mhurhangee/patent-ind-claim-en huggingface dataset:
Use of a composition comprising - 60 - 98 wt.% of polypropylene - 2 - 40 wt.% of low density polyethylene - 0.1 - 10 wt.% of compatibiliser wherein - the compatibiliser is a BAB or AB type of block copolymer comprising a polypropylene block A and a polyester block B, or wherein the compatibiliser is a graft copolymer of the type ABn having a polypropylene backbone A and polyester block(s) B grafted thereon, with n being at least 1, and - the polyester block(s) B have an average M/F ratio from 8 - 32, wherein M is the number of backbone carbon atoms in the polyester not including carbonyl carbon atoms, and F is the number of ester groups in the polyester block(s), - wherein the wt.% is based on the sum of the amount polypropylene, low density polyethylene and compatibiliser, for the manufacture of a foamed article. - 60 - 98 wt.% of polypropylene - 2 - 40 wt.% of low density polyethylene - 0.1 - 10 wt.% of compatibiliser wherein - the compatibiliser is a BAB or AB type of block copolymer comprising a polypropylene block A and a polyester block B, or wherein the compatibiliser is a graft copolymer of the type ABn having a polypropylene backbone A and polyester block(s) B grafted thereon, with n being at least 1, and - the polyester block(s) B have an average M/F ratio from 8 - 32, wherein M is the number of backbone carbon atoms in the polyester not including carbonyl carbon atoms, and F is the number of ester groups in the polyester block(s), - wherein the wt.% is based on the sum of the amount polypropylene, low density polyethylene and compatibiliser,
A component for a vehicle interior comprising: (a) a base comprising an outer surface; and (b) a support comprising an outer surface and configured to move between a raised position and a lowered position; wherein the outer surface of the support and the outer surface of the base comprise a substantially continuous surface when the support is in the raised position; wherein the support is configured to descend into the base to provide a cavity wherein the component further comprises a mechanism configured to move the support between the raised position and the lowered position; wherein the support and the base provide the cavity when the support is in the lowered position, and the mechanism comprises a controller configured to hold the support in the lowered position for a duration of time after removal of a force on the support . (a) a base comprising an outer surface; and (b) a support comprising an outer surface and configured to move between a raised position and a lowered position; wherein the outer surface of the support and the outer surface of the base comprise a substantially continuous surface when the support is in the raised position; wherein the support is configured to descend into the base to provide a cavity wherein the component further comprises a mechanism configured to move the support between the raised position and the lowered position; wherein the support and the base provide the cavity when the support is in the lowered position, and the mechanism comprises a controller configured to hold the support in the lowered position for a duration of time after removal of a force on the support .
A seedling-cutting apparatus comprising: a pair of openable and closable arms that is configured to nip a portion of a stem of a seedling, the stem extending in a Z-direction, the pair of arms extending in parallel with each other in a Y-direction, wherein the arms can be opened and closed by being moved in a X-direction ; and a blade that is provided so as to be capable of reciprocating, in the X-direction, relative to the portion of the stem to cut the stem, wherein at least one of the pair of arms includes a through hole that penetrates a portion of the arm along the X-direction in which the blade reciprocates, wherein when the pair of arms nip the portion of the stem, at least a portion of the through hole faces the portion of the stem, wherein the blade moves through the through hole and cuts the portion of the stem that is nipped and fixed by the pair of arms , and wherein the blade is shaped like a letter y or x as seen looking in the X-direction in which the blade reciprocates. a pair of openable and closable arms that is configured to nip a portion of a stem of a seedling, the stem extending in a Z-direction, the pair of arms extending in parallel with each other in a Y-direction, wherein the arms can be opened and closed by being moved in a X-direction ; and a blade that is provided so as to be capable of reciprocating, in the X-direction, relative to the portion of the stem to cut the stem, wherein at least one of the pair of arms includes a through hole that penetrates a portion of the arm along the X-direction in which the blade reciprocates, wherein when the pair of arms nip the portion of the stem, at least a portion of the through hole faces the portion of the stem, wherein the blade moves through the through hole and cuts the portion of the stem that is nipped and fixed by the pair of arms , and wherein the blade is shaped like a letter y or x as seen looking in the X-direction in which the blade reciprocates.
