mhurhangee/ep-ind-claims huggingface dataset:
A light-emitting instrument comprising: at least an emission source that emits light having a wavelength of 410 nm or longer and 470 nm or shorter and a phosphor or a light transmitting body in which a phosphor is dispersed wherein the phosphor includes an inorganic compound in which an AION crystal, an AION solid solution crystal, or an inorganic crystal having an identical crystal structure to that of the AION crystal includes at least Mn, an A element if necessary, where the A element is a monovalent metal element, a D element if necessary, where the D element is a divalent metal element, an E element, where the E element is F, and a G element if necessary, where the G element is one or two or more kinds of elements other than Mn, the A element, Al, O, N, the D element, and the E element, wherein the phosphor is represented by a composition formula: Mn a A b Al c O d N e D f E g G h, where a+b+c+d+e+f+g+h=1 in the formula, and the parameters: a, b, c, d, e, f, g, and h satisfy: 0.0003 ≤ a ≤ 0.09, 0 ≤ b ≤ 0.24, 0.25 ≤ c ≤0.41, 0.35 ≤ d ≤ 0.56, 0.02 ≤ e ≤ 0.13, 0 ≤ f ≤ 0.10, 0.001 ≤ g ≤ 0.17, and 0 ≤ h ≤ 0.10, and wherein the phosphor emits fluorescence having a peak at a wavelength in a range from 515 nm to 541 nm upon irradiation of the excitation source. 0.0003 ≤ a ≤ 0.09, 0 ≤ b ≤ 0.24, 0.25 ≤ c ≤0.41, 0.35 ≤ d ≤ 0.56, 0.02 ≤ e ≤ 0.13, 0 ≤ f ≤ 0.10, 0.001 ≤ g ≤ 0.17, and 0 ≤ h ≤ 0.10, and
A method for manufacturing a guide rail having a T-shaped cross-section, which includes a first leg and a second leg, a first end of the first leg adjoining a longitudinal side of the second leg, wherein the guide rail is roll-profiled from a flat metal strip such that a. the metal strip is bent through 180° in a turn-over region, the turn-over region forming a second end of the first leg positioned distal to the second leg, b. two doubling regions of the metal strip adjacent to the turn-over region are aligned in parallel by the bending through 180° in the turn-over region, the two doubling regions forming the first leg as a duplicate structure, and c. two regions of the metal strip adjacent to the doubling regions positioned distal to the turn-over region are bent away by 90° from the longitudinal orientation of the doubling regions in opposite directions, these regions being referred to as sublegs and forming the second leg, wherein the metal strip is bent in the turn-over region so that inner sides of the doubling regions are brought into direct surface contact, characterized in that the metal strip is thinned in the turn-over region by means of roll-profiling before or during the bending of the metal strip in the turn-over region, so that, when the metal strip is bent in the turn-over region, the doubling regions are aligned in parallel and brought into direct surface contact. a. the metal strip is bent through 180° in a turn-over region, the turn-over region forming a second end of the first leg positioned distal to the second leg, b. two doubling regions of the metal strip adjacent to the turn-over region are aligned in parallel by the bending through 180° in the turn-over region, the two doubling regions forming the first leg as a duplicate structure, and c. two regions of the metal strip adjacent to the doubling regions positioned distal to the turn-over region are bent away by 90° from the longitudinal orientation of the doubling regions in opposite directions, these regions being referred to as sublegs and forming the second leg, wherein the metal strip is bent in the turn-over region so that inner sides of the doubling regions are brought into direct surface contact, characterized in that the metal strip is thinned in the turn-over region by means of roll-profiling before or during the bending of the metal strip in the turn-over region, so that, when the metal strip is bent in the turn-over region, the doubling regions are aligned in parallel and brought into direct surface contact. wherein the metal strip is bent in the turn-over region so that inner sides of the doubling regions are brought into direct surface contact, characterized in that the metal strip is thinned in the turn-over region by means of roll-profiling before or during the bending of the metal strip in the turn-over region, so that, when the metal strip is bent in the turn-over region, the doubling regions are aligned in parallel and brought into direct surface contact.
