mhurhangee/ep-ind-claims huggingface dataset:
Apparatus for compacting fibrous stalk material in the form of grass, hay, straw or similar biomass, the apparatus comprising at least one pair of press drums (6, 7) which, while rotating in opposite directions, converge to a feed hopper for the stalk material, into which hopper a conveyor track for the straw material to be supplied leads, comprising a drive arrangement for driving the press drums (6, 7) as well as further devices that supply the straw material to the press drums (6, 7), comprising an apparatus for adding additives into the flow of straw material flowing towards the feed hopper, comprising an open-loop and closed-loop control device which is connected to at least one sensor for detecting process parameters of the compacting process and which is also configured to act on at least one actuator in order to change at least one process parameter, the at least one sensor (S1, S2, S3) for detecting at least one process parameter of the compacting process being designed to detect the forces or torques prevailing on the press drums (6, 7) during the compacting process, and it being possible for the forces or torques prevailing on the press drums (6, 7) during the compacting process to be used as a controlled variable for changing the conveying parameters of the apparatus for adding additives and/or to be used as a controlled variable for changing the conveying rate of the flow of stalk material flowing towards the feed hopper, characterised in that the open-loop and closed-loop control device has a data processing device for calculating a specific energy consumption which is derived from the ratio of the detected amount of the straw material supplied to the feed hopper of the press drums (6, 7) and the drive power of the press drums (6, 7) that can be calculated from the detected torques, and a desired specific energy consumption, which corresponds to a predetermined strength of the pellets to be produced, can be entered as a setpoint into the data processing device of the open-loop and closed-loop control device.
A retrieval docking component for an implantable medical device, said retrieval docking component comprising a base and a limiting part, wherein a distal end of the base along an axial direction is configured to be connected to a body of the implantable medical device, wherein a proximal end of the base along the axial direction is connected to the limiting part, wherein the limiting part has a radial outer dimension that is greater than a radial outer dimension of the proximal end of the base; and characterised in that the limiting part comprises at least two accommodation grooves along a circumference thereof, and wherein the accommodation groove is open outwardly along a radial direction of the base and is configured to capture a snare of a delivery device. wherein a distal end of the base along an axial direction is configured to be connected to a body of the implantable medical device, wherein a proximal end of the base along the axial direction is connected to the limiting part, wherein the limiting part has a radial outer dimension that is greater than a radial outer dimension of the proximal end of the base; and characterised in that the limiting part comprises at least two accommodation grooves along a circumference thereof, and wherein the accommodation groove is open outwardly along a radial direction of the base and is configured to capture a snare of a delivery device.
A wire inspection system comprising: a mirror assembly comprising an odd number of sides arranged to form a pyramid structure configured to surround a wire segment (304, 402, 404, 406, 502, 504, 506), wherein a plurality of said sides comprise a mirror, each mirror being sized to occupy less than half of a surface of an associated side; a light source configured to illuminate the wire segment; and at least one camera configured to acquire a plurality of images of the wire segment that are reflected by said plurality of mirrors, wherein each image of the plurality of images shows a different side of the wire segment. a mirror assembly comprising an odd number of sides arranged to form a pyramid structure configured to surround a wire segment (304, 402, 404, 406, 502, 504, 506), wherein a plurality of said sides comprise a mirror, each mirror being sized to occupy less than half of a surface of an associated side; a light source configured to illuminate the wire segment; and at least one camera configured to acquire a plurality of images of the wire segment that are reflected by said plurality of mirrors, wherein each image of the plurality of images shows a different side of the wire segment.
A mechanical resonator, in particular for the regulator member for regulating a mechanical timepiece movement, the resonator comprising: (i) a first layer of silicon cut out from a first crystal plane of the silicon; (ii) a second layer of silicon cut out from a second crystal plane of the silicon; and (iii) at least one separation layer between the first and second layers of silicon (Cs1, Cs2); said mechanical resonator being characterized in that the crystal lattice of the first layer is offset by an angle different from 0°, 45° or 180° relative to the crystal lattice of the second layer, and/or in that the first crystal plane is different from and not equivalent to the second crystal plane. (i) a first layer of silicon cut out from a first crystal plane of the silicon; (ii) a second layer of silicon cut out from a second crystal plane of the silicon; and (iii) at least one separation layer between the first and second layers of silicon (Cs1, Cs2); said mechanical resonator being characterized in that the crystal lattice of the first layer is offset by an angle different from 0°, 45° or 180° relative to the crystal lattice of the second layer, and/or in that the first crystal plane is different from and not equivalent to the second crystal plane. said mechanical resonator being characterized in that the crystal lattice of the first layer is offset by an angle different from 0°, 45° or 180° relative to the crystal lattice of the second layer, and/or in that the first crystal plane is different from and not equivalent to the second crystal plane.
