mhurhangee/patent-ind-claim-en huggingface dataset:
An ultra-thick steel material comprising: by weight %, 0.04 to 0.1% of carbon (C), 0.05 to 0.5% of silicon (Si), 0.01 to 0.05% of aluminum (Al), 1.6 to 2.2% of manganese (Mn), 0.5 to 1.2% of nickel (Ni), 0.005 to 0.050% of niobium (Nb), 0.005 to 0.03% of titanium (Ti), 0.2 to 0.6% of copper (Cu), 100ppm or less of phosphorus (P), and 40ppm or less of sulfur (S) with a remainder of iron (Fe), and inevitable impurities, and in a subsurface area up to t/10, t hereafter being referred to as a thickness, mm, of a steel material, bainite of 90 area% or greater, including 100 area%, as a microstructure of the steel material, wherein a particle size of crystalline grains of the steel material, having a high inclination angle boundary of 15° or higher measured by EBSD, in a subsurface area up to t/10, hereafter being referred to as a thickness, mm, of a steel material, is 10 μm or less, excluding 0μm, wherein the steel material comprises 95 area% or higher, including 100 area%, of a composite structure of acicular ferrite and bainite and 5 area% or lower , including 0 area%, of a martensite-austenite constituent, as a microstructure, in a subsurface area from a t/10 to a t/2, wherein a nil-ductility transition (NDT) temperature of a specimen taken from a surface of the steel material, based on a naval research laboratory-drop weight test (NRL-DWT) regulated in ASTM 208-06, is -60°C or lower, wherein the steel material has yield strength of 460MPa or higher, and wherein a plate thickness of the steel material is 50 to 100mm. by weight %, 0.04 to 0.1% of carbon (C), 0.05 to 0.5% of silicon (Si), 0.01 to 0.05% of aluminum (Al), 1.6 to 2.2% of manganese (Mn), 0.5 to 1.2% of nickel (Ni), 0.005 to 0.050% of niobium (Nb), 0.005 to 0.03% of titanium (Ti), 0.2 to 0.6% of copper (Cu), 100ppm or less of phosphorus (P), and 40ppm or less of sulfur (S) with a remainder of iron (Fe), and inevitable impurities, and in a subsurface area up to t/10, t hereafter being referred to as a thickness, mm, of a steel material, bainite of 90 area% or greater, including 100 area%, as a microstructure of the steel material, wherein a particle size of crystalline grains of the steel material, having a high inclination angle boundary of 15° or higher measured by EBSD, in a subsurface area up to t/10, hereafter being referred to as a thickness, mm, of a steel material, is 10 μm or less, excluding 0μm, wherein the steel material comprises 95 area% or higher, including 100 area%, of a composite structure of acicular ferrite and bainite and 5 area% or lower , including 0 area%, of a martensite-austenite constituent, as a microstructure, in a subsurface area from a t/10 to a t/2, wherein a nil-ductility transition (NDT) temperature of a specimen taken from a surface of the steel material, based on a naval research laboratory-drop weight test (NRL-DWT) regulated in ASTM 208-06, is -60°C or lower, wherein the steel material has yield strength of 460MPa or higher, and wherein a plate thickness of the steel material is 50 to 100mm.
A polypropylene film having a crystal orientation degree of an α-crystal plane measured by wide-angle X-ray diffractometry of 0.78 or more, a sum of thermal shrinkage rates in a width direction and a longitudinal direction after being subjected to heat treatment at 120°C for 10 minutes of 4.0% or less, and a relationship between a stress at 5% elongation in the width direction (TD-F5 value) and a stress at 5% elongation in the longitudinal direction (MD-F5 value) of (MD-F5 value)/(TD-F5 value) > 0.45, wherein the crystal orientation degree of an α-crystal plane, the thermal shrinkage rates and the stress at 5% elongation are measured by the methods described in the specification.
A method of fabricating a leading edge sheath assembly for a blade, comprising: additively manufacturing a core to be solid in a first central portion of the core, perforated in a second outer portion of the core, and micro-latticed in a third intermediate portion of the core, wherein the third intermediate portion is between the first central portion and the second outer portion; securing the core to a mandrel ; electroforming a leading edge sheath directly onto the core and the mandrel ; and removing the mandrel from the core and the leading edge sheath . additively manufacturing a core to be solid in a first central portion of the core, perforated in a second outer portion of the core, and micro-latticed in a third intermediate portion of the core, wherein the third intermediate portion is between the first central portion and the second outer portion; securing the core to a mandrel ; electroforming a leading edge sheath directly onto the core and the mandrel ; and removing the mandrel from the core and the leading edge sheath .
