mhurhangee/ep-ind-claims huggingface dataset:
A lighting device that illuminates a region to be illuminated extending in a first direction and extending in a second direction intersecting with the first direction, the lighting device comprising: a light source that emits coherent light; a plurality of hologram components each of which diffracts the coherent light emitted by the light source to illuminate an entire region of the region to be illuminated, and a shaping optical system for shaping and collimating the coherent light emitted by the light source and causing the coherent light to enter the plurality of hologram components, wherein at least one of the plurality of hologram components diffracts the incident coherent light so that illuminance at both end portions in the second direction of the region to be illuminated is higher than illuminance at a central portion, wherein at least one of the plurality of hologram components includes a plurality of element hologram components, and wherein the element hologram components diffract incident coherent light to illuminate the entire region of the region to be illuminated, wherein the light source emits a laser beam as the coherent light. a light source that emits coherent light; a plurality of hologram components each of which diffracts the coherent light emitted by the light source to illuminate an entire region of the region to be illuminated, and a shaping optical system for shaping and collimating the coherent light emitted by the light source and causing the coherent light to enter the plurality of hologram components, wherein at least one of the plurality of hologram components diffracts the incident coherent light so that illuminance at both end portions in the second direction of the region to be illuminated is higher than illuminance at a central portion, wherein at least one of the plurality of hologram components includes a plurality of element hologram components, and wherein the element hologram components diffract incident coherent light to illuminate the entire region of the region to be illuminated, wherein the light source emits a laser beam as the coherent light.
A steering column having a cylindrical shape as a whole and comprising a column member (10b, 10d-10g), characterized in that the column member (10b, 10d-10g) comprises: a main portion (18, 18b-18f) that is die cast using a light metal alloy, and comprises a convex section (21, 21a, 37, 37a) provided at one location or more in the circumferential direction on a circumferential surface on one end thereof; a cylindrical member (19, 19b-19f) that is made using an iron-based alloy, and comprises a concave section (20, 20a, 36, 36a) at one location or more in the circumferential direction on a circumferential surface on one end thereof that faces the circumferential surface of the main portion (18, 18b-18f), and together with fitting with the main portion (18, 18b-18f), is connected in the axial direction to the main portion (18, 18b-18f) by the engagement of the convex section (21, 21a, 37, 37a) and concave section (20, 20a, 36, 36a); and a ring (22, 22a-22c) that is made using a metal material, and is fitted and fastened on the inner diameter side of a connecting section between the main portion (18, 18b-18f) and the cylindrical member (19, 19b-19f), where the main portion (18, 18b-18f) and the cylindrical member (19, 19b-19f) overlap each other in the axial direction, the ring (22, 22a-22c) having an inner diameter that is equal to or greater than the inner diameter of the portion of the main portion (18, 18b-18f) that is separated in the axial direction from the connecting section, and is equal to or less than the inner diameter of the cylindrical member (19, 19b-19f). a main portion (18, 18b-18f) that is die cast using a light metal alloy, and comprises a convex section (21, 21a, 37, 37a) provided at one location or more in the circumferential direction on a circumferential surface on one end thereof; a cylindrical member (19, 19b-19f) that is made using an iron-based alloy, and comprises a concave section (20, 20a, 36, 36a) at one location or more in the circumferential direction on a circumferential surface on one end thereof that faces the circumferential surface of the main portion (18, 18b-18f), and together with fitting with the main portion (18, 18b-18f), is connected in the axial direction to the main portion (18, 18b-18f) by the engagement of the convex section (21, 21a, 37, 37a) and concave section (20, 20a, 36, 36a); and a ring (22, 22a-22c) that is made using a metal material, and is fitted and fastened on the inner diameter side of a connecting section between the main portion (18, 18b-18f) and the cylindrical member (19, 19b-19f), where the main portion (18, 18b-18f) and the cylindrical member (19, 19b-19f) overlap each other in the axial direction, the ring (22, 22a-22c) having an inner diameter that is equal to or greater than the inner diameter of the portion of the main portion (18, 18b-18f) that is separated in the axial direction from the connecting section, and is equal to or less than the inner diameter of the cylindrical member (19, 19b-19f).
