mhurhangee/ep-ind-claims huggingface dataset:
A conduit for extending across fluid flow regions in a gas turbine engine, the conduit comprising: a first segment forming a first sidewall of the conduit, the first segment comprising a first inner surface and a first outer surface; and a second segment forming a second sidewall of the conduit, the second segment comprising a second inner surface and a second outer surface; wherein the first segment is coupled to the second segment such that the first inner surface and the second inner surface jointly form an inner conduit surface and the first outer surface and the second outer surface jointly form at least a portion of an outer conduit surface, wherein the outer conduit surface has an airfoil geometry, characterised in that the conduit further comprises a third segment and a fourth segment, wherein the third segment couples the first segment to the second segment and forms a leading edge portion of the airfoil geometry of the outer conduit surface, wherein the fourth segment couples the first segment to the second segment and forms a trailing edge portion of the airfoil geometry of the outer conduit surface. a first segment forming a first sidewall of the conduit, the first segment comprising a first inner surface and a first outer surface; and a second segment forming a second sidewall of the conduit, the second segment comprising a second inner surface and a second outer surface; wherein the first segment is coupled to the second segment such that the first inner surface and the second inner surface jointly form an inner conduit surface and the first outer surface and the second outer surface jointly form at least a portion of an outer conduit surface, wherein the outer conduit surface has an airfoil geometry, characterised in that the conduit further comprises a third segment and a fourth segment, wherein the third segment couples the first segment to the second segment and forms a leading edge portion of the airfoil geometry of the outer conduit surface, wherein the fourth segment couples the first segment to the second segment and forms a trailing edge portion of the airfoil geometry of the outer conduit surface.
A method for detecting a mutated PIK3CA polynucleotide, comprising: amplifying a PIK3CA polynucleotide; and detecting the presence of a mutation in the polynucleotide amplified in the amplification step, wherein the mutation is at least one mutation selected from the group consisting of C112T, G113A, G263A, C311G, G317T, G323C, del332-334, G353A, G365A, C370A, T1035A, G1048C, T1132C, T1258C, G1357C, C1616G, G1624A, A1625G, A1625T, G1633A, A1634G, G1635T, C1636A, A1637C, C1981A, A2102C, G2702T, T2725C, T3022C, A3073G, C3074A, G3129T, C3139T, A3140G, A3140T, G3145A in comparison with a wild type PIK3CA polynucleotide, the wild type PIK3CA polynucleotide having a nucleotide sequence of SEQ ID NO.1.
A labyrinth seal for a gas turbine engine comprising: a first annular member positioned on a center axis; a second annular member disposed circumferentially around the first annular member, wherein the first annular member and the second annular member form a leakage flowpath therebetween with an upstream end and a downstream end; a seal land disposed on the second annular member, and positioned radially between the first annular member and the second annular member relative the center axis; and a seal plate disposed on the the first annular member, wherein the seal plate extends radially toward the seal land, wherein the seal plate comprises: a plate body extending between a base and a tip of the seal plate, wherein the plate body extends along a majority of a radial span of the seal plate on a first plane, wherein the tip of the seal plate extends axially and radially outward from the plate body on a second plane, wherein the seal plate further comprises a flange extending radially away from the plate body toward the seal land, and wherein the flange is spaced axially downstream from the tip relative the leakage flowpath, and wherein the tip of the seal plate extends axially upstream. a first annular member positioned on a center axis; a second annular member disposed circumferentially around the first annular member, wherein the first annular member and the second annular member form a leakage flowpath therebetween with an upstream end and a downstream end; a seal land disposed on the second annular member, and positioned radially between the first annular member and the second annular member relative the center axis; and a seal plate disposed on the the first annular member, wherein the seal plate extends radially toward the seal land, wherein the seal plate comprises: a plate body extending between a base and a tip of the seal plate, wherein the plate body extends along a majority of a radial span of the seal plate on a first plane, wherein the tip of the seal plate extends axially and radially outward from the plate body on a second plane, wherein the seal plate further comprises a flange extending radially away from the plate body toward the seal land, and wherein the flange is spaced axially downstream from the tip relative the leakage flowpath, and a plate body extending between a base and a tip of the seal plate, wherein the plate body extends along a majority of a radial span of the seal plate on a first plane, wherein the tip of the seal plate extends axially and radially outward from the plate body on a second plane, wherein the seal plate further comprises a flange extending radially away from the plate body toward the seal land, and wherein the flange is spaced axially downstream from the tip relative the leakage flowpath, and wherein the tip of the seal plate extends axially upstream.
