mhurhangee/patent-ind-claim-en huggingface dataset:
A multirotor aircraft , comprising: at least three proprotors (114-117, 301-304), each proprotor (114-117, 301-304) having a plurality of rotor blades (118-121, 305-308) pivotably attached to a mast assembly ; a rotor blade control system configured to set a negative collective rotor blade pitch angle on an unpowered proprotor of the at least three proprotors (114-117, 301-304) independently of the rotor blade pitch on powered proprotors, the unpowered proprotor being unpowered as a result of an engine failure condition, said rotor blade control system being further configured to control a collective rotor blade pitch angle on each proprotor (114-117, 301-304) independently of the rotor blade pitch on the other proprotors; wherein when a rotor blade pitch angle is changed for one of the at least three proprotors (114-117, 301-304), all rotor blades (118-121, 305-308) on said one of the at least three proprotors (114-117, 301-304) change to a same pitch angle such that cyclic blade control cannot be applied to the proprotor (114-117, 301-304) and control of the movement of the multirotor aircraft is achievable using only collective pitch control on each of the at least three proprotors (114-117, 301-304); wherein the at least three proprotors (114-117, 301-304) are configured to spin freely when disengaged from a power source or when the power source fails; and wherein a rotor blade pitch angle of powered proprotors is a positive angle. at least three proprotors (114-117, 301-304), each proprotor (114-117, 301-304) having a plurality of rotor blades (118-121, 305-308) pivotably attached to a mast assembly ; a rotor blade control system configured to set a negative collective rotor blade pitch angle on an unpowered proprotor of the at least three proprotors (114-117, 301-304) independently of the rotor blade pitch on powered proprotors, the unpowered proprotor being unpowered as a result of an engine failure condition, said rotor blade control system being further configured to control a collective rotor blade pitch angle on each proprotor (114-117, 301-304) independently of the rotor blade pitch on the other proprotors; wherein when a rotor blade pitch angle is changed for one of the at least three proprotors (114-117, 301-304), all rotor blades (118-121, 305-308) on said one of the at least three proprotors (114-117, 301-304) change to a same pitch angle such that cyclic blade control cannot be applied to the proprotor (114-117, 301-304) and control of the movement of the multirotor aircraft is achievable using only collective pitch control on each of the at least three proprotors (114-117, 301-304); wherein the at least three proprotors (114-117, 301-304) are configured to spin freely when disengaged from a power source or when the power source fails; and wherein a rotor blade pitch angle of powered proprotors is a positive angle.
Structural aircraft component comprising a composite sandwich panel (S), comprising: a top layer (T); a bottom layer (B); and a honeycomb core layer (H) sandwiched between the top layer (T) and the bottom layer (B), the honeycomb core layer (H) including an array of hollow cells formed between vertical walls, the array of hollow cells being recessed in the form of a channel network (R) running from a first side face of the sandwich panel (S) through the honeycomb core layer (H) to a second side face of the sandwich panel (S), the second side face being located on the opposite side of the first side face of the sandwich panel (S), the structural aircraft component further comprising: a planar core panel having a space frame structure (T1) of load bearing space frame rods (RM), with at least a portion of the core panel being embedded in the recessed channel network (R) of the honeycomb core layer (H) of the sandwich panel (S). a top layer (T); a bottom layer (B); and a honeycomb core layer (H) sandwiched between the top layer (T) and the bottom layer (B), the honeycomb core layer (H) including an array of hollow cells formed between vertical walls, the array of hollow cells being recessed in the form of a channel network (R) running from a first side face of the sandwich panel (S) through the honeycomb core layer (H) to a second side face of the sandwich panel (S), the second side face being located on the opposite side of the first side face of the sandwich panel (S), the structural aircraft component further comprising: a planar core panel having a space frame structure (T1) of load bearing space frame rods (RM), with at least a portion of the core panel being embedded in the recessed channel network (R) of the honeycomb core layer (H) of the sandwich panel (S).
