mhurhangee/ep-ind-claims huggingface dataset:
A compartmentalized header tank for liquid coolant, the header tank having an intended upright position, when in use, characterized by comprising - a container having an upper portion and a lower portion on an inside thereof, wherein the upper portion being laterally divided into fluid impermeable partitions by at least one downwardly extending divider element, said partitions being open towards the lower portion, and wherein the lower portion being defined by the inside of the container below the at least one divider element; - at least two tank gas outlets, each tank gas outlet being positioned in a respective partition of the container's upper portion; - at least two tank coolant inlets, each tank coolant inlet corresponding to a tank gas outlet, and being positioned below thereof in the respective partition of the corresponding tank gas outlet, and - a tank coolant outlet positioned in a lower portion of the container. - a container having an upper portion and a lower portion on an inside thereof, wherein the upper portion being laterally divided into fluid impermeable partitions by at least one downwardly extending divider element, said partitions being open towards the lower portion, and wherein the lower portion being defined by the inside of the container below the at least one divider element; - at least two tank gas outlets, each tank gas outlet being positioned in a respective partition of the container's upper portion; - at least two tank coolant inlets, each tank coolant inlet corresponding to a tank gas outlet, and being positioned below thereof in the respective partition of the corresponding tank gas outlet, and - a tank coolant outlet positioned in a lower portion of the container.
An anti-counterfeiting closure, attachable to an opening on a container, comprising: a cap rotatably attachable to the opening; a disc fitted on an underside facing of the cap so as to retain the disc between the cap and the container when a closing torque is applied to attach the closure to the opening, wherein at least one anti-rotation rib is formed on the inner facing of the cap to engage the disc; and a wireless communication tag; wherein at least one anti-back-off rib is formed on the disc characterized in that when an opening torque is applied to release the closure from the container, the at least one anti-back-off rib engages the container to cause the cap to rotate in comparison to the disc; wherein the cap includes a central section; wherein the at least one anti-back-off rib is formed on said central section; wherein at least one tab bridge initially attaches the central section to a periphery portion of the cap and wherein the at least one tab bridge becomes disconnected upon engagement of the at least one anti-back off rib; and wherein the wireless communication tag is incorporated along a said tab bridge. a cap rotatably attachable to the opening; a disc fitted on an underside facing of the cap so as to retain the disc between the cap and the container when a closing torque is applied to attach the closure to the opening, wherein at least one anti-rotation rib is formed on the inner facing of the cap to engage the disc; and a wireless communication tag; wherein at least one anti-back-off rib is formed on the disc characterized in that when an opening torque is applied to release the closure from the container, the at least one anti-back-off rib engages the container to cause the cap to rotate in comparison to the disc; wherein the cap includes a central section; wherein the at least one anti-back-off rib is formed on said central section; wherein at least one tab bridge initially attaches the central section to a periphery portion of the cap and wherein the at least one tab bridge becomes disconnected upon engagement of the at least one anti-back off rib; and wherein the wireless communication tag is incorporated along a said tab bridge.
A wet-chemical method of producing a black silicon substrate, the method comprising: soaking a crystalline silicon wafer in a volume of a diluted inorganic compound catalytic solution and an etchant solution, wherein the diluted inorganic compound catalytic solution comprises chlorauric acid, and wherein the etchant solution comprises an acetonitrile and acetic acid solution combined with a hydrofluoric acid and hydrogen peroxide etching solution, the acetonitrile and acetic acid solution, the hydrofluoric acid and the hydrogen peroxide being in a 1:1:1 volume ratio.
A fastener-driving tool comprising: a housing; a workpiece-contacting element movably connected to said housing, said workpiece-contacting element being movable between a rest position and an activated position; a trigger movably connected to said housing, said trigger being movable between a rest position and an activated position; a control valve including an actuating pin; an actuation lever movably connected to said trigger, said actuation lever being movable between a rest position and an actuating position adjacent to said actuating pin; and a trigger control mechanism associated with said actuation lever and configured for moving and holding said actuation lever in said actuating position, characterized in that in a powered mode, said trigger control mechanism causes said-actuation lever to move and remain in said actuating position such that the tool is actuated each time said workpiece-contacting element contacts a workpiece and moves to said activated position causing said actuation lever to contact said actuating pin and initiate an actuation of the tool; and wherein in a non-powered mode, said actuation lever does not move to said actuating position such that the tool is actuated each time said workpiece-contacting element and said trigger are each respectively moved from said rest position to said activated position in a designated sequence. a housing; a workpiece-contacting element movably connected to said housing, said workpiece-contacting element being movable between a rest position and an activated position; a trigger movably connected to said housing, said trigger being movable between a rest position and an activated position; a control valve including an actuating pin; an actuation lever movably connected to said trigger, said actuation lever being movable between a rest position and an actuating position adjacent to said actuating pin; and a trigger control mechanism associated with said actuation lever and configured for moving and holding said actuation lever in said actuating position, characterized in that in a powered mode, said trigger control mechanism causes said-actuation lever to move and remain in said actuating position such that the tool is actuated each time said workpiece-contacting element contacts a workpiece and moves to said activated position causing said actuation lever to contact said actuating pin and initiate an actuation of the tool; and wherein in a non-powered mode, said actuation lever does not move to said actuating position such that the tool is actuated each time said workpiece-contacting element and said trigger are each respectively moved from said rest position to said activated position in a designated sequence.