A method comprising: at a transceiver located on an aircraft, generating sensor data based on reflections received at a sensor of the transceiver based on signals sent by an emitter of the transceiver; at a processor (36, 50); determining a speed and a trajectory of a wingtip light module of an aircraft; determining dimensions of a three-dimensional envelope based on the speed and the trajectory of the wingtip light module, and based on predefined vertical boundary information; and determining targets if a portion of the generated sensor data within the three-dimensional envelope is greater than a predefined threshold; and on a display device, presenting an indication of a nearest target at the associated distance range relative to the aircraft at least in part by presenting at least a partial outline of an airport structure associated with the sensor data identifying the nearest target, wherein the outline of the airport structure is based on previously stored airport information. at a transceiver located on an aircraft, generating sensor data based on reflections received at a sensor of the transceiver based on signals sent by an emitter of the transceiver; at a processor (36, 50); determining a speed and a trajectory of a wingtip light module of an aircraft; determining dimensions of a three-dimensional envelope based on the speed and the trajectory of the wingtip light module, and based on predefined vertical boundary information; and determining targets if a portion of the generated sensor data within the three-dimensional envelope is greater than a predefined threshold; and determining a speed and a trajectory of a wingtip light module of an aircraft; determining dimensions of a three-dimensional envelope based on the speed and the trajectory of the wingtip light module, and based on predefined vertical boundary information; and determining targets if a portion of the generated sensor data within the three-dimensional envelope is greater than a predefined threshold; and on a display device, presenting an indication of a nearest target at the associated distance range relative to the aircraft at least in part by presenting at least a partial outline of an airport structure associated with the sensor data identifying the nearest target, wherein the outline of the airport structure is based on previously stored airport information.
An injector module for a combustion section of a gas turbine engine comprising: an injector stem having a bulbous portion, a forward side and an aft side, the injector stem extending along an injector longitudinal axis between an inlet end and an outlet end of the injector module; a first fuel line of a first fuel circuit at least partly extending through the injector stem, the first fuel line having a first outlet disposed at the outlet end of the injector stem; a second fuel line of a second fuel circuit at least partly extending through the injector stem, the second fuel line having a second outlet disposed at the outlet end of the injector stem; the first outlet and the second outlet being spaced apart and having different orientations relative to the injector longitudinal axis; and the first fuel line being thermally coupled to the second fuel line wherein the first fuel line includes a first longitudinal segment, an outlet segment and a wrap segment that extends about the second fuel line to thermally couple the first fuel line to the second fuel line; wherein the second fuel line includes an inlet and the second fuel line includes a turn between the inlet and the outlet; wherein the wrap segment wraps about the turn of the second fuel line; wherein the wrap segment is axially curved and wraps about the bulbous portion of the stem, proximate the outlet end; and wherein the wrap segment curves from the forward side to the aft side and back toward the outlet segment. an injector stem having a bulbous portion, a forward side and an aft side, the injector stem extending along an injector longitudinal axis between an inlet end and an outlet end of the injector module; a first fuel line of a first fuel circuit at least partly extending through the injector stem, the first fuel line having a first outlet disposed at the outlet end of the injector stem; a second fuel line of a second fuel circuit at least partly extending through the injector stem, the second fuel line having a second outlet disposed at the outlet end of the injector stem; the first outlet and the second outlet being spaced apart and having different orientations relative to the injector longitudinal axis; and the first fuel line being thermally coupled to the second fuel line wherein the first fuel line includes a first longitudinal segment, an outlet segment and a wrap segment that extends about the second fuel line to thermally couple the first fuel line to the second fuel line; wherein the second fuel line includes an inlet and the second fuel line includes a turn between the inlet and the outlet; wherein the wrap segment wraps about the turn of the second fuel line; wherein the wrap segment is axially curved and wraps about the bulbous portion of the stem, proximate the outlet end; and wherein the wrap segment curves from the forward side to the aft side and back toward the outlet segment.
