mhurhangee/ep-ind-claims huggingface dataset:
A clock recovery apparatus to recover an encoder clock for received packets, said apparatus being adapted for use in a communications system and comprising: a packet receiver configured to detect information that is representative of the encoder clock for the received packets; a voltage controlled oscillator for generating a local system time clock, the voltage controlled oscillator having an input that allows the frequency of the system time clock to be adjusted in proportion to a control signal received on the input; a feedback loop comprising a jitter calculator for generating an error signal that represents the difference between the frequency of the local system time clock and the frequency of the representative encoder clock; and a low-pass filter circuit adapted to filter the error signal to produce a control signal for feeding back to the voltage controlled oscillator, characterized in that the information representative of the encoder clock comprises packet count information and transport rate information retrieved from a header portion of one or more of the received packets. a packet receiver configured to detect information that is representative of the encoder clock for the received packets; a voltage controlled oscillator for generating a local system time clock, the voltage controlled oscillator having an input that allows the frequency of the system time clock to be adjusted in proportion to a control signal received on the input; a feedback loop comprising a jitter calculator for generating an error signal that represents the difference between the frequency of the local system time clock and the frequency of the representative encoder clock; and a low-pass filter circuit adapted to filter the error signal to produce a control signal for feeding back to the voltage controlled oscillator, characterized in that the information representative of the encoder clock comprises packet count information and transport rate information retrieved from a header portion of one or more of the received packets.
A method for manufacturing a three-dimensional object, the method comprising: providing an ink composition, wherein the ink composition includes a carrier vehicle, tungsten carbide particles, at least one dispersing agent, at least one binder, and cobalt particles, wherein the carrier vehicle includes at least one glycol ether; and wherein the cobalt particles are cobalt and/or organo cobalt compound; dispensing the ink composition from a print head to form a three-dimensional object using an additive process in which successive layers of the ink composition are laid down, wherein each layer from the ink composition is dispensed onto a previously dispensed solid layer from the ink composition; and heat treating the dispensed ink composition by: heating the dispensed ink composition up to a first temperature sufficient to evaporate, or disintegrate and evaporate, all organic material in the dispensed ink composition; and further heating the heated dispensed ink composition up to a second temperature sufficient to melt the cobalt particles and sinter the tungsten carbide particles. providing an ink composition, wherein the ink composition includes a carrier vehicle, tungsten carbide particles, at least one dispersing agent, at least one binder, and cobalt particles, wherein the carrier vehicle includes at least one glycol ether; and wherein the cobalt particles are cobalt and/or organo cobalt compound; dispensing the ink composition from a print head to form a three-dimensional object using an additive process in which successive layers of the ink composition are laid down, wherein each layer from the ink composition is dispensed onto a previously dispensed solid layer from the ink composition; and heat treating the dispensed ink composition by: heating the dispensed ink composition up to a first temperature sufficient to evaporate, or disintegrate and evaporate, all organic material in the dispensed ink composition; and further heating the heated dispensed ink composition up to a second temperature sufficient to melt the cobalt particles and sinter the tungsten carbide particles. heating the dispensed ink composition up to a first temperature sufficient to evaporate, or disintegrate and evaporate, all organic material in the dispensed ink composition; and further heating the heated dispensed ink composition up to a second temperature sufficient to melt the cobalt particles and sinter the tungsten carbide particles.
