mhurhangee/patent-ind-claim-en huggingface dataset:
A multi-component absorbable/disintegratable, fiber-reinforced, radiopaque composite, non-migrating stent for a urinogenital conduit comprising: a load-bearing, radiopaque central coil, said coil comprising an absorbable polyester/inorganic radiopaque hybrid composition; said coil being shrouded with a knitted mesh comprising an absorbable multifilament yarn, to provide a knitted core; said knitted core being impregnated with a polymer matrix comprising an absorbable, segmented, polyaxial copolyester and a hydrophilic polymeric additive having a molecular weight of 1 to 70 kDa, the additive being selected from the group consisting of polyethylene glycol, and polyethylene glycol end-grafted with at least one monomer selected from the group consisting of l -lactide, glycolide, trimethylene carbonate, ε-caprolactone, p-dioxanone, 1,5-dioxepan-2-one and a morpholinedione, wherein said polymer matrix which impregnates said knitted core is absorbable, highly compliant, hydrowettable and tubular in shape; said stent being sterilized with high-energy radiation at a dose between 25 and 40 kGy; wherein the stent exhibits a one- to ten-week, radio-modulated absorption/disintegration and strength retention profile. a load-bearing, radiopaque central coil, said coil comprising an absorbable polyester/inorganic radiopaque hybrid composition; said coil being shrouded with a knitted mesh comprising an absorbable multifilament yarn, to provide a knitted core; said knitted core being impregnated with a polymer matrix comprising an absorbable, segmented, polyaxial copolyester and a hydrophilic polymeric additive having a molecular weight of 1 to 70 kDa, the additive being selected from the group consisting of polyethylene glycol, and polyethylene glycol end-grafted with at least one monomer selected from the group consisting of l -lactide, glycolide, trimethylene carbonate, ε-caprolactone, p-dioxanone, 1,5-dioxepan-2-one and a morpholinedione, wherein said polymer matrix which impregnates said knitted core is absorbable, highly compliant, hydrowettable and tubular in shape; said stent being sterilized with high-energy radiation at a dose between 25 and 40 kGy; wherein the stent exhibits a one- to ten-week, radio-modulated absorption/disintegration and strength retention profile.
A polycarbonate resin composition comprising, per 100 parts by mass of a polycarbonate resin (A), (i) 0.02 to 1 parts by mass of a sesamol group-containing benzotriazole ultraviolet absorber (B1) having a maximum absorption wavelength of at least 375 nm in the absorption curve determined according to JIS K 7105 using the following formula, or (ii) 0.08 to 1 parts by mass of a sesamol group-containing benzotriazole ultraviolet absorber (B2) having a maximum absorption wavelength of at least 360 nm and less than 375 nm in the absorption curve determined according to JIS K 7105 using the following formula; and 0.01 to 0.5 parts by mass of a stabilizer (C), wherein the stabilizer (C) is at least one selected from the group consisting of a phosphorus stabilizer and a phenolic stabilizer, wherein the phosphorus stabilizer is an aromatic phosphite compound represented by one of the following general formulas and : wherein, R 1 , R 2 , and R 3 each independently represent an aryl group having 6 to 30 carbon atoms, and wherein, R 4 and R 5 each independently represent an aryl group having 6 to 30 carbon atoms, [absorbance of the polycarbonate resin that contains 0.005% by mass of the ultraviolet absorber] - [absorbance of only the polycarbonate resin]. (i) 0.02 to 1 parts by mass of a sesamol group-containing benzotriazole ultraviolet absorber (B1) having a maximum absorption wavelength of at least 375 nm in the absorption curve determined according to JIS K 7105 using the following formula, or (ii) 0.08 to 1 parts by mass of a sesamol group-containing benzotriazole ultraviolet absorber (B2) having a maximum absorption wavelength of at least 360 nm and less than 375 nm in the absorption curve determined according to JIS K 7105 using the following formula; and 0.01 to 0.5 parts by mass of a stabilizer (C), wherein the stabilizer (C) is at least one selected from the group consisting of a phosphorus stabilizer and a phenolic stabilizer, wherein the phosphorus stabilizer is an aromatic phosphite compound represented by one of the following general formulas and : wherein, R 1 , R 2 , and R 3 each independently represent an aryl group having 6 to 30 carbon atoms, and wherein, R 4 and R 5 each independently represent an aryl group having 6 to 30 carbon atoms, [absorbance of the polycarbonate resin that contains 0.005% by mass of the ultraviolet absorber] - [absorbance of only the polycarbonate resin]. 0.01 to 0.5 parts by mass of a stabilizer (C), wherein the stabilizer (C) is at least one selected from the group consisting of a phosphorus stabilizer and a phenolic stabilizer, wherein the phosphorus stabilizer is an aromatic phosphite compound represented by one of the following general formulas and : wherein, R 1 , R 2 , and R 3 each independently represent an aryl group having 6 to 30 carbon atoms, and wherein, R 4 and R 5 each independently represent an aryl group having 6 to 30 carbon atoms, [absorbance of the polycarbonate resin that contains 0.005% by mass of the ultraviolet absorber] - [absorbance of only the polycarbonate resin].
