mhurhangee/ep-ind-claims huggingface dataset:
An electrode comprising a layer composite, comprising - a current collector, - a base layer in contact with said current collector, said base layer comprising a particulate electroactive material, and - a portion disposed on said base layer, wherein said portion comprises a functional material having a structure different from a structure of the particulate electroactive material in the base layer, said functional material being selected from the group consisting of electronically conducting materials and electroactive materials and mixtures thereof, wherein said portion disposed on said base layer consists of a first layer disposed on said base layer and a second layer disposed on said first layer, wherein said second layer has an external surface facing away from the base layer, wherein the surface roughness R z of said external surface of said portion is 5 μm or less, wherein the surface roughness R z is the mean peak to valley roughness calculated by imaging the surface with a non-contact 3D optical microscope, wherein said first layer and said second layer each comprise a functional material having a structure different from the structure of the particulate electroactive material in the base layer, wherein said functional material in said first layer is a particulate material having a mean maximum cross-sectional dimension which is 50 % or less of the mean maximum cross-sectional dimension of the particulate material in the base layer and wherein said functional material in said second layer is a particulate material having a mean maximum cross-sectional dimension which is 50 % or less of the mean maximum cross-sectional dimension of the particulate material in the first layer, wherein the mean maximum cross-sectional dimension determined through analysis of scanning electron microscope images of the particles. - a current collector, - a base layer in contact with said current collector, said base layer comprising a particulate electroactive material, and - a portion disposed on said base layer, wherein said portion comprises a functional material having a structure different from a structure of the particulate electroactive material in the base layer, said functional material being selected from the group consisting of electronically conducting materials and electroactive materials and mixtures thereof,
A charged particle beam device comprising: an ion beam optics column which irradiates a sample with an ion beam; an electron beam optics column which irradiates the sample with an electron beam; a first sample stage on which the sample is mounted and which is capable of planar movement and tilt movement; a detector which detects a signal generated from the sample; and a second sample stage on which the sample or the detector can be mounted and which is capable of tilting with a cross point of an optical axis of the electron beam optics column and an optical axis of the ion beam optics column as a center; characterized in that in a configuration where the detector is mounted on the second sample stage, said second sample stage can be rotated within a plane including both of the optical axes with the cross point as a center and in that a distance between the detector and the sample can be varied by moving the second sample stage. an ion beam optics column which irradiates a sample with an ion beam; an electron beam optics column which irradiates the sample with an electron beam; a first sample stage on which the sample is mounted and which is capable of planar movement and tilt movement; a detector which detects a signal generated from the sample; and a second sample stage on which the sample or the detector can be mounted and which is capable of tilting with a cross point of an optical axis of the electron beam optics column and an optical axis of the ion beam optics column as a center;
An electromagnetic relay, comprising: a fixed contact module comprising a fixed terminal and a fixed contact joined to the fixed terminal by riveting; a movable contact module comprising a movable spring and a movable contact that is joined to the movable spring by riveting and disposed to face the fixed contact; an armature formed of a magnetic material and configured to move the movable contact module to bring the movable contact into and out of contact with the fixed contact; an electromagnet configured to generate a magnetic field to move the armature; and characterised by a film (13, 24, 49) formed on a surface (43a, 43b) of: a contact of at least one of the fixed contact module and the movable contact module; and at least one of the fixed terminal and the movable spring; wherein the film (13, 24, 49) has a thermal conductivity higher than a thermal conductivity of the contact of the contact module on which the film is formed. a fixed contact module comprising a fixed terminal and a fixed contact joined to the fixed terminal by riveting; a movable contact module comprising a movable spring and a movable contact that is joined to the movable spring by riveting and disposed to face the fixed contact; an armature formed of a magnetic material and configured to move the movable contact module to bring the movable contact into and out of contact with the fixed contact; an electromagnet configured to generate a magnetic field to move the armature; and characterised by a film (13, 24, 49) formed on a surface (43a, 43b) of: a contact of at least one of the fixed contact module and the movable contact module; and at least one of the fixed terminal and the movable spring; wherein the film (13, 24, 49) has a thermal conductivity higher than a thermal conductivity of the contact of the contact module on which the film is formed.
