mhurhangee/ep-ind-claims huggingface dataset:
A method of preparing a nucleic acid library from a sample comprising; (i) reacting a sample comprising a plurality of cellular nucleic acids each having a terminal 3'-modified dideoxynucleotide (ddNTP) comprising a 3'-azido moiety, with a plurality of adaptor nucleic acids each comprising a terminal 5'-modified ddNTP comprising a 5'-alkynyl moiety, wherein the 3' functional moiety and 5' functional moiety react in a click chemistry reaction to form a modified backbone linkage comprising the structure thereby forming a plurality of ligated-nucleic acids; and (ii) amplifying the plurality of ligated-nucleic acids thereby preparing a nucleic acid library from the sample, wherein the terminal 3'-modified ddNTP is incorporated into each of the plurality of cellular nucleic acids by contacting the plurality of cellular nucleic acids with a template independent polymerase, and wherein the template independent polymerase is TdT. (i) reacting a sample comprising a plurality of cellular nucleic acids each having a terminal 3'-modified dideoxynucleotide (ddNTP) comprising a 3'-azido moiety, with a plurality of adaptor nucleic acids each comprising a terminal 5'-modified ddNTP comprising a 5'-alkynyl moiety, wherein the 3' functional moiety and 5' functional moiety react in a click chemistry reaction to form a modified backbone linkage comprising the structure thereby forming a plurality of ligated-nucleic acids; and (ii) amplifying the plurality of ligated-nucleic acids thereby preparing a nucleic acid library from the sample, wherein the terminal 3'-modified ddNTP is incorporated into each of the plurality of cellular nucleic acids by contacting the plurality of cellular nucleic acids with a template independent polymerase, and wherein the template independent polymerase is TdT.
A self-propelled work machine, comprising: a machine frame supportable by a plurality of ground engaging units (14, 16, 18, 20); a support device connected between said machine frame and at least one of said ground engaging units, said support device including a lifting column adapted to controllably raise and lower said associated connected ground engaging unit relative to said machine frame; a first actuator connected to said support device and adapted to move said one ground engaging unit between projecting and retracted positions relative to said machine frame; a second actuator connected to said lifting column and adapted to cause at least a portion of said lifting column to rotate about a lifting column axis relative to said machine frame; and a controller associated with and adapted to coordinate the actuation of said first and second actuators (42, 44) to maintain the same rotational direction of said ground engaging unit in each of said projecting and retracted positions, characterized in that said second actuator is positioned at a location linearly spaced apart from said first actuator along said lifting column axis; and said second actuator is a rotary actuator having a rotor operatively engaged with a portion of said lifting column. a machine frame supportable by a plurality of ground engaging units (14, 16, 18, 20); a support device connected between said machine frame and at least one of said ground engaging units, said support device including a lifting column adapted to controllably raise and lower said associated connected ground engaging unit relative to said machine frame; a first actuator connected to said support device and adapted to move said one ground engaging unit between projecting and retracted positions relative to said machine frame; a second actuator connected to said lifting column and adapted to cause at least a portion of said lifting column to rotate about a lifting column axis relative to said machine frame; and a controller associated with and adapted to coordinate the actuation of said first and second actuators (42, 44) to maintain the same rotational direction of said ground engaging unit in each of said projecting and retracted positions, characterized in that said second actuator is positioned at a location linearly spaced apart from said first actuator along said lifting column axis; and said second actuator is a rotary actuator having a rotor operatively engaged with a portion of said lifting column.
