mhurhangee/ep-ind-claims huggingface dataset:
A power transfer unit for a vehicle, comprising: a first shaft configured to receive an input torque from a first vehicle component; a second shaft configured to selectively receive the torque from the first shaft and transmit the torque to a second vehicle component, the second shaft having a first end and a second end; an engaging mechanism configured to operate in a first mode and a second mode, when in the first mode the engaging mechanism selectively couples the second shaft to the first shaft, when in the second mode the second shaft is decoupled from the first shaft; a housing configured to enclose at least a portion of the power transfer unit; and a seal system (70, 170) having a first seal and a second seal, the first seal being disposed between the housing and the second end of the second shaft, the second seal being disposed between the housing and the first end of the second shaft, wherein a first fluid is retained in a volume enclosed by the first and second seals (70a, 70b); characterized in that a needle bearing is provided between the first shaft and the second shaft to permit efficient rotation of the first shaft relative to the second shaft when the second shaft is decoupled from the first shaft. a first shaft configured to receive an input torque from a first vehicle component; a second shaft configured to selectively receive the torque from the first shaft and transmit the torque to a second vehicle component, the second shaft having a first end and a second end; an engaging mechanism configured to operate in a first mode and a second mode, when in the first mode the engaging mechanism selectively couples the second shaft to the first shaft, when in the second mode the second shaft is decoupled from the first shaft; a housing configured to enclose at least a portion of the power transfer unit; and a seal system (70, 170) having a first seal and a second seal, the first seal being disposed between the housing and the second end of the second shaft, the second seal being disposed between the housing and the first end of the second shaft, wherein a first fluid is retained in a volume enclosed by the first and second seals (70a, 70b); characterized in that a needle bearing is provided between the first shaft and the second shaft to permit efficient rotation of the first shaft relative to the second shaft when the second shaft is decoupled from the first shaft.
Feeding trough receptacle comprising a main body having a base, at least one side wall and a rim on the side wall, and comprising an interior which is enclosed by an inner surface of the base and an inner surface of the at least one side wall, characterised in that, in the region of the rim on the side wall, a protrusion which protrudes inwardly into the interior relative to the adjacent inner surface of the side wall is formed on the side wall, which protrusion runs along the rim, - is formed by plastic deformation of a semi-finished sheet-metal part, in particular by beading, or - is formed as a round tube, in particular as a circular tube, and is welded centrally onto the adjacent side wall. - is formed by plastic deformation of a semi-finished sheet-metal part, in particular by beading, or - is formed as a round tube, in particular as a circular tube, and is welded centrally onto the adjacent side wall.
A solar module comprising a front glass and a rear glass, which are fixedly connected to one another by at least one intermediate layer, wherein a plurality of solar cells connected in series are arranged between the front glass and the rear glass, and a passive cooling structure with one or more heat sinks is arranged on a surface of the rear glass away from the plurality of solar cells, characterized in that: the passive cooling structure has a contact surface at which the passive cooling structure is in thermal contact with the rear glass for heat transfer, wherein the contact surface covers at least 90% of a photovoltaically active surface of the solar module; an area ratio of a surface of the passive cooling structure away from the rear glass and the contact surface is at least 3, preferably at least 5, and in particular preferably larger than 7; each of the one or more heat sinks is made of a material that has a ratio of thermal conductivity and density of at least 0.02 W•cm 2 /(g•K), preferably at least 0.05 W•cm 2 /(g•K); the passive cooling structure has a mass area density that is a mass of the passive cooling structure per contact area, and that is smaller than 0.6 g/cm 2, preferably smaller than 0.5 g/cm 2, and in particular preferably smaller than 0.4 g/cm 2; a resistance area product of the passive cooling structure that is a product of an electrical contact resistance and a contact area between the passive cooling structure and the rear glass is larger than 4×10 11 ohm•cm 2, preferably larger than 2×10 12 ohm•cm 2, and in particular preferably larger than 1×10 13 Ohm•cm 2. the passive cooling structure has a contact surface at which the passive cooling structure is in thermal contact with the rear glass for heat transfer, wherein the contact surface covers at least 90% of a photovoltaically active surface of the solar module; an area ratio of a surface of the passive cooling structure away from the rear glass and the contact surface is at least 3, preferably at least 5, and in particular preferably larger than 7; each of the one or more heat sinks is made of a material that has a ratio of thermal conductivity and density of at least 0.02 W•cm 2 /(g•K), preferably at least 0.05 W•cm 2 /(g•K); the passive cooling structure has a mass area density that is a mass of the passive cooling structure per contact area, and that is smaller than 0.6 g/cm 2, preferably smaller than 0.5 g/cm 2, and in particular preferably smaller than 0.4 g/cm 2; a resistance area product of the passive cooling structure that is a product of an electrical contact resistance and a contact area between the passive cooling structure and the rear glass is larger than 4×10 11 ohm•cm 2, preferably larger than 2×10 12 ohm•cm 2, and in particular preferably larger than 1×10 13 Ohm•cm 2.