A processor for use in a system for obtaining a blood flow velocity measurement based on an angiogram obtained from a subject, wherein the processor is adapted to: obtain an angiogram of a vessel of the subject, the angiogram comprising a plurality of angiogram image frames, wherein the angiogram is representative of the vessel including a contrast agent therein, and wherein the contrast agent has been provided to the vessel in bursts, thereby providing contrast data within the angiogram; for each angiogram image frame of the angiogram that includes contrast data: estimate an instantaneous blood flow velocity based on the contrast data; calculate a confidence value of the angiogram image frame based on the contrast data; and estimate a point within a cardiac cycle represented by the angiogram image frame; estimate a period of the cardiac cycle; and generate a velocity curve representing the blood flow velocity within the vessel over the cardiac cycle based on the period of the cardiac cycle, the estimated instantaneous blood flow velocity of each angiogram image frame, the confidence value of each angiogram image frame and the point within the cardiac cycle represented by each angiogram image frame. obtain an angiogram of a vessel of the subject, the angiogram comprising a plurality of angiogram image frames, wherein the angiogram is representative of the vessel including a contrast agent therein, and wherein the contrast agent has been provided to the vessel in bursts, thereby providing contrast data within the angiogram; for each angiogram image frame of the angiogram that includes contrast data: estimate an instantaneous blood flow velocity based on the contrast data; calculate a confidence value of the angiogram image frame based on the contrast data; and estimate a point within a cardiac cycle represented by the angiogram image frame; estimate an instantaneous blood flow velocity based on the contrast data; calculate a confidence value of the angiogram image frame based on the contrast data; and estimate a point within a cardiac cycle represented by the angiogram image frame; estimate a period of the cardiac cycle; and generate a velocity curve representing the blood flow velocity within the vessel over the cardiac cycle based on the period of the cardiac cycle, the estimated instantaneous blood flow velocity of each angiogram image frame, the confidence value of each angiogram image frame and the point within the cardiac cycle represented by each angiogram image frame.
A retaining member for a pressing device for a cast-resin dry-type electric transformer, comprising a disk configured to form a support base for the pressing device on a winding of the cast-resin dry-type electric transformer and legs for mounting astride the winding , wherein the distance between said legs is adjustable to adapt to the winding section .
A composition for optical stereolithography, comprising: (A) a diallyl phthalate-based polymer; (B) radical polymerizable compounds having a methacrylic group and/or an acrylic group; (C) a radical polymerization initiator; and (D) a sensitizer, wherein the (B) radical polymerizable compounds having a methacrylic group and/or an acrylic group comprises at least (B1) a radical polymerizable compound of an epoxy (meth)acrylate having a methacrylic group and/or an acrylic group, and/or (B2) a radical polymerizable compound of a dioxane (meth)acrylate having a methacrylic group and/or an acrylic group, wherein the (D) sensitizer is a polyfunctional thiol compound, an acridine-based sensitizer, a coumarin-based sensitizer, or an anthracene-based sensitizer, wherein the composition for optical stereolithography contains: 0.5 to 10% by mass of the (A) diallyl phthalate-based polymer; 5 to 43% by mass of a total content of the (B 1) and (B2) radical polymerizable compounds, 20 to 95% by mass of a radical polymerizable compound in the (B) radical polymerizable compounds other than the (B1) and (B2) radical polymerizable compounds, 0.1 to 5% by mass of the (C) radical polymerization initiator, and 0.1 to 5% by mass of the (D) sensitizer. (A) a diallyl phthalate-based polymer; (B) radical polymerizable compounds having a methacrylic group and/or an acrylic group; (C) a radical polymerization initiator; and (D) a sensitizer, wherein the (B) radical polymerizable compounds having a methacrylic group and/or an acrylic group comprises at least (B1) a radical polymerizable compound of an epoxy (meth)acrylate having a methacrylic group and/or an acrylic group, and/or (B2) a radical polymerizable compound of a dioxane (meth)acrylate having a methacrylic group and/or an acrylic group, wherein the (D) sensitizer is a polyfunctional thiol compound, an acridine-based sensitizer, a coumarin-based sensitizer, or an anthracene-based sensitizer, wherein the composition for optical stereolithography contains: 0.5 to 10% by mass of the (A) diallyl phthalate-based polymer; 5 to 43% by mass of a total content of the (B 1) and (B2) radical polymerizable compounds, 20 to 95% by mass of a radical polymerizable compound in the (B) radical polymerizable compounds other than the (B1) and (B2) radical polymerizable compounds, 0.1 to 5% by mass of the (C) radical polymerization initiator, and 0.1 to 5% by mass of the (D) sensitizer.