An applicator for magnetic therapy comprising a housing with an outer wall , which defines an application surface to be applied to a patient, and in which at least one electrically conductive coil is housed for generating a magnetic field; wherein: the housing comprises: an outer shell forming the outer wall ; and an inner shell forming a seat for housing the coil , wherein the inner shell comprises a bottom wall facing the outer wall formed by the outer shell ; in the housing, a refrigerating device is provided, comprising at least one refrigerating duct adapted to circulate a refrigerating fluid and arranged between the coil and the application surface ; wherein the at least one refrigerating duct is arranged between the coil and a surface of the bottom wall of the inner shell facing the outer wall of the outer shell ; a gap is formed between the bottom wall of the inner shell and the outer wall of the outer shell for thermally insulating the coil and the application surface from each other; and spacing elements are arranged in the thermal insulation gap between the outer wall of the outer shell and the bottom wall of the inner shell . the housing comprises: an outer shell forming the outer wall ; and an inner shell forming a seat for housing the coil , wherein the inner shell comprises a bottom wall facing the outer wall formed by the outer shell ; in the housing, a refrigerating device is provided, comprising at least one refrigerating duct adapted to circulate a refrigerating fluid and arranged between the coil and the application surface ; wherein the at least one refrigerating duct is arranged between the coil and a surface of the bottom wall of the inner shell facing the outer wall of the outer shell ; a gap is formed between the bottom wall of the inner shell and the outer wall of the outer shell for thermally insulating the coil and the application surface from each other; and spacing elements are arranged in the thermal insulation gap between the outer wall of the outer shell and the bottom wall of the inner shell .
A method of manufacturing an article for forming an aerosol, the method comprising the steps of: a) providing a cover layer which comprises, defines or provides a mould surface for defining the periphery of an article for forming an aerosol; b) depositing a substance which is at least partially fluid and comprises aerosol-forming substrate into the mould surface ; and c) causing or allowing the substance to at least partially solidify thereby to provide an article for forming an aerosol having a periphery formed from the cover layer, wherein the mould surface circumscribes the moulded aerosol-forming substrate. a) providing a cover layer which comprises, defines or provides a mould surface for defining the periphery of an article for forming an aerosol; b) depositing a substance which is at least partially fluid and comprises aerosol-forming substrate into the mould surface ; and c) causing or allowing the substance to at least partially solidify thereby to provide an article for forming an aerosol having a periphery formed from the cover layer, wherein the mould surface circumscribes the moulded aerosol-forming substrate.
An electrode for metal-ion battery, the electrode comprising an active layer in electrical contact with a current collector, wherein the active layer comprises: (i) a plurality of porous particles comprising an electroactive material selected from silicon, silicon oxide of the formula SiO x wherein 0 < x ≤ 1.5, germanium, tin, aluminium and mixtures thereof, wherein the porous particles have a D 50 particle diameter of at least 0.8 μm and no more than 35 μm, an intra-particle porosity of less than 30%, and are secondary particles comprising electroactive material-containing primary particles and further comprising carbon; and (ii) a plurality of carbon particles selected from one or more of graphite, soft carbon and hard carbon and having a D 50 particle diameter in the range of from 1 to 100 μm wherein the active layer comprises at least 50% by weight of the carbon particles (ii), and wherein the ratio of the D 50 particle diameter of the carbon particles (ii) to the D 50 particle diameter of the porous particles (i) is in the range of from 1.5 to 30; wherein the active layer in a dry, uncharged state has a density in the range of from 0.6 to 1.8 g/cm 3 ; wherein the D 50 particle diameter is the diameter below which 50% by volume of the particle population is found determined by laser diffraction as defined in the description. (i) a plurality of porous particles comprising an electroactive material selected from silicon, silicon oxide of the formula SiO x wherein 0 < x ≤ 1.5, germanium, tin, aluminium and mixtures thereof, wherein the porous particles have a D 50 particle diameter of at least 0.8 μm and no more than 35 μm, an intra-particle porosity of less than 30%, and are secondary particles comprising electroactive material-containing primary particles and further comprising carbon; and (ii) a plurality of carbon particles selected from one or more of graphite, soft carbon and hard carbon and having a D 50 particle diameter in the range of from 1 to 100 μm wherein the active layer comprises at least 50% by weight of the carbon particles (ii), and wherein the ratio of the D 50 particle diameter of the carbon particles (ii) to the D 50 particle diameter of the porous particles (i) is in the range of from 1.5 to 30; wherein the active layer in a dry, uncharged state has a density in the range of from 0.6 to 1.8 g/cm 3 ; wherein the D 50 particle diameter is the diameter below which 50% by volume of the particle population is found determined by laser diffraction as defined in the description.