A method of forming a coated article using combustion deposition, the method comprising: providing a glass substrate having at least one surface to be coated; introducing a single-source precursor to be combusted by a flame, the single-source precursor being alkaline earth metal and fluorine inclusive; combusting at least a portion of the precursor to form a combusted material, the combusted material comprising non-vaporized material; and providing the glass substrate in an area so that the glass substrate is heated sufficiently to allow the combusted material to form the coating, directly or indirectly, on the glass substrate, wherein the coating is a metal fluoride coating. providing a glass substrate having at least one surface to be coated; introducing a single-source precursor to be combusted by a flame, the single-source precursor being alkaline earth metal and fluorine inclusive; combusting at least a portion of the precursor to form a combusted material, the combusted material comprising non-vaporized material; and providing the glass substrate in an area so that the glass substrate is heated sufficiently to allow the combusted material to form the coating, directly or indirectly, on the glass substrate, wherein the coating is a metal fluoride coating.
A method of manufacturing a coil assembly for an electric rotating machine by interlacing a plurality of coil wires each having a plurality of turn portions formed therein, characterized by comprising: a placing step for placing a pair of first and second coil wires at predetermined positions with respect to each other; a first rotating step for rotating, while keeping engagement between a first turn portion of the first coil wire and a first turn portion of the second coil wire, at least one of the first and second coil wires to engage a second turn portion of the first coil wire with a second turn portion of the second coil wire; and a second rotating step for rotating, while keeping engagement between the second turn portion of the first coil wire and the second turn portion of the second coil wire, at least one of the first and second coil wires to engage a third turn portion of the first coil wire with a third turn portion of the second coil wire. a placing step for placing a pair of first and second coil wires at predetermined positions with respect to each other; a first rotating step for rotating, while keeping engagement between a first turn portion of the first coil wire and a first turn portion of the second coil wire, at least one of the first and second coil wires to engage a second turn portion of the first coil wire with a second turn portion of the second coil wire; and a second rotating step for rotating, while keeping engagement between the second turn portion of the first coil wire and the second turn portion of the second coil wire, at least one of the first and second coil wires to engage a third turn portion of the first coil wire with a third turn portion of the second coil wire.
A Geiger-mode detector device operable for detecting a low-level input signal, the device comprising: at least one semiconductor layer (20, 22) configured to provide an avalanche p-n or p-i-n junction; a first electrically conductive electrode and a second electrically conductive electrode operable to provide a voltage bias across said avalanche p-n or p-i-n junction; and a composite dielectric layer disposed between one of said first and second electrodes and the at least one semiconductor layer (20, 22); characterized in that: said semiconductor layer (20, 22) is a compound semiconductor layer; and the device is configured to be operable in a Geiger mode such that with said voltage bias biasing the avalanche p-n or p-i-n junction in or above the breakdown region said composite dielectric layer provides negative feedback for quenching the avalanche process predominantly through capacitive feedback. at least one semiconductor layer (20, 22) configured to provide an avalanche p-n or p-i-n junction; a first electrically conductive electrode and a second electrically conductive electrode operable to provide a voltage bias across said avalanche p-n or p-i-n junction; and a composite dielectric layer disposed between one of said first and second electrodes and the at least one semiconductor layer (20, 22); said semiconductor layer (20, 22) is a compound semiconductor layer; and the device is configured to be operable in a Geiger mode such that with said voltage bias biasing the avalanche p-n or p-i-n junction in or above the breakdown region said composite dielectric layer provides negative feedback for quenching the avalanche process predominantly through capacitive feedback.
