mhurhangee/ep-ind-claims huggingface dataset:
An article processing apparatus which is used in a production line of an article and processes the article, comprising: a storage case configured to store an electric circuit portion, the electric circuit portion configured to control the article processing apparatus, the article processing apparatus characterized in that: the storage case has an opening at a side surface thereof, and a lid which seals the opening, wherein the storage case has an upper surface which is inclined downward toward the side surface side, and an amount of protrusion of a lower end of the upper surface from the side surface is greater than an amount of protrusion of the lid from the side surface, wherein the storage case includes a protruding portion which is disposed along at least an upper side edge portion of the opening and is covered by the lid, the protruding portion has an overhanging portion which overhangs toward outside from the side surface and extends along the side surface, and the overhanging portion is inclined downward such that at least one end portion in an extension direction thereof serves as a lower end. a storage case configured to store an electric circuit portion, the electric circuit portion configured to control the article processing apparatus, the article processing apparatus characterized in that: the storage case has an opening at a side surface thereof, and a lid which seals the opening, wherein the storage case has an upper surface which is inclined downward toward the side surface side, and an amount of protrusion of a lower end of the upper surface from the side surface is greater than an amount of protrusion of the lid from the side surface, wherein the storage case includes a protruding portion which is disposed along at least an upper side edge portion of the opening and is covered by the lid, the protruding portion has an overhanging portion which overhangs toward outside from the side surface and extends along the side surface, and the overhanging portion is inclined downward such that at least one end portion in an extension direction thereof serves as a lower end.
A grinding device for machining a surface, having: a grinding machine coupled to a manipulator with a motor and a grinding tool driven by the motor; a controller which is designed for: controlling the grinding machine in order to adjust the speed of the grinding tool, positioning the grinding machine by means of the manipulator in order to contact the surface with the grinding tool while the grinding machine is operated at a first speed (n 0), detecting contact between the grinding tool and the surface, and increasing the speed of the grinding tool from the first speed (n 0) to a second speed (n 1) in response to the detection of a contact. a grinding machine coupled to a manipulator with a motor and a grinding tool driven by the motor; a controller which is designed for: controlling the grinding machine in order to adjust the speed of the grinding tool, positioning the grinding machine by means of the manipulator in order to contact the surface with the grinding tool while the grinding machine is operated at a first speed (n 0), detecting contact between the grinding tool and the surface, and increasing the speed of the grinding tool from the first speed (n 0) to a second speed (n 1) in response to the detection of a contact. controlling the grinding machine in order to adjust the speed of the grinding tool, positioning the grinding machine by means of the manipulator in order to contact the surface with the grinding tool while the grinding machine is operated at a first speed (n 0), detecting contact between the grinding tool and the surface, and increasing the speed of the grinding tool from the first speed (n 0) to a second speed (n 1) in response to the detection of a contact.
A computer implemented method for designing a part comprising the steps of: - providing a surface and a base curve lying on the surface; - sampling the base curve (C 0) into a list of base points ( B i); - determining a grid of points of perpendicular geodesic curves ( SPQ i), the points belonging to a respective level, each level corresponding to a respective geodesic distance to the base curve (C 0), wherein each perpendicular geodesic curve ( SPC i) lies on the surface and departs perpendicularly from the base curve (C 0) at a respective base point ( B i); then, - computing a plurality of parallel geodesic curves (C 1,...,C n) lying on the surface by using the grid of points, each parallel geodesic curve corresponding to a respective level; and - displaying a representation of the part. - providing a surface and a base curve lying on the surface; - sampling the base curve (C 0) into a list of base points ( B i); - determining a grid of points of perpendicular geodesic curves ( SPQ i), the points belonging to a respective level, each level corresponding to a respective geodesic distance to the base curve (C 0), wherein each perpendicular geodesic curve ( SPC i) lies on the surface and departs perpendicularly from the base curve (C 0) at a respective base point ( B i); then, - computing a plurality of parallel geodesic curves (C 1,...,C n) lying on the surface by using the grid of points, each parallel geodesic curve corresponding to a respective level; and - displaying a representation of the part.
