mhurhangee/ep-ind-claims huggingface dataset:
A system for controlling the cyclic pitch of blades of a propeller of a turbomachine, the propeller comprising a set of blades movable in rotation around an axis of rotation (r) relative to a stator frame of reference of the turbomachine, the blades being arranged in a plane normal to the axis of rotation (r) of the propeller, called normal plane, the system being such that it comprises: - a plate assembly that can be inclined relative to the normal plane, - an articulation system articulating the plate assembly relative to the blades so that an inclination of the plate assembly causes a cyclic modification of the pitch of the blades, and such that it comprises: - a force sensor, mounted fixed in the stator frame of reference, the force sensor being suitable for measuring a force exerted in the normal plane by an air flow at the inlet of the propeller blades, - a cylinder suitable for inclining the plate assembly, the cylinder being suitable to be actuated in response to a force measured by the force sensor. the system being such that it comprises: - a plate assembly that can be inclined relative to the normal plane, - an articulation system articulating the plate assembly relative to the blades so that an inclination of the plate assembly causes a cyclic modification of the pitch of the blades, - a plate assembly that can be inclined relative to the normal plane, - an articulation system articulating the plate assembly relative to the blades so that an inclination of the plate assembly causes a cyclic modification of the pitch of the blades, and such that it comprises: - a force sensor, mounted fixed in the stator frame of reference, the force sensor being suitable for measuring a force exerted in the normal plane by an air flow at the inlet of the propeller blades, - a cylinder suitable for inclining the plate assembly, the cylinder being suitable to be actuated in response to a force measured by the force sensor. - a force sensor, mounted fixed in the stator frame of reference, the force sensor being suitable for measuring a force exerted in the normal plane by an air flow at the inlet of the propeller blades, - a cylinder suitable for inclining the plate assembly, the cylinder being suitable to be actuated in response to a force measured by the force sensor.
A method of operating a control node for communication with at least one wireless device, the communication being structured in frames comprising several subframes, the method comprising: transmitting a control channel in a search area in only a subset of the subframes, the search area comprising a configurable time span and the subset of the subframes in which the control channel is transmitted being indicated by a bit map.
A component carrier, wherein the component carrier comprises: a stack comprising a plurality of electrically conductive layer structures and a plurality of electrically insulating layer structures; a first electronic component and a second electronic component laminated in the stack; a first block and a second block arranged in the stack below the first electronic component and the second electronic component; and a third block and a fourth block arranged in the stack above the first electronic component and the second electronic component, wherein said blocks (112, 114, 116, 118) are thermally conductive, and wherein each of said blocks (112, 114, 116, 118) is electrically and thermally coupled with at least one of the first electronic component and the second electronic component, wherein said stack comprises a first core within which the first electronic component and the second electronic component are arranged, a second core within which the first block and the second block are arranged, and a third core within which the third block and the fourth block are arranged, each of said second core and third core comprises a centrally electrically insulating layer structure covered on each of the two opposing surfaces with a respective electrically conductive layer structure, said first electronic component and a second electronic component being connected to one of said electrically conductive layer structures of each said second core and third core through a respective connection medium. a stack comprising a plurality of electrically conductive layer structures and a plurality of electrically insulating layer structures; a first electronic component and a second electronic component laminated in the stack; a first block and a second block arranged in the stack below the first electronic component and the second electronic component; and a third block and a fourth block arranged in the stack above the first electronic component and the second electronic component, wherein said blocks (112, 114, 116, 118) are thermally conductive, and wherein each of said blocks (112, 114, 116, 118) is electrically and thermally coupled with at least one of the first electronic component and the second electronic component, wherein said stack comprises a first core within which the first electronic component and the second electronic component are arranged, a second core within which the first block and the second block are arranged, and a third core within which the third block and the fourth block are arranged, each of said second core and third core comprises a centrally electrically insulating layer structure covered on each of the two opposing surfaces with a respective electrically conductive layer structure, said first electronic component and a second electronic component being connected to one of said electrically conductive layer structures of each said second core and third core through a respective connection medium.