A polymerization reactor for production of a super absorbent polymer, the reactor comprising: a composition supply part for supplying a monomer composition solution; a central pipe connected to the composition supply part ; a composition distribution part including a water storage tank located at a discharge port of the central pipe , a distribution pipe connected to the water storage tank so that the monomer composition solution can overflow from the water storage tank to the distribution pipe , and an ultrasonic device installed inside the water storage tank ; a conveyor belt located under the composition distribution part and on which the monomer composition solution is dropped; and an energy supply part for supplying polymerization energy to the monomer composition solution on the conveyor belt , wherein the ultrasonic device is configured to supply bubbles to the monomer composition solution flowing into the water storage tank . a composition supply part for supplying a monomer composition solution; a central pipe connected to the composition supply part ; a composition distribution part including a water storage tank located at a discharge port of the central pipe , a distribution pipe connected to the water storage tank so that the monomer composition solution can overflow from the water storage tank to the distribution pipe , and an ultrasonic device installed inside the water storage tank ; a conveyor belt located under the composition distribution part and on which the monomer composition solution is dropped; and an energy supply part for supplying polymerization energy to the monomer composition solution on the conveyor belt , wherein the ultrasonic device is configured to supply bubbles to the monomer composition solution flowing into the water storage tank .
A machine for plasma treatment of granular polymer material, in particular polyethylene, comprising: - a treatment cell , which delimits a treatment volume (V) for a granular polymer material, ; - a negative-pressure source in fluid communication (SP) with the treatment volume (V); - a gas-supply unit configured for introducing one or more treatment gases for the granular polymer material into said treatment volume (V); and - an electrode for generation of plasma set inside the treatment cell , wherein: - said electrode has an elongated shape with a first dimension (D26) oriented in a main direction of development (X) and a second dimension (d26) oriented in a secondary direction of development (Y); the machine being characterized in that said treatment cell comprises a stirrer device configured for stirring the granular polymer material that, in use, is present within the treatment cell , and in that the ratio between said first dimension (D26) and said second dimension (d26) is comprised between 20:1 and 15:1. - a treatment cell , which delimits a treatment volume (V) for a granular polymer material, ; - a negative-pressure source in fluid communication (SP) with the treatment volume (V); - a gas-supply unit configured for introducing one or more treatment gases for the granular polymer material into said treatment volume (V); and - an electrode for generation of plasma set inside the treatment cell , - said electrode has an elongated shape with a first dimension (D26) oriented in a main direction of development (X) and a second dimension (d26) oriented in a secondary direction of development (Y);
A method of producing a polyolefin microporous membrane containing 90 mass% or greater of a polypropylene resin, having a maximum pore size of less than 29.0 nm and a mean flow pore size of less than 18.0 nm as measured by the bubble point method using a porometer and having a maximum pore size of a pore on a surface of the polyolefin microporous membrane of 300 nm or less as observed by SEM, the method comprising steps to : a step of preparing a polyolefin solution by melt-kneading a polyolefin resin containing 90 mass% or greater of a polypropylene resin, a crystallization controlling agent, and a solvent for membrane formation; a step of forming a gel sheet by extruding and cooling the polyolefin solution; a stretching step of stretching the gel sheet; a step of removing the solvent for membrane formation from the gel sheet after the stretching; and a step of drying the sheet after removing the solvent for membrane formation; characterized in that the used crystallization controlling agent includes aromatic metal phosphate-based nucleating agents and mixtures of these. a step of preparing a polyolefin solution by melt-kneading a polyolefin resin containing 90 mass% or greater of a polypropylene resin, a crystallization controlling agent, and a solvent for membrane formation; a step of forming a gel sheet by extruding and cooling the polyolefin solution; a stretching step of stretching the gel sheet; a step of removing the solvent for membrane formation from the gel sheet after the stretching; and a step of drying the sheet after removing the solvent for membrane formation; characterized in that the used crystallization controlling agent includes aromatic metal phosphate-based nucleating agents and mixtures of these.
A rotorcraft , comprising: a rotor comprising a plurality of rotor blades , wherein each of the plurality of rotor blades comprises: a plurality of blade segments (310a-c); one or more attachment fittings configured to couple the plurality of blade segments (310a-c); and one or more actuators (330a-b) configured to adjust a relative orientation of each blade segment of the plurality of blade segments (310a-c) to other blade segments of the plurality of blade segments (310a-c) of the rotor blade ; characterised in that the one or more actuators (330a-b) comprise one or more linear motors (334a-b) configured to adjust the orientation of the plurality of blade segments (310a-c), and wherein the one or more actuators (330a-b) comprise one or more hydraulic clamps (332a-b) configured to lock the orientation of the plurality of blade segments (310a-c). a rotor comprising a plurality of rotor blades , wherein each of the plurality of rotor blades comprises: a plurality of blade segments (310a-c); one or more attachment fittings configured to couple the plurality of blade segments (310a-c); and one or more actuators (330a-b) configured to adjust a relative orientation of each blade segment of the plurality of blade segments (310a-c) to other blade segments of the plurality of blade segments (310a-c) of the rotor blade ; characterised in that the one or more actuators (330a-b) comprise one or more linear motors (334a-b) configured to adjust the orientation of the plurality of blade segments (310a-c), and a plurality of blade segments (310a-c); one or more attachment fittings configured to couple the plurality of blade segments (310a-c); and one or more actuators (330a-b) configured to adjust a relative orientation of each blade segment of the plurality of blade segments (310a-c) to other blade segments of the plurality of blade segments (310a-c) of the rotor blade ; characterised in that the one or more actuators (330a-b) comprise one or more linear motors (334a-b) configured to adjust the orientation of the plurality of blade segments (310a-c), and wherein the one or more actuators (330a-b) comprise one or more hydraulic clamps (332a-b) configured to lock the orientation of the plurality of blade segments (310a-c).