A computer-implemented method comprising: determining identification information of a vehicle entering a space within a structure or a building; determining an intended route of the vehicle within the space; determining venue map data corresponding to the intended route, the venue map data indicating one or more safety devices disposed at one or more predefined locations, within the structure or the building, along the intended route; receiving information regarding a current location of the vehicle, the information being detected by the one or more safety devices; repeatedly tracking a current location of the vehicle as the vehicle moves within the space; controlling the one or more safety devices to guide the vehicle to follow the intended route using the venue map data and the tracked location of the vehicle by, in response to determining that the vehicle is in proximity to a first safety device of the one or more safety devices, instructing the first safety device to emit an alert, wherein the first safety device is in front of the vehicle. determining identification information of a vehicle entering a space within a structure or a building; determining an intended route of the vehicle within the space; determining venue map data corresponding to the intended route, the venue map data indicating one or more safety devices disposed at one or more predefined locations, within the structure or the building, along the intended route; receiving information regarding a current location of the vehicle, the information being detected by the one or more safety devices; repeatedly tracking a current location of the vehicle as the vehicle moves within the space; controlling the one or more safety devices to guide the vehicle to follow the intended route using the venue map data and the tracked location of the vehicle by, in response to determining that the vehicle is in proximity to a first safety device of the one or more safety devices, instructing the first safety device to emit an alert, wherein the first safety device is in front of the vehicle.
System for drainage of water occurring on a transport area, such as for example surface water, having at least two drainage gutter modules and having at least one holder by means of which the drainage gutter modules are connected, wherein, by means of a spacer of the holder , a spacing for receiving an in particular firm and/or pourable adhesive bonding means and/or sealing means is formed between the connected drainage gutter modules , characterized in that the spacer has two substantially C-shaped profiles which are each arranged oppositely on an outer side of the holder .
Crown head for a timepiece, in particular for a diving watch, comprising a cap comprising a cover and an axial skirt , a tube which is designed to be secured in a case of the timepiece, a sealing gasket disposed between the tube and the axial skirt , and a central pipe which is designed to be engaged with the tube , the central pipe and the cap forming an assembly which can be placed in different axial positions relative to the tube , the crown head also comprising a safety valve comprising a discharge channel which is designed to be able to be in fluid communication with the inside of the case when the valve is in an open configuration, in order to discharge excess fluid, the said safety valve also comprising a piston fitted inside the central pipe and an elastic member designed to cooperate with the piston , which is configured to be displaced axially according to the pressure variations inside the case, the crown head also comprising blocking means which prevent separation of the cap and the tube , wherein the blocking means are in the form of a shoulder arranged on the inner wall of the tube , and comprising a support surface against which a head of a guide screw integral with the piston can abut, and in the form of a rim which is provided at the base of the central pipe , and is designed to abut against a shoulder provided on the piston .
Method for non-contact measurement of the contour of a workpiece edge of a workpiece , wherein the workpiece edge adjoins a workpiece surface with extension in a first main direction X, and wherein the workpiece edge has an edge height h in the extension of the first main direction X, and wherein the workpiece edge is illuminated by at least one light source , so that a light beam incident on the workpiece edge in an extension in the first main direction X at an angle of incidence α with respect to the first main direction X is reflected into an associated reflected light beam , and wherein each reflected light beam has a contour-dependent exit angle β as a function of the contour of the workpiece edge in the extension of the first main direction X, wherein the reflected light beams are detected by at least one optical sensor with a detection direction Y, wherein the at least one optical sensor has an imaging height H, wherein the imaging height H is the dimension of the light-sensitive sensor in an extension substantially parallel to the first main direction X, and wherein the contour of the workpiece edge is calculated on the basis of the radiation intensity of the reflected light beams detected by the optical sensor as a function of the contour-dependent exit angle β in relation to the angle of incidence α, wherein the workpiece edge as well as the optical sensor have a spatially invariable position during the measurement and wherein the workpiece edge is illuminated at different angles of incidence α by means of at least one light source , wherein a plurality of sequentially illuminating light sources are arranged approximately in the shape of a circular arc around the workpiece edge , wherein the plane defined by the circular arc segment is arranged substantially perpendicular to the extent of the workpiece edge , and wherein the light sources are offset relative to one another in such a way that the workpiece edge is illuminated at a defined angular offset φ when neighbouring light sources are illuminated.