A spheroidal graphite cast iron having excellent strength and toughness, which has (a) a composition comprising by mass 3.4-4% of C, 1.9-2.8% of Si, 0.02-0.06% of Mg, 0.2-1% of Mn, 0.2-2% of Cu, 0-0.1% of Sn, 0.85-3% of (Mn + Cu + 10 x Sn), 0.05% or less of P, and 0.02% or less of S, the balance being Fe and inevitable impurities; (b) a duplex matrix structure comprising by area 2-40% of fine ferrite phases and 60-98% of fine pearlite phases, the maximum length of said ferrite phases being 300 μm or less; and (c) said pearlite phases being formed around graphite particles dispersed in said duplex matrix structure; characterized in that the number ratio of graphite particles each having a pearlite-surrounded ratio, defined as a percentage of the total length of peripheral portions of each graphite particle in contact with pearlite phases to its entire peripheral length, of 50-95% is 50% or more based on the total number of graphite particles per a unit area. (a) a composition comprising by mass 3.4-4% of C, 1.9-2.8% of Si, 0.02-0.06% of Mg, 0.2-1% of Mn, 0.2-2% of Cu, 0-0.1% of Sn, 0.85-3% of (Mn + Cu + 10 x Sn), 0.05% or less of P, and 0.02% or less of S, the balance being Fe and inevitable impurities; (b) a duplex matrix structure comprising by area 2-40% of fine ferrite phases and 60-98% of fine pearlite phases, the maximum length of said ferrite phases being 300 μm or less; and (c) said pearlite phases being formed around graphite particles dispersed in said duplex matrix structure;
Method for integrating a hologram into a security document body that comprises a laminated body, said method comprising: providing a holographic film having a backing substrate layer and a photo layer; providing additional substrate layers; processing a lamination to from the laminated body, in which the holographic film collates together with the additional substrate layers (110- 150) in a substrate layer stack and combines together with the additional substrate layers in a lamination process to from the laminated body, characterized in that directly onto the photo layer a curable protective sheet is lined, prior to the lamination process, on the holographic film. providing a holographic film having a backing substrate layer and a photo layer; providing additional substrate layers; processing a lamination to from the laminated body, in which the holographic film collates together with the additional substrate layers (110- 150) in a substrate layer stack and combines together with the additional substrate layers in a lamination process to from the laminated body, characterized in that directly onto the photo layer a curable protective sheet is lined, prior to the lamination process, on the holographic film.
A gas turbine comprising: a rotator arranged to be rotated by combustion gas produced by a combustor that burns fuel; and a casing that is formed by connecting a plurality of casing members (61U-66U) divided in plurality by a plane perpendicular to the rotational axis of the rotator, the casing storing the rotator in an inside thereof, and including an inner connection portion (62Uhbi,63Uhai) for connecting a first casing member with a second casing member different from the first casing member among the casing members at the inside of the first and second casing members (62U,63U) in the radial direction of the rotator, wherein the inner connection portion (62Uhbi,63Uhai) is provided at a divided part divided by the plane perpendicular to the rotational axis, the inner connection portion (62Uhbi,63Uhai) includes a first inner connection portion (62Uhbi) formed on the first casing member and projected in a direction toward a rotational axis of the rotator, a second inner connection portion (63Uhai) formed on the second casing member and projected in the direction toward the rotational axis of the rotator, the first inner connection portion (62Uhbi) and the second inner connection portion (63Uhai) are connected by a connection member, and the inner connection portion (62Uhbi,63Uhai) is provided at a portion of a combusting unit chamber in which the combustor is disposed. a rotator arranged to be rotated by combustion gas produced by a combustor that burns fuel; and a casing that is formed by connecting a plurality of casing members (61U-66U) divided in plurality by a plane perpendicular to the rotational axis of the rotator, the casing storing the rotator in an inside thereof, and including an inner connection portion (62Uhbi,63Uhai) for connecting a first casing member with a second casing member different from the first casing member among the casing members at the inside of the first and second casing members (62U,63U) in the radial direction of the rotator, wherein
A securing system for securing a component to a core engine casing in a gas turbine engine, the system having: a core engine casing formed from a front casing portion and a rear casing portion, the casing portions having respective casing flanges (43, 44) at which the casing portions are detachably joined together, and a component flange extending from a component, the component flange being configured so that, when the casing portions are joined together, the component flange is trapped between the casing flanges; wherein one of the casing flanges projects inwards from the casing to form an airtight seal with the component flange on the inside of the casing, and characterised in that the other of the casing flanges projects outwards from the casing to form an airtight seal with the component flange on the outside of the casing. a core engine casing formed from a front casing portion and a rear casing portion, the casing portions having respective casing flanges (43, 44) at which the casing portions are detachably joined together, and a component flange extending from a component, the component flange being configured so that, when the casing portions are joined together, the component flange is trapped between the casing flanges; wherein one of the casing flanges projects inwards from the casing to form an airtight seal with the component flange on the inside of the casing, and characterised in that the other of the casing flanges projects outwards from the casing to form an airtight seal with the component flange on the outside of the casing.