A cutting tool for forming a final opening in a stack that includes at least two layers and a pilot opening having a pilot-opening dimension and extending through at least one of the at least two layers, the cutting tool comprising: a shank ; a first portion including a first coating and a second coating , wherein the first coating at least partially covers the first portion ; and a second portion between the shank and the first portion , wherein the second portion includes the second coating , and wherein the second coating at least partially covers the second portion ; wherein the first portion includes a first end surface and a first side surface , the first side surface having a maximum first side-surface diameter that is smaller than the pilot-opening dimension; the first coating substantially completely covers the first end surface ; the second portion includes a second end surface and a second side surface , the second side surface having at least one second side-surface diameter that is greater than the maximum first side-surface diameter; and the second coating includes a different material than the first coating , the second coating covering at least a portion of the second end surface , wherein: the first coating and the second coating at least partially overlap along the first portion ; the second portion is adjacent to the first portion ; the first end surface is substantially disc shaped; and the second end surface is a substantially annular ring. a shank ; a first portion including a first coating and a second coating , wherein the first coating at least partially covers the first portion ; and a second portion between the shank and the first portion , wherein the second portion includes the second coating , and wherein the second coating at least partially covers the second portion ; wherein the first portion includes a first end surface and a first side surface , the first side surface having a maximum first side-surface diameter that is smaller than the pilot-opening dimension; the first coating substantially completely covers the first end surface ; the second portion includes a second end surface and a second side surface , the second side surface having at least one second side-surface diameter that is greater than the maximum first side-surface diameter; and the second coating includes a different material than the first coating , the second coating covering at least a portion of the second end surface , wherein: the first coating and the second coating at least partially overlap along the first portion ; the second portion is adjacent to the first portion ; the first end surface is substantially disc shaped; and the second end surface is a substantially annular ring. the first coating and the second coating at least partially overlap along the first portion ; the second portion is adjacent to the first portion ; the first end surface is substantially disc shaped; and the second end surface is a substantially annular ring.
Propulsion unit for an aircraft, said propulsion unit comprising: - at least a fan rotor having a longitudinal axis XX, - at least two gas generator housed each in a primary flow duct and designed to generate each a primary flow, each gas generator comprising at least a compressor, a combustion chamber and at least one turbine, - at least one power turbine driving at its periphery said fan rotor of longitudinal axis XX, - a central duct from which converge the primary flow duct of each gas generator and that feeds the power turbine with the primary flow, said central duct being surrounded by an external fairing , said central duct being upstream of the power turbine with regard to the longitudinal axis XX, characterized in that it comprises first movable means arranged so as to divert at least part of the primary flow (F1) to the outside of said external fairing and upstream of the turbine engine in order to generate thrust reversal, the first movable means being arranged upstream of the power turbine with regard to the longitudinal axis XX. - at least a fan rotor having a longitudinal axis XX, - at least two gas generator housed each in a primary flow duct and designed to generate each a primary flow, each gas generator comprising at least a compressor, a combustion chamber and at least one turbine, - at least one power turbine driving at its periphery said fan rotor of longitudinal axis XX, - a central duct from which converge the primary flow duct of each gas generator and that feeds the power turbine with the primary flow, said central duct being surrounded by an external fairing , said central duct being upstream of the power turbine with regard to the longitudinal axis XX,
A heat-sealable, liquid impervious fabric, comprising: a breathable, liquid impervious thermoplastic film layer having a first melting point; and a nonwoven layer bonded to a first surface of the thermoplastic film layer, the nonwoven layer having a second melting point that is higher than the first melting point of the thermoplastic film layer; the heat-sealable, liquid impervious fabric having an overall moisture vapor transmission rate (MVTR) of at least 800 g/m2/day as determined by ASTM E96-00, wherein a difference between the first melting point and the second melting point is less than 15°C. a breathable, liquid impervious thermoplastic film layer having a first melting point; and a nonwoven layer bonded to a first surface of the thermoplastic film layer, the nonwoven layer having a second melting point that is higher than the first melting point of the thermoplastic film layer; the heat-sealable, liquid impervious fabric having an overall moisture vapor transmission rate (MVTR) of at least 800 g/m2/day as determined by ASTM E96-00, wherein a difference between the first melting point and the second melting point is less than 15°C.