Aircraft wing with a spoiler and an actuator powered mechanism, the spoiler being movable from a reference position with a deflection angle α ref to a given target deflection angle α target by the actuator powered mechanism, wherein the spoiler is interconnected with the aircraft wing exclusively via a strip element and via the actuator powered mechanism, wherein an upstream edge of the spoiler is being interconnected with the aircraft wing exclusively via the strip element made of a resilient flexible material, wherein a downstream edge of the strip element is extending along the whole upstream edge of the spoiler or at least along a major part of the upstream edge of the spoiler and wherein a whole upstream edge of the strip element is connected to an upper surface of the aircraft wing, characterized in that - the actuator powered mechanism is constructed and arranged such that when moving the spoiler from the reference angle α ref to the given target deflection angle α target, the strip element is being bent with a constant strain along the strip element, wherein a cross-section of the strip element for all deflection angles α adopts the form of a ring segment with a radius R(α). - the actuator powered mechanism is constructed and arranged such that when moving the spoiler from the reference angle α ref to the given target deflection angle α target, the strip element is being bent with a constant strain along the strip element, wherein a cross-section of the strip element for all deflection angles α adopts the form of a ring segment with a radius R(α).
A vane arc segment (62;162;262;362) comprising: radially inner and outer platforms (64/66); and an airfoil mechanically clamped between the platforms (64/66), the airfoil having an airfoil section that extends radially between radially inner and outer fairing platforms (74/76;174/176;274/.276;374/376), at least one of the fairing platforms (74/76;174/176;274/276;374/376) including forward and aft sides (82a/82b), circumferential sides (84a/84b), and a gas path side and an opposed radial side, and that the radial side includes a plurality of protrusions that have faces that are oriented substantially normal to, respectively, radial, tangential, and axial load transmission directions of the airfoil such that the faces, respectively, bear radial, tangential, and axial load transmissions of the airfoil, wherein the plurality of protrusions includes first and second rails (90a/90b) that extend circumferentially along the forward and aft sides (82a/82b); characterised in that the plurality of protrusions include a tab that extends axially from the first rail. radially inner and outer platforms (64/66); and an airfoil mechanically clamped between the platforms (64/66), the airfoil having an airfoil section that extends radially between radially inner and outer fairing platforms (74/76;174/176;274/.276;374/376), at least one of the fairing platforms (74/76;174/176;274/276;374/376) including forward and aft sides (82a/82b), circumferential sides (84a/84b), and a gas path side and an opposed radial side, and that the radial side includes a plurality of protrusions that have faces that are oriented substantially normal to, respectively, radial, tangential, and axial load transmission directions of the airfoil such that the faces, respectively, bear radial, tangential, and axial load transmissions of the airfoil, wherein the plurality of protrusions includes first and second rails (90a/90b) that extend circumferentially along the forward and aft sides (82a/82b); characterised in that the plurality of protrusions include a tab that extends axially from the first rail.
An electronic device, comprising: Circuitry configured to detect a size of a face from a captured image; obtain a distortion correction parameter curve based on the size of the face; and correct a distortion of the face within the captured image by utilizing the distortion correction parameter curve based on the size of the face, wherein distortion correction is performed by a warping component whereby the warping component is based on the obtained distortion correction parameter curve, and wherein the warping component strengthens a warping effect when the size of the face increases from a first smaller size to a second larger size, and the warping component weakens the warping effect when the size of the face increases from the second larger size to a third larger size. Circuitry configured to detect a size of a face from a captured image; obtain a distortion correction parameter curve based on the size of the face; and correct a distortion of the face within the captured image by utilizing the distortion correction parameter curve based on the size of the face, wherein distortion correction is performed by a warping component whereby the warping component is based on the obtained distortion correction parameter curve, and wherein the warping component strengthens a warping effect when the size of the face increases from a first smaller size to a second larger size, and the warping component weakens the warping effect when the size of the face increases from the second larger size to a third larger size. detect a size of a face from a captured image; obtain a distortion correction parameter curve based on the size of the face; and correct a distortion of the face within the captured image by utilizing the distortion correction parameter curve based on the size of the face, wherein distortion correction is performed by a warping component whereby the warping component is based on the obtained distortion correction parameter curve, and wherein the warping component strengthens a warping effect when the size of the face increases from a first smaller size to a second larger size, and the warping component weakens the warping effect when the size of the face increases from the second larger size to a third larger size.
