mhurhangee/ep-ind-claims huggingface dataset:
A method for beampattern generation in a multiple-input multiple-output, MIMO, radar system with a uniform linear array of antenna elements, comprising: mapping, with a processing device, an input signal comprising Gaussian random variables, RVs, onto finite-alphabet non-constant-envelope, FANCE, symbols using a predetermined non-linear mapping function in which the mapping of the Gaussian RVs onto the FANCE symbols depends on a sum of Kummer confluent hypergeometric functions for M regions of the FANCE symbols; and transmitting FANCE waveforms through the uniform linear array of radar antenna elements to obtain a corresponding beampattern, the FANCE waveforms based upon the mapping of the Gaussian RVs onto the FANCE symbols. mapping, with a processing device, an input signal comprising Gaussian random variables, RVs, onto finite-alphabet non-constant-envelope, FANCE, symbols using a predetermined non-linear mapping function in which the mapping of the Gaussian RVs onto the FANCE symbols depends on a sum of Kummer confluent hypergeometric functions for M regions of the FANCE symbols; and transmitting FANCE waveforms through the uniform linear array of radar antenna elements to obtain a corresponding beampattern, the FANCE waveforms based upon the mapping of the Gaussian RVs onto the FANCE symbols.
A system for imaging biopsy samples (12, 14) obtained from a patient comprising: a radiation source operative to emit radiation rays and selectively adjustable between a first scanning position and a second scanning position; a radiation detector operative to receive the radiation rays and having a surface that defines a first imaging region, a second imaging region, and a third imaging region; a collimator having a body having a static shape and defining an opening, the collimator being adapted to be coupled to the radiation source such that the collimator is disposed adjacent to the radiation source and then being selectively adjustable between a first imaging position and a second imaging position by rotating and/or translating the body in relation to the radiation source; and wherein the position/orientation of the body in relation to the radiation detector in the first imaging position allows one or more of the radiation rays to pass from the radiation source, through the opening, and into the second imaging region while restricting the radiation rays via the body from passing into the first imaging region when the radiation source is in the first scanning position, and the position/orientation of the body in relation to the radiation detector in the second imaging position allows one or more of the radiation rays to pass from the radiation source, through the opening, and into the third imaging region while restricting the radiation rays via the body from passing into the first imaging region when the radiation source is in the second scanning position. a radiation detector operative to receive the radiation rays and having a surface that defines a first imaging region, a second imaging region, and a third imaging region; a collimator having a body having a static shape and defining an opening, the collimator being adapted to be coupled to the radiation source such that the collimator is disposed adjacent to the radiation source and then being selectively adjustable between a first imaging position and a second imaging position by rotating and/or translating the body in relation to the radiation source; and wherein the position/orientation of the body in relation to the radiation detector in the first imaging position allows one or more of the radiation rays to pass from the radiation source, through the opening, and into the second imaging region while restricting the radiation rays via the body from passing into the first imaging region when the radiation source is in the first scanning position, and the position/orientation of the body in relation to the radiation detector in the second imaging position allows one or more of the radiation rays to pass from the radiation source, through the opening, and into the third imaging region while restricting the radiation rays via the body from passing into the first imaging region when the radiation source is in the second scanning position.
A refueling drogue coupling system, said system comprising: a fluid passage extending from a coupling inlet to a coupling outlet, said fluid passage comprising a valve seat circumscribing said fluid passage proximate said coupling outlet; a valve plug assembly comprising a valve plug configured to engage said seat to prevent flow through said fluid passage and an actuator assembly comprising a bias member; a coupling latch assembly coupled to said coupling outlet, said coupling latch assembly comprising a latch member configured to matingly engage a complementary latch-receiving member of a refueling probe, said coupling latch assembly further comprising a latch member actuator operatively coupled to said latch member to permit said latch member to move from a first locked position to a second unlocked position; characterized in that said system further comprises: a probe position sensor configured to detect a position of the refueling probe; a hose tension sensor configured to measure a tension in a hose coupled to said coupling inlet; and a drogue controller positioned on said refueling drogue coupling system and communicatively coupled to said latch member actuator, said probe position sensor, and said hose tension sensor. a fluid passage extending from a coupling inlet to a coupling outlet, said fluid passage comprising a valve seat circumscribing said fluid passage proximate said coupling outlet; a valve plug assembly comprising a valve plug configured to engage said seat to prevent flow through said fluid passage and an actuator assembly comprising a bias member; a coupling latch assembly coupled to said coupling outlet, said coupling latch assembly comprising a latch member configured to matingly engage a complementary latch-receiving member of a refueling probe, said coupling latch assembly further comprising a latch member actuator operatively coupled to said latch member to permit said latch member to move from a first locked position to a second unlocked position; a probe position sensor configured to detect a position of the refueling probe; a hose tension sensor configured to measure a tension in a hose coupled to said coupling inlet; and a drogue controller positioned on said refueling drogue coupling system and communicatively coupled to said latch member actuator, said probe position sensor, and said hose tension sensor.