A method for transmitting broadcast service data in a digital broadcasting communication system, the method comprising: mapping (502, 504, 506) a plurality of broadcast services of a first type to a first zone, and mapping (502, 504, 506) a plurality of broadcast services of a second type to a second zone; and transmitting a frame comprising a P2 preamble, the first zone and the second zone, wherein each of the plurality of broadcast services of the first type is carried in one sub-slice in the time domain per frame, according to a first number of sub-slices allocated for the first zone, wherein the first number is 1, wherein each of the plurality of broadcast services of the second type is sliced to a plurality of sub-slices in the time domain per frame, according to a second number of sub-slices allocated for the second zone, wherein all sub-slices belonging to the same broadcast service of each of the plurality of broadcast services of the second type have a same length, and wherein the P2 preamble comprises information about the second number, information about modulation scheme, and information about coding rate, characterized in that a sub-slice interval is the same for each of the plurality of broadcast services of the second type, the sub-slice interval indicating an interval between two successive sub-slices belonging to the same broadcast service of each of the plurality of broadcast services of the second type, and in that the sub-slice interval is determined by dividing a length of the second zone to which each of the plurality of broadcast services of the second type is mapped, by the second number. mapping (502, 504, 506) a plurality of broadcast services of a first type to a first zone, and mapping (502, 504, 506) a plurality of broadcast services of a second type to a second zone; and transmitting a frame comprising a P2 preamble, the first zone and the second zone, wherein each of the plurality of broadcast services of the first type is carried in one sub-slice in the time domain per frame, according to a first number of sub-slices allocated for the first zone, wherein the first number is 1, wherein each of the plurality of broadcast services of the second type is sliced to a plurality of sub-slices in the time domain per frame, according to a second number of sub-slices allocated for the second zone, wherein all sub-slices belonging to the same broadcast service of each of the plurality of broadcast services of the second type have a same length, and wherein the P2 preamble comprises information about the second number, information about modulation scheme, and information about coding rate, characterized in that a sub-slice interval is the same for each of the plurality of broadcast services of the second type, the sub-slice interval indicating an interval between two successive sub-slices belonging to the same broadcast service of each of the plurality of broadcast services of the second type, and in that the sub-slice interval is determined by dividing a length of the second zone to which each of the plurality of broadcast services of the second type is mapped, by the second number.
A lighting device comprising: a plurality of groups of light-emitting elements (LEEs) (120; 1201-1205; 60-64; 1031-1039), each of the groups of LEEs (120; 1201-1205; 60-64; 1031-1039) comprising one or more LEEs and configured to provide a combined nominal light output when energized under nominal operating conditions, wherein the groups of LEEs are independently energizable; and a controller operatively connected to the groups of LEEs (120; 1201-1205; 60-64; 1031-1039) and configured to determine a binary dimming code based on a dimming signal, the binary dimming code having a plurality of bits, each of the groups of LEEs (120; 1201-1205; 60-64; 1031-1039) is associated with a respective bit of the dimming code, the controller further configured to energize each of the groups of LEEs (120; 1201-1205; 60-64; 1031-1039) based on a bit value of the respective bit of the dimming code, characterized in that different ones of the groups of LEEs (120; 1201-1205; 60-64; 1031-1039) include different numbers of LEEs, wherein the numbers of LEEs per group are based on a predetermined dimming function. a plurality of groups of light-emitting elements (LEEs) (120; 1201-1205; 60-64; 1031-1039), each of the groups of LEEs (120; 1201-1205; 60-64; 1031-1039) comprising one or more LEEs and configured to provide a combined nominal light output when energized under nominal operating conditions, wherein the groups of LEEs are independently energizable; and a controller operatively connected to the groups of LEEs (120; 1201-1205; 60-64; 1031-1039) and configured to determine a binary dimming code based on a dimming signal, the binary dimming code having a plurality of bits, each of the groups of LEEs (120; 1201-1205; 60-64; 1031-1039) is associated with a respective bit of the dimming code, the controller further configured to energize each of the groups of LEEs (120; 1201-1205; 60-64; 1031-1039) based on a bit value of the respective bit of the dimming code, characterized in that different ones of the groups of LEEs (120; 1201-1205; 60-64; 1031-1039) include different numbers of LEEs, wherein the numbers of LEEs per group are based on a predetermined dimming function.
