mhurhangee/ep-ind-claims huggingface dataset:
Method for operating an electric tool (100, 1100), wherein the electric tool (100, 1100) has a sensor (120, 1120, 2120) which is embodied as an acceleration sensor or rotational speed sensor, characterized in that in the method for operating an electric tool it is checked whether the sensor (120, 1120, 2120) or a transmission path (125, 1125, 2125) between the sensor (120, 1120, 2120) and an evaluation circuit (110, 1110) have a fault.
Use of a poultry feed additive composition which is a flowable mixture of phytogenic compounds comprising at least a. an oil component which is microencapsulated essential thyme oil, and b. a saponin component which is saponin containing particulate dried Quillaja bark powder, which mixture contains at least 0.5% saponin component (w/w), and the oil component in an effective ratio of at least 0.2:1 (w/w, oil component per saponin component), for improving the feed conversion efficiency in antibiotic-free poultry production. a. an oil component which is microencapsulated essential thyme oil, and b. a saponin component which is saponin containing particulate dried Quillaja bark powder,
One-piece penetrator, preferably with a caliber of less than 40 mm, for armor-piercing ammunition, comprising a nose-sided, in particular ogival, sacrificial section and an adjoining penetration core, a circumferential depression being formed at the transition between the sacrificial section and the penetration core and/or on the penetration core, which has two opposing recess flanks (23, 25) and a recess base connecting the recess flanks (23, 25), at least one profiled step (29, 31) being provided on the recess base, the recess being realized as a tapered notch characterized in that the recess has a sharp-edged notch base with a radius of less than 0.8 mm.
An azimuth estimation method, the method comprising: obtaining, by a terminal device, multi-channel sampling signals and buffering the multi-channel sampling signals; performing, by the terminal device, wakeup word detection on one or more sampling signals of the multi-channel sampling signals, and determining a wakeup word detection score for each channel of the one or more sampling signals; performing a spatial spectrum estimation on the buffered multi-channel sampling signals to obtain a spatial spectrum estimation result, when the wakeup word detection scores of the one or more sampling signal indicates that a wakeup word exists in the one or more sampling signals, the wakeup word being comprised in a target voice; and determining, by the terminal device, an azimuth of the target voice according to the spatial spectrum estimation result and a highest wakeup word detection score. obtaining, by a terminal device, multi-channel sampling signals and buffering the multi-channel sampling signals; performing, by the terminal device, wakeup word detection on one or more sampling signals of the multi-channel sampling signals, and determining a wakeup word detection score for each channel of the one or more sampling signals; performing a spatial spectrum estimation on the buffered multi-channel sampling signals to obtain a spatial spectrum estimation result, when the wakeup word detection scores of the one or more sampling signal indicates that a wakeup word exists in the one or more sampling signals, the wakeup word being comprised in a target voice; and determining, by the terminal device, an azimuth of the target voice according to the spatial spectrum estimation result and a highest wakeup word detection score.
Box body of a commercial vehicle, in particular of a lorry, trailer or semitrailer, having a wall panel and a transport cooling machine, wherein the wall panel has an assembly opening to receive the transport cooling machine, wherein the transport cooling machine is arranged in sections in the assembly opening and wherein at least one seal is provided in the assembly opening between the wall panel and the transport cooling machine, characterised in that the seal (20, 34, 40, 50, 60, 70, 80, 101, 102, 104, 106) comprises at least one foamed plastic and that the seal has at least one seal chamber which is outwardly at least substantially closed and is filled with a foamed plastic and/or has at least one retaining profile (31, 42, 51, 62, 71) which maintains the foamed plastic under compression in a direction perpendicular to the wall panel.