A method of reworking a component, comprising: removing a casting defect from a component manufactured of a non-fusion weldable base alloy to form a cavity; and being characterised by the following steps: at least partially filling the cavity with a multiple of layers of a multiple of laser powder deposition spots, each of the multiple of laser powder deposition spots formed of a filler alloy, wherein the filler alloy is a fusion weldable powder material, wherein each laser powder deposition spot overlays the adjacent laser powder deposition spot by 50%, as the multiple of laser powder deposition spots in each layer form a matrix of overlapping laser powder deposition spots, wherein the cavity has inclined walls, and the outermost laser powder deposition spots are located at least partially on the wall of the cavity, as the inclined angle of the wall permits each layer to at least partially overlap the wall as well as permit the laser from the laser powder deposition system direct access into the cavity. removing a casting defect from a component manufactured of a non-fusion weldable base alloy to form a cavity; and being characterised by the following steps: at least partially filling the cavity with a multiple of layers of a multiple of laser powder deposition spots, each of the multiple of laser powder deposition spots formed of a filler alloy, wherein the filler alloy is a fusion weldable powder material, wherein each laser powder deposition spot overlays the adjacent laser powder deposition spot by 50%, as the multiple of laser powder deposition spots in each layer form a matrix of overlapping laser powder deposition spots, wherein the cavity has inclined walls, and the outermost laser powder deposition spots are located at least partially on the wall of the cavity, as the inclined angle of the wall permits each layer to at least partially overlap the wall as well as permit the laser from the laser powder deposition system direct access into the cavity. at least partially filling the cavity with a multiple of layers of a multiple of laser powder deposition spots, each of the multiple of laser powder deposition spots formed of a filler alloy, wherein the filler alloy is a fusion weldable powder material, wherein each laser powder deposition spot overlays the adjacent laser powder deposition spot by 50%, as the multiple of laser powder deposition spots in each layer form a matrix of overlapping laser powder deposition spots, wherein the cavity has inclined walls, and the outermost laser powder deposition spots are located at least partially on the wall of the cavity, as the inclined angle of the wall permits each layer to at least partially overlap the wall as well as permit the laser from the laser powder deposition system direct access into the cavity.
A carboxyl group-containing polymer composition comprising: a carboxyl group-containing polymer that is a copolymer of monomers containing an α,β-unsaturated carboxylic acid (a-1) and a compound (a-2) having at least two ethylenically unsaturated groups in its molecule; and a nonionic surfactant having an HLB value of 5 to 8, wherein the carboxyl group-containing polymer composition is produced by a method comprising a step of copolymerizing the monomers, wherein the nonionic surfactant is added into a system when a polymerization degree of the α,β-unsaturated carboxylic acid (a-1) reaches 5% or more to less than 70% in the step, and wherein an alcohol gel A prepared by the following preparation method has a viscosity of 5,000 mPa s or more at 25°C, as measure by the method described in the description, the alcohol gel A has a light transmittance of 95% or more at a wavelength of 425 nm, as measure by the method described in the description, and the preparation method of the alcohol gel A includes homogeneously mixing 0.75 parts by mass of the carboxyl group-containing polymer composition, 51.70 parts by mass of ion exchange water, and 96.0 parts by mass of ethanol with each other, and then adding an ethanol solution of triethanolamine having a concentration of 50% by mass to the resulting mixture until a pH of the mixture reaches 7.0, followed by stirring until the mixture becomes homogeneous to prepare the alcohol gel A. a carboxyl group-containing polymer that is a copolymer of monomers containing an α,β-unsaturated carboxylic acid (a-1) and a compound (a-2) having at least two ethylenically unsaturated groups in its molecule; and a nonionic surfactant having an HLB value of 5 to 8, wherein the carboxyl group-containing polymer composition is produced by a method comprising a step of copolymerizing the monomers, wherein the nonionic surfactant is added into a system when a polymerization degree of the α,β-unsaturated carboxylic acid (a-1) reaches 5% or more to less than 70% in the step, and wherein an alcohol gel A prepared by the following preparation method has a viscosity of 5,000 mPa s or more at 25°C, as measure by the method described in the description, the alcohol gel A has a light transmittance of 95% or more at a wavelength of 425 nm, as measure by the method described in the description, and the preparation method of the alcohol gel A includes homogeneously mixing 0.75 parts by mass of the carboxyl group-containing polymer composition, 51.70 parts by mass of ion exchange water, and 96.0 parts by mass of ethanol with each other, and then adding an ethanol solution of triethanolamine having a concentration of 50% by mass to the resulting mixture until a pH of the mixture reaches 7.0, followed by stirring until the mixture becomes homogeneous to prepare the alcohol gel A.
