mhurhangee/patent-ind-claim-en huggingface dataset:
An ultra high pressure pump being coupled to a waterjet cutting machine (W); the water jet cutting machine comprising a cutting head (H) controlled to open and close; the ultra high pressure pump comprising a servo motor coupled to a piston having a head arranged within a cylinder to define a pumping chamber , whereby the servo motor rotation causes reciprocal displacement of the piston to pressurise fluid in the pumping chamber to pressures greater than 3447,3786 bar (50,000 psi); the servo motor having a feedback loop coupled to a computer; the feedback loop including a pressure feedback signal; characterized by the feedback loop being configured to control the pump pressure in real time to store and hold pressure whilst the cutting head is closed and otherwise maintain pressure to suit waterjet cutting without feedback from the cutting head. store and hold pressure whilst the cutting head is closed and otherwise maintain pressure to suit waterjet cutting without feedback from the cutting head.
A nonwoven fabric polishing roll having a through hole into which a rotating shaft of a polishing machine is inserted, comprising: a polishing portion formed by stacking a plurality of circular nonwoven fabrics having an aperture that forms the through hole; and two circular support plates located one at each of both ends in the stacking direction of the polishing portion , having an aperture that forms the through hole, characterized in that the circular support plates have an external diameter that is substantially the same as that of the circular nonwoven fabric; and the circular support plates include nonwoven fabric that is hardened in a compressed state. a polishing portion formed by stacking a plurality of circular nonwoven fabrics having an aperture that forms the through hole; and two circular support plates located one at each of both ends in the stacking direction of the polishing portion , having an aperture that forms the through hole, characterized in that the circular support plates have an external diameter that is substantially the same as that of the circular nonwoven fabric; and the circular support plates include nonwoven fabric that is hardened in a compressed state.
Multi-aperture imaging device (11; 1000; 2000; 3000; 4000; 4000'; 5000; 6000) comprising: at least one image sensor (12; 12a-h); and an array of juxtaposed optical channels (16a-h), wherein each optical channel (16a-d) comprises optics (64a-h) for projecting at least one partial area (74a-d) of an object area (26; 72) on an image sensor area (58a-d) of the image sensor (12; 12a-h); beam-deflecting means for deflecting an optical path (22a-d) of the optical channels (16a-d) in beam-deflecting areas (1002a-c) of the beam-deflecting means ; wherein the beam-deflecting means is formed as an array of facets (68a-d; 68i) arranged along a line-extension direction (z; 146) of the array of optical channels (16a-d) and wherein one facet (68a-d; 68i) is allocated to each optical channel (16a-d) and wherein each facet comprises at least one beam-deflecting area (1002a-c); wherein a stray light suppressing structure is arranged between a first beam-deflecting area of a first facet and a second beam-deflecting area of a juxtaposed second facet , which is configured to reduce transition of stray light between the first beam-deflecting area and the second beam-deflecting area . at least one image sensor (12; 12a-h); and an array of juxtaposed optical channels (16a-h), wherein each optical channel (16a-d) comprises optics (64a-h) for projecting at least one partial area (74a-d) of an object area (26; 72) on an image sensor area (58a-d) of the image sensor (12; 12a-h); beam-deflecting means for deflecting an optical path (22a-d) of the optical channels (16a-d) in beam-deflecting areas (1002a-c) of the beam-deflecting means ; wherein the beam-deflecting means is formed as an array of facets (68a-d; 68i) arranged along a line-extension direction (z; 146) of the array of optical channels (16a-d) and wherein one facet (68a-d; 68i) is allocated to each optical channel (16a-d) and wherein each facet comprises at least one beam-deflecting area (1002a-c); wherein a stray light suppressing structure is arranged between a first beam-deflecting area of a first facet and a second beam-deflecting area of a juxtaposed second facet , which is configured to reduce transition of stray light between the first beam-deflecting area and the second beam-deflecting area .
