mhurhangee/ep-ind-claims huggingface dataset:
A method for printing a decoration on the surface of a workpiece by means of digital printing equipment, the printing equipment comprising at least one application unit for applying a liquid to the workpiece and at least one dryer unit for drying the workpiece, the method comprising the following steps: a. providing information in an electric control unit of the printing equipment about the expected moisture of the workpiece to be dried, b. determining drying parameters with which the at least one dryer unit can be operated on the basis of the information provided, and c. drying the workpiece by means of at least one dryer unit using the determined drying parameters characterized in that, after drying by means of at least one dryer unit, the moisture of the surface of the workpiece is measured by means of at least one moisture sensor and compared with a predetermined target value, a measure of the deviation of the measured moisture from the predetermined target value being included in the future determination of the drying parameters. a. providing information in an electric control unit of the printing equipment about the expected moisture of the workpiece to be dried, b. determining drying parameters with which the at least one dryer unit can be operated on the basis of the information provided, and c. drying the workpiece by means of at least one dryer unit using the determined drying parameters
A method of producing a radiolabeled aryl compound represented by the formula: Ar-X wherein Ar is a C 6-14 aryl group optionally having substituent (s), and X is 211 At or 210 At, or a salt thereof, which comprises reacting an aryl boronic acid compound represented by the formula: Ar-Y wherein Ar is as defined above, and Y is a borono group (-B 2) or an ester group thereof, or a salt thereof, with a radionuclide 211 At or 210 At, in the presence of an oxidizing agent selected from an alkali metal iodide, an alkali metal bromide, N-bromosuccinimide, N-chlorosuccinimide and hydrogen peroxide, in water, in an organic solvent-free system. Ar is a C 6-14 aryl group optionally having substituent (s), and X is 211 At or 210 At, or a salt thereof, which comprises reacting an aryl boronic acid compound represented by the formula: Ar-Y wherein Ar is as defined above, and Y is a borono group (-B 2) or an ester group thereof, or a salt thereof, with a radionuclide 211 At or 210 At, in the presence of an oxidizing agent selected from an alkali metal iodide, an alkali metal bromide, N-bromosuccinimide, N-chlorosuccinimide and hydrogen peroxide, in water, in an organic solvent-free system. Ar is as defined above, and Y is a borono group (-B 2) or an ester group thereof, or a salt thereof, with a radionuclide 211 At or 210 At, in the presence of an oxidizing agent selected from an alkali metal iodide, an alkali metal bromide, N-bromosuccinimide, N-chlorosuccinimide and hydrogen peroxide, in water, in an organic solvent-free system.
Device carrier for cable guide channels, consisting of a lower part and a frame, which can be pivoted from a parking position into an assembly end position by means of lateral pintles, wherein the lower part consists of a housing with a base and side elements, in which slots that are open to the outside are incorporated at the top and bottom, said slots in each case passing into a horizontal elongate hole and wherein equally spaced apart laterally protruding pintles cooperating with the slots of the lower part are formed laterally on the frame, wherein to reach the assembly position, the pintles of the frame are guided in the elongate holes of the side elements of the lower part and held therein by an end plate formed on the pintles, characterised in that clamping profiles, which cooperate with locking tongues formed laterally on the side elements of the frame to prevent displacement, are formed on the two side elements of the lower part, in that incorporated on the clamping profile of the side wall of the lower part is a groove, which runs transversely to the longitudinal side of the side wall and in which the end of the locking tongue engages, in that the clamping profile on the side elements of the lower part consists of an edge and a groove, in that the locking tongue is strip-shaped and resilient.
Occupancy detection and/or classification system for an automotive vehicle, comprising at least one radar module for detecting the presence of an object within the vehicle interior, characterized in that said at least one radar module comprises an antenna system having a frequency dependent main lobe direction and in that said occupancy detection and/or classification system comprises a control module for operating said at least one radar module at a plurality of frequencies, wherein said antenna system comprises at least two antennas, each of said at least two antennas having an individual frequency dependency of its main lobe direction, and wherein the respective individual frequency dependencies of the main lobe direction of said at least two antennas are different from one each other.