A method for determining a magnetic vector field in a predetermined area, said method comprising: - determining distribution data comprising values of a first of three components of a magnetic field along a first direction, for a predetermined area defined on a predetermined surface, said predetermined surface being defined by a second and a third direction, wherein said first, second and third directions constitute an orthogonal set of axes; - determining distribution data comprising values of the second and the third component of said magnetic field in said second and said third direction respectively, for said predetermined area defined in said predetermined surface; characterized in that determining distribution data comprising values of the second and the third component is based on making use of intrinsic physical relations between the first, second and third components of said magnetic field distribution; and wherein determining distribution data of said second and third components comprises performing a Fourier transformation, followed by performing calculations based on intrinsic physical relationships between the magnetic field components, followed by an inverse Fourier transformation - determining distribution data comprising values of a first of three components of a magnetic field along a first direction, for a predetermined area defined on a predetermined surface, said predetermined surface being defined by a second and a third direction, wherein said first, second and third directions constitute an orthogonal set of axes; - determining distribution data comprising values of the second and the third component of said magnetic field in said second and said third direction respectively, for said predetermined area defined in said predetermined surface;
Central actuator (10, 10', 10"), in particular for a solenoid valve of an oscillating motor camshaft adjuster, comprising a housing which encloses the central actuator (10, 10', 10"), a pole tube and a pole core which are arranged within at least one coil which generates a magnetic field, and an actuating tappet (20, 20', 20") which is arranged on an armature (28, 28', 28") which is configured such that it can be displaced in the axial direction in an armature space, a termination element for closing the armature space being provided, which termination element comprises at least one pole core insert, with a central bore, and a bearing bush which is arranged in the central bore of the pole core insert, the actuating tappet (20, 20', 20") being arranged axially displaceably in the bearing bush, the termination element comprising, furthermore, a termination cover, characterized in that the termination element is provided as a unit which can be preassembled, the termination cover having a central bore, in which the bearing bush is arranged, and the bearing bush being produced by way of a plastic injection moulding method, the termination cover and the pole core insert being provided as insert parts which are provided such that they are encapsulated by the material of the bearing bush in the region of the central bores (24, 43).
Washing machine with a device for irradiation with UV light, said device having: - a fluid passage for receiving fluid and/or flowing through of fluid, - at least one UV light source which is arranged completely within the fluid passage, - an energy source for the at least one UV light source, the energy source being arranged completely outside the fluid passage, - energy transfer means (18, 22, 118, 122, 219) for a wireless and contactless transmission of energy from the energy source to the at least one UV light source, wherein the fluid passage is a receptacle housing for a drum of the washing machine, the drum being configured to rotate in the receptacle housing and the receptacle housing being not rotatable, at least a part of the energy transfer means being arranged on the outside of the receptacle housing, and the at least one UV light source being arranged in the receptacle housing, wherein - only one energy source is provided both for the UV light source and for a drive motor for the drum of the washing machine, - the energy source comprises a power controller or a converter, and characterized in that: - the energy transfer means comprise a microwave device outside of the fluid passage with at least one microwave generator and at least one microwave antenna, the UV light source being an electrodeless microwave lamp, or - the energy transfer means comprise an induction device (18, 118) outside of the fluid passage (11, 111) with at least one induction generator and with at least one external induction coil, the UV light source (25, 125) being an inductively coupled induction lamp. - a fluid passage for receiving fluid and/or flowing through of fluid, - at least one UV light source which is arranged completely within the fluid passage, - an energy source for the at least one UV light source, the energy source being arranged completely outside the fluid passage, - energy transfer means (18, 22, 118, 122, 219) for a wireless and contactless transmission of energy from the energy source to the at least one UV light source, wherein the fluid passage is a receptacle housing for a drum of the washing machine, the drum being configured to rotate in the receptacle housing and the receptacle housing being not rotatable, at least a part of the energy transfer means being arranged on the outside of the receptacle housing, and the at least one UV light source being arranged in the receptacle housing, - only one energy source is provided both for the UV light source and for a drive motor for the drum of the washing machine, - the energy source comprises a power controller or a converter, and - the energy transfer means comprise a microwave device outside of the fluid passage with at least one microwave generator and at least one microwave antenna, the UV light source being an electrodeless microwave lamp, or - the energy transfer means comprise an induction device (18, 118) outside of the fluid passage (11, 111) with at least one induction generator and with at least one external induction coil, the UV light source (25, 125) being an inductively coupled induction lamp.
A method to output a pose of a textureless object, the method comprising: obtaining, by a processing device, a single image of the textureless object, wherein the single image indicates the pose of the textureless object; generating, by the processing device, a three dimensional model of the textureless object from a plurality of viewpoints and a plurality of scales captured at each one of the plurality of viewpoints, the plurality of viewpoints and the plurality of scales obtained from image data of the textureless object; matching, by the processing device, the single image with a plurality of discretized renders of the three dimensional model via a multi-level illumination invariant tree structure to obtain an alignment of the single image with the discretized render, the multi-level illumination invariant tree structure being a tree structure having a plurality of levels, each of the plurality of levels representing patches extracted from each of the plurality of discretized renders; and outputting, by the processing device, the pose of the textureless object based on the alignment. obtaining, by a processing device, a single image of the textureless object, wherein the single image indicates the pose of the textureless object; generating, by the processing device, a three dimensional model of the textureless object from a plurality of viewpoints and a plurality of scales captured at each one of the plurality of viewpoints, the plurality of viewpoints and the plurality of scales obtained from image data of the textureless object; matching, by the processing device, the single image with a plurality of discretized renders of the three dimensional model via a multi-level illumination invariant tree structure to obtain an alignment of the single image with the discretized render, the multi-level illumination invariant tree structure being a tree structure having a plurality of levels, each of the plurality of levels representing patches extracted from each of the plurality of discretized renders; and outputting, by the processing device, the pose of the textureless object based on the alignment.