A shapeable passer for surgical cable or suture, comprising: one or more malleable stiffener elements; and a flexible tubular extrusion, comprising: at least one first lumen (12a, 12b; 16) configured to receive a leading end (40, 42) of at least one surgical cable or suture (44, 46), said at least one lumen having a leading end and one trailing end (20; 36, 38); and at least one second lumen configured to contain a respective one of said stiffener elements, each of said lumens having a leading end and a trailing end, said lumens being configured to be parallel to one another lengthwise along a long axis of said extrusion, characterized in that said one trailing end (20, 36, 38) of said at least one first lumen is configured to be open and flared to facilitate manual insertion of a leading end of said surgical cable or suture into said lumen; and in that a portion of said passer containing one or more of said malleable stiffener elements is configured to be intraoperatively shaped as desired, the leading end of at least one of said second lumens, which is configured to contain a respective one of said malleable stiffener elements, is sealed, capped or tipped. one or more malleable stiffener elements; and a flexible tubular extrusion, comprising: at least one first lumen (12a, 12b; 16) configured to receive a leading end (40, 42) of at least one surgical cable or suture (44, 46), said at least one lumen having a leading end and one trailing end (20; 36, 38); and at least one second lumen configured to contain a respective one of said stiffener elements, each of said lumens having a leading end and a trailing end, said lumens being configured to be parallel to one another lengthwise along a long axis of said extrusion, at least one first lumen (12a, 12b; 16) configured to receive a leading end (40, 42) of at least one surgical cable or suture (44, 46), said at least one lumen having a leading end and one trailing end (20; 36, 38); and at least one second lumen configured to contain a respective one of said stiffener elements, each of said lumens having a leading end and a trailing end, said lumens being configured to be parallel to one another lengthwise along a long axis of said extrusion, characterized in that said one trailing end (20, 36, 38) of said at least one first lumen is configured to be open and flared to facilitate manual insertion of a leading end of said surgical cable or suture into said lumen; and in that a portion of said passer containing one or more of said malleable stiffener elements is configured to be intraoperatively shaped as desired, the leading end of at least one of said second lumens, which is configured to contain a respective one of said malleable stiffener elements, is sealed, capped or tipped.
An engine comprising an EGR apparatus which refluxes a portion of exhaust gas from an exhaust system to an intake system as EGR gas, wherein differential pressure detecting means which detects differential pressure between intake pressure in the intake system and exhaust pressure in the exhaust system is mounted on a head cover which covers an upper portion of a cylinder head, an intake pressure taking-out passage which is in communication with the intake system is formed in the cylinder head, an intake pressure introducing passage which is connected to the differential pressure detecting means is formed in the head cover, and the intake pressure taking-out passage and the intake pressure introducing passage are in communication with each other characterized in that the differential pressure detecting means and the exhaust system are in communication with each other through an external exhaust pressure taking-out pipe, and the exhaust pressure taking-out pipe is installed such that it faces a cooling fan disposed on one side surface of a cylinder block.
A cart (100, 200, 500, 600) comprising: a chassis connected to a plurality of wheels (151, 152, 153, 154); a basket mounted on the chassis and adapted to store one or more items therein; and a bridge element which is formed as an integral part of the cart and is adapted to fit onto an edge of a vehicular trunk, wherein the bridge element of the cart (100, 200, 500, 600) is at an area of said cart (100, 200, 500, 600) located between said basket and said wheels (151, 152, 153, 154); characterized in that the bridge element is suspended from and moveable on one or more rails that are fixedly connected to the basket substantially in parallel to a long axis of the basket. a chassis connected to a plurality of wheels (151, 152, 153, 154); a basket mounted on the chassis and adapted to store one or more items therein; and a bridge element which is formed as an integral part of the cart and is adapted to fit onto an edge of a vehicular trunk, wherein the bridge element of the cart (100, 200, 500, 600) is at an area of said cart (100, 200, 500, 600) located between said basket and said wheels (151, 152, 153, 154); characterized in that the bridge element is suspended from and moveable on one or more rails that are fixedly connected to the basket substantially in parallel to a long axis of the basket.
A method for wireless communications by a user equipment, UE (115, 115-a, 115-b), comprising: receiving (310, 1305), from an edge data network via a wireless network, an indication of one or more performance indicators for an application client that is unaware that edge service support is available via the edge data network; receiving (315, 1310), from the edge data network via the wireless network, an edge service support message indicating edge service support for the application client; transmitting (320, 350, 1205), to the edge data network via the wireless network, an indication of an adjustment to the one or more performance indicators for the application client operating on the UE to receive service from the edge data network, the adjustment to the one or more performance indicators based at least in part on a UE-modified performance profile for the application client; and communicating (330, 370, 1210) application data traffic with the edge data network via the wireless network to provide edge service to the application client in accordance with the one or more adjusted performance indicators. receiving (310, 1305), from an edge data network via a wireless network, an indication of one or more performance indicators for an application client that is unaware that edge service support is available via the edge data network; receiving (315, 1310), from the edge data network via the wireless network, an edge service support message indicating edge service support for the application client; transmitting (320, 350, 1205), to the edge data network via the wireless network, an indication of an adjustment to the one or more performance indicators for the application client operating on the UE to receive service from the edge data network, the adjustment to the one or more performance indicators based at least in part on a UE-modified performance profile for the application client; and communicating (330, 370, 1210) application data traffic with the edge data network via the wireless network to provide edge service to the application client in accordance with the one or more adjusted performance indicators.