A zero mode waveguide substrate (300;500;600) for use in chemical or biochemical analyses, comprising: a transparent substrate layer (306;400,408;506;606); an opaque metallic cladding layer (304;410;504;604); and a core (302;412;502;602) of a zero mode waveguide formed by an aperture disposed through the cladding layer (304;410;504;604); characterised in that the aperture extends at least partially into the transparent substrate layer (306;400,408;506; 606) forming a lower surface recessed in the transparent substrate layer (306;400,408;506; 606). a transparent substrate layer (306;400,408;506;606); an opaque metallic cladding layer (304;410;504;604); and a core (302;412;502;602) of a zero mode waveguide formed by an aperture disposed through the cladding layer (304;410;504;604); characterised in that the aperture extends at least partially into the transparent substrate layer (306;400,408;506; 606) forming a lower surface recessed in the transparent substrate layer (306;400,408;506; 606).
A device (26, 28) for checking in pieces of baggage of passengers, in particular for use at an airport, comprising a container (32, 34) for receiving a piece of baggage, and a separate cover, wherein in a loading position, accessible to a passenger, of the container (32, 34), the cover is transferable from an open position, which unblocks access to the interior of the container (32, 34), to a closed position, in which access to the interior of the container (32, 34) is blocked, wherein, when the cover is closed, the container (32, 34) is transferable to an unloading condition, in which the piece of baggage can be automatically unloaded from the container (32, 34) in a manner inaccessible to the passenger, wherein the container is delimited by three delimiting parts and a belt conveyor which in an initial position forms the bottom of the container (32, 34) and the position of which can be varied, and the remaining sides of the container can be closed by the cover, and wherein the belt conveyor is moved to an unloading position with the cover closed, for transferring the container (32, 34) to the unloading condition, characterized in that the belt conveyor is moved to the unloading position such that this causes the bottom of the container (32, 34) to open while the belt conveyor conveys the piece of baggage in the opposite direction, so that the piece of baggage falls downwards through the bottom that opens or is received by a transport container placed below.
A flow body (2, 88, 102) comprising: - a curved suction skin having a first perforation, a leading edge and two skin sections extending therefrom, wherein each skin section has an outer end (20, 22) facing away from the leading edge, - an interior suction duct (42, 98, 109, 117) having a second perforation (44, 105, 120, 122, 126) and extending through an inside of the curved suction skin in a distance from the leading edge, - two sidewall members (54, 56), connected to the outer ends (20, 22) of the skin sections, wherein the sidewall members (54, 56) are made of a composite material, and - at least one inner spar (112, 114) delimiting the interior suction duct (42, 98, 109, 117), wherein the curved suction skin comprises a profiled contour shape, which determines a pressure distribution over at least one of the two skin sections when air flows over the curved suction skin, wherein the pressure distribution comprises a stagnation point, a suction peak and a local pressure maximum downstream of the suction peak and upstream a trailing edge of the flow body, and wherein the first perforation extends from the stagnation point to the local pressure maximum. - a curved suction skin having a first perforation, a leading edge and two skin sections extending therefrom, wherein each skin section has an outer end (20, 22) facing away from the leading edge, - an interior suction duct (42, 98, 109, 117) having a second perforation (44, 105, 120, 122, 126) and extending through an inside of the curved suction skin in a distance from the leading edge, - two sidewall members (54, 56), connected to the outer ends (20, 22) of the skin sections, wherein the sidewall members (54, 56) are made of a composite material, and - at least one inner spar (112, 114) delimiting the interior suction duct (42, 98, 109, 117),
An additive fabrication device configured to produce three-dimensional objects by sintering a source material, the additive fabrication device comprising: a chamber; a material deposition mechanism; a fabrication platform arranged within the chamber configured to receive source material from the material deposition mechanism; and an electronic component module (100, 350) coupled to the chamber opposite the fabrication platform, characterized in that the electronic component module comprises: at least one gas intake channel; a primary channel coupled to the at least one gas intake channel and comprising an orifice at a first end; an electronic component arranged at least partially within the primary channel at a second end of the primary channel, the second end opposing the first end of the primary channel; and at least one gas exhaust channel coupled to a side of the primary channel, wherein the at least one gas exhaust channel is oriented away from the electronic component. a chamber; a material deposition mechanism; a fabrication platform arranged within the chamber configured to receive source material from the material deposition mechanism; and an electronic component module (100, 350) coupled to the chamber opposite the fabrication platform, characterized in that the electronic component module comprises: at least one gas intake channel; a primary channel coupled to the at least one gas intake channel and comprising an orifice at a first end; an electronic component arranged at least partially within the primary channel at a second end of the primary channel, the second end opposing the first end of the primary channel; and at least one gas exhaust channel coupled to a side of the primary channel, wherein the at least one gas exhaust channel is oriented away from the electronic component. at least one gas intake channel; a primary channel coupled to the at least one gas intake channel and comprising an orifice at a first end; an electronic component arranged at least partially within the primary channel at a second end of the primary channel, the second end opposing the first end of the primary channel; and at least one gas exhaust channel coupled to a side of the primary channel, wherein the at least one gas exhaust channel is oriented away from the electronic component.