A modular mould set comprising a plurality of mould parts (2, 5, 50, 500) for the construction of casting moulds (1, 10) for casting concrete wall segments (8, 80) of a tower wall of a tower having an angular cross-section of a wind turbine, having the following mould parts (2, 5, 50, 500): • a plurality of identically formed corner mould parts each having an angled inner shell and an angled outer shell, • a plurality of identically formed base wall mould parts each having a flat inner shell and a flat outer shell, • a plurality of wall mouldings (5, 50, 500) each having a flat inner shell and a flat outer shell and formed in different mould widths, wherein the corner mould parts, the base wall mould parts and the wall mould parts (5, 50, 500) have identical heights and wherein in each case any two parts of the corner mould parts, base wall mould parts and wall mould parts (5, 50, 500) can be connected to one another at lateral edges extending substantially along the height of the mould parts (2, 5, 50, 500) to form a casting mould (1, 5, 50, 500), 10) can be connected to one another in such a way that in each case the inner shells (3, 6) of the interconnected mould parts (2, 5, 50, 500) are joined together to form a continuous inner shell and in each case the outer shells (4, 7) of the interconnected mould parts (2, 5, 50, 500) are joined together to form a continuous outer shell. • a plurality of identically formed corner mould parts each having an angled inner shell and an angled outer shell, • a plurality of identically formed base wall mould parts each having a flat inner shell and a flat outer shell, • a plurality of wall mouldings (5, 50, 500) each having a flat inner shell and a flat outer shell and formed in different mould widths,
A framework with walls or slabs made of plasterboard, which comprises a plurality of vertical or horizontal profiled elements, a front upright member, and a rear upright member, which are connected by horizontal crossmembers, and a first element adapted to act as an upper lintel for said front upright member and said rear upright member and also by a rail/guide for sliding trolleys for supporting a door, said framework being further constituted by brackets for centering an upper framework and for support for said walls or slabs made of plasterboard, characterized in that each one of said brackets for centering said upper framework and for support for said slabs of plasterboard is essentially L-shaped so as to define a first appendage, which supports a lower edge of a slab or wall made of plasterboard and which abuts against an underlying plug, and a second appendage against which the slab or wall abuts, and characterized in that between said first and second appendages (17, 19) there is a recess, facing in the direction opposite to said wall or slab, which has a depth that is such as to allow the insertion, for each pair of said brackets arranged facing each other, of said first element.
Dental material from the group of composites, prosthetic base materials, adhesives, varnishes and fissure sealants comprising inorganic particles as dental filling materials having antimicrobial properties, at least one antimicrobial agent being applied onto the inorganic particles which is adsorbed or bound to the particles via ionic interaction or van der Waals interaction - from the group of dipole-dipole, dipole-induced dipole, induced dipole-induced dipole interactions, the agent being selected from the group consisting of iminopyridinium derivatives, octenidine salts, dequalinium salts, sanguinarine and poly-[2-(2-ethoxy)-ethoxyethyl)guanidinium chloride], and the dental filling material belonging to the group consisting of a dental glass, barium-aluminum-silicate glass, SiO 2, ZrO 2 and YbF 3.