A compound represented by a chemical formula below: wherein R 1 and R 2 are each an aliphatic hydrocarbon group, X is a single bond or a hydrocarbon group having 1 or more and 5 or less carbon atoms, a total number of carbon atoms of R 1, R 2, and X is 2 or more and 39 or less, A 1 is -O(-A 11 O) m -H or -O(-A 12 O) p -H, A 2 is -O-R 3 O(-A 21 O) n -H or - O(-A 22 O) q+1 -H, R 3 is an alkanediyl group having 4 or more and 18 or less carbon atoms, m pieces of A 11 and n pieces of A 21 are each independently an alkanediyl group having 2 or more and 3 or less carbon atoms, p pieces of A 12 and q + 1 pieces of A 22 are each independently an alkanediyl group having 2 or more and 8 or less carbon atoms, at least one piece of A 22 among the q + 1 pieces of A 22 is a linear alkane-α,ω-diyl group having 3 or more and 8 or less carbon atoms, m, n, p, and q are an average value and are each independently 0 or more, a total of m and n is more than 0 and 50 or less, and a total of p and q is more than 0 and 50 or less.
A sheet-shaped pouch made of an exterior material for a secondary battery, in which an internal space configured to accommodate an electrode assembly constituted by electrodes and separators is defined, the exterior material comprising: a first metal part; a second metal part spaced apart from the first metal part; and a first adhesive part provided between the first metal part and the second metal part to adhere to each of the first metal part and the second metal part, wherein the first metal part is provided closer to the internal space than the second metal part, and the first metal part has a thermal conductivity greater than a thermal conductivity of the second metal part. a first metal part; a second metal part spaced apart from the first metal part; and a first adhesive part provided between the first metal part and the second metal part to adhere to each of the first metal part and the second metal part, wherein the first metal part is provided closer to the internal space than the second metal part, and the first metal part has a thermal conductivity greater than a thermal conductivity of the second metal part.
A transfer system for receiving a film applicator from an elongate member, holding the film applicator, and transferring the film applicator to a second elongate member, the transfer system comprising, a transfer cart comprising: a frame comprising an upper end portion,a lower end portion, a mounting platform, and legs wherein each leg has an upper end and a lower end and the upper end of each leg is connected to the mounting platform; an ambulation device connected to the lower ends of the legs of the frame; and a transfer fixture mounted on the mounting platform, said transfer fixture comprising: a pair of beams (320, 322) spaced apart to define a channel there between characterised in that each beam comprises an upper outwardly turned flange and a lower outwardly turned flange connected by a web and wherein the upper flange of each beam comprises a track surface, and the lower flange of each beam is connected to the mounting platform; and an elongate transfer member positioned in said channel, said elongate transfer member comprising a web and a base flange connected to an upper end of the web and wherein a lower end of the web is connected to the mounting platform of the frame such that the base flange of the elongate transfer member is substantially parallel with the upper flanges of the beams. a frame comprising an upper end portion,a lower end portion, a mounting platform, and legs wherein each leg has an upper end and a lower end and the upper end of each leg is connected to the mounting platform; an ambulation device connected to the lower ends of the legs of the frame; and a transfer fixture mounted on the mounting platform, said transfer fixture comprising: a pair of beams (320, 322) spaced apart to define a channel there between characterised in that each beam comprises an upper outwardly turned flange and a lower outwardly turned flange connected by a web and wherein the upper flange of each beam comprises a track surface, and the lower flange of each beam is connected to the mounting platform; and an elongate transfer member positioned in said channel, said elongate transfer member comprising a web and a base flange connected to an upper end of the web and wherein a lower end of the web is connected to the mounting platform of the frame such that the base flange of the elongate transfer member is substantially parallel with the upper flanges of the beams. a pair of beams (320, 322) spaced apart to define a channel there between characterised in that each beam comprises an upper outwardly turned flange and a lower outwardly turned flange connected by a web and wherein the upper flange of each beam comprises a track surface, and the lower flange of each beam is connected to the mounting platform; and an elongate transfer member positioned in said channel, said elongate transfer member comprising a web and a base flange connected to an upper end of the web and wherein a lower end of the web is connected to the mounting platform of the frame such that the base flange of the elongate transfer member is substantially parallel with the upper flanges of the beams.