Household refrigeration device, having a refrigeration compartment, at least one shelf mounted in the refrigeration compartment, and an inner container delimiting the refrigeration compartment and having a rear wall and opposing side walls (3a, 3b), each of said side walls (3a, 3b) having, for the formation of at least one pair of opposing support means, at least one of the support means in each case, wherein the opposing support means are designed to mount the shelf in the refrigeration compartment with two opposing, lateral edge sections (6a, 6b) of the shelf lying on the support means and with a trailing edge of the shelf facing the rear wall of the inner container, characterised in that the shelf has two edge termination parts (8a, 8b) each extending separately from one another in the region of the two lateral edge sections (6a, 6b) of the shelf and clipped onto its trailing edge, and in that the lateral edges of the shelf are free of any edge termination parts.
A cable tray assembly for installing one or more cable harnesses (14, 16, 18) in a rail vehicle body, comprising a main tray having at least a first cable channel extending in a longitudinal direction of the cable tray assembly and a second cable channel at a distance from and parallel to the first cable channel, wherein the first cable channel has a flat bottom and at least one side wall extending parallel to the longitudinal axis, the second cable channel has a flat bottom and at least one side wall extending parallel to the longitudinal axis, and the cable tray assembly further comprises an auxiliary tray (44, 144) provided with an auxiliary tray plate (46, 146) for holding one or more pieces of electrical equipment (20, 120), the auxiliary tray plate (46, 146) facing the main tray at a distance from the main tray and legs (50, 150) extending from the auxiliary tray plate (46, 146) towards the main tray, the legs (50, 150) being attached to attachment portions of the main tray in a releasable manner, characterised in that the main tray has plastically deformable bridges connecting the first channel and second channel, the bridges being bent, so that the flat bottom of the first channel and the flat bottom of the second channel are in different planes.
Method for recovery of energy in an aircraft fitted with a passenger cabin having an air flow regulated in terms of pressure and temperature using an ECS air conditioning system powered by a load compressor, and auxiliary power generation, characterised in that it consists in providing that: - when the aircraft is on the ground, known as "ground" mode, the thermal energy dissipated by auxiliary power generation is recovered by heat exchange in its exhaust so as to power the cycle of a recovery turbocharger in order to produce mechanical energy in addition to auxiliary power generation; - when the aircraft is at altitude, known as "altitude" mode, in which the cabin air is pressurised to a sufficient level, said turbocharger, driven at least partly by the air recovered as it leaves the cabin and then heated by heat exchange in the exhaust, produces compression in addition to that of the load compressor, so as to provide the compression rate required to power the ECS. - when the aircraft is on the ground, known as "ground" mode, the thermal energy dissipated by auxiliary power generation is recovered by heat exchange in its exhaust so as to power the cycle of a recovery turbocharger in order to produce mechanical energy in addition to auxiliary power generation; - when the aircraft is at altitude, known as "altitude" mode, in which the cabin air is pressurised to a sufficient level, said turbocharger, driven at least partly by the air recovered as it leaves the cabin and then heated by heat exchange in the exhaust, produces compression in addition to that of the load compressor, so as to provide the compression rate required to power the ECS.
A gas turbine system comprising: a gas turbine having a compressor section, a turbine section and a combustor section disposed downstream from the compressor section and upstream from the turbine section, the combustor section in fluid communication with a fuel supply via a fuel supply line; a water circuit fluidly coupled to and extending between a first feed water supply line and a return water line, the water circuit comprising a first water lin, extending between the first feed water supply line and the return water line; an extraction-air line extending between an inlet port on the compressor section and an outlet port; a first heat exchanger thermally coupling the first water line to the extraction-air line for transferring heat from a flow of extraction-air within the extraction-air line to a flow of water within the water circuit; and a second heat exchanger thermally coupling the first water line to the fuel supply line for transferring heat from the flow of water within the water circuit to a flow of fuel within the fuel supply line, characterized in that the second heat exchanger is disposed immediately downstream from the first heat exchanger with respect to the flow water within the water circuit such that the water from the first heat exchanger enters the second heat exchanger. a gas turbine having a compressor section, a turbine section and a combustor section disposed downstream from the compressor section and upstream from the turbine section, the combustor section in fluid communication with a fuel supply via a fuel supply line; a water circuit fluidly coupled to and extending between a first feed water supply line and a return water line, the water circuit comprising a first water lin, extending between the first feed water supply line and the return water line; an extraction-air line extending between an inlet port on the compressor section and an outlet port; a first heat exchanger thermally coupling the first water line to the extraction-air line for transferring heat from a flow of extraction-air within the extraction-air line to a flow of water within the water circuit; and a second heat exchanger thermally coupling the first water line to the fuel supply line for transferring heat from the flow of water within the water circuit to a flow of fuel within the fuel supply line, characterized in that the second heat exchanger is disposed immediately downstream from the first heat exchanger with respect to the flow water within the water circuit such that the water from the first heat exchanger enters the second heat exchanger.