A packet processing method, wherein the method comprises: receiving, by a provider edge, PE, device, a first Virtual Extensible Local Area Network, VxLAN, encapsulated packet sent by a network virtualization edge, NVE, device, wherein the PE device and the NVE device are located in a same data center, DC, and the first VxLAN encapsulated packet comprises a first VxLAN network identifier, VNI; parsing, by the PE device, the first VxLAN encapsulated packet to obtain the first VNI, and obtaining, according to a correspondence between a VNI and a virtual private network, VPN, routing and forwarding, VRF, table, a first VRF table that corresponds to the first VNI; and searching, by the PE device, the first VRF table for a route according to a destination Internet Protocol, IP, address of the first VxLAN encapsulated packet, and forwarding the first VxLAN encapsulated packet, wherein the method further comprises: deploying, by the PE device, a Border Gateway Protocol, BGP, and receiving, by the PE device, a BGP route update message sent by the NVE device, wherein the BGP route update message comprises a VxLAN tunnel end point, VTEP, address and a VNI that corresponds to the VTEP address; and learning, by the PE device, the VTEP address in the BGP route update message to a VRF table according to a correspondence between the VNI and the VRF table. receiving, by a provider edge, PE, device, a first Virtual Extensible Local Area Network, VxLAN, encapsulated packet sent by a network virtualization edge, NVE, device, wherein the PE device and the NVE device are located in a same data center, DC, and the first VxLAN encapsulated packet comprises a first VxLAN network identifier, VNI; parsing, by the PE device, the first VxLAN encapsulated packet to obtain the first VNI, and obtaining, according to a correspondence between a VNI and a virtual private network, VPN, routing and forwarding, VRF, table, a first VRF table that corresponds to the first VNI; and searching, by the PE device, the first VRF table for a route according to a destination Internet Protocol, IP, address of the first VxLAN encapsulated packet, and forwarding the first VxLAN encapsulated packet, wherein the method further comprises: deploying, by the PE device, a Border Gateway Protocol, BGP, and receiving, by the PE device, a BGP route update message sent by the NVE device, wherein the BGP route update message comprises a VxLAN tunnel end point, VTEP, address and a VNI that corresponds to the VTEP address; and learning, by the PE device, the VTEP address in the BGP route update message to a VRF table according to a correspondence between the VNI and the VRF table. deploying, by the PE device, a Border Gateway Protocol, BGP, and receiving, by the PE device, a BGP route update message sent by the NVE device, wherein the BGP route update message comprises a VxLAN tunnel end point, VTEP, address and a VNI that corresponds to the VTEP address; and learning, by the PE device, the VTEP address in the BGP route update message to a VRF table according to a correspondence between the VNI and the VRF table.
An air bag (102,320) having a tether (30,130), the tether (30, 130) formed into a hook (155,157) or hooks (155, 157) and a loop or eye configured to be looped about a structure including an inflator to which the air bag and tether are to be secured.
A combustor for a gas turbine engine, the combustor comprising: an axial fuel injection system in communication with a combustion chamber, said axial fuel injection system operable to supply between sixteen percent and thirty-five percent of a combustion airflow; a radial fuel injection system that communicates with said combustion chamber downstream of said axial fuel injection system, said radial fuel injection system operable to supply between thirty percent and sixty percent of said combustion airflow; and a multiple of dilution holes in communication with the combustion chamber and downstream of said radial fuel injection system, said multiple of dilution holes operable to supply between five percent and twenty percent of said combustion airflow, wherein said combustion chamber is defined between an inner liner and an outer liner, and wherein the combustor further comprises a forward assembly between said inner liner and said outer liner, wherein said forward assembly includes a bulkhead liner that defines a bulkhead height, and wherein said inner liner and said outer liner are radially spaced between one hundred percent and two hundred percent of said bulkhead height axially proximate to said radial fuel injection system. an axial fuel injection system in communication with a combustion chamber, said axial fuel injection system operable to supply between sixteen percent and thirty-five percent of a combustion airflow; a radial fuel injection system that communicates with said combustion chamber downstream of said axial fuel injection system, said radial fuel injection system operable to supply between thirty percent and sixty percent of said combustion airflow; and a multiple of dilution holes in communication with the combustion chamber and downstream of said radial fuel injection system, said multiple of dilution holes operable to supply between five percent and twenty percent of said combustion airflow, wherein said combustion chamber is defined between an inner liner and an outer liner, and wherein the combustor further comprises a forward assembly between said inner liner and said outer liner, wherein said forward assembly includes a bulkhead liner that defines a bulkhead height, and wherein said inner liner and said outer liner are radially spaced between one hundred percent and two hundred percent of said bulkhead height axially proximate to said radial fuel injection system.