A cartridge for an e-vaping device , the cartridge comprising: a housing ; a plurality of reservoirs (22-1, 22N) positioned within the housing , the plurality of reservoirs (22-1, 22-N) configured to hold different pre-vapor formulations; a dispensing interface coupled to the plurality of reservoirs (22-1, 22-N), the dispensing interface being configured to draw the different pre-vapor formulations from the plurality of reservoirs (22-1, 22-N) to a common location; and a heater coupled to the dispensing interface , the heater being configured to simultaneously vaporize the different pre-vapor formulations at the common location to form a vapor, wherein the dispensing interface includes: a trunk coupled to the heater ; a plurality of separate roots (32-1, 32-N) extending from the trunk into separate, respective reservoirs (22-1, 22-N) of the plurality of reservoirs; a plurality of wicks coupled together to form the trunk, wherein separate wicks of the plurality of wicks include separate roots of the plurality of separate roots; and a divider assembly partitioning at least two separate wicks of the plurality of wicks, the divider assembly being configured to mitigate pre-vaporization mixing of separate pre-vapor formulations drawn to the trunk via the at least two separate wicks. a housing ; a plurality of reservoirs (22-1, 22N) positioned within the housing , the plurality of reservoirs (22-1, 22-N) configured to hold different pre-vapor formulations; a dispensing interface coupled to the plurality of reservoirs (22-1, 22-N), the dispensing interface being configured to draw the different pre-vapor formulations from the plurality of reservoirs (22-1, 22-N) to a common location; and a heater coupled to the dispensing interface , the heater being configured to simultaneously vaporize the different pre-vapor formulations at the common location to form a vapor, wherein the dispensing interface includes: a trunk coupled to the heater ; a plurality of separate roots (32-1, 32-N) extending from the trunk into separate, respective reservoirs (22-1, 22-N) of the plurality of reservoirs; a plurality of wicks coupled together to form the trunk, wherein separate wicks of the plurality of wicks include separate roots of the plurality of separate roots; and a divider assembly partitioning at least two separate wicks of the plurality of wicks, the divider assembly being configured to mitigate pre-vaporization mixing of separate pre-vapor formulations drawn to the trunk via the at least two separate wicks. a trunk coupled to the heater ; a plurality of separate roots (32-1, 32-N) extending from the trunk into separate, respective reservoirs (22-1, 22-N) of the plurality of reservoirs; a plurality of wicks coupled together to form the trunk, wherein separate wicks of the plurality of wicks include separate roots of the plurality of separate roots; and a divider assembly partitioning at least two separate wicks of the plurality of wicks, the divider assembly being configured to mitigate pre-vaporization mixing of separate pre-vapor formulations drawn to the trunk via the at least two separate wicks.
An engine reduction gear system , comprising: at least two self-contained, independent engine reduction gearboxes , each capable of connecting to an aircraft engine , wherein each of the engine reduction gearboxes provides redundant, reduced speed to a main rotor gearbox via a shaft ; wherein each of the self-contained, independent engine reduction gearboxes is defined as further comprising: a self-contained lubrication system; an internal oil pump, oil filter, and oil monitoring system; wherein each engine reduction gearbox can be independently connected and disconnected from the main rotor gearbox ; and wherein the two engine reduction gearboxes do not provide power to any accessories and characterized in that it further comprises an input gear , an idler gear connected to the input gear , an output gear connected to the idler gear , that control the speed and torque exiting each of the reduction gearboxes and that reduce the speed of rotation from the engine prior to entering the main rotor gearbox , and supporting bearings. at least two self-contained, independent engine reduction gearboxes , each capable of connecting to an aircraft engine , wherein each of the engine reduction gearboxes provides redundant, reduced speed to a main rotor gearbox via a shaft ; wherein each of the self-contained, independent engine reduction gearboxes is defined as further comprising: a self-contained lubrication system; an internal oil pump, oil filter, and oil monitoring system; wherein each engine reduction gearbox can be independently connected and disconnected from the main rotor gearbox ; and wherein the two engine reduction gearboxes do not provide power to any accessories and characterized in that it further comprises an input gear , an idler gear connected to the input gear , an output gear connected to the idler gear , that control the speed and torque exiting each of the reduction gearboxes and that reduce the speed of rotation from the engine prior to entering the main rotor gearbox , and supporting bearings. a self-contained lubrication system; an internal oil pump, oil filter, and oil monitoring system; wherein each engine reduction gearbox can be independently connected and disconnected from the main rotor gearbox ; and wherein the two engine reduction gearboxes do not provide power to any accessories and characterized in that it further comprises an input gear , an idler gear connected to the input gear , an output gear connected to the idler gear , that control the speed and torque exiting each of the reduction gearboxes and that reduce the speed of rotation from the engine prior to entering the main rotor gearbox , and supporting bearings.