A method for controlling a heated mixer, situated downstream of a Urea-Water Solution (UWS) injector, to reduce NOx emission in an exhaust system from combustion engines, wherein the exhaust system has a Selective Catalytic Reduction (SCR) catalyst situated downstream of the UWS injector and the heated mixer, the method comprising the steps of: a) determining a NOx reduction efficiency of the SCR catalyst; b) evaluating at least one reductant Uniformity Index (UI) based on operating parameters of the exhaust system and a mixer power calculation map; and c) modifying a mixer temperature of the heated mixer by regulating power to the heated mixer based on said at least one reductant UI in order to improve said at least one reductant UI and/or improve said NOx reduction efficiency. a) determining a NOx reduction efficiency of the SCR catalyst; b) evaluating at least one reductant Uniformity Index (UI) based on operating parameters of the exhaust system and a mixer power calculation map; and c) modifying a mixer temperature of the heated mixer by regulating power to the heated mixer based on said at least one reductant UI in order to improve said at least one reductant UI and/or improve said NOx reduction efficiency.
Method for measuring the contamination of a transport box for the atmospheric shipping and storage of substrates in which the concentration of at least one gaseous species inside the transport box is measured by a measurement device comprising at least one gas analyser and a measurement line connecting said at least one gas analyser to an interface , the interface placing the measurement line in communication with the internal atmosphere of at least one transport box , characterized in that a gas flow containing water vapour is supplied to the measurement device.
A seating arrangement for a vehicle comprising: - two adjacent seats , spaced apart by a gap; - a bridging mechanism which can be positioned between said seats for forming a bed; characterised in that - each of said seats comprises a hollow pedestal ; and - the bridging mechanism comprises two bridging parts , each bridging part being movably mounted to one of said adjacent seats , and being movable between a normal, retracted position inside said hollow pedestal and an extended, sleeping position outside said hollow pedestal, between said adjacent seats . - two adjacent seats , spaced apart by a gap; - a bridging mechanism which can be positioned between said seats for forming a bed; characterised in that - each of said seats comprises a hollow pedestal ; and - the bridging mechanism comprises two bridging parts , each bridging part being movably mounted to one of said adjacent seats , and being movable between a normal, retracted position inside said hollow pedestal and an extended, sleeping position outside said hollow pedestal, between said adjacent seats .
A method for forwarding a packet, applicable to each non-uniform memory architecture, NUMA, node included in a network function virtualization, NFV, device, wherein the each NUMA node comprises a forwarding group comprising a receiving core (Data-Rx1) and a forwarding core (Data-Fwd7), wherein at least one core of a plurality of cores (Data-Rx1, Data-Fwd4 - Data-Fwd8) included in the each NUMA node and at least one core of the other cores of said plurality of cores (Data-Rx1, Data-Fwd4 - Data-Fwd8) being configured as a receiving core (Data-Rx1) and a forwarding core (Data-Fwd7) of the forwarding group of the each NUMA node respectively, and the method comprises: reading, by said receiving core (Data-Rx1) in said forwarding group of the each NUMA node, a packet from an ingress interface, wherein the ingress interface is an interface corresponding to said forwarding group ; sending, by said receiving core (Data-Rx1) in said forwarding group of the each NUMA node, said packet to said forwarding core (Data-Fwd7) in said forwarding group of the each NUMA node; and sending, by said forwarding core (Data-Fwd7) in the forwarding group of the each NUMA node said packet to a corresponding egress interface. reading, by said receiving core (Data-Rx1) in said forwarding group of the each NUMA node, a packet from an ingress interface, wherein the ingress interface is an interface corresponding to said forwarding group ; sending, by said receiving core (Data-Rx1) in said forwarding group of the each NUMA node, said packet to said forwarding core (Data-Fwd7) in said forwarding group of the each NUMA node; and sending, by said forwarding core (Data-Fwd7) in the forwarding group of the each NUMA node said packet to a corresponding egress interface.
A flexible web substrate material having opposed front and back sides and extending ir an X-Y plane, the front side being provided with a first electrode layer and further provided with at least one thin film to form a plurality of thin film device stacks; the thin film device stack comprising an electrically active region; the thin film device stack extending from the X - Y plane in a Z direction perpendicular to the X - Y plane to a distance T; the web substrate material having at least one protective structure which prevents contact of the electrically active region of the thin film device stack with the back side of the substrate material or with a machine roller during web transport, wherein the protective structure is applied to at least one of the front side and the back side of the substrate, the first electrode, the at least one thin film, and a plurality of discrete thin film device stacks which are continuous in-line stripes; neighbouring thin film device stacks having a zone of electrical interconnection between them, and wherein the at least one protective structure is located at least partially in a zone of electrical interconnection , wherein the protective structure is deposited as a continuous bead of material, in discrete units or as an intermittent bead of material; the at least one protective structure extending in the Z direction to a distance S from the X - Y plane, the distance S being greater than the distance T, characterized in that the ratio of the distance S to the distance T is at least 10: 1. the thin film device stack comprising an electrically active region; the thin film device stack extending from the X - Y plane in a Z direction perpendicular to the X - Y plane to a distance T; the web substrate material having at least one protective structure which prevents contact of the electrically active region of the thin film device stack with the back side of the substrate material or with a machine roller during web transport, wherein the protective structure is applied to at least one of the front side and the back side of the substrate, the first electrode, the at least one thin film, and a plurality of discrete thin film device stacks which are continuous in-line stripes; neighbouring thin film device stacks having a zone of electrical interconnection between them, and wherein the at least one protective structure is located at least partially in a zone of electrical interconnection , wherein the protective structure is deposited as a continuous bead of material, in discrete units or as an intermittent bead of material; the at least one protective structure extending in the Z direction to a distance S from the X - Y plane, the distance S being greater than the distance T, characterized in that the ratio of the distance S to the distance T is at least 10: 1.