An aircraft tire pressure loop link for electromagnetically coupling a magnetic field between an electromagnetic transceiver coil of a wheel axle and a tire pressure sensor receiver coil spaced apart from the electromagnetic transceiver coil of the wheel axle for powering a tire pressure sensor, comprising: a first single metal loop configured to be mounted on a carrier ring configured to encircle a wheel axle adjacent to the electromagnetic transceiver coil of the wheel axle; a second single metal loop configured to be mounted adjacent to a tire pressure sensor transceiver coil; and a pair of spaced apart electrically conductive connecting arms (114, 115, 116) electrically connected between said first single metal loop and said second single metal loop, said pair of spaced apart electrically conductive connecting arms (114, 115, 116) being configured to carry current generated in the first single metal loop from the electromagnetic transceiver coil of the wheel axle to the second single metal loop, whereby current induced in the first single metal loop travels via the pair of spaced apart electrically conductive connecting arms (114, 115, 116) a distance from the electromagnetic transceiver coil of the wheel axle to the second single metal loop, to generate flux in the tire pressure sensor receiver coil for powering the tire pressure sensor, the aircraft tire pressure loop link. a first single metal loop configured to be mounted on a carrier ring configured to encircle a wheel axle adjacent to the electromagnetic transceiver coil of the wheel axle; a second single metal loop configured to be mounted adjacent to a tire pressure sensor transceiver coil; and a pair of spaced apart electrically conductive connecting arms (114, 115, 116) electrically connected between said first single metal loop and said second single metal loop, said pair of spaced apart electrically conductive connecting arms (114, 115, 116) being configured to carry current generated in the first single metal loop from the electromagnetic transceiver coil of the wheel axle to the second single metal loop, whereby current induced in the first single metal loop travels via the pair of spaced apart electrically conductive connecting arms (114, 115, 116) a distance from the electromagnetic transceiver coil of the wheel axle to the second single metal loop, to generate flux in the tire pressure sensor receiver coil for powering the tire pressure sensor, the aircraft tire pressure loop link.
A tire comprising: a circular tire frame formed from a resin material; and a reinforcing metal cord member that is wound on an outer circumference of the tire frame, at least a portion of the reinforcing metal cord member being covered, via an adhesion layer including a hot melt adhesive, with a covering composition that comprises at least one thermoplastic material selected from the group consisting of a thermoplastic resin and a thermoplastic elastomer, wherein the hot-melt adhesive comprises at least one kind selected from a modified olefin-based resin, an ethylene-ethyl acrylate copolymer, or an ethylene-vinyl acetate copolymer. a circular tire frame formed from a resin material; and
A fluid control valve, comprising: a first valve body including an outlet, a first inlet, and a first cavity formed through an upper surface in fluid communication with the first inlet; a second valve body having a bottom surface disposed on and coupled in a fluid-tight manner to the upper surface, the second valve body including a second inlet and a second cavity having a lip, the second cavity formed through the bottom surface and in selectable communication with the second inlet; and a valve member, including a sealing element disposed on a portion of a valve stem, supported within the first and second valve bodies (102, 120) for displacement between at least a first valve position and a second valve position, wherein the outlet is in selectable fluid communication with the first inlet and the second inlet and comprises a plurality of passages (110a, 110b). a first valve body including an outlet, a first inlet, and a first cavity formed through an upper surface in fluid communication with the first inlet; a second valve body having a bottom surface disposed on and coupled in a fluid-tight manner to the upper surface, the second valve body including a second inlet and a second cavity having a lip, the second cavity formed through the bottom surface and in selectable communication with the second inlet; and a valve member, including a sealing element disposed on a portion of a valve stem, supported within the first and second valve bodies (102, 120) for displacement between at least a first valve position and a second valve position, wherein the outlet is in selectable fluid communication with the first inlet and the second inlet and comprises a plurality of passages (110a, 110b).