Method for producing electrically conductive bushings through a semiconductive or non-conductive substrate, which is particularly suitable for electric applications, wherein the front side of the substrate is provided with one or more layers as well as with at least one electrically conducting contact structure within or on said layer(s), comprising the steps: (a) providing said semiconductive or non-conductive substrate (b) forming at least one recess starting from the said front side that extends through the said layer(s), beside the said at least one conducting contact structure, (c) applying an electrically conductive structure which extends, at least starting from the said conductive contact structure, up to the base of the at least one recess, such that it forms an electrically conductive contact point, (d) forming, from its rear side, at least one recess in the substrate, such that this recess ends on the front side of the substrate below that location or below one of the locations where the electrically conductive contact point or one of the said electrically conductive contact points is situated, and is completely covered by the latter, (e) applying from the rear side of the substrate an electrically conductive structure, which establishes a conductive connection between the respective contact point and the rear-side surface (10, 11, 12) of the substrate through the said recess or at least one of the recesses, wherein the or each rear-side recess has a cross-sectional area which becomes smaller in the direction of the front side of the substrate and/or wherein the or each front-side recess has a cross-sectional area which becomes smaller in the direction of the said contact point. (a) providing said semiconductive or non-conductive substrate (b) forming at least one recess starting from the said front side that extends through the said layer(s), beside the said at least one conducting contact structure, (c) applying an electrically conductive structure which extends, at least starting from the said conductive contact structure, up to the base of the at least one recess, such that it forms an electrically conductive contact point, (d) forming, from its rear side, at least one recess in the substrate, such that this recess ends on the front side of the substrate below that location or below one of the locations where the electrically conductive contact point or one of the said electrically conductive contact points is situated, and is completely covered by the latter, (e) applying from the rear side of the substrate an electrically conductive structure, which establishes a conductive connection between the respective contact point and the rear-side surface (10, 11, 12) of the substrate through the said recess or at least one of the recesses,
An optical fiber transmission link comprising a multimode optical fiber for propagating light comprising a set of optical signals according to a set of propagation modes, each propagation mode being associated with a power value, said multimode optical fiber comprising fiber slices, wherein the optical fiber transmission link comprises at least one scrambler, each scrambler being inserted between two fiber slices, each scrambler being configured to determine a permutation of said propagation modes depending on the power values associated with said propagation modes, wherein each scrambler comprises a permutation unit for permuting the modes two by two, by applying a permutation matrix of dimension N t × N t, with N t designating the number of modes used by the scrambler, the permutation matrix associating each of the propagation modes used by the transmitter with another mode, wherein the permutation unit is configured to permute a mode associated with the i -th higher power value with the mode associated with the i -th lower power value, with i being comprised between 1 and a value representing the output of a floor function applied to N t /2, and wherein each scrambler is configured to redistribute the optical signals according to said permutation of said propagation modes.
A method for providing the location of a portable mobile remote unit, PRU (501, 510), associated with a telecommunications network comprising: i) obtaining at the network geographic boundary information within which the location of the PRU should be disclosed; ii) requesting for the location of PRUs within said geographic boundary, iii) obtaining the location of a PRU within the network and determining whether the PRU is within the said geographic boundary; iv) forwarding the location of the PRU to the network upon determination that the PRU is within the said geographic boundary. i) obtaining at the network geographic boundary information within which the location of the PRU should be disclosed; ii) requesting for the location of PRUs within said geographic boundary, iii) obtaining the location of a PRU within the network and determining whether the PRU is within the said geographic boundary; iv) forwarding the location of the PRU to the network upon determination that the PRU is within the said geographic boundary.