Method for integrating at least one fuel cell unit for integration into a structural component of a vehicle, comprising the steps of: - determining an available receiving space in an interior structural component of the vehicle, that allows receiving a fuel cell unit through insertion from outside the structural component into the receiving space, - providing at least two casing parts (36, 76) that are assembleable to a closed casing, - providing at least one fuel cell having an anode, a cathode and an electrolyte, - assembling the casing parts (36, 76) and the at least one fuel cell to form the fuel cell unit, and - inserting the at least one fuel cell unit into the receiving space of the structural component, wherein at least one of the casing parts (36, 76) is manufactured using an additive manufacturing method such that the fuel cell unit precisely fits into the determined receiving space, wherein one of the casing parts (36, 76) comprises an exterior fuel inlet and an interior fuel distributor for leading a fuel from the exterior fuel inlet to at least one fuel outlet couplable with each of the at least one fuel cell, and wherein one of the casing parts (36, 76) comprises an exterior oxidant inlet and an interior oxidant distributor for leading an oxidant from the exterior oxidant inlet to at least one oxidant outlet couplable with each of the at least one fuel cell. - determining an available receiving space in an interior structural component of the vehicle, that allows receiving a fuel cell unit through insertion from outside the structural component into the receiving space, - providing at least two casing parts (36, 76) that are assembleable to a closed casing, - providing at least one fuel cell having an anode, a cathode and an electrolyte, - assembling the casing parts (36, 76) and the at least one fuel cell to form the fuel cell unit, and - inserting the at least one fuel cell unit into the receiving space of the structural component,
Friction damper comprising a. a housing having a longitudinal axis, b. a plunger that can be displaced along the longitudinal axis, c. a friction unit for producing a direction-dependent frictional force on the plunger, wherein the friction unit comprises at least one friction lining that is in frictional contact with the plunger and a friction lining support, on which the at least one friction lining is held, wherein the friction lining support is arranged so as to be displaceable relative to the plunger between a pull-out position and an insertion position, d. a switching unit for variable setting of the frictional force, wherein the switching unit comprises i. a switchable actuator, ii. a locking element, iii. a force transmission unit (47, 48, 50, 52), which is mechanically coupled to the actuator and to the locking unit, wherein the force transmission unit (47, 48, 50, 52) comprises a threaded spindle, wherein the locking element has a spindle nut that interacts with the threaded spindle and is designed integrally on the locking element. a. a housing having a longitudinal axis, b. a plunger that can be displaced along the longitudinal axis, c. a friction unit for producing a direction-dependent frictional force on the plunger, wherein the friction unit comprises at least one friction lining that is in frictional contact with the plunger and a friction lining support, on which the at least one friction lining is held, wherein the friction lining support is arranged so as to be displaceable relative to the plunger between a pull-out position and an insertion position, d. a switching unit for variable setting of the frictional force, wherein the switching unit comprises i. a switchable actuator, ii. a locking element, iii. a force transmission unit (47, 48, 50, 52), which is mechanically coupled to the actuator and to the locking unit, wherein the force transmission unit (47, 48, 50, 52) comprises a threaded spindle, i. a switchable actuator, ii. a locking element, iii. a force transmission unit (47, 48, 50, 52), which is mechanically coupled to the actuator and to the locking unit, wherein the force transmission unit (47, 48, 50, 52) comprises a threaded spindle,
An air jet loom with a control device, wherein the air jet loom injects compressed air through a nozzle (140, 141, 142, 160) in accordance with opening or closing of an electromagnetic valve (145, 146, 163) to thereby control traveling of a weft yarn, the control device comprising: a control unit configured to supply, to the electromagnetic valve, an overexcitation voltage that determines a rise characteristic of an injection pressure of the nozzle while the electromagnetic valve is opening and the injection pressure of the nozzle rising, and to supply, to the electromagnetic valve, a holding voltage for keeping the electromagnetic valve open after the rising of the injection pressure of the nozzle is completed; and characterized in that the control device further comprises a pressure detection unit configured to detect a pressure of the compressed air that has passed through the electromagnetic valve, and in that the control unit adjusts the overexcitation voltage based on a detection result by the pressure detection unit. a control unit configured to supply, to the electromagnetic valve, an overexcitation voltage that determines a rise characteristic of an injection pressure of the nozzle while the electromagnetic valve is opening and the injection pressure of the nozzle rising, and to supply, to the electromagnetic valve, a holding voltage for keeping the electromagnetic valve open after the rising of the injection pressure of the nozzle is completed; and characterized in that the control device further comprises a pressure detection unit configured to detect a pressure of the compressed air that has passed through the electromagnetic valve, and in that the control unit adjusts the overexcitation voltage based on a detection result by the pressure detection unit.
A computer-implemented method, comprising: collecting a group of historical data relating to operation of an industrial asset on timed interval: determining whether the collected group of historical data corresponds to a transitory period of the industrial asset, wherein: upon the collected group of historical data corresponding to the transitory period, reading a full set of sensor values and making the full set of sensor values available to an analytics engine; when the collected group of historical data does not correspond to the transitory period, reading and storing a minimal subset of sensor values necessary to detect a start or an end of the transitory period; characterised by: determining whether the full set of sensor values corresponds to the end of the transitory period; wherein upon determining the full set of sensor values corresponds to the end of the transitory period, switching to reading a minimal subset of sensor values and storing the minimal subset of sensor values necessary to detect the start or the end of a subsequent transitory period. upon the collected group of historical data corresponding to the transitory period, reading a full set of sensor values and making the full set of sensor values available to an analytics engine; when the collected group of historical data does not correspond to the transitory period, reading and storing a minimal subset of sensor values necessary to detect a start or an end of the transitory period; characterised by: determining whether the full set of sensor values corresponds to the end of the transitory period; wherein upon determining the full set of sensor values corresponds to the end of the transitory period, switching to reading a minimal subset of sensor values and storing the minimal subset of sensor values necessary to detect the start or the end of a subsequent transitory period. determining whether the full set of sensor values corresponds to the end of the transitory period; wherein upon determining the full set of sensor values corresponds to the end of the transitory period, switching to reading a minimal subset of sensor values and storing the minimal subset of sensor values necessary to detect the start or the end of a subsequent transitory period.