Usage of a laminated structure of conducting layers and insulating layers comprising a plurality of contacting holes penetrating one or more conducting layers of said laminated structure, wherein each contacting hole comprises an insulating sleeve and a conducting pin arranged therein which contacts an associated conducting layer with one end portion end and extends to the outside of said laminated structure with a second end portion, as a bus plate for mounting a phase power converter for converting an electric AC current supplied by an electric generator into an electric AC current of a grid, in a busbar system which is accommodated in the nacelle of a wind turbine, wherein said laminated structure comprises a first and second laminated sub structure, electrically insulated from each other, wherein the first laminated sub structure is adapted to be electrically connected to the grid and to the output terminals of a first circuit breaker, and in that said second laminated sub structure is adapted to be connected to an output side of said phase power converter and to the input terminals of said first circuit breaker, wherein said phase power converter and at least said first circuit breaker and/or further electrical components like capacitors and/or inductors are mounted to conducting pins extending out of the contacting holes on the same side of the laminated structure 1, and wherein said laminated structure 1 comprises a front side, which is formed of an insulating material, to which the phase power converter is mounted, and an electrically conducting rear side, which is formed by an uncoated layer of sheet metal which is electrically connected to protective earth of the grid.
A method for channel assessment in unlicensed spectrum, the method comprising receiving, by a first device, a first clear channel assessment, CCA, configuration from a second device, the first CCA configuration indicating one or more channels of the unlicensed spectrum each with a respective CCA bandwidth; performing, by the first device, medium access measurements in accordance with the first CCA configuration, and transmitting results of the medium access measurements to the second device; and receiving, by the first device, a second CCA configuration from the second device, the second CCA configuration indicating one or more channels of the unlicensed spectrum each with a respective CCA bandwidth, the second CCA configuration being different from the first CCA configuration. receiving, by a first device, a first clear channel assessment, CCA, configuration from a second device, the first CCA configuration indicating one or more channels of the unlicensed spectrum each with a respective CCA bandwidth; performing, by the first device, medium access measurements in accordance with the first CCA configuration, and transmitting results of the medium access measurements to the second device; and receiving, by the first device, a second CCA configuration from the second device, the second CCA configuration indicating one or more channels of the unlicensed spectrum each with a respective CCA bandwidth, the second CCA configuration being different from the first CCA configuration.
Method of producing a heat exchanger, the heat exchanger comprising; a coolant housing being of rectangular parallelepipedic shape with two opposing wide side walls and two header plates; tubes extending in parallel through said housing between the two header plates; an inlet air tank and an outlet air tank each comprising a cowling tightly fitting one of said header plates each and having an air inlet and an air outlet, respectively; and said coolant housing has two opposing narrow side walls (24, 25) tightly fitting said wide side walls and said header plates and defining together with these wide side walls and header plates a first coolant tank and a second coolant tank opposing the first one; characterized by the steps of: assembling of at least the wide side walls, the two header plates, the tubes, and the cowlings to a unit; brazing of said unit by heating thereof in a furnace; and welding of at least one of said two opposing narrow side walls (24, 25) to said unit in order to enclose said coolant housing. assembling of at least the wide side walls, the two header plates, the tubes, and the cowlings to a unit; brazing of said unit by heating thereof in a furnace; and welding of at least one of said two opposing narrow side walls (24, 25) to said unit in order to enclose said coolant housing.
