mhurhangee/patent-ind-claim-en huggingface dataset:
A steel sheet for hot stamping use, a chemical composition of the steel sheet comprising, by mass%, C: 0.35% to 0.75%, Si: 0.005% to 0.25%, Mn: 0.5% to 3.0%, sol. Al: 0.0002% to 3.0%, Cr: 0.05% to 1.00%, B: 0.0005% to 0.010%, Nb: 0.01% to 0.15%, Mo: 0.005% to 1.00%, Ti: 0% to 0.15%, Ni: 0 to 3.00%, P: 0.10% or less, S: 0.10% or less, N: 0.010% or less, and a balance of Fe and unavoidable impurities, a microstructure of the steel sheet comprising at least one of lower bainite, martensite, and tempered martensite in an area ratio of 90% or more, a grain boundary solid solution ratio Z defined by Z=(mass% of one or both of Nb and Mo at grain boundaries)/(mass% of one or both of Nb and Mo at time of melting) being 0.4 or more, which is determined in accordance with the description, an X-ray random intensity ratio of <111> of the crystal grains forming the above lower bainite, martensite, or tempered martensite being 2.8 or more, which is determined in accordance with the description, number densities of total of grain size 50 nm or less cementite and epsilon carbides being 1×10 16 /m 2 or more, which is determined in accordance with the description. a chemical composition of the steel sheet comprising, by mass%, C: 0.35% to 0.75%, Si: 0.005% to 0.25%, Mn: 0.5% to 3.0%, sol. Al: 0.0002% to 3.0%, Cr: 0.05% to 1.00%, B: 0.0005% to 0.010%, Nb: 0.01% to 0.15%, Mo: 0.005% to 1.00%, Ti: 0% to 0.15%, Ni: 0 to 3.00%, P: 0.10% or less, S: 0.10% or less, N: 0.010% or less, and a balance of Fe and unavoidable impurities, a microstructure of the steel sheet comprising at least one of lower bainite, martensite, and tempered martensite in an area ratio of 90% or more, a grain boundary solid solution ratio Z defined by Z=(mass% of one or both of Nb and Mo at grain boundaries)/(mass% of one or both of Nb and Mo at time of melting) being 0.4 or more, which is determined in accordance with the description, an X-ray random intensity ratio of <111> of the crystal grains forming the above lower bainite, martensite, or tempered martensite being 2.8 or more, which is determined in accordance with the description, number densities of total of grain size 50 nm or less cementite and epsilon carbides being 1×10 16 /m 2 or more, which is determined in accordance with the description.
A self-reacting center wheel nut assembly including: a center wheel nut ; a reaction ring ; and a lock collar assembly . the center wheel nut having a first end to nonrotatably engage with an action portion of a driver assembly and a second end to rotatably engage with a wheel; the reaction ring having a first end to nonrotatably engage with a reaction portion of a driver assembly and a second end to nonrotatably engage with the lock collar assembly ; and the lock collar assembly having a first end to nonrotatably engage with the reaction ring and a tapered second end to nonrotatably engage with a matching tapered recess in the center of a wheel. a center wheel nut ; a reaction ring ; and a lock collar assembly . the center wheel nut having a first end to nonrotatably engage with an action portion of a driver assembly and a second end to rotatably engage with a wheel; the reaction ring having a first end to nonrotatably engage with a reaction portion of a driver assembly and a second end to nonrotatably engage with the lock collar assembly ; and the lock collar assembly having a first end to nonrotatably engage with the reaction ring and a tapered second end to nonrotatably engage with a matching tapered recess in the center of a wheel.
An open-loop current transducer configured for mounting around a primary conductor bar having a substantially rectangular cross-section with a width (W) and height (H), the width being greater than the height, the current transducer comprising an insulating support surrounding a central passage through which the primary conductor extends when mounted to the current transducer, the insulating support having at least two parts, a first support part and a second support part mountable together around the primary conductor bar , the current transducer further comprising a plurality of discrete magnetic field sensors arranged within the insulating support around the primary conductor bar, the current transducer further comprising a mounting bracket attached to a branch of the insulating support , wherein the mounting bracket comprises at least one mounting pillar having a plurality of height adjustment locating holes , and a mounting flange comprising a primary conductor fixing member configured for attachment of the mounting bracket to the primary conductor, the insulating support comprising at least one fixing hole alignable with one of the plurality of height adjustment locating holes, through which a height fixing pin of the current transducer is inserted to locate the height of the mounting bracket relative to the branch of the insulating support comprising the fixing hole such that a height position of the primary conductor bar relative to the insulating support is adjusted, wherein the mounting bracket comprises a support receiving cradle having a general U-shape cross-sectional profile, having side walls that extend to an upper edge beyond a top side of the branch of the insulating support.