A stern tube sealing device (100; 300) which is adapted to seal an outer periphery of a propeller shaft in a marine vessel, said stern tube sealing device (100; 300) comprising: a seal housing through which said propeller shaft is inserted; a first seal ring that is arranged in a first seal ring chamber formed in said seal housing, and has a sealing surface which slides with respect to a wall surface of said first seal ring chamber, or an outer peripheral surface of said propeller shaft; and a second seal ring that is arranged in a second seal ring chamber formed in said seal housing at an inboard side of said first seal ring chamber, and has a sealing surface which slides with respect to a wall surface of said second seal ring chamber, or the outer peripheral surface of said propeller shaft; wherein said first seal ring chamber is in communication with an outside of the marine vessel, and said first seal ring chamber and said second seal ring chamber are in communication with each other through sliding portions between the wall surface of said first seal ring chamber or the outer peripheral surface of said propeller shaft and the sealing surface of said first seal ring; wherein outboard water is filled into said first seal ring chamber; characterized in that clear water is sealingly enclosed in said second seal ring chamber; and the pressure of the clear water in said second seal ring chamber is lower than the pressure of the water in said first seal ring chamber. a seal housing through which said propeller shaft is inserted; a first seal ring that is arranged in a first seal ring chamber formed in said seal housing, and has a sealing surface which slides with respect to a wall surface of said first seal ring chamber, or an outer peripheral surface of said propeller shaft; and a second seal ring that is arranged in a second seal ring chamber formed in said seal housing at an inboard side of said first seal ring chamber, and has a sealing surface which slides with respect to a wall surface of said second seal ring chamber, or the outer peripheral surface of said propeller shaft; wherein said first seal ring chamber is in communication with an outside of the marine vessel, and said first seal ring chamber and said second seal ring chamber are in communication with each other through sliding portions between the wall surface of said first seal ring chamber or the outer peripheral surface of said propeller shaft and the sealing surface of said first seal ring; wherein outboard water is filled into said first seal ring chamber; characterized in that clear water is sealingly enclosed in said second seal ring chamber; and the pressure of the clear water in said second seal ring chamber is lower than the pressure of the water in said first seal ring chamber.
Sleeving device for arranging a sleeve around a product, such as a container, comprising a frame, a foil feeding unit for feeding foil, a mandrel for opening the foil suspended in the frame, the mandrel having a substantially tubular outer surface around which the foil is fed, a cutting unit (10, 24) for cutting a sleeve from the foil and a sleeve discharging unit (9, 19) for arranging a sleeve around a container, characterized in that the sleeving device further comprises an inside sleeves electrical discharge unit which comprises: • a static charge collector (28, 150) arranged on the mandrel to collect static electrical charge from the inside of the foil/sleeve and comprising electrically conductive material arranged along a least a part of a circumferential surface of the mandrel, and • an electrical discharger mounted on the frame at a short distance from the static charge collector for discharging the static charge collector and connected to the earth. • a static charge collector (28, 150) arranged on the mandrel to collect static electrical charge from the inside of the foil/sleeve and comprising electrically conductive material arranged along a least a part of a circumferential surface of the mandrel, and • an electrical discharger mounted on the frame at a short distance from the static charge collector for discharging the static charge collector and connected to the earth.
Valve train for gas exchange valves in an internal combustion engine, comprising at least one main camshaft, at least one cam carrier which is axially displaceable on the main camshaft and comprises at least one cam group having at least three cams which have different cam profiles, devices for axially displacing the cam carrier on the main camshaft into a number, corresponding to the number of cams in the cam group, of separate displacement positions, and a locking device comprising a spring-loaded ball for locking the cam carrier in the separate displacement positions, characterised in that the main camshaft is mounted in fixed rotary bearings on either side of the cam carrier, and in that the spring-loaded ball of the locking device is arranged in a recess in the main camshaft and presses the cam carrier against a fixed axial stop (3, 18) in two outer displacement positions.