mhurhangee/ep-ind-claims huggingface dataset:
A data processing method, the method performed by a transmitter, the method comprising: generating first data, wherein generating the first data comprises one of: performing differential encoding on second data to generate third data, and performing spreading or modulation processing on the third data by using a sequence to generate the first data; performing spreading or modulation processing on the second data by using a sequence to generate fourth data, and performing differential encoding on the fourth data to generate the first data; and performing spreading or modulation processing on the second data by using a sequence to generate the first data; wherein the second data comprises data information, and the data information comprises: data bits, or one or more data symbols generated by performing encoding and modulation on data bits, wherein the data bits comprise user identity information, sequence information and reference signal information. performing differential encoding on second data to generate third data, and performing spreading or modulation processing on the third data by using a sequence to generate the first data; performing spreading or modulation processing on the second data by using a sequence to generate fourth data, and performing differential encoding on the fourth data to generate the first data; and performing spreading or modulation processing on the second data by using a sequence to generate the first data; wherein the second data comprises data information, and the data information comprises: data bits, or one or more data symbols generated by performing encoding and modulation on data bits, wherein the data bits comprise user identity information, sequence information and reference signal information.
An injector for launching a lancet to provide a pricking, the injector comprising: a plunger capable of launching the lancet in a pricking direction, the lancet being in attachment to the plunger; an injector housing which surrounds the plunger; and an injector cap capable of being attached and detached with respect to the injector housing, wherein the injector cap has a first raised portion at an inner face of the cap, characterized by that the injector housing has a pair of banks in an outer face of the housing, and also a second raised portion at a groove region provided inside the banks (250a, 250b). a plunger capable of launching the lancet in a pricking direction, the lancet being in attachment to the plunger; an injector housing which surrounds the plunger; and an injector cap capable of being attached and detached with respect to the injector housing, wherein the injector cap has a first raised portion at an inner face of the cap, characterized by that
A solid-fuel burning and drying unit capable of carbonized drying and burning of toxic gases, comprising a main body, a fuel cell configured in a combustion zone of said main body; a barrier surface which separates the combustion zone from an upper hot zone of the main body and enables combustion of toxic and volatile gases in the combustion zone without mixing with the atmosphere; flue gas cavities provided in the barrier surface providing an outlet of flue gas from the combustion zone towards the outer wall of the upper, hot zone; fuel supply elements and fuel discharge pipe (19.2) that deliver fuel to be burned into the fuel cell; a drying unit contained in said main body and comprising a coil rotated by a motor reducer; wherein the damp fuel is dried in said drying unit by heat from the combustion zone and by frictional heat generated by rotating said coil through the fuel by means of said motor reducer. a main body, a fuel cell configured in a combustion zone of said main body; a barrier surface which separates the combustion zone from an upper hot zone of the main body and enables combustion of toxic and volatile gases in the combustion zone without mixing with the atmosphere; flue gas cavities provided in the barrier surface providing an outlet of flue gas from the combustion zone towards the outer wall of the upper, hot zone; fuel supply elements and fuel discharge pipe (19.2) that deliver fuel to be burned into the fuel cell; a drying unit contained in said main body and comprising a coil rotated by a motor reducer; wherein the damp fuel is dried in said drying unit by heat from the combustion zone and by frictional heat generated by rotating said coil through the fuel by means of said motor reducer.
A transport trailer for carrying an oversize load, the transport trailer comprising: a trailer comprising an elongated body that extends in a length direction and that has an upper base surface; a support assembly that is configured to support the oversize load and that is pivotably coupled to the trailer to move between a first position and a second position, wherein in the first position, the support assembly extends over the upper base surface and beyond the trailer in a width direction that is transverse to the length direction to define a wide load overhang that extends beyond the trailer in the width direction, and wherein in the second position, the support assembly is positioned at an incline relative to the first position to one of reduce and eliminate the wide load overhang, characterized in that the support assembly comprises a box that is configured to receive the oversize load when the support assembly is in the first position and to contain the oversize load for transport when the support assembly is in the second position. a trailer comprising an elongated body that extends in a length direction and that has an upper base surface; a support assembly that is configured to support the oversize load and that is pivotably coupled to the trailer to move between a first position and a second position, wherein in the first position, the support assembly extends over the upper base surface and beyond the trailer in a width direction that is transverse to the length direction to define a wide load overhang that extends beyond the trailer in the width direction, and wherein in the second position, the support assembly is positioned at an incline relative to the first position to one of reduce and eliminate the wide load overhang, characterized in that the support assembly comprises a box that is configured to receive the oversize load when the support assembly is in the first position and to contain the oversize load for transport when the support assembly is in the second position.
