mhurhangee/ep-ind-claims huggingface dataset:
A microprocessor comprising an instruction pipeline that includes or is associated with: an instruction cache configured to cache instructions for fetching into the instruction pipeline; a branch target cache configured to store branch target information for known branch instructions; a first branch history table configured to store first branch prediction information; a second branch history table configured to store second branch prediction information; and branch control logic configured to predict branch instructions as taken or not taken according to the first branch prediction information for branch instructions that are branch target cache hits prior to decoding the branch instructions, and to predict branch instructions as taken or not taken according to the second branch prediction information for branch instructions that are branch target cache misses; wherein the first branch history table and the branch target cache are configured to be accessible in M cycles of the instruction pipeline; and the second branch history table is configured to be accessible in N cycles of the instruction pipeline, wherein M and N are first and second numbers, with M being smaller than N. an instruction cache configured to cache instructions for fetching into the instruction pipeline; a branch target cache configured to store branch target information for known branch instructions; a first branch history table configured to store first branch prediction information; a second branch history table configured to store second branch prediction information; and branch control logic configured to predict branch instructions as taken or not taken according to the first branch prediction information for branch instructions that are branch target cache hits prior to decoding the branch instructions, and to predict branch instructions as taken or not taken according to the second branch prediction information for branch instructions that are branch target cache misses; wherein the first branch history table and the branch target cache are configured to be accessible in M cycles of the instruction pipeline; and the second branch history table is configured to be accessible in N cycles of the instruction pipeline, wherein M and N are first and second numbers, with M being smaller than N.
A first communication device operating as access point and comprising a wireless communication unit configured to - set first information identifying a basic service set, BSS, of the first communication device, wherein the first information is BSS Color information of the first communication device, - set second information specifying another BSS included in a same extended service set, ESS, wherein the second information is ESS Color mask information expressing the BSS Color information of all the other second communication devices, operating as access points, set in the same ESS by a format of a bit mask for a bitmap indicating the BSS Color information of the first communication device, the ESS Color mask information having the same bit length as the BSS Color information, wherein all pieces of BSS Color information in the ESS can be derived with the bit mask format, and - notify a third communication device, operating as station, of the first information and the second information. - set first information identifying a basic service set, BSS, of the first communication device, wherein the first information is BSS Color information of the first communication device, - set second information specifying another BSS included in a same extended service set, ESS, wherein the second information is ESS Color mask information expressing the BSS Color information of all the other second communication devices, operating as access points, set in the same ESS by a format of a bit mask for a bitmap indicating the BSS Color information of the first communication device, the ESS Color mask information having the same bit length as the BSS Color information, wherein all pieces of BSS Color information in the ESS can be derived with the bit mask format, and - notify a third communication device, operating as station, of the first information and the second information.
A radiation delivery device comprising: a rotatable source component (10, 81, 110) including a plurality of radiation sources (11, 82, 112); a shielding body; and a collimator component for directing radiation from the radiation sources to a common focal area, wherein the collimator component comprises a primary collimator body (30, 83, 300) including one or more sets of primary collimator passages (31,310) for directing the radiation from the radiation sources, wherein the primary collimator body is rotatable to align the radiation sources with the primary collimator passages, wherein the rotatable source component is positioned within an interior cavity of the primary collimator body and is rotatable from a position of the radiation sources facing the shielding body to a position of the radiation sources facing passages (31, 52, 310, 520) of the primary collimator body for directing the radiation emitted by the radiation sources. a rotatable source component (10, 81, 110) including a plurality of radiation sources (11, 82, 112); a shielding body; and a collimator component for directing radiation from the radiation sources to a common focal area, wherein the collimator component comprises a primary collimator body (30, 83, 300) including one or more sets of primary collimator passages (31,310) for directing the radiation from the radiation sources, wherein the primary collimator body is rotatable to align the radiation sources with the primary collimator passages, wherein the rotatable source component is positioned within an interior cavity of the primary collimator body and is rotatable from a position of the radiation sources facing the shielding body to a position of the radiation sources facing passages (31, 52, 310, 520) of the primary collimator body for directing the radiation emitted by the radiation sources.