An apparatus for the detection of microbiological activity in an industrial process, the apparatus comprising: a plurality of satellite units (202a, 202b...) configured to sample a liquid from the industrial process at a plurality of respective locations, in which each satellite unit is configured to periodically analyse a sample, each satellite unit being configured to carry out an impedance analysis to count and measure the size of particles passing through an orifice, in which each satellite unit is configured to generate sample results data corresponding to the number and size of particles in each sample; wherein the apparatus is characterised by: a processing unit configured to compare the sample results data to a predetermined criterion and to generate an alert signal if the sample results data is outside of the predetermined criterion or establishes a trend approaching the predetermined criterion; and, a main analysis unit in the form of a combined impedance and fluorescence system, configured to perform combined impedance and fluorescence analysis of a sample of liquid from the industrial process following generation of the alert signal. a plurality of satellite units (202a, 202b...) configured to sample a liquid from the industrial process at a plurality of respective locations, in which each satellite unit is configured to periodically analyse a sample, each satellite unit being configured to carry out an impedance analysis to count and measure the size of particles passing through an orifice, in which each satellite unit is configured to generate sample results data corresponding to the number and size of particles in each sample; wherein the apparatus is characterised by: a processing unit configured to compare the sample results data to a predetermined criterion and to generate an alert signal if the sample results data is outside of the predetermined criterion or establishes a trend approaching the predetermined criterion; and, a main analysis unit in the form of a combined impedance and fluorescence system, configured to perform combined impedance and fluorescence analysis of a sample of liquid from the industrial process following generation of the alert signal. a processing unit configured to compare the sample results data to a predetermined criterion and to generate an alert signal if the sample results data is outside of the predetermined criterion or establishes a trend approaching the predetermined criterion; and, a main analysis unit in the form of a combined impedance and fluorescence system, configured to perform combined impedance and fluorescence analysis of a sample of liquid from the industrial process following generation of the alert signal.
Storage device with at least one carrier unit (12a-d) and with at least one storage unit (14a-d), which is configured for an accommodation and/or storage of consumer goods (16a-d) in at least one accommodation region (18a-d), and is in at least one application state releasably connected to the carrier unit (12a-d) in a one-sided fashion, i.e. on precisely one side of the storage unit (14a-d), wherein the storage unit (14a-d) is displaceable relative to the carrier unit (12a-d), wherein the storage unit (14a-d) comprises at least one at least substantially plate-shaped base body (20a-d) and at least one guiding unit (24a-d) that is arranged on the base body (20a-d), said guiding unit (24a-d) being configured to at least partially guide the base body (20a-d) in a displacement of the storage unit (14a-d) relative to the carrier unit (12a-d), wherein the storage unit comprises at least one abutment, which at least partially delimits a movement of the storage unit relative to the carrier unit in the displacement of the storage unit relative to the carrier unit, characterised in that, for a release from the carrier unit, the storage unit is configured to overcome the abutment by tilting the base body relative to the carrier unit.
A wing of an aircraft comprising: a wing leading edge, a wing trailing edge, and a wing surface defined by a wing upper surface and a wing lower surface, the wing extending from a wing root to a wingtip having a wingtip chord; a winglet extending from the wingtip and having a winglet leading edge, a winglet trailing edge, a winglet inboard surface, a winglet outboard surface, a winglet root having a winglet root chord (Cwi), and a winglet tip, wherein an intersection of the winglet leading edge with the wingtip is located aft of the wing leading edge at the wingtip; and a flow fence disposed on the wing surface inboard from the winglet in a top planform view of the wing, where in an outboard side view of the winglet the flow fence extends from a first position located on the wing upper surface which overlaps with the winglet to a second position located on the wing lower surface, where in the top planform view of the wing an inboard spacing of the flow fence from the wingtip does not exceed 100% of a length of the winglet root chord (Cwi), wherein the flow fence is adapted to delay and/or prevent airflow separation on the winglet inboard surface at high angle of sideslip, increasing lateral stability and linearizing aircraft behavior at high angle of sideslip, wherein the flow fence is adapted to generate vortices between the flow fence and the winglet by airflow flowing from the wing lower surface to the wing upper surface around the wingtip and the wing leading edge, wherein the vortices redirect airflow to limit low-pressure peaks on the winglet leading edge. a wing leading edge, a wing trailing edge, and a wing surface defined by a wing upper surface and a wing lower surface, the wing extending from a wing root to a wingtip having a wingtip chord; a winglet extending from the wingtip and having a winglet leading edge, a winglet trailing edge, a winglet inboard surface, a winglet outboard surface, a winglet root having a winglet root chord (Cwi), and a winglet tip, wherein an intersection of the winglet leading edge with the wingtip is located aft of the wing leading edge at the wingtip; and a flow fence disposed on the wing surface inboard from the winglet in a top planform view of the wing, where in an outboard side view of the winglet the flow fence extends from a first position located on the wing upper surface which overlaps with the winglet to a second position located on the wing lower surface, where in the top planform view of the wing an inboard spacing of the flow fence from the wingtip does not exceed 100% of a length of the winglet root chord (Cwi), wherein the flow fence is adapted to delay and/or prevent airflow separation on the winglet inboard surface at high angle of sideslip, increasing lateral stability and linearizing aircraft behavior at high angle of sideslip, wherein the flow fence is adapted to generate vortices between the flow fence and the winglet by airflow flowing from the wing lower surface to the wing upper surface around the wingtip and the wing leading edge, wherein the vortices redirect airflow to limit low-pressure peaks on the winglet leading edge.