Method for determining the position of a rotor of a machine, the rotor being equipped with at least one excitation winding, the excitation winding being connected to a chopper, the machine including n stator windings, n being an integer, the rotor being magnetically coupled to each of the n stator windings of the machine, this machine being connected to a driving device able to drive it in a full-wave or pulse-width-modulation mode, characterized in that the method includes the following steps: - inhibiting the driving device; - applying an excitation voltage that varies over time to the rotor, by means of the chopper; - measuring an electromotive force (e 1, e 2 or... e n) induced in each of the stator windings; - determining a position of the rotor when it has stopped or is moving at low speed, via at least one operation of comparing the induced electromotive forces and at least one operation of comparing an induced electromotive force and a common reference; and - implementing commands of the driving device, depending on the determined position of the rotor. - inhibiting the driving device; - applying an excitation voltage that varies over time to the rotor, by means of the chopper; - measuring an electromotive force (e 1, e 2 or... e n) induced in each of the stator windings; - determining a position of the rotor when it has stopped or is moving at low speed, via at least one operation of comparing the induced electromotive forces and at least one operation of comparing an induced electromotive force and a common reference; and - implementing commands of the driving device, depending on the determined position of the rotor.
A gastroretentive dosage form comprising an immediate release portion and an extended release portion, wherein the immediate release portion comprises an immediate release drug layer containing pyridostigmine bromide, wherein the extended release portion comprises a core and a permeable elastic membrane surrounding the core, wherein the core comprises pyridostigmine bromide, an acid, a gas-generating agent, and a water-soluble hydrophilic polymer that swells via imbibition of gastric fluid, wherein the permeable elastic membrane comprises a plasticizer and a copolymer based on ethyl acrylate, methyl methacrylate, and trimethylammonioethyl methacrylate chloride, and wherein the dosage form provides an extended release, with reduced initial burst release, of pyridostigmine bromide, for at least about 14 hours.
An arrangement of a mounting plate cover on a front mounting plate of a vehicle, in particular a commercial vehicle, having a front mounting plate for mounting accessory equipment as required, and having a mounting plate cover which can be fastened releasably thereto as front-side protective covering, characterized in that the mounting plate cover is held releasably on the front mounting plate by means of at least one magnetic connection.
A process for producing hot-rolled steel strip with a tensile strength of between 760 and 940 MPa and a hole expansion ratio of at least 50%, the steel having a final microstructure comprising ferrite, bainite and at least 3% of martensite, wherein the total volume of the ferrite phase and the bainite phase is not smaller than 80%, wherein the martensite is distributed within the bainite phase, optionally also tempered martensite, retained austenite and/or fine carbides having an average diameter of not larger than 30 nm, and wherein the microstructure does not contain pearlite and/or coarse Fe 3 C, the steel consisting of, in weight%: • 0.07 to 0.15% C • 0.65 to 1.30% Mn • 0.6 to 1.4% Cr • 0.005 to 0.35% Si • 0.03% P or less • up to 0.05% S • up to 0.001% B • 0.07 to 0.2% Ti • 0.003 to 0.6% Al • up to 0.01%N • Optionally calcium in an amount consistent with a calcium treatment for MnS inclusion control or REM in an amount consistent with a treatment for MnS inclusion control; • remainder iron and inevitable impurities associated with the steelmaking process; the process comprising: • providing a steel slab or thick strip of said composition, optionally calcium treated, by: ∘ continuous casting, or ∘ by thin slab casting, or ∘ by belt casting, or ∘ by strip casting; • optionally followed by reheating the steel slab or strip at a reheating temperature of at most 1300°C; • hot rolling the slab or thick strip and finishing the hot-rolling process at a hot rolling finishing temperature above Ar 3 so that the steel is still austenitic during the last hot-rolling pass; • cooling the hot rolled strip by means of continuous cooling or interrupted cooling at a cooling rate of at least 20°C/s to a coiling temperature of between Ms and Bs. • 0.07 to 0.15% C • 0.65 to 1.30% Mn • 0.6 to 1.4% Cr • 0.005 to 0.35% Si • 0.03% P or less • up to 0.05% S • up to 0.001% B • 0.07 to 0.2% Ti • 0.003 to 0.6% Al • up to 0.01%N • Optionally calcium in an amount consistent with a calcium treatment for MnS inclusion control or REM in an amount consistent with a treatment for MnS inclusion control; • remainder iron and inevitable impurities associated with the steelmaking process; • providing a steel slab or thick strip of said composition, optionally calcium treated, by: ∘ continuous casting, or ∘ by thin slab casting, or ∘ by belt casting, or ∘ by strip casting; ∘ continuous casting, or ∘ by thin slab casting, or ∘ by belt casting, or ∘ by strip casting; • optionally followed by reheating the steel slab or strip at a reheating temperature of at most 1300°C; • hot rolling the slab or thick strip and finishing the hot-rolling process at a hot rolling finishing temperature above Ar 3 so that the steel is still austenitic during the last hot-rolling pass; • cooling the hot rolled strip by means of continuous cooling or interrupted cooling at a cooling rate of at least 20°C/s to a coiling temperature of between Ms and Bs.