A trailer having a kingpin or having a drawbar for coupling a tractor unit on a coupling side of the trailer , wherein the trailer has, on its coupling side , a detectable pattern for identifying the trailer, characterised in that a predefined distance between the detectable pattern of the coupling side of the trailer and the kingpin or the drawbar is stored in the pattern , wherein, in particular, the predefined distance is stored in a color code or a barcode or a matrix code or the like.
Method for insulating, from electromagnetic waves, a housing of an electrical connection device , this housing being made of an electrically insulating material and comprising at least one cavity (4; 5), and the insulation method consisting in the following: - sealing the cavity or cavities (4; 5) of the housing of the electrical connection device ; - subsequently metallizing at least part of the exterior surface of this housing ; - characterized in that: - the cavity or cavities (4; 5) of the housing of the electrical connection device is or are sealed by overmolding an overmolding material onto this housing ; - after metallization, the overmolding material and the housing of the electrical connection device are separated. - sealing the cavity or cavities (4; 5) of the housing of the electrical connection device ; - subsequently metallizing at least part of the exterior surface of this housing ; - characterized in that: - the cavity or cavities (4; 5) of the housing of the electrical connection device is or are sealed by overmolding an overmolding material onto this housing ; - after metallization, the overmolding material and the housing of the electrical connection device are separated.
A method for manufacturing a spindly wood element having at least one textured surface after machining including relief geometric shapes asymmetrically extending on the surface of the spindly element and randomly and non-repeatedly distributed on the entirety of said surface at least in a surface distribution and/or in thickness/depth, such that said machining is performed by virtue of the translation of the spindly element along a travelling direction (F) corresponding to the longitudinal direction of said element, preferably on a facer-planer , and the implementation of at least one machining tool arranged on at least one rotating shaft extending in a direction transverse to the travelling direction (F), the shaft being on the one hand rotatably movable in a direction opposite to the travelling direction (F) of the element and on the other hand axially translationally movable, transversely to the travelling direction (F), and characterised in that the element is dedicated to the manufacture of a staircase handrail and in that the machining tool includes a knife the profile of which includes unevenly alternating recesses and convexities with cutting edges.
An interlayer film for laminated glass, being obtained by mixing a first film material containing a first polyvinyl acetal resin, a second film material containing a second polyvinyl acetal resin and a plasticizer and a third film material containing a third polyvinyl acetal resin and a plasticizer, the second film material being a recovered material which has been used at least one time for obtaining an interlayer film, wherein the absolute value of the difference between the content of the hydroxyl group of the first polyvinyl acetal resin and the content of the hydroxyl group of the second polyvinyl acetal resin contained together with the plasticizer in the second film material is greater than or equal to 0.5% by mole and less than or equal to 13% by mole, wherein the absolute value of the difference between the content of the hydroxyl group of the first polyvinyl acetal resin and the content of the hydroxyl group of the third polyvinyl acetal resin contained together with the plasticizer in the third film material is less than or equal to 13% by mole, wherein the content of the hydroxyl group of the first polyvinyl acetal resin is higher than the content of the hydroxyl group of the second polyvinyl acetal resin contained together with the plasticizer in the second film material, wherein the content of the second polyvinyl acetal resin is greater than or equal to 0.1% by weight and less than or equal to 10% by weight in 100% by weight of the total of the first polyvinyl acetal resin and the second polyvinyl acetal resin, and wherein the second film material contains the plasticizer in an amount of greater than or equal to 40 parts by weight relative to 100 parts by weight of the second polyvinyl acetal resin.