Method for reducing a risk of tampering and/or spoofing of location data of an object over time, the method comprising the steps of: - providing a signals-in-space receiver to the object, the signals-in-space receiver comprising an antenna for receiving an encrypted navigation signal (10a, 10b, 10c, 10d), an A/D converter for discretizing the encrypted navigation signal (10a, 10b, 10c, 10d) into encrypted navigation data, a memory unit for storing the encrypted navigation data and an interface for connecting a reader to the memory unit, wherein a decryption key for decrypting the encrypted navigation data is not provided in the signals-in-space receiver; - receiving the encrypted navigation signal (10a, 10b, 10c, 10d) over time by the signals-in-space receiver through its antenna; - discretizing the encrypted navigation signal (10a, 10b, 10c, 10d) over time by the A/D converter into encrypted navigation data; - storing the encrypted navigation data over time in the memory unit; - connecting the reader with the memory unit of the signals-in-space receiver; - transferring the encrypted navigation data over time from the memory unit to the reader; - decrypting in the reader the encrypted navigation data over time and retrieving the location data of the object over time, characterized by - checking from the retrieved location data over time where the object has been. - providing a signals-in-space receiver to the object, the signals-in-space receiver comprising an antenna for receiving an encrypted navigation signal (10a, 10b, 10c, 10d), an A/D converter for discretizing the encrypted navigation signal (10a, 10b, 10c, 10d) into encrypted navigation data, a memory unit for storing the encrypted navigation data and an interface for connecting a reader to the memory unit, wherein a decryption key for decrypting the encrypted navigation data is not provided in the signals-in-space receiver; - receiving the encrypted navigation signal (10a, 10b, 10c, 10d) over time by the signals-in-space receiver through its antenna; - discretizing the encrypted navigation signal (10a, 10b, 10c, 10d) over time by the A/D converter into encrypted navigation data; - storing the encrypted navigation data over time in the memory unit; - connecting the reader with the memory unit of the signals-in-space receiver; - transferring the encrypted navigation data over time from the memory unit to the reader; - decrypting in the reader the encrypted navigation data over time and retrieving the location data of the object over time, - checking from the retrieved location data over time where the object has been.
A binder for secondary battery contained in an electrode mixture, the binder comprising: a binder molecule exhibiting an adhesion to a current collector and the active material particles; and a magnetic material displaying magnetism for a magnetic field applied from outside., wherein the binder molecule includes at least one anion substituent group and is at least one selected from the group consisting of polyvinylidene fluoride, polyvinyl alcohol, carboxymethylcellulose, starch, hydroxypropylcellulose, regenerated cellulose, polyvinylpyrrolidone, tetrafluoroethylene, polyethylene, polypropylene, ethylene-propylene-diene terpolymer (EPDM), especially sulfonated EPDM, styrene butylene rubber, and fluorine rubber, or a copolymer thereof, the magnetic material is a cationic metal and is at least one selected from the group consisting of Al, Mg, Ni, Co, Fe, Cr, V, Cu, Zn, Zr, Nb, Mo, Sr, Sb, W and Ti, and the magnetic material is chemically bonded to the binder molecule. a binder molecule exhibiting an adhesion to a current collector and the active material particles; and a magnetic material displaying magnetism for a magnetic field applied from outside., wherein the binder molecule includes at least one anion substituent group and is at least one selected from the group consisting of polyvinylidene fluoride, polyvinyl alcohol, carboxymethylcellulose, starch, hydroxypropylcellulose, regenerated cellulose, polyvinylpyrrolidone, tetrafluoroethylene, polyethylene, polypropylene, ethylene-propylene-diene terpolymer (EPDM), especially sulfonated EPDM, styrene butylene rubber, and fluorine rubber, or a copolymer thereof, the magnetic material is a cationic metal and is at least one selected from the group consisting of Al, Mg, Ni, Co, Fe, Cr, V, Cu, Zn, Zr, Nb, Mo, Sr, Sb, W and Ti, and the magnetic material is chemically bonded to the binder molecule.