Method for avoiding a collision of a motor vehicle with an object (P1, P2) detected by a detection device on the vehicle in a surrounding area of the motor vehicle , characterized in that when the object (P1, P2) is detected in the surrounding area , a collision area is determined as a function of predetermined maximum wheel steering angles on both sides of the motor vehicle , and a collision-avoiding measure for the motor vehicle is initiated if the object (P1, P2) is located within the collision area .
A processing device for fragmenting nucleic acids contained within a sample , the device comprising: an inlet portion having a volume for receiving the sample containing nucleic acids, the inlet portion having a funnel-shaped portion; a channel coupled to and in fluid communication with the inlet portion, the channel having a volume; a shearing region coupled to and in fluid communication with the channel and adapted to fragment the nucleic acids in the sample upon flow of the sample through the shearing region, the shearing region comprising an orifice having an internal orifice diameter or inner width of between about 10 microns and about 100 microns, and a length of between about 100 microns and about 20 mm, wherein the inlet portion has an entrance having a cross-sectional area that is five times or more greater than the cross-sectional area of the channel and the inlet portion has a volume that is more than two times greater than a volume of the channel, so that a sample height (h) is maintained over the shearing region that is constant during flow of a majority of the sample through the shearing region and thereby a constant pressure is maintained at an entrance of the shearing region during flow of a majority of a sample through the shearing region for a sample that has a sample volume that is at least 2 times the channel volume; and a collection portion in fluid communication with the shearing region and for receiving the sample containing the fragmented nucleic acids from the shearing region. an inlet portion having a volume for receiving the sample containing nucleic acids, the inlet portion having a funnel-shaped portion; a channel coupled to and in fluid communication with the inlet portion, the channel having a volume; a shearing region coupled to and in fluid communication with the channel and adapted to fragment the nucleic acids in the sample upon flow of the sample through the shearing region, the shearing region comprising an orifice having an internal orifice diameter or inner width of between about 10 microns and about 100 microns, and a length of between about 100 microns and about 20 mm, wherein the inlet portion has an entrance having a cross-sectional area that is five times or more greater than the cross-sectional area of the channel and the inlet portion has a volume that is more than two times greater than a volume of the channel, so that a sample height (h) is maintained over the shearing region that is constant during flow of a majority of the sample through the shearing region and thereby a constant pressure is maintained at an entrance of the shearing region during flow of a majority of a sample through the shearing region for a sample that has a sample volume that is at least 2 times the channel volume; and a collection portion in fluid communication with the shearing region and for receiving the sample containing the fragmented nucleic acids from the shearing region.
A method carried out on a network-enabled device for providing a cloud-based multi-function firewall (114A-114D), wherein the network-enabled device comprises a user device (102A-B, 107), the method comprising: detecting one or more available network connections provided by the network-enabled device; blocking the one or more detected network connections; retrieving device information associated with the network-enabled device; transmitting the device information from the network-enabled device to a secure cloud to configure a virtual private network, VPN, connection between the secure cloud and the network-enabled device; receiving cloud information from the secure cloud, the cloud information specifying a cloud server in the secure cloud and being generated by the secure cloud based on the device information; updating domain name service, DNS, and routing functions at the network-enabled device based on the cloud information to forward network requests to the cloud server specified in the cloud information; and establishing the VPN connection to the cloud server in the secure cloud based on the cloud information, wherein any network traffic between the network-enabled device and the one or more detected networks is routed through the VPN connection to the cloud-based multi-function firewall implemented on the cloud server. detecting one or more available network connections provided by the network-enabled device; blocking the one or more detected network connections; retrieving device information associated with the network-enabled device; transmitting the device information from the network-enabled device to a secure cloud to configure a virtual private network, VPN, connection between the secure cloud and the network-enabled device; receiving cloud information from the secure cloud, the cloud information specifying a cloud server in the secure cloud and being generated by the secure cloud based on the device information; updating domain name service, DNS, and routing functions at the network-enabled device based on the cloud information to forward network requests to the cloud server specified in the cloud information; and establishing the VPN connection to the cloud server in the secure cloud based on the cloud information, wherein any network traffic between the network-enabled device and the one or more detected networks is routed through the VPN connection to the cloud-based multi-function firewall implemented on the cloud server.