Adherent stromal cells (ASC) for use in a method of treating a breast carcinoma, wherein said ASC originate from placenta tissue.
An ankle prosthesis comprising: ▪ a main body , having a foot portion configured to rest on a walking surface; ▪ stump supporting means , configured to couple with a leg prosthetic element; ▪ linear actuation means , comprising a coupling between a screw element and a nut screw element having a friction coefficient lower than 0.16, wherein said stump supporting means , said screw element and said nut screw element are constrained to said main body according to a substantially four-bar linkage configuration , so that a relative rotation between said supporting means and said main body is allowed and so that said actuation means is configured to act as damping element along a damping direction (S) and is movable between an advanced position (P sup ) and a rearward position (Pint) with respect to said damping direction (S), wherein said foot portion comprises a first and a second contact position during a resting phase on the walking surface, wherein to said first and second contact position corresponds a respective opposite movement of said actuation means between said advanced position (P sup ) and said rearward position (P inf ) during a damping condition of the loads transferred on said main body by the leg element. ▪ a main body , having a foot portion configured to rest on a walking surface; ▪ stump supporting means , configured to couple with a leg prosthetic element; ▪ linear actuation means , comprising a coupling between a screw element and a nut screw element having a friction coefficient lower than 0.16,
A composite semipermeable membrane wherein a skin layer containing a polyamide-based resin obtained by polymerizing a polyfunctional amine component and a polyfunctional acid halide component is formed on a surface of a porous support, wherein the polyfunctional amine component consists of piperazine, and in the skin layer, an absorption peak intensity obtained by a transmission method of FT-IR (Fourier transform infrared spectroscopy) and derived from a C=O stretching vibration of an amide group is 0.06 or more, wherein the absorption peak intensity derived from C=O stretching vibration of an amide group is measured according to the method disclosed in the description. the polyfunctional amine component consists of piperazine, and in the skin layer, an absorption peak intensity obtained by a transmission method of FT-IR (Fourier transform infrared spectroscopy) and derived from a C=O stretching vibration of an amide group is 0.06 or more, wherein the absorption peak intensity derived from C=O stretching vibration of an amide group is measured according to the method disclosed in the description.
A method for texturing food and/or nutraceutical products of the "sponge cake" or "solid foam" type comprising at least: (a) Transformation by controlled grinding of a preparation of at least one food, able to preserve the desired organoleptic properties, able to obtain a ground material, wherein the ground material is a liquid or paste with a particle size of less than 5 mm, (b) Addition of a structure molecule at an inactive state to said ground material to obtain a mixture, wherein the structure molecule is chosen from among the group comprising the following constituents: Egg white, albumin, ovalbumin, agar, pectin, gellan, carob gum or a mixture of at least two of said constituents, (c) Pressurization of the mixture obtained in step (b) by the incorporation of dissolved gas into said mixture, (d) Mechanical expansion n obtained by reducing the pressure of the mixture obtained in step (c), wherein the mechanical expansion is achieved by reducing the pressure by at least 6 bar, preferably between 6 and 20 bar, preferably between 10 and 18 bar, (e) Activation of the structure molecule, characterized in that the structure molecule activation is a thermal activation configured to obtain a core temperature of said mixture of between 60 °C and 150 °C, and the time for activating the structure molecule in step (e) is