20), said cross head being further provided with at least two opposite sliding shoes (40, 42) arranged to respectively face onto said tracks (18, 20), characterized in that one of said sliding shoes is equipped with a surface for making contact with said tracks (18, 20) having a different oil distribution arrangement shape and/or size with respect to the contact surface of the opposite sliding shoe, wherein the tracks (18, 20) have lubricating oil inlet holes (44, 46) to cover lubricating oil over all of the contact surfaces filling all the spaces between the tracks (18, 20) and the sliding shoes (40, 42).