A gas vent clogging detection device comprising: a resin decomposition gas concentration detection sensor configured to detect concentration of a resin decomposition gas of a resin supplied to a cavity space of a mold device, the resin decomposition gas being exhausted from a gas vent of the mold device; and a determination unit configured to determine whether or not the gas vent of the mold device is clogged on the basis of the resin decomposition gas concentration detected by the resin decomposition gas concentration detection sensor. a resin decomposition gas concentration detection sensor configured to detect concentration of a resin decomposition gas of a resin supplied to a cavity space of a mold device, the resin decomposition gas being exhausted from a gas vent of the mold device; and a determination unit configured to determine whether or not the gas vent of the mold device is clogged on the basis of the resin decomposition gas concentration detected by the resin decomposition gas concentration detection sensor.
A device for torque measurement of friction, the device comprising: a cylindrical core comprising an exterior surface having at least one protrusion or indent; and a cap having a central cavity in which the cylindrical core is received coaxially so that a top end of the cylindrical core is proximal to a first end of the cap, the cap comprising at least one protrusion or indent on a surface of the central cavity, wherein the device comprises at least one first protrusion on either of the cylindrical core or the cap, wherein the at least one first protrusion provides a pulsed interference contact with at least one of a second protrusion or an indent on the other of the cylindrical core or the cap, when the cap may rotate about the core. a cylindrical core comprising an exterior surface having at least one protrusion or indent; and a cap having a central cavity in which the cylindrical core is received coaxially so that a top end of the cylindrical core is proximal to a first end of the cap, the cap comprising at least one protrusion or indent on a surface of the central cavity, wherein the device comprises at least one first protrusion on either of the cylindrical core or the cap, wherein the at least one first protrusion provides a pulsed interference contact with at least one of a second protrusion or an indent on the other of the cylindrical core or the cap, when the cap may rotate about the core.
An aircraft comprising a pressurized cabin, a circuit for exhausting air from the cabin to the outside of the aircraft, an auxiliary power unit of the type including a combustion chamber for fuel, and an architecture for supplying air to the auxiliary power unit, the architecture including: a duct for supplying air to the auxiliary power unit, and a circuit for injecting air coming from the pressurized cabin into the supply duct of the auxiliary power unit, the aircraft being characterized in that the architecture includes - a unit for controlling the flow of air supplied to the auxiliary power unit, - a valve for admitting air from outside the aircraft, positioned at the inlet of the supply duct, the opening of said valve being controlled by the control unit, and in that the circuit for injecting air coming from the pressurized cabin includes a distribution valve the opening whereof is controlled by the control unit to draw a proportion of a flow of air circulating in the exhaust circuit, wherein the circuit for injecting air is connected to the circuit for exhausting air toward the outside of the aircraft through the distribution valve, and in that the circuit for injecting air further includes at its exit a nozzle for injecting said proportion into the supply duct of the auxiliary power unit. a duct for supplying air to the auxiliary power unit, and a circuit for injecting air coming from the pressurized cabin into the supply duct of the auxiliary power unit, the aircraft being characterized in that the architecture includes - a unit for controlling the flow of air supplied to the auxiliary power unit, - a valve for admitting air from outside the aircraft, positioned at the inlet of the supply duct, the opening of said valve being controlled by the control unit, and in that the circuit for injecting air coming from the pressurized cabin includes a distribution valve the opening whereof is controlled by the control unit to draw a proportion of a flow of air circulating in the exhaust circuit, wherein the circuit for injecting air is connected to the circuit for exhausting air toward the outside of the aircraft through the distribution valve, and in that the circuit for injecting air further includes at its exit a nozzle for injecting said proportion into the supply duct of the auxiliary power unit. - a unit for controlling the flow of air supplied to the auxiliary power unit, - a valve for admitting air from outside the aircraft, positioned at the inlet of the supply duct, the opening of said valve being controlled by the control unit, and in that the circuit for injecting air coming from the pressurized cabin includes a distribution valve the opening whereof is controlled by the control unit to draw a proportion of a flow of air circulating in the exhaust circuit, wherein the circuit for injecting air is connected to the circuit for exhausting air toward the outside of the aircraft through the distribution valve, and in that the circuit for injecting air further includes at its exit a nozzle for injecting said proportion into the supply duct of the auxiliary power unit.
A structural system for constructing single-layer structures, said structural system comprising bars, with at least one coaxial hole in each end of the bar, joined to nodes by means of joining screws, wherein a bushing with interior threading embedded and fastened in the coaxial holes of the ends of the bar houses the joining screw that fastens the bar-node (1, joint; characterized by each node having at least one threaded through hole intended to receive the joining screw.