A product or kit for use in the prevention and/or treatment of lung metastasis associated to osteosarcoma, the product or kit comprising: A) an IL-8 inhibitor, and B) at least one IL-6 inhibitor and/or at least one gp130 inhibitor, A) and B) being two separate formulations for simultaneous, separate or sequential use. A) an IL-8 inhibitor, and B) at least one IL-6 inhibitor and/or at least one gp130 inhibitor,
Surgical milling tool for removing bone or cartilaginous tissue, with a milling head (14, 50, 60) with a central holding element, wherein the central holding element has a through-opening which extends along the rotational axis of the milling head and in which a guide rod can be mounted rotatably in order to position the milling head, wherein a shank is connected with the central holding element by a bayonet connection, wherein the bayonet connection comprises a bayonet slot and a bayonet pin, wherein a transverse slot is provided in the bayonet slot, wherein the bayonet pin can be locked into the transverse slot during distal movement of the shank, wherein a viewing window is arranged between an outer edge and the central holding element of the milling head (14, 50, 60), characterised in that the central holding element has a guide slot for guiding the guide rod through into the through-opening, and in that the bayonet slot branches off the guide slot.
A method of diagnosing lung cancer in a patient comprising the step of: determining the level of an RNA molecule in a blood sample from a patient, wherein the RNA molecule comprises a nucleotide sequence according to SEQ ID NO: 1.
A composition comprising a continuous phase and a discontinuous phase incorporated therein, wherein the continuous phase comprises a first polymeric material and wherein the discontinuous phase comprises particles, said particles comprising a filler material and an encapsulating coating of a second polymeric material, wherein the backbones of the first and second polymeric materials are the same.
Front unit for a touring binding, comprising a base that is designed for fastening to a gliding board and defines a gliding board plane, and a front clamping means for clamping a front portion of a gliding board boot, which clamping means comprises a lefthand engagement element and a right-hand engagement element, which are clamped in each case on bearing portions (20l, 20r) such that they are movable between an engagement position for clamping a gliding board boot and a release position for releasing a gliding board boot, a portion of the engagement elements (181, 18r) that is remote from the bearing portions (20l, 20r) comprising coupling means (22l, 22r) that are designed for being coupled to front lefthand and right-hand counter-coupling means (24l, 24r) of a gliding board boot, and the coupling means (22l, 22r) defining a transverse axis that extends transversely to a gliding board longitudinal axis, about which transverse axis a gliding board boot clamped on the coupling means (22l, 22r) can be pivoted, the front clamping means being rotatably mounted on the base in order to allow, when the front clamping means is in an engagement position, rotation of the front clamping means and of the gliding board boot about a common vertical axis that extends substantially orthogonally to the gliding board plane, and the front unit further comprising a rotation-locking mechanism, which prevents rotation of the front clamping means about the vertical axis when the touring binding is in a touring position, characterised in that the front unit further comprises a disengaging assembly (84, 86) that converts a rotational movement of the front clamping means about the vertical axis relative to the base into an adjusting movement of the front clamping means from the engagement position into a release position, the rotational movement itself being converted into the opening movement of the clamping means, such that the opening process is directly associated with the rotational movement, the disengaging assembly (84, 86) comprising a cam mechanism.
A medical device comprising: an elongated inner tubular member including a proximal portion and a distal portion and defining an outer surface and a lumen; and an elongated tubular reinforcing member having an inner surface, the reinforcing member being disposed about the proximal portion of the inner tubular member such that the distal portion of the inner tubular member is free of the reinforcing member, and such that at least a portion of the outer surface of the inner tubular member along the proximal portion is spaced from the inner surface of the reinforcing member; characterized in that the spacing between the outer surface of the inner tubular member and the inner surface of the reinforcing member is unfilled by any other structure of the medical device. an elongated inner tubular member including a proximal portion and a distal portion and defining an outer surface and a lumen; and an elongated tubular reinforcing member having an inner surface, the reinforcing member being disposed about the proximal portion of the inner tubular member such that the distal portion of the inner tubular member is free of the reinforcing member, and such that at least a portion of the outer surface of the inner tubular member along the proximal portion is spaced from the inner surface of the reinforcing member; characterized in that the spacing between the outer surface of the inner tubular member and the inner surface of the reinforcing member is unfilled by any other structure of the medical device.