An actuator system for a reduced-head hard disk drive, HDD,, the system comprising a head-stack assembly, HSA, characterized in that the actuator system further comprises: a ball screw cam assembly, wherein the HSA is translatably coupled with the cam assembly; a multi-phase claw-pole stepper motor disposed within and affixed to a screw of the cam assembly, and configured to drive rotation of the screw to drive translation of the HSA along an axis of the screw; and a fixed shaft around which the stepper motor is positioned; wherein the stepper motor is rotatable about the fixed shaft, the stepper motor comprising: a hollow tubular permanent magnet affixed to an inner diameter of the cam assembly or screw, wherein the tubular permanent magnet is a rotor of the stepper motor, at least one circular coil (320a, 320b) disposed within the tubular permanent magnet, and at least one pair of mated claw-pole structures (321a, 321b) disposed within the tubular permanent magnet and in which the at least one coil (320a, 320b) is disposed, wherein the at least one pair of mated claw-pole structures (321a, 321b) is a stator of the stepper motor. a ball screw cam assembly, wherein the HSA is translatably coupled with the cam assembly; a multi-phase claw-pole stepper motor disposed within and affixed to a screw of the cam assembly, and configured to drive rotation of the screw to drive translation of the HSA along an axis of the screw; and a fixed shaft around which the stepper motor is positioned; wherein the stepper motor is rotatable about the fixed shaft, the stepper motor comprising: a hollow tubular permanent magnet affixed to an inner diameter of the cam assembly or screw, wherein the tubular permanent magnet is a rotor of the stepper motor, at least one circular coil (320a, 320b) disposed within the tubular permanent magnet, and at least one pair of mated claw-pole structures (321a, 321b) disposed within the tubular permanent magnet and in which the at least one coil (320a, 320b) is disposed, wherein the at least one pair of mated claw-pole structures (321a, 321b) is a stator of the stepper motor.
A combustor thermal shield comprising: a combustor panel comprising a first material composition; a transition region comprising a third material composition disposed radially outward of the combustor panel and forming a unitary body with the combustor panel; and an attachment stud comprising a cylindrical boss extending radially outward of the transition region and comprising a second material composition; wherein the combustor panel, transition region and attachment stud are formed using an additive material deposition process and the third material composition comprises a gradient from the first material composition to the second material composition. a combustor panel comprising a first material composition; a transition region comprising a third material composition disposed radially outward of the combustor panel and forming a unitary body with the combustor panel; and an attachment stud comprising a cylindrical boss extending radially outward of the transition region and comprising a second material composition; wherein the combustor panel, transition region and attachment stud are formed using an additive material deposition process and the third material composition comprises a gradient from the first material composition to the second material composition.
Method for producing luminescent substances based on doped, oxidic nanocrystals, wherein the method comprises the following steps: a1) introducing host lattice ions, wherein the host lattice ions are elements of the II to VI main group of the periodic table of elements, as organometallic complexes or volatile inorganic compounds, into at least a first vaporiser; a2) introducing dopant ions, wherein the dopant ions are ions of the rare earth elements, as organometallic complexes or volatile inorganic compounds, into a second vaporiser; b) respectively converting the complexes or compounds mentioned in step a1) and a2) into the gas phase; c) respectively transporting the resulting gas phases by means of one or more carrier gases and/or carrier gas mixtures into at least one heating zone of at least one reactor and supplying one or more reaction gases and/or reaction gas mixtures, d) decomposing the complexes or compounds in the heating zone of the reactor at a pressure of between 1 and 1500 mbar, with the immediate formation of the oxidic nanocrystals, and e) separating the oxidic nanocrystals in at least one adsorption trap. a1) introducing host lattice ions, wherein the host lattice ions are elements of the II to VI main group of the periodic table of elements, as organometallic complexes or volatile inorganic compounds, into at least a first vaporiser; a2) introducing dopant ions, wherein the dopant ions are ions of the rare earth elements, as organometallic complexes or volatile inorganic compounds, into a second vaporiser; b) respectively converting the complexes or compounds mentioned in step a1) and a2) into the gas phase; c) respectively transporting the resulting gas phases by means of one or more carrier gases and/or carrier gas mixtures into at least one heating zone of at least one reactor and supplying one or more reaction gases and/or reaction gas mixtures, d) decomposing the complexes or compounds in the heating zone of the reactor at a pressure of between 1 and 1500 mbar, with the immediate formation of the oxidic nanocrystals, and e) separating the oxidic nanocrystals in at least one adsorption trap.
A pressure equalization balloon, wherein the volume of the pressure equalization balloon is connected to a further volume whose pressure is to maintain a value which is as constant as possible even in the event of a forced change in volume, characterised in that the equalization balloon is produced from a thermoplastic elastomer and the balloon before first use was overstretched beyond the maximum intended regulating volume and is then relaxed to the range of the regulating volume, wherein the overstretching volume is at least 2 times the maximum regulating volume, so that the modulus of elasticity of the TPE changes in such a way that the pressure within the equalization balloon remains constant at least within a predetermined regulating volume range of the equalization balloon as the volume of the equalization balloon increases at a pressure rising above a desired regulating value and decreases at a pressure decreasing below the desired regulating value, wherein the regulating volume includes the range of from 20 cm 3 to 100 cm 3.