A deflector panel for being disposed at an axially upstream end of a combustor assembly of a gas turbine engine, comprising: an outer radial end; an inner radial end located radially inboard of the outer radial end relative to an engine central longitudinal axis; two circumferential ends (82a, 82b) extending between the outer radial end and the inner radial end, each circumferential end (82a, 82b) including a panel scallop at least partially defining a deflector opening capable of receiving a fuel nozzle of the combustor; and a plurality of studs extending from the deflector panel; characterized in that: the plurality of studs are disposed in the circumferential centermost 50% of the deflector panel. an outer radial end; an inner radial end located radially inboard of the outer radial end relative to an engine central longitudinal axis; two circumferential ends (82a, 82b) extending between the outer radial end and the inner radial end, each circumferential end (82a, 82b) including a panel scallop at least partially defining a deflector opening capable of receiving a fuel nozzle of the combustor; and a plurality of studs extending from the deflector panel; characterized in that: the plurality of studs are disposed in the circumferential centermost 50% of the deflector panel.
A nonwoven sheet for a filter, the nonwoven sheet comprising a substrate layer and a surface layer over at least one side of the substrate layer, wherein the substrate layer comprises a fiber aggregate nonwoven structural member, wherein the fiber aggregate nonwoven structural member consists of a thermal adhesive fiber, wherein the thermal adhesive fibers are melt-bonded to fix the fibers of the fiber aggregate nonwoven structural member, wherein the substrate layer has an average thickness of not less than 0.2 mm to less than 1 mm and an apparent density of 30 to 170 kg/m 3, and the thermal adhesive fibers arc substantially uniformly melt-bonded in a surface direction of the substrate layer, wherein the surface layer comprises a fiber aggregate nonwoven structural member having an apparent density higher than the apparent density of the substrate layer, wherein an apparent density ratio of the substrate layer relative to the surface layer (ratio of the substrate layer/the surface layer) is 1/1.5 to 1/10 and wherein in accordance with JIS L1913, the thickness of the fiber aggregate nonwoven structural member is measured, and the apparent density is calculated therefrom.
A gas turbine engine comprising a rotor and a stator which define first, second and third cavities (52, 54, 56); the rotor and stator define a seal therebetween and which is located for sealing between the second and third cavities (54, 56), the rotor comprises an annular drive arm and an aperture in the drive arm through which a radial direction gas flow passes from the first cavity, radially inward of the drive arm, to the second cavity, further gas passes through the seal from the second cavity to the third cavity to provide cooling thereto, the seal comprising a rotating part and a static part, the rotating part comprising an annular flow control feature that comprises an angled surface and extends axially over at least a portion of the aperture to deflect at least a part of the gas that enters the second cavity towards a seal plate of the rotor and away from the seal, characterised in that the surface is arcuate.
A plasticizer composition comprising: a cyclohexane-1,2-diester-based substance of the following Chemical Formula 1; and a citrate-based substance of the following Chemical Formula 2: wherein in Chemical Formula 1 and Chemical Formula 2: R 1 and R 2 each independently are a C8 to C10 alkyl group; and R 3 to R 5 each independently are a C5 to C10 alkyl group, wherein a weight ratio of the cyclohexane-1,2-diester-based substance of Chemical Formula 1 and the citrate-based substance of Chemical Formula 2 is 95:5 to 5:95, and wherein a plasticizer composition is excluded, which comprises: a cyclohexane-1,2-diester-based substance in which two alkyl groups bonded to a diester group each independently are a C4 to C12 alkyl group; an epoxidized alkyl ester composition comprising one or more compounds represented by the following Chemical Formula 1: in Chemical Formula 1, wherein R 1 is a C8 to C20 alkyl group comprising one or more epoxy groups, and R 2 is a C4 to C10 alkyl group; and a citrate-based substance represented by the following Chemical Formula 3: in Chemical Formula 3, wherein R 5 to R 7 each independently are a C4 to C10 alkyl group. a cyclohexane-1,2-diester-based substance of the following Chemical Formula 1; and a citrate-based substance of the following Chemical Formula 2: wherein in Chemical Formula 1 and Chemical Formula 2: R 1 and R 2 each independently are a C8 to C10 alkyl group; and R 3 to R 5 each independently are a C5 to C10 alkyl group, wherein a weight ratio of the cyclohexane-1,2-diester-based substance of Chemical Formula 1 and the citrate-based substance of Chemical Formula 2 is 95:5 to 5:95, and wherein a plasticizer composition is excluded, which comprises: a cyclohexane-1,2-diester-based substance in which two alkyl groups bonded to a diester group each independently are a C4 to C12 alkyl group; an epoxidized alkyl ester composition comprising one or more compounds represented by the following Chemical Formula 1: in Chemical Formula 1, wherein R 1 is a C8 to C20 alkyl group comprising one or more epoxy groups, and R 2 is a C4 to C10 alkyl group; and a citrate-based substance represented by the following Chemical Formula 3: in Chemical Formula 3, wherein R 5 to R 7 each independently are a C4 to C10 alkyl group. a cyclohexane-1,2-diester-based substance in which two alkyl groups bonded to a diester group each independently are a C4 to C12 alkyl group; an epoxidized alkyl ester composition comprising one or more compounds represented by the following Chemical Formula 1: in Chemical Formula 1, wherein R 1 is a C8 to C20 alkyl group comprising one or more epoxy groups, and R 2 is a C4 to C10 alkyl group; and a citrate-based substance represented by the following Chemical Formula 3: in Chemical Formula 3, wherein R 5 to R 7 each independently are a C4 to C10 alkyl group.