Wing for a rotary vane pump, in particular for a vacuum pump, whereby the wing can be guided by a rotor in a pump space around a rotating axis and in a lengthwise direction in the rotor perpendicular to the rotating axis, with a top side and bottom side for attaching to the base and roof of the pump space, with a front side as well as a back side opposite the front side for demarcating pressure chambers, with at least one face side for the gliding attachment on a cover-side inner wall of the pump space, whereby the wing has a base body with two fastening sections consisting of an initial plastic material and a form-locking wing end on each fastening section that forms the respective face side made from a second plastic material, such that the respective fastening section is covered by the respective wing end, distinguished by the fact that the respective fastening section has at least one recess (36, 38, 40, 42) that runs perpendicular in a cross-wise fashion to the front and back side (16, 18), whereby the recesses, viewed lengthwise, have indentations, and whereby the recesses (36, 38) are situated in the middle segment of the respective fastening section.
A method in an interface node (140, 150) for protecting an Ethernet ring from a superloop going through the Ethernet ring, wherein the Ethernet ring comprises a pair of interface nodes (140, 150) between the Ethernet ring and a Virtual Private Local area network Service, VPLS,-domain, the method comprising the steps of: - receiving in the interface node (140, 150) a priority message indicating a priority level for each Ethernet ring (120, 130) connected to the VPLS-domain, wherein the priority messages are periodically transmitted in the VPLS-domain; - receiving in the interface node (140, 150) a withdrawal message intended to indicate that the other interface node (140, 150) is malfunctioning; and - transmitting from the interface node (140, 150) a signal failure message to the Ethernet ring in a case any other Ethernet rings has a lower priority level than said Ethernet ring. - receiving in the interface node (140, 150) a priority message indicating a priority level for each Ethernet ring (120, 130) connected to the VPLS-domain, wherein the priority messages are periodically transmitted in the VPLS-domain; - receiving in the interface node (140, 150) a withdrawal message intended to indicate that the other interface node (140, 150) is malfunctioning; and - transmitting from the interface node (140, 150) a signal failure message to the Ethernet ring in a case any other Ethernet rings has a lower priority level than said Ethernet ring.
Aircraft rotor comprising: a rotor blade having a longitudinal length with opposite proximal and distal ends, and a lateral width between opposite leading and trailing edges, and a recess formed in the rotor blade adjacent the rotor blade trailing edge; and a balancing weight (92,92') attached to the rotor blade at a position that is intermediate the rotor blade proximal and distal ends and is adjacent the rotor blade trailing edge, the balancing weight (92, 92') being attached to the rotor blade in the recess, characterised in that: the rotor blade recess has an aerodynamic shape with the recess being longitudinally narrow toward the rotor blade leading edge and the recess being wider toward the rotor blade trailing edge. a rotor blade having a longitudinal length with opposite proximal and distal ends, and a lateral width between opposite leading and trailing edges, and a recess formed in the rotor blade adjacent the rotor blade trailing edge; and a balancing weight (92,92') attached to the rotor blade at a position that is intermediate the rotor blade proximal and distal ends and is adjacent the rotor blade trailing edge, the balancing weight (92, 92') being attached to the rotor blade in the recess, characterised in that: the rotor blade recess has an aerodynamic shape with the recess being longitudinally narrow toward the rotor blade leading edge and the recess being wider toward the rotor blade trailing edge. the rotor blade recess has an aerodynamic shape with the recess being longitudinally narrow toward the rotor blade leading edge and the recess being wider toward the rotor blade trailing edge.