Aircraft comprising a fuselage and a trimmable horizontal stabilizer in its rear zone actuated by a trimming actuator; the trimmable horizontal stabilizer comprising a load-bearing structure extending in the span direction; the load-bearing structure having a portion disposed inside the rear fuselage that includes at least one pivot element coupled to a pivoting device for rotating about a lateral axis and a connection fitting with the trimming actuator such that: - the rear fuselage comprises at least a first section having a resistant fuselage, i.e. comprising a skin reinforced by longitudinal stringers and transversal frames, and a second section, aft to the first section, having a non resistant fuselage, i.e. a fairing; - said portion of the load-bearing structure and said trimming actuator are disposed inside the second section of the rear fuselage; - the at least one pivot element is mounted on the forward side of said portion of the load-bearing structure and coupled to the first section of the rear fuselage; - the connection fitting is mounted on the rearward side of said portion of the load-bearing structure and the trimming actuator is disposed so that it exerts a force in the direction of the Z-axis of the aircraft over the connection fitting during a trimming operation; - the aircraft also comprises a supporting structure of the trimming actuator in the second section arranged for transmitting the trimming actuator loads to the first section; - the first section of the rear fuselage comprises a bulkhead including the pivoting device to which is coupled the at least one pivot element of the trimmable horizontal stabilizer; characterized in that the supporting structure of the trimming actuator comprises upper and lower longitudinal beams (53, 55) joined to the bulkhead and extended to a position aft to the connection fitting and a vertical beam joined to the rear ends of the upper and lower longitudinal beams (53, 55). - the rear fuselage comprises at least a first section having a resistant fuselage, i.e. comprising a skin reinforced by longitudinal stringers and transversal frames, and a second section, aft to the first section, having a non resistant fuselage, i.e. a fairing; - said portion of the load-bearing structure and said trimming actuator are disposed inside the second section of the rear fuselage; - the at least one pivot element is mounted on the forward side of said portion of the load-bearing structure and coupled to the first section of the rear fuselage; - the connection fitting is mounted on the rearward side of said portion of the load-bearing structure and the trimming actuator is disposed so that it exerts a force in the direction of the Z-axis of the aircraft over the connection fitting during a trimming operation; - the aircraft also comprises a supporting structure of the trimming actuator in the second section arranged for transmitting the trimming actuator loads to the first section; - the first section of the rear fuselage comprises a bulkhead including the pivoting device to which is coupled the at least one pivot element of the trimmable horizontal stabilizer;
A delivery device for delivering a stent to a body lumen and expanding the stent, the delivery device comprising: a first axis; a second axis perpendicular to the first axis; an expandable central balloon comprising first and second opposite sides and centered on the intersection of the first and second axes (210, 212); a first expandable side balloon positioned adjacent to the first side of the central balloon and centered on the first axis; and, a second expandable side balloon positioned adjacent to the second side of the central balloon and centered on the first axis; characterized by a first width of the device measured along the first axis being greater than a second width of the device measured along the second axis. a first axis; a second axis perpendicular to the first axis; an expandable central balloon comprising first and second opposite sides and centered on the intersection of the first and second axes (210, 212); a first expandable side balloon positioned adjacent to the first side of the central balloon and centered on the first axis; and, a second expandable side balloon positioned adjacent to the second side of the central balloon and centered on the first axis; characterized by a first width of the device measured along the first axis being greater than a second width of the device measured along the second axis.
