mhurhangee/patent-ind-claim-en huggingface dataset:
A method of manufacturing a bearing seal comprising the steps of: feeding a steel coil of a preselected width into a ring rolling machine , cutting a divided length of the steel coil and rolling the length of steel coil into a closed coil ring having a butted joint, the butted joint of the closed coil ring is welded to form a welded steel coil ring , transferring the welded steel coil ring to a weld bead removal station , then transferring to a weld flattening machine wherein any weld bead at the butted joint between the two cut ends of the steel coil ring is flattened to form a flattened steel coil ring, transferring the flattened steel coil ring to a first pre-forming machine wherein a first profile is formed in the flattened steel coil ring to form a first profiled steel coil ring , transferring the first profiled steel coil ring to a second pre-forming machine wherein a second profile is formed in the first profiled steel coil ring to form a second profiled steel coil ring , characterised by transferring the second profiled steel coil ring to a third pre-forming machine wherein a third profile is formed in the second profiled steel coil ring to form a third profiled steel coil ring, and transferring the third profiled steel coil ring to a final forming machine wherein a final profile is formed in the third profiled steel coil ring to form a final profiled steel coil bearing seal , wherein the first profile formed in the flattened steel coil ring is formed at an angle of about 90°, and wherein the second profile formed in the first profiled steel coil ring is formed at an angle of about 90°. feeding a steel coil of a preselected width into a ring rolling machine , cutting a divided length of the steel coil and rolling the length of steel coil into a closed coil ring having a butted joint, the butted joint of the closed coil ring is welded to form a welded steel coil ring , transferring the welded steel coil ring to a weld bead removal station , then transferring to a weld flattening machine wherein any weld bead at the butted joint between the two cut ends of the steel coil ring is flattened to form a flattened steel coil ring, transferring the flattened steel coil ring to a first pre-forming machine wherein a first profile is formed in the flattened steel coil ring to form a first profiled steel coil ring , transferring the first profiled steel coil ring to a second pre-forming machine wherein a second profile is formed in the first profiled steel coil ring to form a second profiled steel coil ring , characterised by transferring the second profiled steel coil ring to a third pre-forming machine wherein a third profile is formed in the second profiled steel coil ring to form a third profiled steel coil ring, and transferring the third profiled steel coil ring to a final forming machine wherein a final profile is formed in the third profiled steel coil ring to form a final profiled steel coil bearing seal , wherein the first profile formed in the flattened steel coil ring is formed at an angle of about 90°, and wherein the second profile formed in the first profiled steel coil ring is formed at an angle of about 90°.
An aircraft management system , comprising: a flight plan diversion prediction system including a rerouting control unit that is configured to generate a plurality of reroute options for an aircraft , wherein the rerouting control unit is configured to determine a clearpoint for the plurality of reroute options based on the current location, heading, and airspeed of the aircraft in relation to the current location, airspeed and direction of the in-flight hazard, allowing the rerouting control unit to predict the future position of the aircraft and the future position of the in-flight hazard, wherein the clearpoint is a location at which the aircraft will be clear of the in-flight hazard, and wherein the rerouting control unit is configured to determine the clearpoint by comparing the predicted future position of the aircraft and the predicted future position of the in-flight hazard, wherein the plurality of reroute options is generated based on an analysis of the current position of the aircraft , the predicted future position of the aircraft , the current position of an in-flight hazard, and the predicted future position of the in-flight hazard with each of the plurality of reroute options starting at the clearpoint , wherein the flight plan diversion prediction system further comprises a monitor in communication with the rerouting control unit , and wherein the rerouting control unit is configured to show the plurality of reroute options on the monitor . a flight plan diversion prediction system including a rerouting control unit that is configured to generate a plurality of reroute options for an aircraft , wherein the rerouting control unit is configured to determine a clearpoint for the plurality of reroute options based on the current location, heading, and airspeed of the aircraft in relation to the current location, airspeed and direction of the in-flight hazard, allowing the rerouting control unit to predict the future position of the aircraft and the future position of the in-flight hazard, wherein the clearpoint is a location at which the aircraft will be clear of the in-flight hazard, and wherein the rerouting control unit is configured to determine the clearpoint by comparing the predicted future position of the aircraft and the predicted future position of the in-flight hazard, wherein the plurality of reroute options is generated based on an analysis of the current position of the aircraft , the predicted future position of the aircraft , the current position of an in-flight hazard, and the predicted future position of the in-flight hazard with each of the plurality of reroute options starting at the clearpoint , wherein the flight plan diversion prediction system further comprises a monitor in communication with the rerouting control unit , and wherein the rerouting control unit is configured to show the plurality of reroute options on the monitor .