A method for detecting the angular positions of the blades of a rotor wheel of a turbine engine , the turbine engine having at least two rotor wheels each having a stream of air passing therethrough and being coupled together directly or indirectly, the first wheel having a first number of blades (31 to 35) regularly distributed around its circumference and the second wheel having a second number of blades regularly distributed around its circumference, wherein the method comprises detecting the passage of each blade (31 to 35) of the first wheel past a first sensor , detecting the passage of each blade (171 to 177) of the second wheel past a second sensor , calculating the time intervals between the passage of a blade of the first wheel and the passages of each of the blades (171 to 177) of the second wheel , and determining the relative angular position of each blade (31 to 35) of the first wheel relative to the angular positions of the blades (171 to 177) of the second wheel , the first number of blades of the first wheel and the second number of blades of the second wheel being distinct and mutually prime.
A conjugate, or a pharmaceutically acceptable salt thereof, having a structure B-L-X, wherein B comprises a fibroblast activation protein (FAP) inhibitor; L comprises a bivalent linker; and X comprises a near infrared (NIR) dye, a radioactive imaging agent, or a therapeutic agent effective against cancer cells and/or cancer-associated fibroblasts (CAF); wherein B has a structure or wherein R 1 and R 2 are the same or different, and are each independently selected from the group consisting of hydrogen, halogen, and C 1 -C 4 alkyl; R 3 is a C 1 -C 4 alkyl, nitrile, or isonitrile; R 4 , R 5 , and R 6 are the same or different, and are each independently selected from the group consisting of hydrogen, halogen, and C 1 -C 4 alkyl; and n is an integer from 1 to 8. wherein B comprises a fibroblast activation protein (FAP) inhibitor; L comprises a bivalent linker; and X comprises a near infrared (NIR) dye, a radioactive imaging agent, or a therapeutic agent effective against cancer cells and/or cancer-associated fibroblasts (CAF); wherein B has a structure or wherein R 1 and R 2 are the same or different, and are each independently selected from the group consisting of hydrogen, halogen, and C 1 -C 4 alkyl; R 3 is a C 1 -C 4 alkyl, nitrile, or isonitrile; R 4 , R 5 , and R 6 are the same or different, and are each independently selected from the group consisting of hydrogen, halogen, and C 1 -C 4 alkyl; and n is an integer from 1 to 8.
An apparatus for joining modular floor coverings, the apparatus comprising: a plate having an upper surface and a lower surface, said lower surface being substantially smooth and said upper surface having a perimeter edge and being divided into a flat central zone and a set of three or more edge zones , each edge zone extending transversely along said perimeter edge between said perimeter edge and said flat central zone ; a plurality of sharp projections extending upwardly at spaced locations from each edge zone, said projections having a top and body portion, the top being tapered to promote piercing engagement with a floor covering backing and the body extending upwards from the upper surface at an angle of less than 90 degrees, and said projections extending inwardly from each of said three or more edge zones towards said central zone ; and wherein said plate is adapted to be positioned on a supporting surface to join a set of modular floor covering units having a backing positioned on said upper surface of said plate, and wherein said plurality of sharp projections are adapted to engage said backing to secure said modular floor covering units; wherein the apparatus further comprises an adhesive layer positioned on said lower surface, said adhesive layer covered by a releasable backing. a plate having an upper surface and a lower surface, said lower surface being substantially smooth and said upper surface having a perimeter edge and being divided into a flat central zone and a set of three or more edge zones , each edge zone extending transversely along said perimeter edge between said perimeter edge and said flat central zone ; a plurality of sharp projections extending upwardly at spaced locations from each edge zone, said projections having a top and body portion, the top being tapered to promote piercing engagement with a floor covering backing and the body extending upwards from the upper surface at an angle of less than 90 degrees, and said projections extending inwardly from each of said three or more edge zones towards said central zone ; and wherein said plate is adapted to be positioned on a supporting surface to join a set of modular floor covering units having a backing positioned on said upper surface of said plate, and wherein said plurality of sharp projections are adapted to engage said backing to secure said modular floor covering units; wherein the apparatus further comprises an adhesive layer positioned on said lower surface, said adhesive layer covered by a releasable backing.