less than 5 minutes, the activated structure molecule thereby providing a structured network within said mixture set in shape, which results in a product having a density less than 0.4 g/cm 3 . (a) Transformation by controlled grinding of a preparation of at least one food, able to preserve the desired organoleptic properties, able to obtain a ground material, wherein the ground material is a liquid or paste with a particle size of less than 5 mm, (b) Addition of a structure molecule at an inactive state to said ground material to obtain a mixture, wherein the structure molecule is chosen from among the group comprising the following constituents: Egg white, albumin, ovalbumin, agar, pectin, gellan, carob gum or a mixture of at least two of said constituents, (c) Pressurization of the mixture obtained in step (b) by the incorporation of dissolved gas into said mixture, (d) Mechanical expansion n obtained by reducing the pressure of the mixture obtained in step (c), wherein the mechanical expansion is achieved by reducing the pressure by at least 6 bar, preferably between 6 and 20 bar, preferably between 10 and 18 bar, (e) Activation of the structure molecule,
A method for forming an isoporous graded film of a multiblock poly(isoprene-b-styrene-b-4-vinylpyridine) triblock terpolymer, wherein the isoporous graded film has pores of a size from 5 nm to 100 nm, the method comprising the steps of: a) forming a film comprising the multiblock poly(isoprene-b-styrene-b-4-vinylpyridine) triblock terpolymer having a hydrogen-bonding block that can self-assemble on a substrate using a deposition solution comprising the multiblock copolymer and a solvent system, wherein the solvent system is 70/30 1,4-dioxane and tetrahydrofuran by weight; b) removing a portion of the solvent system from the film; and c) contacting the film from step b) with a phase separation solvent system, such that the mesoporous, isoporous graded film is formed, and wherein the phase separation solvent system is a non-solvent for the multiblock copolymer and the 1,4-dioxane is miscible with the non-solvent. a) forming a film comprising the multiblock poly(isoprene-b-styrene-b-4-vinylpyridine) triblock terpolymer having a hydrogen-bonding block that can self-assemble on a substrate using a deposition solution comprising the multiblock copolymer and a solvent system, wherein the solvent system is 70/30 1,4-dioxane and tetrahydrofuran by weight; b) removing a portion of the solvent system from the film; and c) contacting the film from step b) with a phase separation solvent system, such that the mesoporous, isoporous graded film is formed, and
An adhesive composition comprising, on the basis of the total weight thereof: 0.5 to 4.0 % by weight of the epoxy compound; 1.0 to 8.0 % by weight of the isocyanate compound; 1.7 to 22 % by weight of the rubber latex; 1.0 to 8.0 % by weight of the polyurethane dispersion (PUD) resin; 0.1 to 2.0 % by weight of the amine compound; and 69 to 92 % by weight of the solvent, wherein the epoxy compound and the isocyanate compound have a weight ratio of 1:1 to 1:10. 0.5 to 4.0 % by weight of the epoxy compound; 1.0 to 8.0 % by weight of the isocyanate compound; 1.7 to 22 % by weight of the rubber latex; 1.0 to 8.0 % by weight of the polyurethane dispersion (PUD) resin; 0.1 to 2.0 % by weight of the amine compound; and 69 to 92 % by weight of the solvent, wherein the epoxy compound and the isocyanate compound have a weight ratio of 1:1 to 1:10.
A molecular marker for distinguishing a plant having an allele for a double-flowering characteristic, said distinguishing comprising detecting at least one SNP mutation selected from the group consisting of: 1. a C nucleotide at position number 320 of SEQ ID NO: 1 and 2. a C nucleotide at position number 247 in SEQ ID NO: 1, the marker comprising a sequence of at least 20 consecutive nucleotides of SEQ ID NO: 1, or the complementary sequence thereof, said molecular marker preferably being isolated. 1. a C nucleotide at position number 320 of SEQ ID NO: 1 and 2. a C nucleotide at position number 247 in SEQ ID NO: 1,