A method for artificially ageing stone blocks , in particular concrete blocks, clinker bricks and natural stone blocks, said method having the following features: according to which the stone blocks are conveyed through an ageing duct and the stone blocks are placed in this case in such a manner on a base of the ageing duct that a stone block surface of the stone blocks to be treated is aligned transversely with respect to the feed direction of the stone blocks through the ageing duct ; according to which several stone blocks placed one behind another are combined to form a stone block row and at least two stone block rows arranged side by side with reference to the feed direction are pushed together through the ageing duct ; and according to which the stone blocks , whilst they are being pushed through the ageing duct , are made to vibrate such that the stone blocks strike against an upper boundary of the ageing duct , characterized in that the ageing duct comprises a width or an extension between the two lateral boundaries of at least 45 cm, and in that in top view the stone blocks comprise the form of a trapezium, wherein the stone blocks are aligned in such a manner prior to being pushed through the ageing duct that the basic surfaces of the trapezoidal stone blocks extending parallel to one another are aligned transversely with respect to the feed direction. according to which the stone blocks are conveyed through an ageing duct and the stone blocks are placed in this case in such a manner on a base of the ageing duct that a stone block surface of the stone blocks to be treated is aligned transversely with respect to the feed direction of the stone blocks through the ageing duct ; according to which several stone blocks placed one behind another are combined to form a stone block row and at least two stone block rows arranged side by side with reference to the feed direction are pushed together through the ageing duct ; and according to which the stone blocks , whilst they are being pushed through the ageing duct , are made to vibrate such that the stone blocks strike against an upper boundary of the ageing duct , characterized in that the ageing duct comprises a width or an extension between the two lateral boundaries of at least 45 cm, and in that in top view the stone blocks comprise the form of a trapezium, wherein the stone blocks are aligned in such a manner prior to being pushed through the ageing duct that the basic surfaces of the trapezoidal stone blocks extending parallel to one another are aligned transversely with respect to the feed direction.
A power system, comprising N power supplies and M DC-to-AC units, wherein N is an integer greater than 1, and M is an integer greater than 1; each power supply of the N power supplies is configured with a positive output terminal and a negative output terminal, and each DC-to-AC unit of the M DC-to-AC units is configured with a positive input terminal, a negative input terminal, and an output terminal; the positive output terminal of a first power supply of the N power supplies is coupled to the positive input terminal of a first DC-to-AC unit of the M DC-to-AC units; the negative output terminal of an n th power supply of the N power supplies is coupled in series to the positive output terminal of an (n+1) th power supply of the N power supplies to form a first node , wherein n is an integer greater than 0 and less than N; the negative output terminal of an N th power supply of the N power supplies is coupled to the negative input terminal of an M th DC-to-AC unit of the M DC-to-AC units; the negative input terminal of an m th DC-to-AC unit of the M DC-to-AC units is coupled in series to the positive input terminal of an (m+1) th DC-to-AC unit of the M DC-to-AC units to form a second node , wherein m is an integer greater than 0 and less than M; characterized in that at least one first node and at least one second node are coupled; and output terminals of the DC-to-AC units are isolated for output. each power supply of the N power supplies is configured with a positive output terminal and a negative output terminal, and each DC-to-AC unit of the M DC-to-AC units is configured with a positive input terminal, a negative input terminal, and an output terminal; the positive output terminal of a first power supply of the N power supplies is coupled to the positive input terminal of a first DC-to-AC unit of the M DC-to-AC units; the negative output terminal of an n th power supply of the N power supplies is coupled in series to the positive output terminal of an (n+1) th power supply of the N power supplies to form a first node , wherein n is an integer greater than 0 and less than N; the negative output terminal of an N th power supply of the N power supplies is coupled to the negative input terminal of an M th DC-to-AC unit of the M DC-to-AC units; the negative input terminal of an m th DC-to-AC unit of the M DC-to-AC units is coupled in series to the positive input terminal of an (m+1) th DC-to-AC unit of the M DC-to-AC units to form a second node , wherein m is an integer greater than 0 and less than M; characterized in that at least one first node and at least one second node are coupled; and output terminals of the DC-to-AC units are isolated for output.