A plant comprising: a fabric filter system comprising one or more fabric filter chambers with each fabric filter chamber comprising a plurality of fabric filter bags, an inlet equipped with one or more movable damper panels or an outlet equipped with one or more movable damper panels, and a control device operative to affect positioning of the one or more damper panels based at least in part on one or more fabric filter bag dust cake formation measurements the panel arranged at an inlet of each fabric filter chamber and/or at an outlet of each fabric filter chamber is adjustable to control gas velocity through the fabric filter chamber during a period of time from filter bag cleaning up until dust cake formation on surfaces of the filter bags within the fabric filter chamber.
An image processing apparatus comprising: control means configured to: write, to a first storage area (521 to 524) for transfer, images transferred from iris image pick-up means (401 to 404) for performing image pick-up of an iris of a moving subject; read out the images from the first storage area (521 to 524) at a frame interval corresponding to a movement speed of the moving subject; write the read out images to a second storage area for image processing; and execute processing using the images written to the second storage area. write, to a first storage area (521 to 524) for transfer, images transferred from iris image pick-up means (401 to 404) for performing image pick-up of an iris of a moving subject; read out the images from the first storage area (521 to 524) at a frame interval corresponding to a movement speed of the moving subject; write the read out images to a second storage area for image processing; and execute processing using the images written to the second storage area.
A method for controlling an uplink transmission power in a wireless communication system, the method comprising: Receiving (1115, 1210, 1510, 1600) information indicating a reference downlink carrier among a plurality of downlink carriers for measuring a pathloss; measuring the pathloss of the indicated reference downlink carrier; receiving a transmit power control, TPC, command; determining (1200, 1215) the uplink transmission power based on the TPC command and the measured pathloss; and transmitting data using the determined uplink transmission power. Receiving (1115, 1210, 1510, 1600) information indicating a reference downlink carrier among a plurality of downlink carriers for measuring a pathloss; measuring the pathloss of the indicated reference downlink carrier; receiving a transmit power control, TPC, command; determining (1200, 1215) the uplink transmission power based on the TPC command and the measured pathloss; and transmitting data using the determined uplink transmission power.
A fault current limiter, i.e. FCL, comprising: a ring-shaped core structure comprising: i) a first magnetisable ring-shaped core member; ii) a second magnetisable ring-shaped core member, spaced from the first core member: a plurality of permanent magnets arranged to cause at least part of the core members to become magnetically saturated in normal operation; an AC magnetomotive force source configured to generate a varying magnetic flux in at least a portion of the first and second magnetisable core members, wherein the AC magnetomotive force source is an AC coil and the AC coil is wound around the region of the magnetisable core where an overcoming of saturation is to be achieved; and; the plurality of permanent magnets being positioned to provide a magnetic circuit within at least part of the magnetisable core members, wherein the permanent magnets are positioned to bridge the gap between the first and second magnetisable ring-shaped core members, wherein the ring-shaped core structure comprises a polygonal shaped ring wherein permanent magnets are positioned at corners/vertices of the core structure and characterized in that the permanent magnets have a body which includes limbs extending in different directions following the shape of the adjacent core member, and wherein the body includes limbs (27, 28) extending at inclined angles corresponding to the angle between the connected sides of the polygonal shaped ring. a ring-shaped core structure comprising: i) a first magnetisable ring-shaped core member; ii) a second magnetisable ring-shaped core member, spaced from the first core member: a plurality of permanent magnets arranged to cause at least part of the core members to become magnetically saturated in normal operation; i) a first magnetisable ring-shaped core member; ii) a second magnetisable ring-shaped core member, spaced from the first core member: a plurality of permanent magnets arranged to cause at least part of the core members to become magnetically saturated in normal operation; an AC magnetomotive force source configured to generate a varying magnetic flux in at least a portion of the first and second magnetisable core members, wherein the AC magnetomotive force source is an AC coil and the AC coil is wound around the region of the magnetisable core where an overcoming of saturation is to be achieved; and; the plurality of permanent magnets being positioned to provide a magnetic circuit within at least part of the magnetisable core members, wherein the permanent magnets are positioned to bridge the gap between the first and second magnetisable ring-shaped core members, wherein the ring-shaped core structure comprises a polygonal shaped ring wherein permanent magnets are positioned at corners/vertices of the core structure and characterized in that the permanent magnets have a body which includes limbs extending in different directions following the shape of the adjacent core member, and wherein the body includes limbs (27, 28) extending at inclined angles corresponding to the angle between the connected sides of the polygonal shaped ring.
