mhurhangee/patent-ind-claim-en huggingface dataset:
An inertial locking system to be placed between a removable equipment , usable in an aircraft, and a support , said locking system being able to take up a first state, so-called locking state, in which the equipment can be detached from the support , and a second state, so-called over-locking state, in which the removable equipment is prevented from being ejected due to an acceleration (A) for example in the event of a crash or dynamic test and said locking system comprising a clipping system and a lock associated therewith, said lock being movable between a rest position and an active position allowing the system to be over-locked, the transition from the rest position to the active position of the lock being generated by the acceleration (A) in the event of a crash or dynamic test, characterized in that said clipping system comprises: - two elastically deformable legs each provided with a protrusion on their free ends, the two legs being fixed to one of the removable equipment and the support , and - an opening of corresponding shape made in the other of the removable equipment and the support . - two elastically deformable legs each provided with a protrusion on their free ends, the two legs being fixed to one of the removable equipment and the support , and - an opening of corresponding shape made in the other of the removable equipment and the support .
An aerodynamic dome component for a wind turbine , the aerodynamic dome characterized by : an outer ring comprising a plurality of arcuate ring segments ; a central axle disposed relative to the outer ring ; a plurality of radially extending tensioning members coupled to the outer ring at a first end and to the central axle at a second end , wherein the outer ring , the plurality of radially extending tensioning members and the central axle together form an underlying dome support structure ; and a skin-like covering enveloping at least a portion of the underlying dome support structure to form at least a portion of the aerodynamic dome component and define a front dome portion . an outer ring comprising a plurality of arcuate ring segments ; a central axle disposed relative to the outer ring ; a plurality of radially extending tensioning members coupled to the outer ring at a first end and to the central axle at a second end , wherein the outer ring , the plurality of radially extending tensioning members and the central axle together form an underlying dome support structure ; and a skin-like covering enveloping at least a portion of the underlying dome support structure to form at least a portion of the aerodynamic dome component and define a front dome portion .
An impeller for a centrifugal blast wheel machine , the impeller comprising: a hub provided at one end of the impeller , the hub being configured to be coupled to a motor ; a tapered section provided at an opposite end of the hub , the tapered section defining a media inlet to receive blast media; a plurality of drop-shaped vanes positioned between the hub and the tapered section, the plurality of drop-shaped vanes being spaced from one another on peripheries of the hub and the tapered section, the plurality of drop-shaped vanes defining a plurality of impeller media outlets constructed and arranged to allow egress of blast media upon rotation of the impeller , wherein each vane is drop-shaped having a leading side directed toward a direction of rotation of the impeller and a trailing side opposite the leading side wherein the plurality of drop-shaped vanes being spaced equidistant from one another on peripheries of the hub and the tapered section, wherein the plurality of drop-shaped vanes is spaced from a control cage at a predetermined distance, and wherein each drop-shaped vane has an angle of the leading side between 50° and 70°, preferably an angle between 55° and 60° and a radius of the trailing side between 3 mm and 8 mm, preferably between 4 mm and 7 mm. a hub provided at one end of the impeller , the hub being configured to be coupled to a motor ; a tapered section provided at an opposite end of the hub , the tapered section defining a media inlet to receive blast media; a plurality of drop-shaped vanes positioned between the hub and the tapered section, the plurality of drop-shaped vanes being spaced from one another on peripheries of the hub and the tapered section, the plurality of drop-shaped vanes defining a plurality of impeller media outlets constructed and arranged to allow egress of blast media upon rotation of the impeller , wherein each vane is drop-shaped having a leading side directed toward a direction of rotation of the impeller and a trailing side opposite the leading side wherein the plurality of drop-shaped vanes being spaced equidistant from one another on peripheries of the hub and the tapered section, wherein the plurality of drop-shaped vanes is spaced from a control cage at a predetermined distance, and wherein each drop-shaped vane has an angle of the leading side between 50° and 70°, preferably an angle between 55° and 60° and a radius of the trailing side between 3 mm and 8 mm, preferably between 4 mm and 7 mm.