A fuel injection valve (11a, 11b) that has a plurality of injection holes (a1-a6; b1-b6; c1-c6) and is adapted to inject fuel into a cylinder of an internal combustion engine, the cylinder having a ring-shaped space including an area of strong tumble flow (A2, A6; B2, B6; C6, C4, C3, C1) formed in the cylinder and a space including an area of weak tumble flow (A1, A3-A5; B1, B3-B5; C2, C5) formed in the cylinder, characterized by: a first group of injection holes (a2, a6; b2, b6; c6, c4, c3, c1) for injecting fuel toward the ring-shaped space including the area of strong tumble flow (A2, A6; B2, B6; C6, C4, C3, C1); and a second group of injection holes (a1, a3-a5; b1, b3-b5; c2, c5) for injecting fuel toward the space including the area of weak tumble flow (A1, A3-A5; B1, B3-B5; C2, C5), wherein a fuel spray with the smallest penetration force from the first group of injection holes (a2, a6; b2, b6; c6, c4, c3, c1) has a penetration force larger than a fuel spray with the largest penetration force from the second group of injection holes, wherein a plurality of the ring-shaped spaces are formed, and the second group of injection holes (a1, a3-a5; b1, b3-b5; c2, c5) inject fuel toward the space of weak tumble flow formed between the plurality of spaces. a first group of injection holes (a2, a6; b2, b6; c6, c4, c3, c1) for injecting fuel toward the ring-shaped space including the area of strong tumble flow (A2, A6; B2, B6; C6, C4, C3, C1); and a second group of injection holes (a1, a3-a5; b1, b3-b5; c2, c5) for injecting fuel toward the space including the area of weak tumble flow (A1, A3-A5; B1, B3-B5; C2, C5), wherein a fuel spray with the smallest penetration force from the first group of injection holes (a2, a6; b2, b6; c6, c4, c3, c1) has a penetration force larger than a fuel spray with the largest penetration force from the second group of injection holes, wherein a plurality of the ring-shaped spaces are formed, and the second group of injection holes (a1, a3-a5; b1, b3-b5; c2, c5) inject fuel toward the space of weak tumble flow formed between the plurality of spaces.
A hydraulic percussion apparatus, comprising: - a guide body including a bore and an annular housing arranged on the guide body and opening into the bore, - a striking piston slidably mounted inside the bore and arranged to be alternately driven by an incompressible fluid, and - a sealing device mounted in the annular housing arranged on the guide body to achieve sealing between the guide body and the striking piston, the sealing device comprising at least: - one inner sealing ring comprising an inner sealing portion, the inner sealing portion being annular and including a sealing lip intended to sealingly cooperate with the outer surface of the striking piston, - one outer sealing element distinct from the inner sealing ring and mounted around the inner sealing portion, the outer sealing element being annular and intended to sealingly bear at the bottom of the annular housing, characterized in that the inner sealing ring includes: - an annular protective portion axially shifted relative to the inner sealing portion, the protective portion being internally delimited by at least one converging protective surface, the converging protective surface being annular and converging towards the sealing lip, and - an annular groove opening into the inside of the inner sealing ring, the annular groove being disposed between the sealing lip and the converging protective surface, and in that the protective portion is arranged to delimit, in use, an annular flowing passageway with the striking piston. - a guide body including a bore and an annular housing arranged on the guide body and opening into the bore, - a striking piston slidably mounted inside the bore and arranged to be alternately driven by an incompressible fluid, and - a sealing device mounted in the annular housing arranged on the guide body to achieve sealing between the guide body and the striking piston, the sealing device comprising at least: - one inner sealing ring comprising an inner sealing portion, the inner sealing portion being annular and including a sealing lip intended to sealingly cooperate with the outer surface of the striking piston, - one outer sealing element distinct from the inner sealing ring and mounted around the inner sealing portion, the outer sealing element being annular and intended to sealingly bear at the bottom of the annular housing, - an annular protective portion axially shifted relative to the inner sealing portion, the protective portion being internally delimited by at least one converging protective surface, the converging protective surface being annular and converging towards the sealing lip, and - an annular groove opening into the inside of the inner sealing ring, the annular groove being disposed between the sealing lip and the converging protective surface,
An apparatus for producing bundles from articles, which are connected to each other by an adhesive agent at adhesion points, at which the articles in the finished bundle abut on each other immediately and/or merely spaced apart from one another by the adhesive agent, the apparatus comprising a device by means of which at least a part of the entirety of the adhesion points of articles that are to be connected to each other to form a bundle are provided with adhesive agent, characterised by a drying device for at least the adhesion points that are, in terms of their entirety, at least partly to be provided with adhesive agent, the drying device being integrated into the device and/or arranged immediately before the device in relation to a transport path (120, 121) of the articles to the device.
A vaccine for use in vaccinating a subject against a disorder, wherein the vaccine comprises: (a) an adjuvant comprising a flagellin-based agent, comprising an amino acid sequence having at least 95% identity to SEQ ID NO:2, having TLR5 agonist activity and an aluminum gel or salt, wherein the ratio (w/w) of flagellin-based agent to aluminum gel or salt is about 1:500; and (b) an antigen associated with the disorder. (a) an adjuvant comprising a flagellin-based agent, comprising an amino acid sequence having at least 95% identity to SEQ ID NO:2, having TLR5 agonist activity and an aluminum gel or salt, wherein the ratio (w/w) of flagellin-based agent to aluminum gel or salt is about 1:500; and (b) an antigen associated with the disorder.