A pattern forming method comprising: preparing (ST110) a pattern paper comprising a fiber material whereby a pattern to be formed on a pattern forming target is formed by the pattern paper , wherein the pattern paper comprises: a pattern forming layer comprising the fiber material comprising carbon fiber, polyketone fiber, aramid, silica, polyester, polyurethane, or nylon, and having a surface where an original form of the pattern is formed; and a reinforced fiber layer provided on a rear surface of the pattern forming layer and comprising rubber, silicon, or metal fiber; impregnating (ST120) the pattern paper with a releasing agent penetrating into the fiber material, in which the pattern forming layer and the reinforced layer are bonded; and forming (ST130) the pattern on the pattern forming target by arranging the pattern paper on a lower mold , or on a lower mold and an upper mold , of a mold comprising the upper mold and the lower mold , and adhering the pattern paper to the pattern forming target by combining the upper mold and the lower mold . a pattern forming layer comprising the fiber material comprising carbon fiber, polyketone fiber, aramid, silica, polyester, polyurethane, or nylon, and having a surface where an original form of the pattern is formed; and a reinforced fiber layer provided on a rear surface of the pattern forming layer and comprising rubber, silicon, or metal fiber; impregnating (ST120) the pattern paper with a releasing agent penetrating into the fiber material, in which the pattern forming layer and the reinforced layer are bonded; and forming (ST130) the pattern on the pattern forming target by arranging the pattern paper on a lower mold , or on a lower mold and an upper mold , of a mold comprising the upper mold and the lower mold , and adhering the pattern paper to the pattern forming target by combining the upper mold and the lower mold .
Apparatus for cleaning or processing a surface , the apparatus having a light source for illuminating the surface with light and an optical detection device for detecting the light reflected by the surface , characterised in that the optical detection device has a plurality of filter elements and at least one sensor element which are arranged and designed to detect the light reflected from the surface by this one light source with respect to at least four different spectral ranges, wherein the detection device has a sensor element assigned jointly to the filter elements , wherein the filter elements are arranged displaceably relative to the sensor element and for each measurement in each case one of the filter elements is held in the optical axis of the light reflected from the surface so that the sensor element can successively measure the differing spectral components of the light.
A radiation generating system comprising one or more first light sources and one or more second light sources , wherein: - the one or more first light sources and the one or more second light sources are solid state light sources; - the one or more first light sources are configured to generate in an operational mode first light source light having a first centroid wavelength (λc1) defined within a wavelength range of at maximum 380 nm; - the one or more second light sources are configured to generate in an operational mode second light source light having a second centroid wavelength (λc2) defined within the wavelength range of at maximum 420 nm; wherein the second centroid wavelength (λc2) > the first centroid wavelength (λc1); - the radiation generating system is configured to provide a beam of radiation comprising one or more of (i) a first beam comprising first light source light having a first beam angle (α1) defined by full width half maxima and (ii) a second beam comprising second light source light having a second beam angle (α2) defined by full width half maxima; wherein the first beam and the second beam at least partly overlap, the radiation generating system being characterized in that the first beam angle (α1) < the second beam angle (α2). - the one or more first light sources and the one or more second light sources are solid state light sources; - the one or more first light sources are configured to generate in an operational mode first light source light having a first centroid wavelength (λc1) defined within a wavelength range of at maximum 380 nm; - the one or more second light sources are configured to generate in an operational mode second light source light having a second centroid wavelength (λc2) defined within the wavelength range of at maximum 420 nm; wherein the second centroid wavelength (λc2) > the first centroid wavelength (λc1); - the radiation generating system is configured to provide a beam of radiation comprising one or more of (i) a first beam comprising first light source light having a first beam angle (α1) defined by full width half maxima and (ii) a second beam comprising second light source light having a second beam angle (α2) defined by full width half maxima; wherein the first beam and the second beam at least partly overlap, the radiation generating system being characterized in that the first beam angle (α1) < the second beam angle (α2).