A high load, high temperature compatible bearing assembly comprising: a shaft formed of refractory steel or high temperature alloy; a roller formed of refractory steel or high temperature alloy and receiving the shaft within a bore in the roller; and at least one bearing ring formed of ceramic and disposed between the shaft and the roller, wherein the bearing ring cooperates with the roller to permit the roller to freely rotate around the shaft. a shaft formed of refractory steel or high temperature alloy; a roller formed of refractory steel or high temperature alloy and receiving the shaft within a bore in the roller; and at least one bearing ring formed of ceramic and disposed between the shaft and the roller, wherein the bearing ring cooperates with the roller to permit the roller to freely rotate around the shaft.
An anhydride polymer comprising a biodegradable backbone that comprises one or more groups that will provide morphine upon hydrolysis of the polymer and one or more pendant residues of a non-steroidal anti-inflammatory.
A spacecraft having a satellite bus comprising: a first arm having a first end pivotably coupled to the anti-nadir face of said satellite bus at a first pivot point and a second end; a first motor coupled to the first end of the first arm at the first pivot point; a first gimbaled platform coupled to the second end of the first arm; a first thruster rotatably coupled via the first gimballed platform to the second end of the first arm, the first arm to selectively pivot about the spacecraft to position the first thruster to generate a change in velocity of the spacecraft to maintain the spacecraft within an orbit station; a second arm having a first end pivotably coupled to said anti-nadir face of said satellite bus at a second pivot point and a second end; a second motor coupled to the first end of the second arm at the second pivot point; a second gimbaled platform coupled to the second end of the second arm; a second thruster coupled via the second gimballed platform to said second end of said second arm; said first pivot point is disposed proximate to a first corner of said satellite bus and said second pivot point is disposed proximate to a second corner of said satellite bus, wherein said second corner is diagonal to said first corner; and said first and second arm (304, 306) has a length substantially equal to a length of the anti-nadir face of the satellite bus. a first arm having a first end pivotably coupled to the anti-nadir face of said satellite bus at a first pivot point and a second end; a first motor coupled to the first end of the first arm at the first pivot point; a first gimbaled platform coupled to the second end of the first arm; a first thruster rotatably coupled via the first gimballed platform to the second end of the first arm, the first arm to selectively pivot about the spacecraft to position the first thruster to generate a change in velocity of the spacecraft to maintain the spacecraft within an orbit station; a second arm having a first end pivotably coupled to said anti-nadir face of said satellite bus at a second pivot point and a second end; a second motor coupled to the first end of the second arm at the second pivot point; a second gimbaled platform coupled to the second end of the second arm; a second thruster coupled via the second gimballed platform to said second end of said second arm; said first pivot point is disposed proximate to a first corner of said satellite bus and said second pivot point is disposed proximate to a second corner of said satellite bus, wherein said second corner is diagonal to said first corner; and said first and second arm (304, 306) has a length substantially equal to a length of the anti-nadir face of the satellite bus.
A stent comprising: a wire formed into stent pattern, wherein a cross-section of the wire includes, an outer member having a lumen, a radiopaque member disposed within and filling a first portion of the lumen, and a biologically or pharmacologically active substance disposed in the remaining, second portion of the lumen; and at least one opening disposed through the outer member through to the second portion of the lumen. a wire formed into stent pattern, wherein a cross-section of the wire includes, an outer member having a lumen, a radiopaque member disposed within and filling a first portion of the lumen, and a biologically or pharmacologically active substance disposed in the remaining, second portion of the lumen; and an outer member having a lumen, a radiopaque member disposed within and filling a first portion of the lumen, and a biologically or pharmacologically active substance disposed in the remaining, second portion of the lumen; and at least one opening disposed through the outer member through to the second portion of the lumen.