A blade state monitoring method comprising: acquiring sensing data from a sensor array, the sensor array including a plurality of sensors, and the plurality of sensors including acoustic sensors, wherein the sensor array is disposed inside a blade of a wind turbine, and the sensing data includes sound data; determining whether there is abnormal data in the sensor data, wherein the abnormal data is sensor data whose index value changes regularly when the sensor data is sound data; and determining that a state of the blade is cracked if there is abnormal data; characterized by further comprising: determining a cracking speed of the blade according to a change amplitude or a change frequency of the abnormal data in a unit time; and/or determining a crack length of the blade according to the amplitude, phase or frequency of the abnormal data. acquiring sensing data from a sensor array, the sensor array including a plurality of sensors, and the plurality of sensors including acoustic sensors, wherein the sensor array is disposed inside a blade of a wind turbine, and the sensing data includes sound data; determining whether there is abnormal data in the sensor data, wherein the abnormal data is sensor data whose index value changes regularly when the sensor data is sound data; and determining that a state of the blade is cracked if there is abnormal data; characterized by further comprising: determining a cracking speed of the blade according to a change amplitude or a change frequency of the abnormal data in a unit time; and/or determining a crack length of the blade according to the amplitude, phase or frequency of the abnormal data. determining a cracking speed of the blade according to a change amplitude or a change frequency of the abnormal data in a unit time; and/or determining a crack length of the blade according to the amplitude, phase or frequency of the abnormal data.
A storage and automatic order picking machine for small piece goods, with at least one storage shelf that has storage areas for the ordered storage of the small piece goods, at least one shelf manipulating unit that can be displaced adjacent to the storage shelf and respectively remove one or more small piece goods from a storage area, as well as transport these small piece goods to at least one delivery point, and at least one belt conveyor with at least one belt that can receive the small piece goods transported to the at least one delivery point at a receiving section of the belt conveyor assigned to the delivery point and transport these small piece goods to a delivery device, characterized in that at least one blocking device is arranged downstream of the receiving section referred to the transport direction of the belt conveyor, wherein said blocking device features a barrier that can be positioned above the belt and prevents the further transport of the piece goods transported up to this point even if the belt continues to move, and in that a control device controls the shelf manipulating unit and the belt conveyor in such a way that the piece goods belonging to a first order are transported to a first delivery point and the piece goods belonging to a following order are transported to a second delivery point and/or subsequently transported to the first delivery point in such a way that the piece goods of the first order lie on the belt conveyor downstream of the piece goods of the following order, wherein the control device controls the blocking device in such a way that the barrier is positioned above the belt in order to block the further transport of the piece goods until the piece goods of the first order have been gathered behind the barrier, the blocking device is then released such that the further transport of the first order can take place and the barrier is subsequently once again positioned above the belt such that the piece goods of the following order are gathered behind the barrier.
A method for generating a computer image of a 3-dimensional scene using a rendering space which is subdivided into a plurality of separate areas, the scene comprising a plurality of objects, the method comprising: a) for at least some of the objects in the scene, storing object data in a memory; b) for two separate areas at a time, deriving control data to link to the object data in the two separate areas, and writing the control data for the two separate areas together in one control stream wherein writing the control data for the two separate areas comprises writing control data, which links to an object which falls in both of the separate areas, only once; c) generating the computer image in the two separate areas by, in parallel: i) deriving depth data for the first separate area from the control data in the control stream and the object data, and deriving image data and shading data for the first separate area from the depth data for display; and ii) deriving depth data for the second separate area from the control data in the control stream and the object data, and deriving image data and shading data for the second separate area from the depth data for display; and d) repeating steps b) and c) until an image has been generated for all the separate areas. a) for at least some of the objects in the scene, storing object data in a memory; b) for two separate areas at a time, deriving control data to link to the object data in the two separate areas, and writing the control data for the two separate areas together in one control stream wherein writing the control data for the two separate areas comprises writing control data, which links to an object which falls in both of the separate areas, only once; c) generating the computer image in the two separate areas by, in parallel: i) deriving depth data for the first separate area from the control data in the control stream and the object data, and deriving image data and shading data for the first separate area from the depth data for display; and ii) deriving depth data for the second separate area from the control data in the control stream and the object data, and deriving image data and shading data for the second separate area from the depth data for display; and i) deriving depth data for the first separate area from the control data in the control stream and the object data, and deriving image data and shading data for the first separate area from the depth data for display; and ii) deriving depth data for the second separate area from the control data in the control stream and the object data, and deriving image data and shading data for the second separate area from the depth data for display; and d) repeating steps b) and c) until an image has been generated for all the separate areas.