A suspension tower comprising: a plate at which an upper end side of a suspension is fixed at a fixing portion (Af, N,W) that is disposed apart from an axis (SA) of the suspension; and a gradually changing rib that is provided upright from the plate and extends from an axis side toward an outer peripheral side at the plate, and that includes a constant level portion whose height from the fixing portion is constant, and a gradually changing portion whose height from the fixing portion gradually decreases from the constant level portion toward the outer peripheral side, wherein a boundary between the constant level portion and the gradually changing portion is adjacent to the fixing portion, characterized in that at the fixing portion, the upper end side of the suspension is fixed by a fastening load from a fastener, the fastening load being applied around a fastening hole formed in the plate; and the boundary between the constant level portion and the gradually changing portion is disposed between a position, at the gradually changing rib , which is a shortest distance from an edge portion of the fastening hole, that is furthest toward an outer peripheral side of the fastening hole, and a position, at the gradually changing rib, which is a shortest distance from a portion of an application range of the fastening load, that is furthest toward an outer peripheral side of the application range of the fastening load. a plate at which an upper end side of a suspension is fixed at a fixing portion (Af, N,W) that is disposed apart from an axis (SA) of the suspension; and a gradually changing rib that is provided upright from the plate and extends from an axis side toward an outer peripheral side at the plate, and that includes a constant level portion whose height from the fixing portion is constant, and a gradually changing portion whose height from the fixing portion gradually decreases from the constant level portion toward the outer peripheral side, wherein a boundary between the constant level portion and the gradually changing portion is adjacent to the fixing portion, characterized in that at the fixing portion, the upper end side of the suspension is fixed by a fastening load from a fastener, the fastening load being applied around a fastening hole formed in the plate; and the boundary between the constant level portion and the gradually changing portion is disposed between a position, at the gradually changing rib , which is a shortest distance from an edge portion of the fastening hole, that is furthest toward an outer peripheral side of the fastening hole, and a position, at the gradually changing rib, which is a shortest distance from a portion of an application range of the fastening load, that is furthest toward an outer peripheral side of the application range of the fastening load.
An embolic protection system for isolating the cerebral vasculature, the system comprising: an elongate outer sheath , having a proximal end and a distal end; an inner member extending through a lumen of the outer sheath ; a distal anchoring mechanism coupled to a distal end region of the inner member ; a proximal filter membrane carried between the inner member and the outer sheath , the proximal filter membrane configured to extend from the left subclavian artery to the brachiocephalic artery ; an aortic support hoop coupled to the proximal filter membrane and configured to seal the proximal filter membrane against the wall of the aorta ; and a handle including a first actuation mechanism coupled to proximal end of the inner member and a second actuation mechanism coupled to the proximal end of the outer sheath . an elongate outer sheath , having a proximal end and a distal end; an inner member extending through a lumen of the outer sheath ; a distal anchoring mechanism coupled to a distal end region of the inner member ; a proximal filter membrane carried between the inner member and the outer sheath , the proximal filter membrane configured to extend from the left subclavian artery to the brachiocephalic artery ; an aortic support hoop coupled to the proximal filter membrane and configured to seal the proximal filter membrane against the wall of the aorta ; and a handle including a first actuation mechanism coupled to proximal end of the inner member and a second actuation mechanism coupled to the proximal end of the outer sheath .
A vehicle control apparatus comprising: an electric power steering configured to support steering of a vehicle and be able to perform torque control; a current-position acquisition unit configured to acquire a current position of the vehicle in a traffic lane where the vehicle is currently traveling; and a target-position control unit configured to perform steering control of the electric power steering in such a manner that the vehicle is caused to run from the current position to a target position and maintains a current traffic lane, characterised in that , by definitions that a first phase (P1) is a predetermined period including a span immediately after reverse turning of steering is determined in the steering control and a second phase (P2) is a period during which steering-turn is performed and does not overlap the first phase (P1), weighting in follow-up control from the current position to the target position is larger in the first phase (P1) than in the second phase (P2). an electric power steering configured to support steering of a vehicle and be able to perform torque control; a current-position acquisition unit configured to acquire a current position of the vehicle in a traffic lane where the vehicle is currently traveling; and a target-position control unit configured to perform steering control of the electric power steering in such a manner that the vehicle is caused to run from the current position to a target position and maintains a current traffic lane, characterised in that , by definitions that a first phase (P1) is a predetermined period including a span immediately after reverse turning of steering is determined in the steering control and a second phase (P2) is a period during which steering-turn is performed and does not overlap the first phase (P1), weighting in follow-up control from the current position to the target position is larger in the first phase (P1) than in the second phase (P2).