A filter insert comprising: a mounting disc; a tube and a closed-ended cylindrical cap, one end of the tube being sealingly affixed around the periphery of the mounting disc; the other end of the tube being sealingly affixed around the periphery of the closed-ended cylindrical cap, wherein the mounting disc and the closed-ended cylindrical cap both comprise cylindrical spigots; an inlet aperture and an outlet aperture in the mounting disc, each aperture communicating via a through hole in the mounting disc with the interior of the tube; a porous tubular filter element located within the tube and being interposed between the inlet aperture and the outlet aperture, the filter element comprising: an outer surface; and an interior surface that is an interference fit with the outer surface of the cylindrical spigots, wherein the outlet aperture is located radially inwardly of the interior surface of the filter element and the inlet aperture is located radially outwardly of the outer surface of the filter element and wherein the tube is at least partially manufactured of a flexible plastics material, and wherein the mounting disc is rigid. a mounting disc; a tube and a closed-ended cylindrical cap, one end of the tube being sealingly affixed around the periphery of the mounting disc; the other end of the tube being sealingly affixed around the periphery of the closed-ended cylindrical cap, wherein the mounting disc and the closed-ended cylindrical cap both comprise cylindrical spigots; an inlet aperture and an outlet aperture in the mounting disc, each aperture communicating via a through hole in the mounting disc with the interior of the tube; a porous tubular filter element located within the tube and being interposed between the inlet aperture and the outlet aperture, the filter element comprising: an outer surface; and an interior surface that is an interference fit with the outer surface of the cylindrical spigots, wherein the outlet aperture is located radially inwardly of the interior surface of the filter element and the inlet aperture is located radially outwardly of the outer surface of the filter element and wherein the tube is at least partially manufactured of a flexible plastics material, and wherein the mounting disc is rigid. an outer surface; and an interior surface that is an interference fit with the outer surface of the cylindrical spigots, wherein the outlet aperture is located radially inwardly of the interior surface of the filter element and the inlet aperture is located radially outwardly of the outer surface of the filter element and wherein the tube is at least partially manufactured of a flexible plastics material, and wherein the mounting disc is rigid.
A composite material, comprising - a first metallic material component, and comprising - a second metallic material component, wherein - the first material component is different from the second material component, and wherein - the second material component is mixed with the first material component, wherein - the first material component forms a cohesive matrix, into which the second material component is embedded in particulate form, wherein - the second material component is embedded into the first material component in the form of particles with a particle size of at least 5 μm to at most 30 μm, wherein - the second material component is more noble than the first material component, - wherein the first material component a) comprises a nickel-based alloy or a malleable iron alloy or consists of a nickel-based alloy or a malleable iron alloy, and/or b) comprises nickel and chromium, wherein the alloy comprises nickel as main component and chromium as the most important minor component, and - wherein the second material component comprises an element selected from a group consisting of iridium, platinum, rhodium, ruthenium, palladium and a rare earth metal, or in that the second material component consists of one of these elements. - a first metallic material component, and comprising - a second metallic material component, wherein - the first material component is different from the second material component, and wherein - the second material component is mixed with the first material component, wherein - the first material component forms a cohesive matrix, into which the second material component is embedded in particulate form, wherein - the second material component is embedded into the first material component in the form of particles with a particle size of at least 5 μm to at most 30 μm, wherein - the second material component is more noble than the first material component, - wherein the first material component a) comprises a nickel-based alloy or a malleable iron alloy or consists of a nickel-based alloy or a malleable iron alloy, and/or b) comprises nickel and chromium, wherein the alloy comprises nickel as main component and chromium as the most important minor component, and a) comprises a nickel-based alloy or a malleable iron alloy or consists of a nickel-based alloy or a malleable iron alloy, and/or b) comprises nickel and chromium, wherein the alloy comprises nickel as main component and chromium as the most important minor component, and - wherein the second material component comprises an element selected from a group consisting of iridium, platinum, rhodium, ruthenium, palladium and a rare earth metal, or in that the second material component consists of one of these elements.