A method of quantifying white spot lesions on a tooth comprising quantifying the grayscale difference between the white spot lesions and the surrounding healthy enamel in the blue channel of a digital color photographic image of the tooth; wherein the method comprises: a) drying the tooth to be evaluated; b) obtaining a digital color photographic image of the tooth; and c) measuring the difference between the grayscale value of at least one pixel in an area of the image depicting at least a portion of the white spot and the grayscale value of at least one pixel in an area of the image depicting at least a portion of the adjacent healthy enamel, wherein the greyscale values are measured only in the blue channel of the image. a) drying the tooth to be evaluated; b) obtaining a digital color photographic image of the tooth; and c) measuring the difference between the grayscale value of at least one pixel in an area of the image depicting at least a portion of the white spot and the grayscale value of at least one pixel in an area of the image depicting at least a portion of the adjacent healthy enamel, wherein the greyscale values are measured only in the blue channel of the image.
A nonvolatile storage device, comprising: a magnetic memory element; and a rectifying element, connected in series to the magnetic memory element; wherein the magnetic memory element has a spin valve structure comprising a free layer having a thickness defined by a first face and a second face and exhibiting ferromagnetism, a first nonmagnetic layer positioned with one face opposing the first face, and a pinned layer sandwiching the first nonmagnetic layer together with the free layer and exhibiting ferromagnetism, and in which the spin valve structure is caused to store information by applying an electric pulse, the magnetic memory element further comprising: a second nonmagnetic layer positioned on the side of the second face of the free layer; and a magnetic change layer sandwiching the second nonmagnetic layer together with the free layer, and comprising a magnetic material the magnetic characteristics of which change according to temperature, wherein the magnetic material of the magnetic change layer is configured so that the change in the magnetic characteristics induces a precession movement of the free layer magnetization. a magnetic memory element; and a rectifying element, connected in series to the magnetic memory element; wherein the magnetic memory element has a spin valve structure comprising a free layer having a thickness defined by a first face and a second face and exhibiting ferromagnetism, a first nonmagnetic layer positioned with one face opposing the first face, and a pinned layer sandwiching the first nonmagnetic layer together with the free layer and exhibiting ferromagnetism, and in which the spin valve structure is caused to store information by applying an electric pulse, the magnetic memory element further comprising: a second nonmagnetic layer positioned on the side of the second face of the free layer; and a magnetic change layer sandwiching the second nonmagnetic layer together with the free layer, and comprising a magnetic material the magnetic characteristics of which change according to temperature, wherein the magnetic material of the magnetic change layer is configured so that the change in the magnetic characteristics induces a precession movement of the free layer magnetization. a second nonmagnetic layer positioned on the side of the second face of the free layer; and a magnetic change layer sandwiching the second nonmagnetic layer together with the free layer, and comprising a magnetic material the magnetic characteristics of which change according to temperature, wherein the magnetic material of the magnetic change layer is configured so that the change in the magnetic characteristics induces a precession movement of the free layer magnetization.
A suction nozzle for a fan with a suction opening for suctioning a valve main flow, characterized in that the suction nozzle comprises an opening edge section which adjoins the suction opening and has at least one local outbreak, wherein, in the outbreak of the opening edge section, a flow insert can be fastened detachably, which forms a bypass leading to the suction opening for a bypass flow leading to the fan main flow, and wherein, in the bypass, measuring means for the volume flow determination of the valve main flow are arranged.
A face mask to cover a user's nose and at least partially cover a user's mouth and configured to deliver oxygen to a user and provide fluid communication with an external conduit, the face mask comprising: a reservoir for containing a pocket of gas; an oxygen inlet port for delivering oxygen to the reservoir; first and second lateral sampling ports (12, 14) on opposing sides of a midline of the face mask, the two lateral sampling ports located above the oxygen inlet port and configured to sample gas from the reservoir; first and second vents (16, 18) on opposing sides of the midline of the face mask and configured to release gas from inside to outside the mask, the first lateral sampling port located near the first vent to allow sampling of exhaled gas as gas is moved past the first lateral sampling port, the second lateral sampling port located near the second vent to allow sampling of exhaled gas as gas is moved past the second lateral sampling port; and a mating part on each of the first and second lateral sampling ports that is configured to enable connection of the respective lateral sampling port to the external conduit. a reservoir for containing a pocket of gas; an oxygen inlet port for delivering oxygen to the reservoir; first and second lateral sampling ports (12, 14) on opposing sides of a midline of the face mask, the two lateral sampling ports located above the oxygen inlet port and configured to sample gas from the reservoir; first and second vents (16, 18) on opposing sides of the midline of the face mask and configured to release gas from inside to outside the mask, the first lateral sampling port located near the first vent to allow sampling of exhaled gas as gas is moved past the first lateral sampling port, the second lateral sampling port located near the second vent to allow sampling of exhaled gas as gas is moved past the second lateral sampling port; and a mating part on each of the first and second lateral sampling ports that is configured to enable connection of the respective lateral sampling port to the external conduit.