mhurhangee/patent-ind-claim-en huggingface dataset:
A monitoring system for an energy storage system comprising a plurality of energy storage cells , comprising - at least one stretchable electronic unit , and - a communication element , the stretchable electronic unit comprising a conductive material and a stretchable sheet , the conductive material being printed on the stretchable sheet , the stretchable electronic unit being arrangeable at least at one of the energy storage cells , the stretchable electronic unit being configured to generate data based on strain applied on the stretchable electronic unit , the stretchable electronic unit comprising a processing element , the processing element being connected to the stretchable electronic unit and configured to parse data generated by the stretchable electronic unit , and the communication element being integrated in the stretchable electronic unit and configured to transfer data generated by the stretchable electronic unit . - at least one stretchable electronic unit , and - a communication element , the stretchable electronic unit comprising a conductive material and a stretchable sheet , the conductive material being printed on the stretchable sheet , the stretchable electronic unit being arrangeable at least at one of the energy storage cells , the stretchable electronic unit being configured to generate data based on strain applied on the stretchable electronic unit , the stretchable electronic unit comprising a processing element , the processing element being connected to the stretchable electronic unit and configured to parse data generated by the stretchable electronic unit , and the communication element being integrated in the stretchable electronic unit and configured to transfer data generated by the stretchable electronic unit .
A heat shield , comprising: a first portion having a first end and a second end ; a second portion integrally formed with the first end of the first portion, the second portion configured to form at least a partially hemmed edge ; and a sealing member having an opening positioned along a longitudinal axis of the sealing member, wherein the partially hemmed edge is adapted and configured to mechanically retain the sealing member, the sealing member being positioned along at least a portion of the partially hemmed edge; characterised in that the opening is a slit comprising a substantially annular end . a first portion having a first end and a second end ; a second portion integrally formed with the first end of the first portion, the second portion configured to form at least a partially hemmed edge ; and a sealing member having an opening positioned along a longitudinal axis of the sealing member, wherein the partially hemmed edge is adapted and configured to mechanically retain the sealing member, the sealing member being positioned along at least a portion of the partially hemmed edge; characterised in that the opening is a slit comprising a substantially annular end .
A method of operation of a radio node that utilizes a Polar encoder, comprising: performing Polar encoding of a plurality of bits to provide a plurality of Polar-encoded code bits; re-ordering the plurality of Polar-encoded code bits to provide a plurality of re-ordered Polar-encoded code bits; storing the plurality of re-ordered Polar-encoded code bits in a circular buffer or linear buffer; extracting a first M bits from the circular buffer or the linear buffer as a plurality of rate-matched Polar-encoded code bits if a desired code rate for the plurality of rate-matched Polar-encoded code bits is within a first code rate region; and extracting M bits from the circular buffer or the linear buffer starting at an (N-M)-th bit of the circular buffer or the linear buffer as the plurality of rate-matched Polar-encoded code bits if the desired code rate for the plurality of rate-matched Polar-encoded code bits is within the second code rate region; wherein M < N. performing Polar encoding of a plurality of bits to provide a plurality of Polar-encoded code bits; re-ordering the plurality of Polar-encoded code bits to provide a plurality of re-ordered Polar-encoded code bits; storing the plurality of re-ordered Polar-encoded code bits in a circular buffer or linear buffer; extracting a first M bits from the circular buffer or the linear buffer as a plurality of rate-matched Polar-encoded code bits if a desired code rate for the plurality of rate-matched Polar-encoded code bits is within a first code rate region; and extracting M bits from the circular buffer or the linear buffer starting at an (N-M)-th bit of the circular buffer or the linear buffer as the plurality of rate-matched Polar-encoded code bits if the desired code rate for the plurality of rate-matched Polar-encoded code bits is within the second code rate region; wherein M < N.
A method for configuring a frame structure, the method comprising: transmitting configuration information of a first period and first indication information to a terminal through broadcast information by a network side device; wherein the first period is a frame period configured for a carrier or a period in which a uplink transmission appears, the first period comprises a plurality of time-domain transmission granularities, and each of the plurality of time-domain transmission granularities comprises one or more symbols; the first indication information is used to indicate whether a time-domain transmission resource available for the uplink transmission exists in the first period or not; and if the time-domain transmission resource available for the uplink transmission exists in the first period, at least a last symbol in a last time-domain transmission granularity in the frame period is used for the uplink transmission, the first indication information is further used to indicate a start position of the time-domain transmission resource available for the uplink transmission, wherein at most one switch point for switching a transmission direction is comprised in the first period, and a switch direction at the switch point is from downlink transmission to uplink transmission. transmitting configuration information of a first period and first indication information to a terminal through broadcast information by a network side device; wherein the first period is a frame period configured for a carrier or a period in which a uplink transmission appears, the first period comprises a plurality of time-domain transmission granularities, and each of the plurality of time-domain transmission granularities comprises one or more symbols; the first indication information is used to indicate whether a time-domain transmission resource available for the uplink transmission exists in the first period or not; and if the time-domain transmission resource available for the uplink transmission exists in the first period, at least a last symbol in a last time-domain transmission granularity in the frame period is used for the uplink transmission, the first indication information is further used to indicate a start position of the time-domain transmission resource available for the uplink transmission, wherein at most one switch point for switching a transmission direction is comprised in the first period, and a switch direction at the switch point is from downlink transmission to uplink transmission.