A feeder insert (1, 1', 1", 1′′′, 100, 100') for use in metal casting in casting molds, having a feeder body (2, 2', 2", 2"', 102, 102') which delimits a feeder cavity (4, 4', 4", 4′′′, 104, 104') for receiving liquid metal, wherein - the feeder body (2, 2', 2", 2′′′, 102, 102') has a first end (6, 6', 6", 6′′′, 106, 106') with a passage opening for the liquid metal and a second end (10, 10', 10", 10′′′, 110, 110') opposite to the first end (6, 6', 6", 106, 106'), and wherein - the feeder body (2, 2', 2", 2′′′, 102, 102') comprises a central axis extending through the passage opening, characterized in that the feeder body (2, 2', 2", 2′′′, 102, 102') is separated at at least one partition plane extending in a direction of the central axis and is formed from at least a first feeder shell (18, 18', 18", 18′′′, 118, 118') and a second feeder shell (20, 20', 20", 20′′′, 120, 120'), wherein the first and second feeder shells (18, 18', 18", 18′′′, 118, 118') are connected to each other to form the feeder body (2, 2', 2", 2′′′, 102, 102')and wherein the first and second feeder shells are substantially identically formed. - the feeder body (2, 2', 2", 2′′′, 102, 102') has a first end (6, 6', 6", 6′′′, 106, 106') with a passage opening for the liquid metal and a second end (10, 10', 10", 10′′′, 110, 110') opposite to the first end (6, 6', 6", 106, 106'), and wherein - the feeder body (2, 2', 2", 2′′′, 102, 102') comprises a central axis extending through the passage opening,
A tension buffer system (2, 3, 5, 7) for a multi-wire pay-off system, said tension buffer system (2, 3, 5, 7) comprising guiding pulleys (4, 4a, 4b) adapted to guide wires (6, 6a, 6b) being paid off, characterized in that said tension buffer system (2, 3, 5, 7) further comprises reversing pulleys, each reversing pulley being adapted to guide a wire (6, 6a, 6b) from one of said guiding pulleys (4, 4a, 4b) and back to one of said guiding pulleys (4,4a, 4b), two of said reversing pulleys being rotatably mounted on a first support, said first support being pivoted around a first support axis lying between said two reversing pulleys so that pivoting brings one of said two reversing pulleys closer to one of said guiding pulleys (4, 4a, 4b) while the other of said two reversing pulleys more remote from another of said guiding pulleys (4, 4a, 4b). said tension buffer system (2, 3, 5, 7) comprising guiding pulleys (4, 4a, 4b) adapted to guide wires (6, 6a, 6b) being paid off, characterized in that said tension buffer system (2, 3, 5, 7) further comprises reversing pulleys, each reversing pulley being adapted to guide a wire (6, 6a, 6b) from one of said guiding pulleys (4, 4a, 4b) and back to one of said guiding pulleys (4,4a, 4b), two of said reversing pulleys being rotatably mounted on a first support, said first support being pivoted around a first support axis lying between said two reversing pulleys so that pivoting brings one of said two reversing pulleys closer to one of said guiding pulleys (4, 4a, 4b) while the other of said two reversing pulleys more remote from another of said guiding pulleys (4, 4a, 4b).
An apparatus, in particular a fitting arrangement for windows, doors or the like, comprising a cover rail which is configured for fastening to a frame or to a leaf frame of the window, of the door or the like; a locking bar displaceable along a longitudinal extent of the cover rail between a release position and a closed position; and at least one locking element arranged at the locking bar, wherein the cover rail comprises a reception section having an inner space in which the locking bar, including the locking element, is arranged; wherein the cover rail has at least one introduction opening which opens into the inner space; wherein the locking element arranged in the inner space releases the introduction opening when the locking bar is in the release position; and wherein the locking element arranged in the inner space at least partly blocks the introduction opening when the locking bar is in the closed position, characterized in that the reception section comprises a cover which at least partly surrounds the inner space, which has a curved outer surface and which projects into a rebate gap formed between a frame and a leaf frame of the window, of the door or the like.
A method of sorting particles in a stream of carrier fluid, the method comprising: - introducing a stream of carrier fluid containing a mixture of particles into a stream of sheath fluid flowing within a flow channel so as to focus the carrier fluid into a core stream. - detecting a particle of interest within the core stream of carrier fluid at a point of detection within the flow channel, - applying a potential difference between a first electrode and one or more additional electrodes so as to generate a divergent electric field localised around a tip of the first electrode, wherein the tip of the first electrode is positioned inside of the flow channel or adjacent to the flow channel in a position in which the divergent electric field is experienced by the sheath fluid and carrier fluid within the flow channel, and - subsequently terminating application of the potential difference, characterised in that the potential difference is applied in response to the detection of a particle of interest, the applied potential difference being sufficient to generate a centripetal force on a volume of carrier fluid within the divergent electric field, said volume of carrier fluid containing the particle of interest, so as to displace said volume of carrier fluid in a direction having a component orthogonal to the direction of flow, such that the particle of interest is diverted into a desired outlet of the flow channel. - introducing a stream of carrier fluid containing a mixture of particles into a stream of sheath fluid flowing within a flow channel so as to focus the carrier fluid into a core stream. - detecting a particle of interest within the core stream of carrier fluid at a point of detection within the flow channel, - applying a potential difference between a first electrode and one or more additional electrodes so as to generate a divergent electric field localised around a tip of the first electrode, wherein the tip of the first electrode is positioned inside of the flow channel or adjacent to the flow channel in a position in which the divergent electric field is experienced by the sheath fluid and carrier fluid within the flow channel, and - subsequently terminating application of the potential difference,