A heating chamber for an aerosol generation device, the heating chamber comprising: a tubular side wall having an open first end, the tubular side wall defining an interior volume of the heating chamber; and a metallic layer in direct contact with the heating chamber and covering a portion of an outer surface of the side wall; characterized by a heater located at least partially on the metallic layer. a tubular side wall having an open first end, the tubular side wall defining an interior volume of the heating chamber; and a metallic layer in direct contact with the heating chamber and covering a portion of an outer surface of the side wall; characterized by a heater located at least partially on the metallic layer.
Method of treating hair characterized in that it comprises a step of applying an anhydrous composition comprising one or more polymers according to the general structure wherein A is a C 2 to C 6 alkylene group and n represents an average number of 5 to 1000 and p represents an average number of 5 to 100 onto wet hair, and a step of blow-drying while brushing hair after application of the said composition..
An isolated, blocking, anti-PD-L1 full-length antibody comprising a heavy chain and a light chain variable region sequence, wherein: (a) the heavy chain comprises an HVR-H1, HVR-H2 and HVR-H3, wherein further: (i) the HVR-H1 sequence is GFTFSX 1 SWIH (SEQ ID NO:1); (ii) the HVR-H2 sequence is AWIX 2 PYGGSX 3 YYADSVKG (SEQ ID NO:2); (iii) the HVR-H3 sequence is RHWPGGFDY, and (SEQ ID NO:3); (b) the light chain comprises an HVR-L1, HVR-L2 and HVR-L3, wherein further: (iv) the HVR-L1 sequence is RASQX 4 X 5 X 6 TX 7 X 8 A (SEQ ID NO:8); (v) the HVR-L2 sequence is SASX 9 LX 10 S (SEQ ID NO:9); (vi) the HVR-L3 sequence is QQX 11 X 12 X 13 X 14 PX 15 T (SEQ ID NO:10); wherein X 1 = D, X 2 = S and X 3 = T, X 4 = D, X 5 = V, X 6 = S, X 7 = A and X 8 = V, X 9 = F and X 10 = Y, X 11 = Y, X 12 = L, X 13 = Y, X 14 = H and X 15 = A, and further comprising: (c) variable region heavy chain framework sequences juxtaposed between the HVRs according to the formula: (HC-FR1)-(HVR-H1)-(HC-FR2)-(HVR-H2)-(HC-FR3)-(HVR-H3)-(HC-FR4), and (d) variable region light chain framework sequences juxtaposed between the HVRs according to the formula: (LC-FR1)-(HVR-L1)-(LC-FR2)-(HVR-L2)-(LC-FR3)-(HVR-L3)-(LC-FR4), wherein the framework sequences of (c) and (d) are derived from human consensus framework sequences, wherein the consensus VH framework sequence is a Kabat subgroup III consensus framework sequence and the consensus VL framework sequence is a Kabat kappa I consensus framework sequence. (a) the heavy chain comprises an HVR-H1, HVR-H2 and HVR-H3, wherein further: (i) the HVR-H1 sequence is GFTFSX 1 SWIH (SEQ ID NO:1); (ii) the HVR-H2 sequence is AWIX 2 PYGGSX 3 YYADSVKG (SEQ ID NO:2); (iii) the HVR-H3 sequence is RHWPGGFDY, and (SEQ ID NO:3); (i) the HVR-H1 sequence is GFTFSX 1 SWIH (SEQ ID NO:1); (ii) the HVR-H2 sequence is AWIX 2 PYGGSX 3 YYADSVKG (SEQ ID NO:2); (iii) the HVR-H3 sequence is RHWPGGFDY, and (SEQ ID NO:3); (b) the light chain comprises an HVR-L1, HVR-L2 and HVR-L3, wherein further: (iv) the HVR-L1 sequence is RASQX 4 X 5 X 6 TX 7 X 8 A (SEQ ID NO:8); (v) the HVR-L2 sequence is SASX 9 LX 10 S (SEQ ID NO:9); (vi) the HVR-L3 sequence is QQX 11 X 12 X 13 X 14 PX 15 T (SEQ ID NO:10); wherein X 1 = D, X 2 = S and X 3 = T, X 4 = D, X 5 = V, X 6 = S, X 7 = A and X 8 = V, X 9 = F and X 10 = Y, X 11 = Y, X 12 = L, X 13 = Y, X 14 = H and X 15 = A, and further comprising: (iv) the HVR-L1 sequence is RASQX 4 X 5 X 6 TX 7 X 8 A (SEQ ID NO:8); (v) the HVR-L2 sequence is SASX 9 LX 10 S (SEQ ID NO:9); (vi) the HVR-L3 sequence is QQX 11 X 12 X 13 X 14 PX 15 T (SEQ ID NO:10); (c) variable region heavy chain framework sequences juxtaposed between the HVRs according to the formula: (HC-FR1)-(HVR-H1)-(HC-FR2)-(HVR-H2)-(HC-FR3)-(HVR-H3)-(HC-FR4), and (d) variable region light chain framework sequences juxtaposed between the HVRs according to the formula: (LC-FR1)-(HVR-L1)-(LC-FR2)-(HVR-L2)-(LC-FR3)-(HVR-L3)-(LC-FR4),