Engine nacelle including a system (10, 110, 210) for preventing icing on an aircraft surface operationally exposed to air; said system (10, 110, 210) being positioned at a covering lip situated at the air inlet of the nacelle; said system (10, 110, 210) extending over exposed surfaces of at least one radially internal side wall adjacent to the lip; said system comprising: a plasma actuator of the dielectric barrier discharge type, to be applied onto said surface operationally exposed to air, and arranged for generating at least one plasma discharge for inducing a flow of ionized hot-air particles towards said surface operationally exposed to air; said actuator comprising: - an intermediate portion of dielectric material, - at least one exposed electrode portion (16, 18) positioned on an outer side, exposed to air, of said intermediate portion, and - at least one covered electrode portion, which is not operationally exposed to air on said outer side because of said intermediate portion; said electrode portions (16, 18, 20) being electrically connectable to a high-voltage electric power generator and being adapted to be energized by said electric power to generate said plasma discharge between them (16, 18, 20); said covered electrode portion being at least partially positioned under an inner side, opposite to said outer side, of said intermediate portion; said system further comprising an insulating portion of dielectric material positioned under said covered electrode portion, to be applied onto said exposed surface of said aircraft; said nacelle being characterized in that said system (10, 110, 210) extends over exposed surfaces of at least one radially external side wall adjacent to the lip, and said system further comprising: - a control module configured for automatically control said generator according to predetermined criteria, allowing for automatic intervention only when particular operating conditions occur; said cooperating conditions corresponding to the fact that the temperature of said surface has gone below said threshold value; - at least one temperature sensor configured for providing the control module with a signal indicating that said temperature has gone below said threshold value; said control module being configured for controlling said generator on the basis of said indicative signal, according to said predetermined criteria. - an intermediate portion of dielectric material, - at least one exposed electrode portion (16, 18) positioned on an outer side, exposed to air, of said intermediate portion, and - at least one covered electrode portion, which is not operationally exposed to air on said outer side because of said intermediate portion; - a control module configured for automatically control said generator according to predetermined criteria, allowing for automatic intervention only when particular operating conditions occur; said cooperating conditions corresponding to the fact that the temperature of said surface has gone below said threshold value; - at least one temperature sensor configured for providing the control module with a signal indicating that said temperature has gone below said threshold value;
A computer implemented method for performing atlas-based segmentation using deep learning, the method comprising: applying a deep learning model to a subject image, the deep learning model trained to generate deep learning segmentation data that identifies an anatomical feature in the subject image, wherein the deep learning model comprises a convolutional neural network; registering an atlas image to the subject image, the atlas image being associated with annotation data that identifies the anatomical feature in the atlas image, wherein the registering uses the deep learning segmentation data to improve a registration result between the atlas image and the subject image by applying the deep learning segmentation data to determine an initial registration estimation or a constraint based on the anatomical feature identified in the subject image; generating a mapped atlas from registering the atlas image to the subject image; and identifying the anatomical feature in the subject image using the mapped atlas. applying a deep learning model to a subject image, the deep learning model trained to generate deep learning segmentation data that identifies an anatomical feature in the subject image, wherein the deep learning model comprises a convolutional neural network; registering an atlas image to the subject image, the atlas image being associated with annotation data that identifies the anatomical feature in the atlas image, wherein the registering uses the deep learning segmentation data to improve a registration result between the atlas image and the subject image by applying the deep learning segmentation data to determine an initial registration estimation or a constraint based on the anatomical feature identified in the subject image; generating a mapped atlas from registering the atlas image to the subject image; and identifying the anatomical feature in the subject image using the mapped atlas.
A method for transmitting modified physical broadcast channel, mPBCH, contents by an evolved Node B, eNB, the method comprising: configuring one or more repetitions of the mPBCH content for transmission, to a user equipment, from a cell at a selected time interval; selecting a scrambling code for the one or more repetitions of mPBCH content transmitted from the cell; and applying the scrambling code to the one or more repetitions of mPBCH content; characterized by selecting the scrambling code based on a function of at least one of a physical cell identifier, a slot number, a subframe number, or an index related to the one or more repetitions of mPBCH content so that distinct scrambling codes are applied the one or more repetitions of the mPBCH content. configuring one or more repetitions of the mPBCH content for transmission, to a user equipment, from a cell at a selected time interval; selecting a scrambling code for the one or more repetitions of mPBCH content transmitted from the cell; and applying the scrambling code to the one or more repetitions of mPBCH content; characterized by selecting the scrambling code based on a function of at least one of a physical cell identifier, a slot number, a subframe number, or an index related to the one or more repetitions of mPBCH content so that distinct scrambling codes are applied the one or more repetitions of the mPBCH content.