A device for checking the tightness of a casing housing lubricated moving members of a transmission gearbox of a rotorcraft, characterised in that the device comprises: -) an aeraulic circuit open to the atmosphere at its downstream end, the aeraulic circuit comprising at its upstream end connection means for leaktight connection to a vent of the casing and being equipped with a depressurisation member for generating a depressurisation within the aeraulic circuit, the operation of the depressurisation member being under the control of control means, and -) means for regulating said depressurisation which is kept stable within the aeraulic circuit relative to a setpoint threshold, the operation of the regulating means being at least under the control of a pressure gauge for measuring the depressurisation generated within the aeraulic circuit. -) an aeraulic circuit open to the atmosphere at its downstream end, the aeraulic circuit comprising at its upstream end connection means for leaktight connection to a vent of the casing and being equipped with a depressurisation member for generating a depressurisation within the aeraulic circuit, the operation of the depressurisation member being under the control of control means, and -) means for regulating said depressurisation which is kept stable within the aeraulic circuit relative to a setpoint threshold, the operation of the regulating means being at least under the control of a pressure gauge for measuring the depressurisation generated within the aeraulic circuit.
Method for determination of pollutants and leachables in dialysis solutions by stir bar sorptive extraction comprising the steps of a. Conditioning of the stir bar coated with a sorptive material to minimize background contamination, b. Stirring the dialysis solution with a coated stir bar, c. Desorption of pollutants and leachables from the coated stir bar, d. Analysis of the pollutants and leachables by GC-MS, characterized in that the stirring occurs for 120-360 minutes and the sorptive material of the stir bar is poly-dimethylsiloxane (PDMS), wherein the conditioning step a) comprises washing in a mixture comprising methanol and dichloromethane. a. Conditioning of the stir bar coated with a sorptive material to minimize background contamination, b. Stirring the dialysis solution with a coated stir bar, c. Desorption of pollutants and leachables from the coated stir bar, d. Analysis of the pollutants and leachables by GC-MS,
A portable weld cooling system comprising: a plurality of weld cooling instruments; said plurality of weld cooling instruments comprising an air compressor and one or more vortex tubes; characterised in that: said plurality of weld cooling instruments also comprises a halo structure, wherein the halo structure comprises an upper halo assembly, a lower halo assembly, a plurality of intake ports, an internal channel and a plurality of exit ports, and wherein the upper halo assembly and lower halo assembly cooperate to form a circle operable to wrap around a pipe section and/or be mounted to a weld support; and the system further comprises a cabinet comprising a storage section, the storage section configured to store the plurality of weld cooling instruments, wherein one or more of the plurality of weld cooling instruments may be removed from the storage section and combined to provide cool air to a weld area created by a weld fusion machine. a plurality of weld cooling instruments; said plurality of weld cooling instruments comprising an air compressor and one or more vortex tubes; characterised in that: said plurality of weld cooling instruments also comprises a halo structure, wherein the halo structure comprises an upper halo assembly, a lower halo assembly, a plurality of intake ports, an internal channel and a plurality of exit ports, and wherein the upper halo assembly and lower halo assembly cooperate to form a circle operable to wrap around a pipe section and/or be mounted to a weld support; and the system further comprises a cabinet comprising a storage section, the storage section configured to store the plurality of weld cooling instruments, wherein one or more of the plurality of weld cooling instruments may be removed from the storage section and combined to provide cool air to a weld area created by a weld fusion machine. said plurality of weld cooling instruments also comprises a halo structure, wherein the halo structure comprises an upper halo assembly, a lower halo assembly, a plurality of intake ports, an internal channel and a plurality of exit ports, and wherein the upper halo assembly and lower halo assembly cooperate to form a circle operable to wrap around a pipe section and/or be mounted to a weld support; and the system further comprises a cabinet comprising a storage section, the storage section configured to store the plurality of weld cooling instruments, wherein one or more of the plurality of weld cooling instruments may be removed from the storage section and combined to provide cool air to a weld area created by a weld fusion machine.