A composition, comprising: (a) 0.5 - 25 percent by weight an alkaline compound; (b) 1-25 percent by weight an alcohol amine compound; (c) 0.1 - 20 percent by weight a hydroxylammonium compound; (d) 5-95 percent by weight an organic solvent; (e) 0.1 - 5 percent by weight a corrosion inhibitor compound, wherein the corrosion inhibitor compound is triazole, benzotriazole, substituted triazole, or substituted benzotriazole; and (f) 2 -25 percent by weight water; wherein the composition is free of a urea and urea derivatives and has a pH of at least 12.4. (a) 0.5 - 25 percent by weight an alkaline compound; (b) 1-25 percent by weight an alcohol amine compound; (c) 0.1 - 20 percent by weight a hydroxylammonium compound; (d) 5-95 percent by weight an organic solvent; (e) 0.1 - 5 percent by weight a corrosion inhibitor compound, wherein the corrosion inhibitor compound is triazole, benzotriazole, substituted triazole, or substituted benzotriazole; and (f) 2 -25 percent by weight water; wherein the composition is free of a urea and urea derivatives and has a pH of at least 12.4.
A wear indicator operable to be secured to a surface of a gas turbine engine, the wear indicator comprising: a first side which delaminates when impacted by a blade of the gas turbine engine; a second side parallel to the first side, the second side operable to be secured to the surface of the gas turbine engine; a mid-section interposed between the first side and the second side, wherein the midsection includes one outer surface between the first side and the second side; characterized in that the wear indicator further comprises: an orifice initiating at the first side and extending through the midsection to the second side; and at least three reference dimensions (ID1, OD3, α) that remain constant when the first side delaminates, wherein the at least three reference dimensions include a diameter of the orifice, an outer diameter of the second side, and an angle (α) between the second side and the outer surface of the midsection. a first side which delaminates when impacted by a blade of the gas turbine engine; a second side parallel to the first side, the second side operable to be secured to the surface of the gas turbine engine; a mid-section interposed between the first side and the second side, wherein the midsection includes one outer surface between the first side and the second side; characterized in that the wear indicator further comprises: an orifice initiating at the first side and extending through the midsection to the second side; and at least three reference dimensions (ID1, OD3, α) that remain constant when the first side delaminates, wherein the at least three reference dimensions include a diameter of the orifice, an outer diameter of the second side, and an angle (α) between the second side and the outer surface of the midsection. an orifice initiating at the first side and extending through the midsection to the second side; and at least three reference dimensions (ID1, OD3, α) that remain constant when the first side delaminates, wherein the at least three reference dimensions include a diameter of the orifice, an outer diameter of the second side, and an angle (α) between the second side and the outer surface of the midsection.