A powder feeding center capable of automatically cleaning, comprising a powder barrel , and further comprising a pressure maintaining housing , wherein a pressure detection device is mounted in the pressure maintaining housing , the powder barrel is mounted in the pressure maintaining housing in a hanging way, a feed hopper that can be closed is disposed on the top of the pressure maintaining housing corresponding to the powder barrel , a pressure stabilizing mouth is provided on the top of the pressure maintaining housing , a powder cleaning mouth is provided at the bottom of the pressure maintaining housing , a pressure stabilizing valve is mounted on the pressure stabilizing mouth, and a powder cleaning valve is mounted on the powder cleaning mouth; both of the top and the bottom of the powder barrel are open, an air intake chamber capable of moving up and down in the pressure maintaining housing is disposed at the bottom of the powder barrel , a fluidization plate capable of communicating the air intake chamber with the powder barrel is fixedly mounted on the top of the air intake chamber , the air intake chamber is driven by a driving device mounted on the pressure maintaining housing , and the air intake chamber is capable of closing the bottom of the powder barrel when moving to a highest point; an air intake is provided on the air intake chamber , the air intake is connected to an air intake telescopic tube , an air intake pipe whose end portion protrudes from the pressure maintaining housing is fixedly mounted on the pressure maintaining housing corresponding to the air intake, the air intake telescopic tube is connected to the air intake pipe , and an air intake valve is mounted on the air intake pipe to control opening or closing thereof; at least one powder outlet is provided on a side wall of the powder barrel , and a powder outlet pipe whose end portion protrudes from the pressure maintaining housing is connected to the powder outlet; and a purging device capable of moving up and down and used for purging an inner cavity of the powder barrel is fixedly mounted on the pressure maintaining housing .
An apparatus comprising: - a tool comprising a first portion and a second portion at least partially surrounding the first portion, wherein the first portion is configured to receive a conductor and the second portion is configured to hold a measurement coil ; and - a holder configured to be detachably attached to the tool , wherein the holder is to be employed to install the tool holding the measurement coil onto a conductor , wherein the first portion is configured to snap fit onto the conductor during installation, and the measurement coil at least partially surrounds the conductor when installed, characterised in that the first portion and the second portion form a one-piece structure of flexible material; the first portion is formed of an open-curved wall and a plurality of interconnected elements configured to extend inwards from the open-curved wall towards a centre portion of the tool to apply a force onto the conductor , when installed, and accommodate the conductor in the centre portion thereof, and the second portion is formed of a plurality of fingers spaced apart, extending outwardly from the first portion , each finger having an inner wall connected to the first portion , an outer wall in parallel with the inner wall and a laterally extending base , defining a recess therebetween, and an aperture opposite the base to allow snap-fitting of the measurement coil into said recess to hold the measurement coil when installed - a tool comprising a first portion and a second portion at least partially surrounding the first portion, wherein the first portion is configured to receive a conductor and the second portion is configured to hold a measurement coil ; and - a holder configured to be detachably attached to the tool , wherein the holder is to be employed to install the tool holding the measurement coil onto a conductor , wherein the first portion is configured to snap fit onto the conductor during installation, and the measurement coil at least partially surrounds the conductor when installed, characterised in that the first portion and the second portion form a one-piece structure of flexible material; the first portion is formed of an open-curved wall and a plurality of interconnected elements configured to extend inwards from the open-curved wall towards a centre portion of the tool to apply a force onto the conductor , when installed, and accommodate the conductor in the centre portion thereof, and the second portion is formed of a plurality of fingers spaced apart, extending outwardly from the first portion , each finger having an inner wall connected to the first portion , an outer wall in parallel with the inner wall and a laterally extending base , defining a recess therebetween, and an aperture opposite the base to allow snap-fitting of the measurement coil into said recess to hold the measurement coil when installed
A method for treating a textile product, comprising bringing the textile product into contact with a treatment liquid obtained by mixing the following component (A), the following component (B) and water: component (A): an internal olefin sulfonate having 16 or more and 24 or less carbons; and component (B): a softening base for textile products; wherein the component (B) is one or more compounds selected from a clay mineral and a silicone compound; and wherein a mass ratio of the content of an internal olefin sulfonate having 16 carbons (A C16 ) and the content of an internal olefin sulfonate having 17 or more and 24 or less carbons (A C17-C24 ), (A C16 ) / (A C17-C24 ), in the component (A) is 0 or more and 0.6 or less. component (A): an internal olefin sulfonate having 16 or more and 24 or less carbons; and component (B): a softening base for textile products; wherein the component (B) is one or more compounds selected from a clay mineral and a silicone compound; and wherein a mass ratio of the content of an internal olefin sulfonate having 16 carbons (A C16 ) and the content of an internal olefin sulfonate having 17 or more and 24 or less carbons (A C17-C24 ), (A C16 ) / (A C17-C24 ), in the component (A) is 0 or more and 0.6 or less.