A stretched multilayer thermoplastic resin film comprising a layer containing a thermoplastic resin on at least one surface of a layer containing a methacrylate resin, wherein methyl methacrylate constitutes at least 90 mol% of all structural units in the methacrylate resin; an intrinsic birefringence of the thermoplastic resin is from -0.005 to 0.005; and a glass transition temperature TgA (°C) of the methacrylate resin and a glass transition temperature TgB (°C) of the thermoplastic resin satisfy the expression 5°C<(TgB-TgA)<50°C, wherein the film has an in-plane retardation Re of 0.0 to 3.0 nm and a thickness direction retardation Rth of -10.0 to 10.0 nm, wherein the thermoplastic resin comprises a (meth)acrylic acid ester structural unit (a) represented by general formula below: (wherein R1 represents a hydrogen atom or a methyl group, and R2 represents a C 1 -C 16 hydrocarbon group), and an aliphatic vinyl structural unit (b) represented by general formula below: (wherein R3 represents a hydrogen atom or a methyl group, and R4 represents a cyclohexyl group or a cyclohexyl group having a C 1 -C 4 hydrocarbon substituent), and wherein the ratio of the sum of the (meth)acrylic acid ester structural unit (a) and the aliphatic vinyl structural unit (b) is 90 to 100 mol% relative to all the structural units in the thermoplastic resin, and wherein the molar ratio between the (meth)acrylic acid ester structural unit (a) and the aliphatic vinyl structural unit (b) is 55:45 to 85:15, characterized in that the film is biaxially stretched, wherein a magnification of stretching in at least one stretching direction is 1.1 to 3.0 times. wherein the film has an in-plane retardation Re of 0.0 to 3.0 nm and a thickness direction retardation Rth of -10.0 to 10.0 nm, wherein the thermoplastic resin comprises a (meth)acrylic acid ester structural unit (a) represented by general formula below: (wherein R1 represents a hydrogen atom or a methyl group, and R2 represents a C 1 -C 16 hydrocarbon group), and an aliphatic vinyl structural unit (b) represented by general formula below: (wherein R3 represents a hydrogen atom or a methyl group, and R4 represents a cyclohexyl group or a cyclohexyl group having a C 1 -C 4 hydrocarbon substituent), and wherein the ratio of the sum of the (meth)acrylic acid ester structural unit (a) and the aliphatic vinyl structural unit (b) is 90 to 100 mol% relative to all the structural units in the thermoplastic resin, and wherein the molar ratio between the (meth)acrylic acid ester structural unit (a) and the aliphatic vinyl structural unit (b) is 55:45 to 85:15, characterized in that the film is biaxially stretched, wherein a magnification of stretching in at least one stretching direction is 1.1 to 3.0 times.
A rotor blade assembly of a wind turbine, the rotor blade assembly comprising: a rotor blade comprising an aerodynamic body having an inboard region and an outboard region, the inboard and outboard regions (24, 26) defining a pressure side, a suction side, a leading edge, and a trailing edge, the inboard region comprising a blade root, the outboard region comprising a blade tip, the rotor blade defining a chord and a span; wherein the inboard region comprises from 0% span to 40% span from the blade root of the rotor blade in a span-wise direction and the outboard region comprises from 40% span to 100% span from the blade root of the rotor blade, the inboard region comprising a transitional region of the rotor blade that comprises a maximum chord, characterized in that a chord slope of the rotor blade in the transitional region ranges from -0.06 to 0.06 from the maximum chord over 15% of the span of the rotor blade, wherein, in the inboard region, the chord slope is not equal to zero. a rotor blade comprising an aerodynamic body having an inboard region and an outboard region, the inboard and outboard regions (24, 26) defining a pressure side, a suction side, a leading edge, and a trailing edge, the inboard region comprising a blade root, the outboard region comprising a blade tip, the rotor blade defining a chord and a span; wherein the inboard region comprises from 0% span to 40% span from the blade root of the rotor blade in a span-wise direction and the outboard region comprises from 40% span to 100% span from the blade root of the rotor blade, the inboard region comprising a transitional region of the rotor blade that comprises a maximum chord, characterized in that a chord slope of the rotor blade in the transitional region ranges from -0.06 to 0.06 from the maximum chord over 15% of the span of the rotor blade, wherein, in the inboard region, the chord slope is not equal to zero.
A blue or violet dye polymer comprising a polyethylene imine covalently bound to a reactive dye, the polyethylene imine having from 6 to 1000000 amine nitrogen atoms, wherein from 20 to 95 mol% of the totality of the protons of the primary and secondary amine nitrogen atoms of the unsubstituted polyethylene imine are substituted by iso-propyl alcohol groups.
A method for determining whether a compound induces a pseudo-allergic-type reaction, the method comprising: contacting the isolated cell comprising a recombinant nucleic acid that expresses mas-related G-protein coupled receptor member X2 (MrgprX2) or MrgprB2 with a candidate compound, detecting activation of MrgprX2 or MrgprB2, wherein activation of MrgprX2 or MrgprB2 determines that the candidate compound induces a pseudo-allergic-type reaction. contacting the isolated cell comprising a recombinant nucleic acid that expresses mas-related G-protein coupled receptor member X2 (MrgprX2) or MrgprB2 with a candidate compound, detecting activation of MrgprX2 or MrgprB2, wherein activation of MrgprX2 or MrgprB2 determines that the candidate compound induces a pseudo-allergic-type reaction.