A method for propeller balancing of an aircraft, the method comprising: operating a propeller in-flight; receiving propeller vibration data during operation of the propeller in-flight; computing, after at least one flight of the aircraft, an average vibration magnitude and an average vibration phase angle based on the propeller vibration data; retrieving propeller configuration data from memory; retrieving, from memory, propeller calibration data comprising at least one influence coefficient indicative of an impact of at least one balancing weight on correcting an imbalance of the propeller; tuning the at least one influence coefficient according to one of the propeller configuration data and a flight condition of the aircraft; determining a propeller balancing solution by identifying, using at least one balance equation and based on the average vibration magnitude, the average vibration phase angle, and the at least one influence coefficient, a value for the at least one balancing weight and a placement location for the at least one balancing weight for correcting the imbalance of the propeller; and generating a balancing need indication by outputting the propeller balancing solution. operating a propeller in-flight; receiving propeller vibration data during operation of the propeller in-flight; computing, after at least one flight of the aircraft, an average vibration magnitude and an average vibration phase angle based on the propeller vibration data; retrieving propeller configuration data from memory; retrieving, from memory, propeller calibration data comprising at least one influence coefficient indicative of an impact of at least one balancing weight on correcting an imbalance of the propeller; tuning the at least one influence coefficient according to one of the propeller configuration data and a flight condition of the aircraft; determining a propeller balancing solution by identifying, using at least one balance equation and based on the average vibration magnitude, the average vibration phase angle, and the at least one influence coefficient, a value for the at least one balancing weight and a placement location for the at least one balancing weight for correcting the imbalance of the propeller; and generating a balancing need indication by outputting the propeller balancing solution.
A gas turbine engine defining axial, radial and circumferential directions and comprising: a duct defined by an axially extending radially inner wall and an axially extending radially outer wall, wherein: an annular array of turning vanes is provided in the duct, the array comprising a set of cambered aerodynamic vanes and a set of cambered strut-vanes, each having leading edges (225, 245) and trailing edges (226, 246); the leading edges of the strut-vanes are axially upstream of the trailing edges of the aerodynamic vanes; the trailing edges of the strut-vanes extend further axially downstream than the trailing edges of the aerodynamic vanes; a tangent (θ 3) to a mean camber line at the trailing edge of the strut-vanes is more closely aligned to the axial direction than is a tangent (θ 2) to a mean camber line at the trailing edge of the aerodynamic vanes; and the mean camber line of the strut-vanes is the same as the mean camber line of at least some of the aerodynamic vanes for axial locations between the leading and trailing edges of the aerodynamic vanes; characterised in that the mean camber line of the strut-vanes turns towards the axial direction by an angle in the range of from 5 degrees and 30 degrees between the axial position of the trailing edge of the aerodynamic vanes and the trailing edge of the strut-vanes. an annular array of turning vanes is provided in the duct, the array comprising a set of cambered aerodynamic vanes and a set of cambered strut-vanes, each having leading edges (225, 245) and trailing edges (226, 246); the leading edges of the strut-vanes are axially upstream of the trailing edges of the aerodynamic vanes; the trailing edges of the strut-vanes extend further axially downstream than the trailing edges of the aerodynamic vanes; a tangent (θ 3) to a mean camber line at the trailing edge of the strut-vanes is more closely aligned to the axial direction than is a tangent (θ 2) to a mean camber line at the trailing edge of the aerodynamic vanes; and the mean camber line of the strut-vanes is the same as the mean camber line of at least some of the aerodynamic vanes for axial locations between the leading and trailing edges of the aerodynamic vanes; characterised in that the mean camber line of the strut-vanes turns towards the axial direction by an angle in the range of from 5 degrees and 30 degrees between the axial position of the trailing edge of the aerodynamic vanes and the trailing edge of the strut-vanes.