A carrier (90; 190; 290; 390; 490) for packaging one or more articles, the carrier comprising: a plurality of outer walls (12, 16, 18, 22a, 22b, 24a, 24b; 112, 116, 118, 122a, 122b, 124a, 124b; 212, 216, 218, 222a, 222b, 224a, 224b; 312, 316, 318, 322a, 322b, 324a, 324b; 412, 416,418, 422a, 422b, 424a, 424b) which define an interior; an intermediate wall (30a, 30b; 130a, 130b; 260a, 260b; 360a, 360b; 460a, 460b) at least partially segregates the interior of the carrier in a first direction; and a first partition structure (P1, P2, P3, P4) divides, at least in part, the interior in a second transverse direction, a second partition structure (P1, P2, P3, P4) divides, at least in part, the interior in the second transverse direction, wherein the first and second partition structures are configured and arranged to be automatically erected in the interior of the carrier in response to unfolding a flat collapsed folded blank when the carrier is erected, characterised in that the first partition structure is struck, at least in part, from at least a first one of the plurality of outer walls so as to define a first window in the at least a first one of the plurality of outer walls at a first end of the carrier, and wherein the second partition structure is struck, at least in part, from at least a second one of the plurality of outer walls so as to define a second window in the at least a second one of the plurality of outer walls at the first end of the carrier. a plurality of outer walls (12, 16, 18, 22a, 22b, 24a, 24b; 112, 116, 118, 122a, 122b, 124a, 124b; 212, 216, 218, 222a, 222b, 224a, 224b; 312, 316, 318, 322a, 322b, 324a, 324b; 412, 416,418, 422a, 422b, 424a, 424b) which define an interior; an intermediate wall (30a, 30b; 130a, 130b; 260a, 260b; 360a, 360b; 460a, 460b) at least partially segregates the interior of the carrier in a first direction; and a first partition structure (P1, P2, P3, P4) divides, at least in part, the interior in a second transverse direction, a second partition structure (P1, P2, P3, P4) divides, at least in part, the interior in the second transverse direction, wherein the first and second partition structures are configured and arranged to be automatically erected in the interior of the carrier in response to unfolding a flat collapsed folded blank when the carrier is erected, characterised in that the first partition structure is struck, at least in part, from at least a first one of the plurality of outer walls so as to define a first window in the at least a first one of the plurality of outer walls at a first end of the carrier, and wherein the second partition structure is struck, at least in part, from at least a second one of the plurality of outer walls so as to define a second window in the at least a second one of the plurality of outer walls at the first end of the carrier.
An E. coli which lacks: (a) a functional msbB gene; and (b) one or more genes involved in production of enteric common antigen. (a) a functional msbB gene; and (b) one or more genes involved in production of enteric common antigen.
Painting installation component, in particular a bell plate for a rotary atomiser, having a) a base body and b) a surface layer at least on a part of the surface of the base body, c) wherein the surface layer reduces the tendency to contamination of the painting installation component and/or improves the cleaning capability of the painting installation component, characterised in that d) the surface layer is generated by ion implantation. a) a base body and b) a surface layer at least on a part of the surface of the base body, c) wherein the surface layer reduces the tendency to contamination of the painting installation component and/or improves the cleaning capability of the painting installation component, d) the surface layer is generated by ion implantation.
Method of hot rolling a slab, particularly a steel slab, wherein the slab is subjected to at least two reshapings at different temperatures in a hot-rolling mill, wherein the slab is actively cooled between two reshapings of that kind and wherein the cooling of the slab is carried in such a manner that the lateral end regions (3, 4) of the slab are subjected to a lower cooling effect than a central region of the slab, characterised in that the cooling process is so controlled with the help of a connected temperature calculation that exceeding of the ferrite precipitation temperature is avoided so that undesired formation of ferrite is excluded, wherein two sliders (10', 11') covering the nozzles of a cooling bar are so displaced in a horizontal direction transversely to the rolling direction that a defined issue width of the cooling jet of the cooling bar is given.
A trailer for two-wheeled vehicle, said trailer comprising a box supported by a chassis itself including an axle equipped with two wheels (113, 123), facing one another in a direction transverse of said trailer, and four shock absorbers (111a, 111b; 121a, 121b) situated respectively on either side of each wheel (113; 123), said trailer being characterized in that it further comprises four retractable casters (420a, 420b; 420c, 420d), each caster being mounted on an axis movable in vertical translation between a first raised position, when the trailer is towed by said two-wheeled vehicle, and a second lowered position, in contact with the ground, when the trailer is not towed by said two-wheeled vehicle and in that, when the casters are in the lowered position in contact with the ground, their position is such that the wheels (113; 123) of the axle do not touch the ground, allowing use of the trailer as a cart.
A method of reconstituting a reconstitutable teverelix-TFA composition having a molar ratio of teverelix (Ac-D-Nal-D-pClPhe-D-Pal-Ser-Tyr-D-Hci-Leu-Lys(iPr)-Pro-D-Ala-NH 2) to trifluoroacetate below the molar ratio required for microcrystal formation, wherein said molar ratio of teverelix to trifluoroacetate is between 1:1 and 1:1.85, said method comprises adding an aqueous reconstitution solution to the reconstitutable teverelix-TFA composition and adjusting the molar ratio of teverelix to trifluoroacetate to at least 1:2.1 by adding trifluoroacetate.