A method for close proximity vehicular data transmission, comprising: detecting, by a processor onboard a vehicle, a predetermined condition for activating a short range radio frequency transceiver (302, 330; 426) onboard the vehicle, wherein the onboard short range RF transceiver (302, 330; 426) is configured to transmit and receive signals within a limited distance from the onboard short range RF transceiver (302, 330; 426); activating, by the processor, the onboard short range RF transceiver (302, 330; 426) in response to at least detecting the predetermined condition; establishing a communications link between the onboard short range RF transceiver (302, 330; 426) and a predetermined mobile communications device (118; 306, 322; 414) assigned to a particular crew member; and transmitting vehicular data from the onboard short range RF transceiver (302, 330; 426) to the predetermined mobile communications device (118; 306, 322; 414); wherein the vehicle is an aircraft (304; 402); characterized in that activating the onboard short range RF transceiver (302, 330; 426) comprises activating the onboard short range RF transceiver (302, 330; 426) in response to detecting i) a weight on wheels condition of the aircraft (304; 402) and ii) a request to activate the onboard short range RF transceiver (302, 330; 426) being within an expected time frame based on at least one of a flight schedule of the aircraft (304; 402), a flight plan of the aircraft (304; 402) and aircraft operational activity recorded by an onboard information system (106; 404). detecting, by a processor onboard a vehicle, a predetermined condition for activating a short range radio frequency transceiver (302, 330; 426) onboard the vehicle, wherein the onboard short range RF transceiver (302, 330; 426) is configured to transmit and receive signals within a limited distance from the onboard short range RF transceiver (302, 330; 426); activating, by the processor, the onboard short range RF transceiver (302, 330; 426) in response to at least detecting the predetermined condition; establishing a communications link between the onboard short range RF transceiver (302, 330; 426) and a predetermined mobile communications device (118; 306, 322; 414) assigned to a particular crew member; and transmitting vehicular data from the onboard short range RF transceiver (302, 330; 426) to the predetermined mobile communications device (118; 306, 322; 414); wherein the vehicle is an aircraft (304; 402); characterized in that activating the onboard short range RF transceiver (302, 330; 426) comprises activating the onboard short range RF transceiver (302, 330; 426) in response to detecting i) a weight on wheels condition of the aircraft (304; 402) and ii) a request to activate the onboard short range RF transceiver (302, 330; 426) being within an expected time frame based on at least one of a flight schedule of the aircraft (304; 402), a flight plan of the aircraft (304; 402) and aircraft operational activity recorded by an onboard information system (106; 404).
A computerized system, comprising: a computer system (12, 14) having an input unit (20, 28), a display unit, one or more processors and one or more non-transitory computer readable medium, the one or more processors executing software to cause the one or more processors to: receive identification information of a structure; display, on the display unit, one or more images depicting the structure; receive a validation from the input unit indicating validation of a location of the structure depicted in the one or more images; generate unmanned aircraft information including flight path information configured to direct an unmanned aircraft to fly a flight path (70, 70a) around the structure and capture sensor data from a camera on the unmanned aircraft while the unmanned aircraft is flying the flight path; receive the sensor data from the unmanned aircraft; and generate a structure report based at least in part on the sensor data. receive identification information of a structure; display, on the display unit, one or more images depicting the structure; receive a validation from the input unit indicating validation of a location of the structure depicted in the one or more images; generate unmanned aircraft information including flight path information configured to direct an unmanned aircraft to fly a flight path (70, 70a) around the structure and capture sensor data from a camera on the unmanned aircraft while the unmanned aircraft is flying the flight path; receive the sensor data from the unmanned aircraft; and generate a structure report based at least in part on the sensor data.