An airfoil comprising: an airfoil section (66; 166) having an airfoil wall defining a leading end , a trailing end , and first and second sides joining the leading end and the trailing end , the first and second sides spanning in a longitudinal direction between first and second ends , the airfoil wall circumscribing an internal core cavity configured to receive cooling air during operation; a first cooling passage network embedded in the first side of the airfoil wall between inner and outer portions of the first side of airfoil wall , the first cooling passage network defining a passage forward edge and a passage aft edge , the first side of the airfoil wall having a portion that tapers in thickness at the passage aft edge ; and a second cooling passage network embedded in the second side of the airfoil wall between inner and outer portions of the second side of airfoil wall , the inner portion of the second side of the airfoil wall including a protrusion located across the internal core cavity from the portion of the first side that tapers in thickness, wherein the airfoil section includes a rib partitioning the internal core cavity into a forward cavity and a trailing cavity , and the protrusion is in the trailing cavity , wherein the trailing cavity constantly converges toward the trailing end of the airfoil section , wherein the protrusion has an apex , a forward side , and an aft side , characterised in that the forward side is steeper than the aft side . an airfoil section (66; 166) having an airfoil wall defining a leading end , a trailing end , and first and second sides joining the leading end and the trailing end , the first and second sides spanning in a longitudinal direction between first and second ends , the airfoil wall circumscribing an internal core cavity configured to receive cooling air during operation; a first cooling passage network embedded in the first side of the airfoil wall between inner and outer portions of the first side of airfoil wall , the first cooling passage network defining a passage forward edge and a passage aft edge , the first side of the airfoil wall having a portion that tapers in thickness at the passage aft edge ; and a second cooling passage network embedded in the second side of the airfoil wall between inner and outer portions of the second side of airfoil wall , the inner portion of the second side of the airfoil wall including a protrusion located across the internal core cavity from the portion of the first side that tapers in thickness, wherein the airfoil section includes a rib partitioning the internal core cavity into a forward cavity and a trailing cavity , and the protrusion is in the trailing cavity , wherein the trailing cavity constantly converges toward the trailing end of the airfoil section , wherein the protrusion has an apex , a forward side , and an aft side , characterised in that the forward side is steeper than the aft side .
A device , comprising: a removeable grid cord having an electrical plug including a plurality of current carrying blades ; a plurality of temperature sensing elements that is configured to transmit a plurality of temperature signals that each indicates a current carrying blade temperature associated with one of the plurality of current carrying blades , wherein the plurality of temperature sensing elements is arranged proximally to the plurality of current carrying blades ; and; a control module that comprises a microprocessor and is configured to perform the steps of receiving the plurality of temperature signals , determining a temperature condition of the electrical plug based on the plurality of temperature signals , and characterised in that the control module is further configured to disrupt electrical power supplied via the electrical plug and carried by an electrical power carrying conductor according to a predetermined pattern to provide a digital signal to an in-cable control protection device indicating the temperature condition of the electrical plug , wherein a first interruption pattern consisting of a single pulse indicates a logic 1 value and a second interruption pattern consisting of a plurality of pulses indicates a logic 0 value. a removeable grid cord having an electrical plug including a plurality of current carrying blades ; a plurality of temperature sensing elements that is configured to transmit a plurality of temperature signals that each indicates a current carrying blade temperature associated with one of the plurality of current carrying blades , wherein the plurality of temperature sensing elements is arranged proximally to the plurality of current carrying blades ; and; a control module that comprises a microprocessor and is configured to perform the steps of receiving the plurality of temperature signals , determining a temperature condition of the electrical plug based on the plurality of temperature signals , and characterised in that the control module is further configured to disrupt electrical power supplied via the electrical plug and carried by an electrical power carrying conductor according to a predetermined pattern to provide a digital signal to an in-cable control protection device indicating the temperature condition of the electrical plug , wherein a first interruption pattern consisting of a single pulse indicates a logic 1 value and a second interruption pattern consisting of a plurality of pulses indicates a logic 0 value.
An apparatus comprising a harvester head reel comprising a bat support ; an extendable bat supported by the bat support , the extendable bat having a first segment and a second segment overlapping the first segment ; a first finger extending from the first segment ; and a second finger extending from the second segment , characterized by comprising an actuator to extend and retract the second segment relative to the first segment based upon an angular position of the bat about a longitudinal axis of the reel as the bat rotates about the longitudinal axis of the reel .