A method of making an article comprises: extruding a layer comprising a melt processable fluoropolymer, wherein the fluoropolymer comprises a copolymer of a tetrafluoroethylene and a perfluoroether, wherein the article has an ultraviolet transmittance of at least 50% when measured at a thickness of 1.016 mm to 1.5748 mm (0.040 inches to 0.062 inches) when exposed to ultraviolet radiation of 200 nm to 280 nm; characterized in that the method comprises cooling the article in liquid to a temperature of less than 25°C, and that the copolymer of tetrafluoroethylene and the perfluoroether is present at a weight percent ratio of 2% to 12%. extruding a layer comprising a melt processable fluoropolymer, wherein the fluoropolymer comprises a copolymer of a tetrafluoroethylene and a perfluoroether, wherein the article has an ultraviolet transmittance of at least 50% when measured at a thickness of 1.016 mm to 1.5748 mm (0.040 inches to 0.062 inches) when exposed to ultraviolet radiation of 200 nm to 280 nm; characterized in that the method comprises cooling the article in liquid to a temperature of less than 25°C, and that the copolymer of tetrafluoroethylene and the perfluoroether is present at a weight percent ratio of 2% to 12%.
A rotor for a turbofan booster section associated with a fan section of a gas turbine engine, the fan section including a fan driven by a shaft , the rotor downstream from the fan, and the rotor comprising: a rotor blade having an airfoil extending in a spanwise direction from 0% span at a root to 100% span at a tip and having a leading edge , a trailing edge and a mean camber line , the airfoil having a delta inlet blade angle defined as a difference between a local inlet blade angle defined by a reference line tangent to the mean camber line at the leading edge at a spanwise location and a second reference line parallel to a center line of the gas turbine engine at the spanwise location and a root inlet blade angle defined by the reference line tangent to the mean camber line at the leading edge at the root and the second reference line parallel to the center line of the gas turbine engine at the root; and a rotor disk coupled to the rotor blade configured to be coupled to the shaft or the fan to rotate with the shaft or the fan, respectively, at the same speed as the shaft and the fan and to receive a portion of a fluid flow from the fan, characterized in that : the delta inlet blade angle decreases in the spanwise direction from the root to a minimum value at greater than 10% span and from the minimum value, the delta inlet blade angle increases to the tip. a rotor blade having an airfoil extending in a spanwise direction from 0% span at a root to 100% span at a tip and having a leading edge , a trailing edge and a mean camber line , the airfoil having a delta inlet blade angle defined as a difference between a local inlet blade angle defined by a reference line tangent to the mean camber line at the leading edge at a spanwise location and a second reference line parallel to a center line of the gas turbine engine at the spanwise location and a root inlet blade angle defined by the reference line tangent to the mean camber line at the leading edge at the root and the second reference line parallel to the center line of the gas turbine engine at the root; and a rotor disk coupled to the rotor blade configured to be coupled to the shaft or the fan to rotate with the shaft or the fan, respectively, at the same speed as the shaft and the fan and to receive a portion of a fluid flow from the fan, characterized in that : the delta inlet blade angle decreases in the spanwise direction from the root to a minimum value at greater than 10% span and from the minimum value, the delta inlet blade angle increases to the tip.
Pitch pellets comprising: - a core constituted of a first composition comprising at least one pitch, said composition having a penetrability at 25°C ranging from 0 to 45 1/10 mm and a ring and ball softening point (RBSP) ranging from 55°C to 175°C, it being understood that the penetrability is measured according to the standard EN 1426 and that the RBSP is measured according to the standard EN 1427, and - a layer coating at least part of the surface of the core, said layer being constituted of a coating composition comprising at least one anticaking agent chosen from pyrogenic silicas, and mixtures thereof. - a core constituted of a first composition comprising at least one pitch, said composition having a penetrability at 25°C ranging from 0 to 45 1/10 mm and a ring and ball softening point (RBSP) ranging from 55°C to 175°C, it being understood that the penetrability is measured according to the standard EN 1426 and that the RBSP is measured according to the standard EN 1427, and - a layer coating at least part of the surface of the core, said layer being constituted of a coating composition comprising at least one anticaking agent chosen from pyrogenic silicas, and mixtures thereof.