A method for an object sensing system comprising: designating a plurality of transmitter and receiver channels for a transmitter antenna array and a receiver antenna array of the object sensing system, wherein a transmitter channel is using one or a combination of antenna elements of the transmitter antenna array and a receiver channel is using one or a combination of antenna elements of the receiver antenna array; scanning the transmitter antenna array and the receiver antenna array through the designated channels to measure channel responses corresponding to each one of the designated channels; forming a measurement matrix comprising entries corresponding to each measured channel response, wherein the designating the plurality of transmitter and receiver channels comprises: forming a transmitter amplitude weight vector, AWV, matrix comprising one or more transmitter AWVs corresponding to each transmitter channel in the plurality of transmitter and receiver channels, and forming a receiver AWV matrix comprising one or more receiver AWVs corresponding to each receiver channel in the plurality of transmitter and receiver channels; deriving a channel matrix from the measurement matrix, the transmitter AWV matrix, and the receiver AWV matrix; and determining a directional vector to or from an object by performing singular value decomposition on the channel matrix to determine at least a largest singular value corresponding to the directional vector to or from the object. designating a plurality of transmitter and receiver channels for a transmitter antenna array and a receiver antenna array of the object sensing system, wherein a transmitter channel is using one or a combination of antenna elements of the transmitter antenna array and a receiver channel is using one or a combination of antenna elements of the receiver antenna array; scanning the transmitter antenna array and the receiver antenna array through the designated channels to measure channel responses corresponding to each one of the designated channels; forming a measurement matrix comprising entries corresponding to each measured channel response, wherein the designating the plurality of transmitter and receiver channels comprises: forming a transmitter amplitude weight vector, AWV, matrix comprising one or more transmitter AWVs corresponding to each transmitter channel in the plurality of transmitter and receiver channels, and forming a receiver AWV matrix comprising one or more receiver AWVs corresponding to each receiver channel in the plurality of transmitter and receiver channels; deriving a channel matrix from the measurement matrix, the transmitter AWV matrix, and the receiver AWV matrix; and determining a directional vector to or from an object by performing singular value decomposition on the channel matrix to determine at least a largest singular value corresponding to the directional vector to or from the object.
A data transfer method, comprising: receiving, by a virtual switch (120, 700), a first data packet; determining, by the virtual switch (120, 700), whether the first data packet is based on an Internet Protocol, IP; extracting, by the virtual switch (120, 700), characteristic information of the first data packet if the first data packet is based on the IP; determining, based on the extracted characteristic information of the first data packet, whether an expedited forwarding rule is configured for a data stream to which the first data packet belongs, wherein the expedited forwarding rule indicates that a second data packet in the data stream to which the first data packet belongs has been verified by a security verification module and a verification result is secure; and if the expedited forwarding rule is configured for the data stream to which the first data packet belongs, bypassing, by the virtual switch (120, 700), the security verification module to send the first data packet to a receive end, wherein if the virtual switch determines that the first data packet is not based on the IP, the method further comprises: forwarding, by the virtual switch (120, 700), the first data packet to the security verification module. receiving, by a virtual switch (120, 700), a first data packet; determining, by the virtual switch (120, 700), whether the first data packet is based on an Internet Protocol, IP; extracting, by the virtual switch (120, 700), characteristic information of the first data packet if the first data packet is based on the IP; determining, based on the extracted characteristic information of the first data packet, whether an expedited forwarding rule is configured for a data stream to which the first data packet belongs, wherein the expedited forwarding rule indicates that a second data packet in the data stream to which the first data packet belongs has been verified by a security verification module and a verification result is secure; and if the expedited forwarding rule is configured for the data stream to which the first data packet belongs, bypassing, by the virtual switch (120, 700), the security verification module to send the first data packet to a receive end, wherein if the virtual switch determines that the first data packet is not based on the IP, the method further comprises: forwarding, by the virtual switch (120, 700), the first data packet to the security verification module.