A device for measuring gas concentration in exhaled air, the device comprising: - a first air inlet configured to introduce air exhaled by a patient into the device, - a second air inlet with a filter configured to introduce filtered ambient air into the device, - an air suction pump , - a sensor configured to measure gas concentration in the exhaled air, - a first valve located downstream of the first air inlet and upstream of the sensor , - a second valve located downstream of the second air inlet and upstream of the sensor , - a third valve located downstream of the sensor and upstream of an air outlet , - a flow meter configured to measure the air flow exhaled by the patient, - a humidity stabiliser configured to stabilise the humidity in the device, and - an air exhaust , characterized in that the humidity stabiliser is arranged downstream of the first air inlet and upstream of the flow meter and the pump is adapted to maintain a constant air flow rate through the sensor when the patient exhales air into the device. - a first air inlet configured to introduce air exhaled by a patient into the device, - a second air inlet with a filter configured to introduce filtered ambient air into the device, - an air suction pump , - a sensor configured to measure gas concentration in the exhaled air, - a first valve located downstream of the first air inlet and upstream of the sensor , - a second valve located downstream of the second air inlet and upstream of the sensor , - a third valve located downstream of the sensor and upstream of an air outlet , - a flow meter configured to measure the air flow exhaled by the patient, - a humidity stabiliser configured to stabilise the humidity in the device, and - an air exhaust , characterized in that the humidity stabiliser is arranged downstream of the first air inlet and upstream of the flow meter and the pump is adapted to maintain a constant air flow rate through the sensor when the patient exhales air into the device.
Kinesiology tape comprising: a first layer of fabric with an adhesive on a first side of the first layer of fabric ; a second layer of fabric coupled to the first layer of fabric , the first layer of fabric and the second layer of fabric forming a receiving portion ; and a support disposed in the receiving portion , the support including a plurality of teeth and a plurality of voids located between the teeth , the support further including a ridge or spine attaching the teeth ; wherein the support is biased so that the teeth and voids facilitate motion in a first plane substantially parallel to the first layer of fabric and resist motion in a second plane substantially perpendicular to the first layer of fabric . a first layer of fabric with an adhesive on a first side of the first layer of fabric ; a second layer of fabric coupled to the first layer of fabric , the first layer of fabric and the second layer of fabric forming a receiving portion ; and a support disposed in the receiving portion , the support including a plurality of teeth and a plurality of voids located between the teeth , the support further including a ridge or spine attaching the teeth ; wherein the support is biased so that the teeth and voids facilitate motion in a first plane substantially parallel to the first layer of fabric and resist motion in a second plane substantially perpendicular to the first layer of fabric .
A prosthetic foot comprising: an attachment member comprising: a first connection portion configured to attach to a stump on a user or another prosthetic device; a second connection portion in a rear portion of the attachment member ; a third connection portion in a front portion of the attachment member ; a first elastic member connected to the attachment member at the third connection portion ; and an actuator connected to the attachment member at the second connection portion , characterized in that a second elastic member is connected to the actuator at a fourth connection portion , the third connection portion providing a rotatable connection, wherein the second elastic member is disposed below the first elastic member characterised in that the third connection portion provides a rotatable connection between the attachment member and the first elastic member. an attachment member comprising: a first connection portion configured to attach to a stump on a user or another prosthetic device; a second connection portion in a rear portion of the attachment member ; a third connection portion in a front portion of the attachment member ; a first connection portion configured to attach to a stump on a user or another prosthetic device; a second connection portion in a rear portion of the attachment member ; a third connection portion in a front portion of the attachment member ; a first elastic member connected to the attachment member at the third connection portion ; and an actuator connected to the attachment member at the second connection portion , characterized in that a second elastic member is connected to the actuator at a fourth connection portion , the third connection portion providing a rotatable connection, wherein the second elastic member is disposed below the first elastic member characterised in that the third connection portion provides a rotatable connection between the attachment member and the first elastic member.
A vehicle turning alarm method comprising: acquiring map information and vehicle information of a vehicle; determining a vehicle status according to the map information and the vehicle information when the vehicle approaches an intersection; acquiring a road curvature according to the map information and acquiring a movement curvature according to the vehicle information; if a difference between the movement curvature and the road curvature is less than or equal to a curvature threshold, or if the difference between the movement curvature and the road curvature is greater than the curvature threshold and a speed of the vehicle is greater than a speed threshold, determining the vehicle status is not a left-turning event and not sending an alert message if the vehicle status is not the left-turning event, whereas if the difference between the movement curvature and the road curvature is greater than the curvature threshold, and the speed of the vehicle is less than or equal to the speed threshold, determining the vehicle status is the left-turning event and sending the alert message; wherein the step of acquiring the movement curvature according to the vehicle information comprises: acquiring a current location (C), a previous location (H), and a predicted location (P) according to the vehicle information and acquiring the movement curvature according to the current location (C), the previous location (H), and the predicted location (P). acquiring map information and vehicle information of a vehicle; determining a vehicle status according to the map information and the vehicle information when the vehicle approaches an intersection; acquiring a road curvature according to the map information and acquiring a movement curvature according to the vehicle information; if a difference between the movement curvature and the road curvature is less than or equal to a curvature threshold, or if the difference between the movement curvature and the road curvature is greater than the curvature threshold and a speed of the vehicle is greater than a speed threshold, determining the vehicle status is not a left-turning event and not sending an alert message if the vehicle status is not the left-turning event, whereas if the difference between the movement curvature and the road curvature is greater than the curvature threshold, and the speed of the vehicle is less than or equal to the speed threshold, determining the vehicle status is the left-turning event and sending the alert message; wherein the step of acquiring the movement curvature according to the vehicle information comprises: acquiring a current location (C), a previous location (H), and a predicted location (P) according to the vehicle information and acquiring the movement curvature according to the current location (C), the previous location (H), and the predicted location (P).