A compound of Formula X, or a pharmaceutically acceptable salt thereof, wherein: R 2' is halogen, and each of R 2 is independently hydrogen, halogen, -CN, -NO 2 , -C(O)OR, -C(O)NR 2 , -NR 2 , -NRC(O)R, -NRC(O)OR, -NRS(O) 2 R, -OR, -P(O)R 2 , -SR, -S(O)R, -S(O) 2 R, -S(O)(NH)R, -S(O) 2 NR 2 , or R; or each R is independently hydrogen or an optionally substituted group selected from C 1-6 aliphatic, a 3-8 membered saturated or partially unsaturated monocyclic carbocyclic ring, phenyl, a 7-10 membered saturated spirobicyclic heterocyclic ring having 1-2 heteroatoms independently selected from nitrogen, oxygen, or sulfur, a 7-10 membered saturated or partially unsaturated fused bicyclic heterocyclic ring having 1-2 heteroatoms independently selected from nitrogen, oxygen, or sulfur, a 4-8 membered saturated or partially unsaturated monocyclic heterocyclic ring having 1-2 heteroatoms independently selected from nitrogen, oxygen, or sulfur, or a 5-6 membered monocyclic heteroaromatic ring having 1-4 heteroatoms independently selected from nitrogen, oxygen, or sulfur; or: two R groups on the same nitrogen are optionally taken together with their intervening atoms to form a 4-7 membered saturated, partially unsaturated, or heteroaryl ring having 0-3 heteroatoms, in addition to the nitrogen, independently selected from nitrogen, oxygen and sulfur, optionally substituted with 1-2 oxo groups. R 2' is halogen, and each of R 2 is independently hydrogen, halogen, -CN, -NO 2 , -C(O)OR, -C(O)NR 2 , -NR 2 , -NRC(O)R, -NRC(O)OR, -NRS(O) 2 R, -OR, -P(O)R 2 , -SR, -S(O)R, -S(O) 2 R, -S(O)(NH)R, -S(O) 2 NR 2 , or R; or each R is independently hydrogen or an optionally substituted group selected from C 1-6 aliphatic, a 3-8 membered saturated or partially unsaturated monocyclic carbocyclic ring, phenyl, a 7-10 membered saturated spirobicyclic heterocyclic ring having 1-2 heteroatoms independently selected from nitrogen, oxygen, or sulfur, a 7-10 membered saturated or partially unsaturated fused bicyclic heterocyclic ring having 1-2 heteroatoms independently selected from nitrogen, oxygen, or sulfur, a 4-8 membered saturated or partially unsaturated monocyclic heterocyclic ring having 1-2 heteroatoms independently selected from nitrogen, oxygen, or sulfur, or a 5-6 membered monocyclic heteroaromatic ring having 1-4 heteroatoms independently selected from nitrogen, oxygen, or sulfur; or: two R groups on the same nitrogen are optionally taken together with their intervening atoms to form a 4-7 membered saturated, partially unsaturated, or heteroaryl ring having 0-3 heteroatoms, in addition to the nitrogen, independently selected from nitrogen, oxygen and sulfur, optionally substituted with 1-2 oxo groups.
A method of coupling a boot toe body to a fin apparatus comprising a fin body coupled to a boot coupling body , the method comprising: connecting a first boot connector on a top portion of the boot coupling body to a first complementary boot connector on a top side of the boot toe body; and connecting a second boot connector on a bottom portion of the boot coupling body to a second complementary boot connector on a bottom side of the boot toe body, wherein: the second complementary boot connector comprises a boot toe retaining surface ; the second boot connector comprises a boot retaining surface on a top side of the bottom portion of the boot coupling body; and connecting the second boot connector to the second complementary boot connector comprises: contacting the boot retaining surface and the boot toe retaining surface; and retaining the second boot connector against movement in a direction towards the fin body. connecting a first boot connector on a top portion of the boot coupling body to a first complementary boot connector on a top side of the boot toe body; and connecting a second boot connector on a bottom portion of the boot coupling body to a second complementary boot connector on a bottom side of the boot toe body, wherein: the second complementary boot connector comprises a boot toe retaining surface ; the second boot connector comprises a boot retaining surface on a top side of the bottom portion of the boot coupling body; and connecting the second boot connector to the second complementary boot connector comprises: contacting the boot retaining surface and the boot toe retaining surface; and retaining the second boot connector against movement in a direction towards the fin body. the second complementary boot connector comprises a boot toe retaining surface ; the second boot connector comprises a boot retaining surface on a top side of the bottom portion of the boot coupling body; and connecting the second boot connector to the second complementary boot connector comprises: contacting the boot retaining surface and the boot toe retaining surface; and retaining the second boot connector against movement in a direction towards the fin body. contacting the boot retaining surface and the boot toe retaining surface; and retaining the second boot connector against movement in a direction towards the fin body.