A method comprising: receiving, at data processing hardware, audio data characterizing speech obtained by a user device; generating, by the data processing hardware, a plurality of audio feature vectors from the audio data using a trained self-supervised model, each audio feature vector being representative of audio features of a portion of the audio data, wherein the trained self-supervised model comprises a deep neural network; generating, by the data processing hardware, using a shallow discriminator model, a score indicating a presence of synthetic speech in the audio data based on the corresponding audio features of each audio feature vector of the plurality of audio feature vectors, wherein the shallow discriminator model is a shallow neural network; determining, by the data processing hardware, whether the score satisfies a synthetic speech detection threshold; and when the score satisfies the synthetic speech detection threshold, determining, by the data processing hardware, that the speech in the audio data obtained by the user device comprises synthetic speech; wherein the shallow discriminator model is trained on training samples, the training samples each including a synthetic speech portion and a human-originated speech portion. receiving, at data processing hardware, audio data characterizing speech obtained by a user device; generating, by the data processing hardware, a plurality of audio feature vectors from the audio data using a trained self-supervised model, each audio feature vector being representative of audio features of a portion of the audio data, wherein the trained self-supervised model comprises a deep neural network; generating, by the data processing hardware, using a shallow discriminator model, a score indicating a presence of synthetic speech in the audio data based on the corresponding audio features of each audio feature vector of the plurality of audio feature vectors, wherein the shallow discriminator model is a shallow neural network; determining, by the data processing hardware, whether the score satisfies a synthetic speech detection threshold; and when the score satisfies the synthetic speech detection threshold, determining, by the data processing hardware, that the speech in the audio data obtained by the user device comprises synthetic speech; wherein the shallow discriminator model is trained on training samples, the training samples each including a synthetic speech portion and a human-originated speech portion.
A method of incrementally forming a workpiece, the method comprising: securing a sacrificial material layer to at least one surface of the workpiece using securing means; imparting a force directly to the sacrificial material layer with at least one forming tool, thereby incrementally forming the workpiece to a desired geometry based on a tool path of the forming tool, while generating tool marks from the forming tool on the sacrificial material layer; and discarding or recycling the sacrificial material layer after the workpiece is formed, whereby the amount of tool marks on the workpiece is reduced. securing a sacrificial material layer to at least one surface of the workpiece using securing means; imparting a force directly to the sacrificial material layer with at least one forming tool, thereby incrementally forming the workpiece to a desired geometry based on a tool path of the forming tool, while generating tool marks from the forming tool on the sacrificial material layer; and discarding or recycling the sacrificial material layer after the workpiece is formed, whereby the amount of tool marks on the workpiece is reduced.
A method for a relaying user equipment, UE, in a wireless communication system, the method comprising: configuring, by the relaying UE, a call order or priority of multiple neighboring UEs, by communicating with at least one of the multiple neighboring UEs; transmitting, by the relaying UE, information informing that the relaying UE is connected to the at least one of multiple neighboring UEs to a network; reporting, by the relaying UE, the call order or priority of the multiple neighboring UEs and a list of the at least one of the multiple neighboring UEs which are connected to the relaying UE to the network; and establishing, by the relaying UE, a call between a selected neighboring UE and a caller UE, when the selected neighboring UE is selected by the caller UE, based on the call order or priority of the multiple neighboring UEs and the list of the at least one of the multiple neighboring UEs, wherein the relaying UE is a 3rd generation partnership project, 3GPP, long-term evolution, LTE, UE router, wherein the neighboring UEs are connected to the relaying UE or in proximity of the relaying UE via non-3GPP radio interface, and wherein the call order or priority includes or does not include the relaying UE. configuring, by the relaying UE, a call order or priority of multiple neighboring UEs, by communicating with at least one of the multiple neighboring UEs; transmitting, by the relaying UE, information informing that the relaying UE is connected to the at least one of multiple neighboring UEs to a network; reporting, by the relaying UE, the call order or priority of the multiple neighboring UEs and a list of the at least one of the multiple neighboring UEs which are connected to the relaying UE to the network; and establishing, by the relaying UE, a call between a selected neighboring UE and a caller UE, when the selected neighboring UE is selected by the caller UE, based on the call order or priority of the multiple neighboring UEs and the list of the at least one of the multiple neighboring UEs, wherein the relaying UE is a 3rd generation partnership project, 3GPP, long-term evolution, LTE, UE router, wherein the neighboring UEs are connected to the relaying UE or in proximity of the relaying UE via non-3GPP radio interface, and wherein the call order or priority includes or does not include the relaying UE.