A method for manufacturing a card body, having: - supplying at least one foil, - personalizing the supplied foil by means of laser engraving, wherein for optimized personalization at least one metal oxide is introduced into the foil, wherein the metal oxide is present substantially at nanoscale, wherein the metal oxide is present in a size range of a particle size between 1 and 100 nanometers, wherein the metal oxide is supplied as a laser additive for optimized personalization, wherein the at least one foil has polylactides PLA, polyvinyl chloride PVC, polycarbonates PC, a mixture of polycarbonate PC and polyethylene terephthalate glycol PETG and/or a polymer, wherein the at least one foil has a plastic matrix, characterized in that the plastic matrix is introduced such that the foil is stabilized. - supplying at least one foil, - personalizing the supplied foil by means of laser engraving, wherein for optimized personalization at least one metal oxide is introduced into the foil,
A fastener retention mechanism for retaining fasteners of a stator assembly in a gas turbine engine, the fastener retention mechanism comprising: a cover comprising a first foot , a second foot , and a cover surface extending between the first foot and the second foot ; characterised in that the fastener retention mechanism further comprises: a base having a first rail and a second rail and a base surface extending therebetween, the first rail and the second rail being in a facing spaced relationship with respect to each other and defining a channel extending therebetween; wherein the cover is releasably connected to the base ; wherein the first foot and the second foot are configured to interlock with the first rail and the second rail , respectively, such that the channel is covered by the cover surface when the cover is secured to the base ; and wherein the cover is secured to the base by the interlocking of the first foot and the second foot with the first rail and the second rail . a cover comprising a first foot , a second foot , and a cover surface extending between the first foot and the second foot ; characterised in that the fastener retention mechanism further comprises: a base having a first rail and a second rail and a base surface extending therebetween, the first rail and the second rail being in a facing spaced relationship with respect to each other and defining a channel extending therebetween; wherein the cover is releasably connected to the base ; wherein the first foot and the second foot are configured to interlock with the first rail and the second rail , respectively, such that the channel is covered by the cover surface when the cover is secured to the base ; and wherein the cover is secured to the base by the interlocking of the first foot and the second foot with the first rail and the second rail . a base having a first rail and a second rail and a base surface extending therebetween, the first rail and the second rail being in a facing spaced relationship with respect to each other and defining a channel extending therebetween; wherein the cover is releasably connected to the base ; wherein the first foot and the second foot are configured to interlock with the first rail and the second rail , respectively, such that the channel is covered by the cover surface when the cover is secured to the base ; and wherein the cover is secured to the base by the interlocking of the first foot and the second foot with the first rail and the second rail .
A system for distributing air to plural aircraft zones, the system comprising: a mix manifold , wherein the plural aircraft zones receive manifold air from the mix manifold; a recirculating fan , the system being characterised by a thermal electronic cooler trim module, TEC, , wherein the TEC is fluidly connected between the recirculating fan and the mix manifold ; the TEC including: multiple TEC zones , each fluidly connected to, and sized relative to heating requirements of, a respective one of the aircraft zones, wherein the TEC is capable of heating and cooling air in the multiple TEC zones; a first TEC inlet , through which a first portion of the recirculated air enters the TEC, is heat treated in a first heating direction, and is exhausted toward the mix manifold; and a second TEC inlet , through which a second portion of the recirculated air enters the TEC zones, is heat treated in a second heating direction, and is exhausted toward the aircraft zones, for mixing with the manifold air. a mix manifold , wherein the plural aircraft zones receive manifold air from the mix manifold; a recirculating fan , the system being characterised by a thermal electronic cooler trim module, TEC, , wherein the TEC is fluidly connected between the recirculating fan and the mix manifold ; the TEC including: multiple TEC zones , each fluidly connected to, and sized relative to heating requirements of, a respective one of the aircraft zones, wherein the TEC is capable of heating and cooling air in the multiple TEC zones; a first TEC inlet , through which a first portion of the recirculated air enters the TEC, is heat treated in a first heating direction, and is exhausted toward the mix manifold; and a second TEC inlet , through which a second portion of the recirculated air enters the TEC zones, is heat treated in a second heating direction, and is exhausted toward the aircraft zones, for mixing with the manifold air. multiple TEC zones , each fluidly connected to, and sized relative to heating requirements of, a respective one of the aircraft zones, wherein the TEC is capable of heating and cooling air in the multiple TEC zones; a first TEC inlet , through which a first portion of the recirculated air enters the TEC, is heat treated in a first heating direction, and is exhausted toward the mix manifold; and a second TEC inlet , through which a second portion of the recirculated air enters the TEC zones, is heat treated in a second heating direction, and is exhausted toward the aircraft zones, for mixing with the manifold air.