An electronic device, comprising: an image sensor that includes an array of unit groups, each unit group comprising at least one image capturing pixel, wherein image-capturing conditions of each unit group are independently controllable; an object recognition unit for recognizing photographic subjects (101, 102, 103, 104, 105); an area sectionalizing unit for designating unit groups of an image-capturing pixel area where a primary subject is to be captured; an image-capturing condition setting unit which sets a first image-capturing condition for unit groups in said first image-capturing pixel area corresponding to an image area of the primary subject and a second image-capturing condition for unit groups in a second image-capturing pixel area corresponding to an image area other than the primary subject; characterized by: an adjustment unit that is configured to adjust the second image-capturing condition in correspondence to an extent of adjustment of the first image-capturing condition. an image sensor that includes an array of unit groups, each unit group comprising at least one image capturing pixel, wherein image-capturing conditions of each unit group are independently controllable; an object recognition unit for recognizing photographic subjects (101, 102, 103, 104, 105); an area sectionalizing unit for designating unit groups of an image-capturing pixel area where a primary subject is to be captured; an image-capturing condition setting unit which sets a first image-capturing condition for unit groups in said first image-capturing pixel area corresponding to an image area of the primary subject and a second image-capturing condition for unit groups in a second image-capturing pixel area corresponding to an image area other than the primary subject; characterized by: an adjustment unit that is configured to adjust the second image-capturing condition in correspondence to an extent of adjustment of the first image-capturing condition.
A method of transformation of a motor transportation vehicle for ground transport and air transport, wherein the motor transportation vehicle comprises a body with a cabin and side pontoons, a front axle and a rear axle, at least one actuation system, wings, wherein each wing is supplemented with two auxiliary supports along its entire span, which supports are connected in their upper or their lower parts via a pivotal bearing, and wherein each wing is divided into two parts approximately in the half of its width, covers (2, 3), and a tail comprising at least one support of tail surfaces, wherein it includes the following transformation steps for transformation of the motor transportation vehicle for air transport to the motor transportation vehicle for ground transport: - minimization of the wings' footprint areas by turning over the wings's rear part together with flaps around the pivotal bearing connecting the auxiliary wing supports; - opening two body covers; - turning the folded wings into a vertical position; - turning the folded wings from the vertical position backwards around a horizontal axis perpendicular to the length of the motor transportation vehicle, followed by closing the body covers; - shortening the length of the motor transportation vehicle by retracting the at least one support of the tail surfaces; and the reversal transformation of the motor transportation vehicle for ground transport to the motor transportation vehicle for air transport includes the following transformation steps: - elongating the length of the motor transportation vehicle by extending the at least one support of the tail surfaces; - opening two body covers; - lifting the folded wings into the vertical position; - turning the folded wings from the vertical position to the horizontal position and closing the body covers; - the reversal maximization of the wings footprint areas. - minimization of the wings' footprint areas by turning over the wings's rear part together with flaps around the pivotal bearing connecting the auxiliary wing supports; - opening two body covers; - turning the folded wings into a vertical position; - turning the folded wings from the vertical position backwards around a horizontal axis perpendicular to the length of the motor transportation vehicle, followed by closing the body covers; - shortening the length of the motor transportation vehicle by retracting the at least one support of the tail surfaces; and - elongating the length of the motor transportation vehicle by extending the at least one support of the tail surfaces; - opening two body covers; - lifting the folded wings into the vertical position; - turning the folded wings from the vertical position to the horizontal position and closing the body covers; - the reversal maximization of the wings footprint areas.
A discontinuous fiber-reinforced composite material comprising a discontinuous reinforcing fiber aggregate of discontinuous reinforcing fibers having a number average fiber length of 3 to 100 mm and a matrix resin, the discontinuous reinforcing fiber aggregate including a plurality of discontinuous reinforcing fiber bundles (1, 21, 22, 23, 36) having a predetermined number of unidirectionally-bundled single yarns of the discontinuous reinforcing fiber, wherein each of the discontinuous reinforcing fiber bundles has a cut surface inclined at a predetermined angle with respect to an orientation direction of the single yarns and the discontinuous reinforcing fiber bundles have different fiber bundle lengths, characterized in that the shorter a discontinuous fiber bundle length, which is defined as a distance between both ends along the orientation direction of the single yarns is, the smaller a tip angle defined as an acute angle at an end of a two-dimensional plane projection of the discontinuous reinforcing fiber bundle is.
Device for assisting a practitioner in adjusting the length of artificial chordae implanted in an heart valve, the device comprising a plurality of gripping elements, each gripping element handling an end of a respective artificial chordae extending outward from the patient so that the device remains outside from the patient, characterized in that the device further comprises a plurality of force sensors, each force sensor being fixed to one of the plurality of gripping elements for measuring a signal representative of a tension of the chordae held by the respective gripping element associated to the force sensor.