Sensor device for monitoring a component of interest, including at least one sensor (22a, 22b) for measuring at least one parameter indicative of condition of said component of interest, signal processing means for processing the signals of the sensor (22a, 22b), and a mounting means for mounting the sensor device close to the component of interest, characterized in that the at least one sensor is formed as an acoustic emission sensor and/or as a vibration sensor, and the mounting means is a cast metal part made of a zinc alloy containing between 3.5% and 4.3% by weight aluminium and between 0.2 % and 3% by weight copper.
A cascaded dielectric barrier discharge device for accelerating an air flow for propelling a vehicle, comprising: a plasma propulsion nozzle having upstream and downstream ends; said propulsion nozzle having an inlet, an interior chamber and an outlet; a dielectric barrier layer along the entire inside periphery of the propulsion nozzle; a first annular electrode around the inside periphery of the upstream end of the propulsion nozzle and external to the dielectric barrier layer; a second annular electrode around the inside periphery of the propulsion nozzle, downstream of the first annular electrode, and internal to the dielectric barrier layer; and a plurality of planarly disbanded annular electrodes (24c - 24n) around the inside periphery of the propulsion nozzle, downstream of the first and second annular electrodes, the plurality of annular electrodes (24c - 24n) having sandwiched dielectric spacers and being cascaded to be concentrically expanding from the inlet through the interior chamber to the outlet of the propulsion nozzle. a plasma propulsion nozzle having upstream and downstream ends; said propulsion nozzle having an inlet, an interior chamber and an outlet; a dielectric barrier layer along the entire inside periphery of the propulsion nozzle; a first annular electrode around the inside periphery of the upstream end of the propulsion nozzle and external to the dielectric barrier layer; a second annular electrode around the inside periphery of the propulsion nozzle, downstream of the first annular electrode, and internal to the dielectric barrier layer; and a plurality of planarly disbanded annular electrodes (24c - 24n) around the inside periphery of the propulsion nozzle, downstream of the first and second annular electrodes, the plurality of annular electrodes (24c - 24n) having sandwiched dielectric spacers and being cascaded to be concentrically expanding from the inlet through the interior chamber to the outlet of the propulsion nozzle.
Stove, in particular a fireplace stove or tiled stove, fireplace insert or similar device for burning solid fuels such as logs, compressed wood products such as briquettes or pellets or mineral fuels such as coal or anthracite, with a stove body in which a combustion chamber (1.3) surrounded by side walls (1.2), a rear wall (1.4), a floor (1.5) and a combustion chamber door (1.1) is provided, and with an exhaust gas system connected to the combustion chamber (1.3), which can be positioned preferably at least in part inside an exhaust gas hood, wherein a catalyst module is assigned to the exhaust gas system, wherein the catalyst module has a number of catalyst elements (4.1), wherein the catalyst elements (4.1) are spaced apart from each other by at least 5 mm and at most 40 mm and between them have a through-flow chamber for exhaust gas, so that a through-flow gap is provided for exhaust gases, characterised in that the catalyst elements (4.1) are porous.