A passenger compartment for a motor vehicle, said compartment comprising: - a ventilation system comprising, - an air duct leading into the interior of the vehicle at the feet of the passengers in the second row, - a grid, - said passenger compartment comprising a bracket, inside the vehicle, comprising lateral flanges, - the grate being integrated into the side flanges of the console and located at the feet of the second row passengers inside the passenger compartment of the vehicle, - the air duct being connected to the grate and sending the air flow into the space inside the vehicle, characterized in that the vehicle passenger compartment comprises a plate which incorporates interfaces for fixing said air duct, said interfaces for fixing said air duct being capable of making said air duct sealingly connected to said grate inside the bracket; the air duct being fitted on the grate. - a ventilation system comprising, - an air duct leading into the interior of the vehicle at the feet of the passengers in the second row, - a grid, - said passenger compartment comprising a bracket, inside the vehicle, comprising lateral flanges, - the grate being integrated into the side flanges of the console and located at the feet of the second row passengers inside the passenger compartment of the vehicle, - the air duct being connected to the grate and sending the air flow into the space inside the vehicle,
An antibody molecule that is specific for the BMP-1-1 isoform, or an antibody molecule that is specific for the BMP-1-3 isoform, for use in treating chronic renal failure in an individual.
Method for the production of three-dimensional objects through a stereolithography machine comprising: - a tank containing a liquid substance suited to solidify when subjected to a selective stimulation; - a modelling plate (6; 6'; 6") comprising a work surface facing the bottom of said tank and suited to support said object; - emission means suited to generate said selective stimulation and convey it towards said tank; said method comprising the step of operating said emission means in such a way as to cause solidification of a plurality of mutually superimposed layers with predefined thickness of said liquid substance, characterized in that said modelling plate (6; 6'; 6") comprises at least one groove made in said work surface along a trajectory and extending to the perimeter edge of said work surface so as to have at least one open end at the level of the lateral surface of said plate (6; 6'; 6"), and in that said emission means are operated in such a way that at least a portion of said liquid substance arranged in said groove remains liquid. - a tank containing a liquid substance suited to solidify when subjected to a selective stimulation; - a modelling plate (6; 6'; 6") comprising a work surface facing the bottom of said tank and suited to support said object; - emission means suited to generate said selective stimulation and convey it towards said tank;
A method for balancing the out-of-balance of a shaft-wheel assembly, comprising a bladed wheel held at the end of a mechanical shaft, implementing a step a) measuring the out-of-balance value of the shaft-wheel assembly with respect to a longitudinal axis of the mechanical shaft, characterized in that the following steps are implementing: b. measuring the position of at least two distinct target areas, present at the surface of the bladed wheel, with respect to the longitudinal axis of the mechanical shaft; then c. removing a quantity of material at the surface of the bladed wheel, to reduce the out-of-balance value of the shaft-wheel assembly, as a function of the measurements made at steps a) and b). b. measuring the position of at least two distinct target areas, present at the surface of the bladed wheel, with respect to the longitudinal axis of the mechanical shaft; then c. removing a quantity of material at the surface of the bladed wheel, to reduce the out-of-balance value of the shaft-wheel assembly, as a function of the measurements made at steps a) and b).