A method for indicating spatial relation information, performed by a base station, the method comprising: sending, by the base station, indication information for Physical Uplink Control Channel, PUCCH, spatial relation information to a terminal, wherein the indication information is sent in a medium access control layer control element, MAC CE, comprising three Octets, the spatial relation information indicated by the indication information is applied to at least two PUCCH resources of the terminal; characterized in that the indication information carries spatial relation information for activation/deactivation of a spatial relation of the PUCCH resources in 8 bits in the third Octet but does not carry any PUCCH resource identifier in the second Octet, and the spatial relation information for activation/deactivation that is included in the 8 bits in the third Octet is used for all PUCCH resources configured for the terminal. sending, by the base station, indication information for Physical Uplink Control Channel, PUCCH, spatial relation information to a terminal, wherein the indication information is sent in a medium access control layer control element, MAC CE, comprising three Octets, the spatial relation information indicated by the indication information is applied to at least two PUCCH resources of the terminal; characterized in that the indication information carries spatial relation information for activation/deactivation of a spatial relation of the PUCCH resources in 8 bits in the third Octet but does not carry any PUCCH resource identifier in the second Octet, and the spatial relation information for activation/deactivation that is included in the 8 bits in the third Octet is used for all PUCCH resources configured for the terminal.
Reinforced masonry comprising at least one wall panel having at least one accessible face almost vertical and adjacent to a set of respective almost horizontal curb elements each one associated with the at least one wall panel; said reinforced masonry comprises a plurality of rod elements fixed, individually or in bundles and by means of fixing material, within respective hollow seats carried out, almost vertically and mutually spaced, at least in the accessible face of the at least one wall panel, wherein each rod element or respective segment is made of composite material comprising carbon and/or glass fibers or other mineral or organic fibres, embedded into an epoxy or polyurethane resin matrix or into adhesive mortar or the like, where the surface of each rod element is provided with gripping means consisting of at least one of adherent sand coating or other rough material, cavities, transverse engravings or protrusions or similar, or it lacks them, characterized in that said reinforced masonry comprises, for each hollow seat or group of hollow seats, a first reinforcing element fixed to portions of the at least one accessible face of the wall panel which are adjacent to the longitudinal development of the hollow seat or group of hollow seats, and rejoining such portions separated by the hollow seat; and in that said reinforced masonry further comprises, for at least one curb element, a second reinforcing element fixed to said curb element and/or to the portions of the wall panel or of the wall panels adjacent to it, and/or in that it comprises at least a second reinforcing element fixed to at least a horizontal portion of the edge of the wall panel; each first reinforcing element is made of fabric, as the quadriaxial type, and each second reinforcing element is of fabric, as unidirectional or bidirectional, or is mat, where such fabrics or mat are in carbon and/or glass fibres and/or other mineral or organic fibres and are embedded into a resinous matrix of the respective first and second reinforcing element, and they adhere to the masonry fixing these reinforcing elements (9, 11) to the masonry itself; the fixing material consisting of at least one of high-strength mortar and building adhesives, also incorporating inerts and/or reinforcing fibres.
A method for providing a data service in a network environment, comprising: providing a data service component on a first node in the network environment, wherein the network environment includes a plurality of nodes (111, 112, 113, 114) interconnected via a network fabric; providing a native data flow between second and third nodes in the network environment, wherein the second and third nodes are different from said first node; using a native packet forwarding mechanism to direct the native data flow in the network fabric to said data service component on the first node; and using said data service component to process one or more data packets in the native data flow in the network fabric such that the native data flow is handled without leaving the network fabric. providing a data service component on a first node in the network environment, wherein the network environment includes a plurality of nodes (111, 112, 113, 114) interconnected via a network fabric; providing a native data flow between second and third nodes in the network environment, wherein the second and third nodes are different from said first node; using a native packet forwarding mechanism to direct the native data flow in the network fabric to said data service component on the first node; and using said data service component to process one or more data packets in the native data flow in the network fabric such that the native data flow is handled without leaving the network fabric.