A minimally invasive surgical instrument comprising: an elongate shaft having a working end, a proximal end, and a shaft axis between the working end and the proximal end; an end effector ; a wrist member having a proximal portion connected to the working end and a distal portion connected to the end effector , wherein the wrist member comprises at least three vertebrae connected in series between the working end of the elongate shaft and the end effector, each vertebra being pivotable relative to an adjacent vertebra by a pivotal coupling around a pivotal axis; at least one of the vertebrae being pivotable relative to an adjacent vertebra by a pitch joint around a pitch axis which is nonparallel to the shaft axis, at least one of the vertebrae being pivotable relative to an adjacent vertebra by a yaw joint around a yaw axis which is nonparallel to the shaft axis and perpendicular to the pitch axis, characterized in that the pivotal axes of at least two adjacent vertebrae are parallel to each other and are either pitch joints or yaw joints. an elongate shaft having a working end, a proximal end, and a shaft axis between the working end and the proximal end; an end effector ; a wrist member having a proximal portion connected to the working end and a distal portion connected to the end effector , wherein the wrist member comprises at least three vertebrae connected in series between the working end of the elongate shaft and the end effector, each vertebra being pivotable relative to an adjacent vertebra by a pivotal coupling around a pivotal axis; at least one of the vertebrae being pivotable relative to an adjacent vertebra by a pitch joint around a pitch axis which is nonparallel to the shaft axis, at least one of the vertebrae being pivotable relative to an adjacent vertebra by a yaw joint around a yaw axis which is nonparallel to the shaft axis and perpendicular to the pitch axis, characterized in that the pivotal axes of at least two adjacent vertebrae are parallel to each other and are either pitch joints or yaw joints.
A method, performed by an entry module , for managing packets in a communication system based on Software Defined Networking, wherein the communication system comprises the entry module , a radio network node , a mobile device , a forwarding module , a service module , a peer device and a management module for managing the forwarding module , the service module and the entry module , wherein a data plane of the communication system comprises the forwarding module , the service module and the entry module and a control plane of the communication system comprises the management module , wherein the mobile device is attached to the radio network node , wherein the method comprises: receiving an Internet Protocol "IP" packet from the peer device , wherein the IP packet includes a destination IP address associated with the mobile device ; obtaining , from a location registry , a location value specifying the radio network node that serves the mobile device associated with the destination IP address, wherein each location value is associated to a respective radio network node to which the mobile device is capable of attaching; obtaining a packet by adding the location value to the packet, wherein the location value is related to a location tag name, indicating the radio network node ; and sending the packet, via the forwarding module , towards the radio network node over a port mapped to the location value, as indicated by the location value of the location tag name. receiving an Internet Protocol "IP" packet from the peer device , wherein the IP packet includes a destination IP address associated with the mobile device ; obtaining , from a location registry , a location value specifying the radio network node that serves the mobile device associated with the destination IP address, wherein each location value is associated to a respective radio network node to which the mobile device is capable of attaching; obtaining a packet by adding the location value to the packet, wherein the location value is related to a location tag name, indicating the radio network node ; and sending the packet, via the forwarding module , towards the radio network node over a port mapped to the location value, as indicated by the location value of the location tag name.
A method for forming a molded part having quasi-isotropic properties, the method comprising: consolidating a first layer formed from a first composite component material and a second layer formed from a second composite component material to create a quasi-isotropic panel , wherein the first composite component material is different from the second composite component material, and wherein the first composite component material and the second composite component material comprise fibers, wherein the fibers of the first component material are oriented in a first orientation, and wherein the fibers of the second composite component material are oriented in a second orientation; dividing the quasi-isotropic panel into a plurality of quasi-flakes ; filling a compression mold with the plurality of quasi-flakes ; and applying heat to the compression mold to form the molded part having quasi-isotropic properties. consolidating a first layer formed from a first composite component material and a second layer formed from a second composite component material to create a quasi-isotropic panel , wherein the first composite component material is different from the second composite component material, and wherein the first composite component material and the second composite component material comprise fibers, wherein the fibers of the first component material are oriented in a first orientation, and wherein the fibers of the second composite component material are oriented in a second orientation; dividing the quasi-isotropic panel into a plurality of quasi-flakes ; filling a compression mold with the plurality of quasi-flakes ; and applying heat to the compression mold to form the molded part having quasi-isotropic properties.