Computer implemented method for generating a model for determining a measurement error in a measurement of concentration of hydrogen that is contained in a gas mixture, wherein the gas mixture comprises hydrogen and a non-hydrogenous carrier gas mixture, wherein - data (4, 40) is provided regarding at least two different non-hydrogenous carrier gas mixture compositions, - different gas mixture compositions are generated based on the data (4, 40), wherein in the case of different gas mixture compositions the non-hydrogenous carrier gas mixture composition and/or the hydrogen content are/is different, - for the gas mixture compositions, hydrogen concentration measured values are determined, and measurement errors are determined on the basis of the hydrogen concentration measured values, - a model is provided that maps data regarding carrier gas mixture compositions and hydrogen concentration measured values to measurement errors, characterised in that the non-hydrogenous carrier gas mixture is a natural gas mixture. - data (4, 40) is provided regarding at least two different non-hydrogenous carrier gas mixture compositions, - different gas mixture compositions are generated based on the data (4, 40), wherein in the case of different gas mixture compositions the non-hydrogenous carrier gas mixture composition and/or the hydrogen content are/is different, - for the gas mixture compositions, hydrogen concentration measured values are determined, and measurement errors are determined on the basis of the hydrogen concentration measured values, - a model is provided that maps data regarding carrier gas mixture compositions and hydrogen concentration measured values to measurement errors,
Single-wheel drive component for a motor vehicle, wherein the single-wheel drive component has a drive unit and a hub carrier, wherein a wheel hub which can be driven by the drive unit is mounted rotatably by means of a wheel bearing on the hub carrier, wherein several unit supports (9, 11) and several further unit supports (10, 12) for mounting the drive unit to a vehicle body of the motor vehicle emanate from the drive unit, wherein on the unit supports (9, 11) and the further unit supports (10, 12) is arranged in each case one unit bearing for the resilient mounting of the drive unit on the vehicle body, characterised in that for mounting the hub carrier on the unit supports (9, 11) and the further unit supports (10, 12), several links (14, 15, 16) are provided which, respectively, are articulated on the one hand on the hub carrier and on the other hand on at least one of the unit supports (9, 11) and the further unit supports (10, 12), wherein on all of the unit supports (9, 11) and the further unit supports (10, 12) is articulated respectively at least one link (14, 15, 16) of the several links (14, 15, 16).
A particle beam therapy system comprising: a synchrotron adapted to accelerate beams of charged particles to a desired energy level and permit extraction of said beams of charged particles exceeding a stability limit for the amplitude of oscillation of the circling beams of charged particles, an irradiation device adapted to irradiate an object with said beams of charged particles, and a beam transport system adapted to conduct said beams of charged particles extracted from said synchrotron to said irradiation device, characterised by a control unit adapted to control the synchrotron and the beam transport system such as to remove part of said beams of charged particles circling in said synchrotron inside the synchrotronor the beam transport system in an extraction preparation period between completion of synchrotron acceleration and start of irradiation and to allow the rest of said circling beams of charged particles to be extracted from said synchrotron and to be conducted to said irradiation device in a subsequent irradiation period. a synchrotron adapted to accelerate beams of charged particles to a desired energy level and permit extraction of said beams of charged particles exceeding a stability limit for the amplitude of oscillation of the circling beams of charged particles, an irradiation device adapted to irradiate an object with said beams of charged particles, and a beam transport system adapted to conduct said beams of charged particles extracted from said synchrotron to said irradiation device, characterised by a control unit adapted to control the synchrotron and the beam transport system such as to remove part of said beams of charged particles circling in said synchrotron inside the synchrotronor the beam transport system in an extraction preparation period between completion of synchrotron acceleration and start of irradiation and to allow the rest of said circling beams of charged particles to be extracted from said synchrotron and to be conducted to said irradiation device in a subsequent irradiation period. to remove part of said beams of charged particles circling in said synchrotron inside the synchrotronor the beam transport system in an extraction preparation period between completion of synchrotron acceleration and start of irradiation and to allow the rest of said circling beams of charged particles to be extracted from said synchrotron and to be conducted to said irradiation device in a subsequent irradiation period.
Universal joint for a steering shaft (23, 25) of a motor vehicle, comprising a universal joint with two pairs of journals arranged at right angles to one another and two joint forks (51, 53) which can be connected to the steering shaft (23, 25) and each have two arms (52, 54) lying opposite one another, in each of which a journal is mounted rotatably about a journal axis in a journal bearing which has a cup-shaped outer bush which is fixed in the arm (52, 54) and is closed at the end face by an outer cup base which is opposite the end face of the journal, wherein rollable rolling elements are arranged between the journal and the outer bush, wherein an inner bush is fixed on the journal, wherein the rolling elements are arranged between the inner bush and the outer bush in a region formed as a rolling element track, and wherein a convexly projecting contact region (58, 64) is arranged on the end face of a journal, which contacts the outer cup base, characterised in in that the contact region (58, 64) is formed integrally on the journal or on the inner bush and projects axially on the end face relative to the rolling element track of the inner bush. wherein an inner bush is fixed on the journal, wherein the rolling elements are arranged between the inner bush and the outer bush in a region formed as a rolling element track, and wherein a convexly projecting contact region (58, 64) is arranged on the end face of a journal, which contacts the outer cup base, characterised in in that the contact region (58, 64) is formed integrally on the journal or on the inner bush and projects axially on the end face relative to the rolling element track of the inner bush.