End stop for a binding device for securing a boot to a gliding board, comprising a fixed part which is intended to be secured to the gliding board, and a mobile part which is mounted on the fixed part with a possibility of relative movement (T) with at least one transverse component and on which two jaws are mounted so as to pivot about a substantially longitudinal axis (Ag, Ad), the end stop comprising a lever that is actuable from the outside of the end stop and takes up a blocking position in which blocking elements that are integral with the lever prevent the jaws from tilting so as to keep the end stop in a closed configuration in which the jaws retain the boot, releasing elements engaging with the blocking elements such that the execution of said movement of the mobile part beyond a predetermined travel with respect to the fixed part causes the lever to pass automatically, in particular from the blocking position, towards a freeing position which is different from the blocking position and in which the blocking elements allow the jaws to tilt, characterized in that these blocking elements are formed by lateral flanks of the lever which, in the blocking position of the lever , bear against bearing surfaces that are integral with the jaws , on their inner face.
A radio frequency coupler (100, 100A to 100C) comprising: a waveguide having an outer conductor and an inner conductor provided in a coaxial tube shape, the waveguide linearly extending from a power supply side, being bent in an L shape at a bend section (10b to 12b), and linearly extending toward an acceleration cavity side; and a refrigerant passage part (20, 20A to 20C) which penetrates the outer conductor and the inner conductor from an outside of the waveguide toward the acceleration cavity side at the bend section (10b to 12b) and is connected to an interior of the inner conductor , the refrigerant passage part (20, 20A to 20C) having a passage tube which causes a refrigerant (C) to flow between an interior of a tip portion of the inner conductor on the acceleration cavity side and the outside of the waveguide , characterised in that a portion of the passage tube , exposed to a radio frequency transmission space (K) formed between the outer conductor and the inner conductor , is formed of an insulator. a waveguide having an outer conductor and an inner conductor provided in a coaxial tube shape, the waveguide linearly extending from a power supply side, being bent in an L shape at a bend section (10b to 12b), and linearly extending toward an acceleration cavity side; and a refrigerant passage part (20, 20A to 20C) which penetrates the outer conductor and the inner conductor from an outside of the waveguide toward the acceleration cavity side at the bend section (10b to 12b) and is connected to an interior of the inner conductor , the refrigerant passage part (20, 20A to 20C) having a passage tube which causes a refrigerant (C) to flow between an interior of a tip portion of the inner conductor on the acceleration cavity side and the outside of the waveguide , characterised in that a portion of the passage tube , exposed to a radio frequency transmission space (K) formed between the outer conductor and the inner conductor , is formed of an insulator.
A wing tip device having a first wing tip device element for attaching at a first wing tip device element root to a tip of an aircraft wing , and a second wing tip device element extending from a second wing tip device element root to a second wing tip device element tip, the second wing tip device element root outboard, when viewed in the wing planform direction, of the first wing tip device element root ; the first wing tip device element having a first wing tip device element leading edge and a first wing tip device element trailing edge , and the second wing tip device element having a second wing tip device element leading edge and a second wing tip device element trailing edge ; wherein the second wing tip device element root is attached at a junction to the first wing tip device element outboard, when viewed in the wing planform direction, of the first wing tip device element root , and wherein the second wing tip device element trailing edge at the junction is forward of the first wing tip device element trailing edge at the junction; and characterised by a fairing between the first and second wing tip device element which extends aft from the second wing tip device element trailing edge at least to the first wing tip device element trailing edge . and a second wing tip device element extending from a second wing tip device element root to a second wing tip device element tip, the second wing tip device element root outboard, when viewed in the wing planform direction, of the first wing tip device element root ; the first wing tip device element having a first wing tip device element leading edge and a first wing tip device element trailing edge , and the second wing tip device element having a second wing tip device element leading edge and a second wing tip device element trailing edge ; wherein the second wing tip device element root is attached at a junction to the first wing tip device element outboard, when viewed in the wing planform direction, of the first wing tip device element root , and wherein the second wing tip device element trailing edge at the junction is forward of the first wing tip device element trailing edge at the junction; and characterised by a fairing between the first and second wing tip device element which extends aft from the second wing tip device element trailing edge at least to the first wing tip device element trailing edge .