A liquid ejecting apparatus comprising: a print head that ejects a liquid; a digital signal output circuit that outputs a digital signal to the print head; and a liquid accommodating container that supplies the liquid to the print head, wherein the print head includes a supply port (SI3) to which the liquid is supplied from the liquid accommodating container, a nozzle plate having a plurality of nozzles that eject the liquid, a substrate that has a first surface and a second surface different from the first surface, a connector to which the digital signal is input, and an integrated circuit to which the digital signal is input via the connector and that outputs an abnormality detection signal indicating presence or absence of an abnormality in the print head, the connector is provided on the first surface, the integrated circuit is provided on the second surface, and characterized in that there is provided: a through hole that penetrates the first surface and the second surface is provided in a mounting region on which the integrated circuit is provided in the substrate. a print head that ejects a liquid; a digital signal output circuit that outputs a digital signal to the print head; and a liquid accommodating container that supplies the liquid to the print head, wherein the print head includes a supply port (SI3) to which the liquid is supplied from the liquid accommodating container, a nozzle plate having a plurality of nozzles that eject the liquid, a substrate that has a first surface and a second surface different from the first surface, a connector to which the digital signal is input, and an integrated circuit to which the digital signal is input via the connector and that outputs an abnormality detection signal indicating presence or absence of an abnormality in the print head, a supply port (SI3) to which the liquid is supplied from the liquid accommodating container, a nozzle plate having a plurality of nozzles that eject the liquid, a substrate that has a first surface and a second surface different from the first surface, a connector to which the digital signal is input, and an integrated circuit to which the digital signal is input via the connector and that outputs an abnormality detection signal indicating presence or absence of an abnormality in the print head, the connector is provided on the first surface, the integrated circuit is provided on the second surface, and characterized in that there is provided: a through hole that penetrates the first surface and the second surface is provided in a mounting region on which the integrated circuit is provided in the substrate.
A supercharger for a vehicle, the supercharger comprising: a lower body housing a compressor ; an upper lid configured to be coupled to the lower body thereby forming a plenum , the upper lid defining an air circulation port ; said supercharger being characterized in that it further comprises a contraction chamber integrally formed in the upper lid adjacent to the air circulation port , the contraction chamber including an attenuator plate defining a tuning neck , the tuning neck defining an inlet to a volume of the contraction chamber and defining part of this volume; wherein the tuning neck includes a predetermined size and shape configured to attenuate a desired sound frequency generated by operation of the supercharger. a lower body housing a compressor ; an upper lid configured to be coupled to the lower body thereby forming a plenum , the upper lid defining an air circulation port ; said supercharger being characterized in that it further comprises a contraction chamber integrally formed in the upper lid adjacent to the air circulation port , the contraction chamber including an attenuator plate defining a tuning neck , the tuning neck defining an inlet to a volume of the contraction chamber and defining part of this volume; wherein the tuning neck includes a predetermined size and shape configured to attenuate a desired sound frequency generated by operation of the supercharger.
A pharmaceutical composition comprising dicycloplatin (DCP) for use in a method of treating or preventing a disease in a subject, wherein the disease is selected from the group consisting of rheumatoid arthritis, gout, lupus, osteoporosis, psoriasis, prostatitis, benign prostatic hyperplasia (BPH), multiple sclerosis, coeliac disease, Sjogren gren's syndrome, Hashimoto's thyroiditis, Graves' disease and graft-versus-host disease (GVHD).
A vehicle pillar member (10, 100; 200; 300; 400; 500) having a length, comprising: a plurality of steel sheets (120A-E; 220A-E; 320A-D; 420A-D; 520A-D) welded along at least one joint line (110a-d; 210a-d; 310a-c; 410a-c; 510a-c) transverse to a longitudinal direction of the vehicle pillar member; for each joint line, the strengths of the steel sheets just above and below the joint line being different; and the joint lines including one or more first joint lines (110a, c; 210a, c; 310a; 410b; 510a, c) inclined with respect to a direction perpendicular to the longitudinal direction of the vehicle pillar member, characterized in that : the one or more joint lines include a second joint line (110b, d; 210b, d; 310b, c; 410a, c; 510b) in at least one of upper and lower ends of the vehicle pillar member, the second joint line being oriented substantially perpendicular to the longitudinal direction, and the strength of the steel sheets (120A, E; 220A, E; 320C, D; 420B, D; 520C) outside the second joint line are smaller than the steel sheet (120B, D; 220B, D; 320A, B; 420A, C; 520B) just inside the second joint line. a plurality of steel sheets (120A-E; 220A-E; 320A-D; 420A-D; 520A-D) welded along at least one joint line (110a-d; 210a-d; 310a-c; 410a-c; 510a-c) transverse to a longitudinal direction of the vehicle pillar member; for each joint line, the strengths of the steel sheets just above and below the joint line being different; and the joint lines including one or more first joint lines (110a, c; 210a, c; 310a; 410b; 510a, c) inclined with respect to a direction perpendicular to the longitudinal direction of the vehicle pillar member, characterized in that : the one or more joint lines include a second joint line (110b, d; 210b, d; 310b, c; 410a, c; 510b) in at least one of upper and lower ends of the vehicle pillar member, the second joint line being oriented substantially perpendicular to the longitudinal direction, and the strength of the steel sheets (120A, E; 220A, E; 320C, D; 420B, D; 520C) outside the second joint line are smaller than the steel sheet (120B, D; 220B, D; 320A, B; 420A, C; 520B) just inside the second joint line.