A method for associating sessions, comprising: receiving (101, 407, 507, 708, 808, 1008, 1208),by a policy control and charging rules function, PCRF, an IP connectivity access network, IP-CAN, session establishment request that carries a local address of a user equipment; characterized by receiving (404, 504, 704, 804, 1004, 1204), by the PCRF, an S9* session establishment request that carries the local address of the user equipment; associating, (102, 408, 508, 709, 809, 1009, 1209) by the PCRF, an IP-CAN session and a S9* session according to the local address of the user equipment; wherein the local address is an IP address or an IP address prefix allocated by a non-3GPP access network to the user equipment. receiving (101, 407, 507, 708, 808, 1008, 1208),by a policy control and charging rules function, PCRF, an IP connectivity access network, IP-CAN, session establishment request that carries a local address of a user equipment; characterized by receiving (404, 504, 704, 804, 1004, 1204), by the PCRF, an S9* session establishment request that carries the local address of the user equipment; associating, (102, 408, 508, 709, 809, 1009, 1209) by the PCRF, an IP-CAN session and a S9* session according to the local address of the user equipment; wherein the local address is an IP address or an IP address prefix allocated by a non-3GPP access network to the user equipment.
A method comprising: receiving, at data processing hardware, a signal indication from an optical transceiver of an optical line terminal, the signal indication comprising: a loss-of-signal indication indicating non-receipt of an upstream optical signal from an optical network unit; or a signal-received indication indicating receipt of the upstream optical signal from the optical network unit; characterised in that the method further comprises: determining, by the data processing hardware, whether the signal indication comprises the loss-of-signal indication; and when the signal indication comprises the loss-of-signal indication, instructing, by the data processing hardware, enablement and disablement of the optical transceiver to transmit a downstream optical signal to the optical network unit at a threshold bit rate, resulting in a modulated downstream optical signal comprising encoded channel information. a loss-of-signal indication indicating non-receipt of an upstream optical signal from an optical network unit; or a signal-received indication indicating receipt of the upstream optical signal from the optical network unit; characterised in that the method further comprises: determining, by the data processing hardware, whether the signal indication comprises the loss-of-signal indication; and when the signal indication comprises the loss-of-signal indication, instructing, by the data processing hardware, enablement and disablement of the optical transceiver to transmit a downstream optical signal to the optical network unit at a threshold bit rate, resulting in a modulated downstream optical signal comprising encoded channel information. determining, by the data processing hardware, whether the signal indication comprises the loss-of-signal indication; and when the signal indication comprises the loss-of-signal indication, instructing, by the data processing hardware, enablement and disablement of the optical transceiver to transmit a downstream optical signal to the optical network unit at a threshold bit rate, resulting in a modulated downstream optical signal comprising encoded channel information.
A system of a cable and a bend limiting device attachable to this cable wherein said cable is connected to a connection point of a floating marine installation or vessel, said bend limiting device comprising at least one elongated sleeve member provided with: - an entrance end, which exhibits an entrance opening into said sleeve member for the cable connected to said connection point; - an exit end, opposite to the entrance end, which exit end exhibits an exit opening for the cable (101") out of said sleeve member; - an outer abutment surface disposed between the entrance end and the exit end, which abutment surface is adapted to be secured against a rigid surface of said marine installation or vessel; - an axially through-going hole between the entrance opening and the exit opening for accommodating a portion of the cable; and - at least one clamping device for securing said sleeve member in a fixed position around said accommodated portion of the cable, wherein - that the outer abutment surface is configured to allow it to be secured against said rigid surface by applying a pulling force on the cable and the sleeve member secured thereto in a direction from the abutment surface to said rigid surface of said marine installation or vessel, characterized in - that the outer abutment surface of the sleeve member is configured to be detached from said rigid surface and run out together with the cable when the application of pulling force on the cable ceases. - an entrance end, which exhibits an entrance opening into said sleeve member for the cable connected to said connection point; - an exit end, opposite to the entrance end, which exit end exhibits an exit opening for the cable (101") out of said sleeve member; - an outer abutment surface disposed between the entrance end and the exit end, which abutment surface is adapted to be secured against a rigid surface of said marine installation or vessel; - an axially through-going hole between the entrance opening and the exit opening for accommodating a portion of the cable; and - at least one clamping device for securing said sleeve member in a fixed position around said accommodated portion of the cable, wherein - that the outer abutment surface is configured to allow it to be secured against said rigid surface by applying a pulling force on the cable and the sleeve member secured thereto in a direction from the abutment surface to said rigid surface of said marine installation or vessel, characterized in - that the outer abutment surface of the sleeve member is configured to be detached from said rigid surface and run out together with the cable when the application of pulling force on the cable ceases.