A superabsorbent polymer resin incorporated with porous superhydrophobic microparticles meeting the following properties i) to ii): i) a BET specific surface area of 700 to 1500 m 2 /g, as determined by BET analyzer, ii) a porosity of 90 % or more, as determined by BET analyzer, wherein the particles have a particle size of 2 nm ~ 50 μm, as determined by ISO 13320, wherein the particles have a superhydrophobicity as large as a water contact angle of 125° or more, as determined by contact angle analyzer KRUSS DSA100, wherein the particles are used in an amount of 0.001 to 1 part by weight, based on 100 parts by weight of the superabsorbent polymer resin, and wherein the particles are silica. i) a BET specific surface area of 700 to 1500 m 2 /g, as determined by BET analyzer, ii) a porosity of 90 % or more, as determined by BET analyzer, wherein the particles have a particle size of 2 nm ~ 50 μm, as determined by ISO 13320, wherein the particles have a superhydrophobicity as large as a water contact angle of 125° or more, as determined by contact angle analyzer KRUSS DSA100, wherein the particles are used in an amount of 0.001 to 1 part by weight, based on 100 parts by weight of the superabsorbent polymer resin, and wherein the particles are silica. wherein the particles have a particle size of 2 nm ~ 50 μm, as determined by ISO 13320, wherein the particles have a superhydrophobicity as large as a water contact angle of 125° or more, as determined by contact angle analyzer KRUSS DSA100, wherein the particles are used in an amount of 0.001 to 1 part by weight, based on 100 parts by weight of the superabsorbent polymer resin, and wherein the particles are silica.
A vehicle behavior control system (A) comprising: a behavior stabilization control module configured to execute a behavior stabilization control so as to stabilize a behavior of a vehicle (CR) by giving a braking force to a turning outer wheel of the vehicle (CR) based on a target braking force (PT), wherein the behavior stabilization control module has a target braking force setting section configured to set the target braking force smaller for a second turn than for a first turn, the first turn being a sharp turn in which the behavior stabilization control is required, occurring first since a straight ahead driving condition or a moderate turn condition where no behavior stabilization control is required, the second turn being an other subsequent sharp turn in which the behavior stabilization control is required after the first turn. a behavior stabilization control module configured to execute a behavior stabilization control so as to stabilize a behavior of a vehicle (CR) by giving a braking force to a turning outer wheel of the vehicle (CR) based on a target braking force (PT), wherein the behavior stabilization control module has a target braking force setting section configured to set the target braking force smaller for a second turn than for a first turn, the first turn being a sharp turn in which the behavior stabilization control is required, occurring first since a straight ahead driving condition or a moderate turn condition where no behavior stabilization control is required, the second turn being an other subsequent sharp turn in which the behavior stabilization control is required after the first turn. a target braking force setting section configured to set the target braking force smaller for a second turn than for a first turn, the first turn being a sharp turn in which the behavior stabilization control is required, occurring first since a straight ahead driving condition or a moderate turn condition where no behavior stabilization control is required, the second turn being an other subsequent sharp turn in which the behavior stabilization control is required after the first turn.
A braiding system , comprising: a plurality of tubes arranged around a longitudinal axis (L), each having an upper portion and a lower portion , wherein individual tubes are configured to receive individual filaments therein; a lower drive unit configured to act against the lower portions of the tubes ; the braiding system being characterized by further comprising: an upper drive unit configured to act against the upper portions of the tubes ; and a mandrel coaxial with the upper and lower drive units ; wherein the upper drive unit and the lower drive unit are configured to act against the upper portions and the lower portions of the tubes in synchronization. a plurality of tubes arranged around a longitudinal axis (L), each having an upper portion and a lower portion , wherein individual tubes are configured to receive individual filaments therein; a lower drive unit configured to act against the lower portions of the tubes ; the braiding system being characterized by further comprising: an upper drive unit configured to act against the upper portions of the tubes ; and a mandrel coaxial with the upper and lower drive units ; wherein the upper drive unit and the lower drive unit are configured to act against the upper portions and the lower portions of the tubes in synchronization. an upper drive unit configured to act against the upper portions of the tubes ; and a mandrel coaxial with the upper and lower drive units ; wherein the upper drive unit and the lower drive unit are configured to act against the upper portions and the lower portions of the tubes in synchronization.