An aircraft comprising: a fuselage; and a payload module coupled to the fuselage, the payload module comprising one or more data storage devices, wherein the payload module is configured to be decoupled from the fuselage during flight upon receipt of a de-coupling input, characterised by: the aircraft comprising an aerofoil that is covered by the payload module when the payload module is coupled to the fuselage and exposed to oncoming air when the payload module is decoupled from the fuselage. a fuselage; and a payload module coupled to the fuselage, the payload module comprising one or more data storage devices, wherein the payload module is configured to be decoupled from the fuselage during flight upon receipt of a de-coupling input,
A computer implemented method comprising generating 4D light-field data representative of at least one volume in an object space of a first optical system occupied by a set of rays of light passing through a pupil of said first optical system and a conjugate, in said object space of the first optical system, of at least one pixel of a sensor associated with said first optical system, said volume occupied by said set of rays of light being called a pixel beam, characterized in that it further comprises - computing a value of a parameter representing a radiance transmitted through an imaged pixel beam associated with at least one element of at least one grid defined on a projection surface located at a distance D from a second optical system and belonging to an intersection between said at least one imaged pixel beam and the projection surface, wherein the grid on the projection surface is a pixel grid and wherein said imaged pixel beam is a conjugate of said at least one pixel beam through the second optical system. - computing a value of a parameter representing a radiance transmitted through an imaged pixel beam associated with at least one element of at least one grid defined on a projection surface located at a distance D from a second optical system and belonging to an intersection between said at least one imaged pixel beam and the projection surface, wherein the grid on the projection surface is a pixel grid and wherein said imaged pixel beam is a conjugate of said at least one pixel beam through the second optical system.
A wind farm aircraft beacon system, comprising: - at least one aircraft beacon device, - at least one camera for recording images, characterized by - an evaluation device for detecting flying object positions by evaluating the camera data, in particular images recorded, and - at least one switching device for switching on or off at least one of the aircraft beacon devices in dependence on the flying object positions detected by the evaluation device. - at least one aircraft beacon device, - at least one camera for recording images, characterized by - an evaluation device for detecting flying object positions by evaluating the camera data, in particular images recorded, and - at least one switching device for switching on or off at least one of the aircraft beacon devices in dependence on the flying object positions detected by the evaluation device.
An optoelectronic sensor system for stimulating and detecting samples, with a surface for the application of the samples and an underlying layer system with a transparent first layer with a first refractive index, into which light can be coupled in for stimulating the sample, and an adjoining second layer with a second, smaller refractive index for generating a total reflection of the coupled light and a spreading planar light wave resulting therefrom in the first layer, wherein the surface for the application of the samples is formed by the surface of the first layer on which a total reflection takes place, in which an evanescent field with a penetration depth of 100 to 500 nm is created, and an optoelectronic sensor layer lying under the second layer, consisting of one or more semiconductor layers based on an organic semiconductor between two electrode layers, of which the electrode layer facing the sample is designed to be translucent at least in some regions, characterized in that the optoelectronic sensor layer is located between two glass layers and that the sensor system is configured for a laser, LED or OLED having a wavelength of 300 to 650 nm to be used as the stimulating light source.
A fluid displacement and pressurization device comprising: a syringe body; a plunger which extends into the syringe body, said plunger comprising a thread and a longitudinal axis; a piston on the plunger and in sealed contact with the syringe body; a control button pressable into the plunger; a threaded cylinder in the syringe body, said threaded cylinder comprising a thread; a pair of control blades (3;4) configured to selectively engage and disengage the thread of the plunger with the thread of the threaded cylinder depending on whether the control button is pressed, wherein when the thread of the threaded cylinder is engaged with the thread of the plunger, the plunger is rotatable to provide micro-movement of the plunger relative to the syringe body, and wherein when the thread of the threaded cylinder is disengaged from the thread of the plunger, the plunger is pushable into the syringe body and pullable out of the syringe body to provide macro-movement of the plunger relative to the syringe body.