A coffee machine having a base , a body extending upwardly from the base , a platform having an upward facing surface and a coupling portion , the platform being supported by and extending outwardly from the body , and a filter basket , characterized in that the filter basket includes: a downward facing bottom surface supported on the upward facing surface , a recess located in the bottom surface of the filter basket to receive the coupling portion of the platform ; at least one downwardly facing locating feature cooperating with the platform to aid alignment of the filter basket with the platform ; wherein the upward facing surface of the platform includes at least one upwardly facing locating feature for engagement with the downwardly facing location feature to at least aid in locating the filter basket in an engaged position with the coupling portion , characterised in that the at least one locating feature is an array of locating features for simultaneous cooperation with the platform to aid alignment of the filter basket with the platform , and the array of locating features consists of protrusions from the bottom surface of the filter basket , and the protrusions are retractable into the bottom surface and biased to protrude from the bottom surface . a downward facing bottom surface supported on the upward facing surface , a recess located in the bottom surface of the filter basket to receive the coupling portion of the platform ; at least one downwardly facing locating feature cooperating with the platform to aid alignment of the filter basket with the platform ; wherein the upward facing surface of the platform includes at least one upwardly facing locating feature for engagement with the downwardly facing location feature to at least aid in locating the filter basket in an engaged position with the coupling portion , characterised in that the at least one locating feature is an array of locating features for simultaneous cooperation with the platform to aid alignment of the filter basket with the platform , and the array of locating features consists of protrusions from the bottom surface of the filter basket , and the protrusions are retractable into the bottom surface and biased to protrude from the bottom surface .
Thermoplastic composition comprising matrix polymer consisting of polyolefin, TPE polyolefin or TPE, carbon nanotubes (CNTs), conductive carbon black and organic liquid salt wherein the proportion of matrix polymer in the composition is from 55% by weight to 81.5% by weight based on the total weight of the sum of matrix polymer, CNT, conductive carbon black and organic liquid salt; and the proportion of CNT in the composition is from 3% by weight to 10% by weight based on the total weight of the sum of matrix polymer, CNT, conductive carbon black and organic liquid salt; and the proportion of conductive carbon black in the composition is from 15% by weight to 30% by weight based on the total weight of the sum of matrix polymer, CNT, conductive carbon black and organic liquid salt; and the proportion of organic liquid salt in the composition is from 0.15% by weight to 5% by weight based on the total weight of the sum of matrix polymer, CNT, conductive carbon black and organic liquid salt; and the sum of matrix polymer, CNTs, conductive carbon black and organic liquid salt is at least 65% by weight based on the total weight of the composition.
Method of manufacturing a rim from a fibrous composite material for bicycle wheels equipped with a disk brake, employing a tool device , wherein the tool device comprises a plurality of tool components (50a-50c), wherein the tool components (50a-50c) comprise two molding devices and one circular device , wherein the molding devices each comprise a flank contact surface for forming a lateral rim flank , and the circular device comprises a rim well contact surface , with the following steps: - At least part of the tool components (50a-50c) is provided, and a first smooth varnish coat is applied to at least one rim contact surface on the tool components (50a-50c); - The first smooth varnish coat is dried; - A first fiber layer of the fibrous composite material is applied to the flank contact surface of the molding devices , forming the outer fiber layers of at least the greater part of the visible surface of the rim flanks ; - At least one first fiber layer of the fibrous composite material is applied to the circular device , forming the rim well ; - The tool components (50a-50c) of the tool device are interconnected, and the tool device is closed/locked; - The tool device is heated up, and the varnish coat firmly bonds with the hardening fibrous composite material; - The tool device is cooled down, and the rim is removed, and spoke holes are made. - At least part of the tool components (50a-50c) is provided, and a first smooth varnish coat is applied to at least one rim contact surface on the tool components (50a-50c); - The first smooth varnish coat is dried; - A first fiber layer of the fibrous composite material is applied to the flank contact surface of the molding devices , forming the outer fiber layers of at least the greater part of the visible surface of the rim flanks ; - At least one first fiber layer of the fibrous composite material is applied to the circular device , forming the rim well ; - The tool components (50a-50c) of the tool device are interconnected, and the tool device is closed/locked; - The tool device is heated up, and the varnish coat firmly bonds with the hardening fibrous composite material; - The tool device is cooled down, and the rim is removed, and spoke holes are made.
A slat support assembly comprising: a slat comprising an outer face and an inner face , a slat support arm which defines an arc having an axis of rotation, wherein the slat support arm is movable to deploy the slat (23 from a leading edge of an aircraft wing about the axis of rotation of the slat support arm ; first and second slat mounting lugs to extend from the inner face of the slat and attach the slat support arm to the slat , wherein the first slat mounting lug is coupled to one end of said slat support arm by a first joint ; and a link arm to extend between the slat support arm and the slat and pivotally mounted to the slat support arm by a second joint and to the second slat mounting lug by a third joint , wherein the second joint is spaced from the first joint along the slat support arm ; wherein a triangular truss is defined by the link arm , a section of the slat support arm between the first and second joints , and a section of the slat between the first and second slat mounting lugs , to prevent rotation of the slat about the first joint on an axis extending parallel to the axis of rotation of the slat support arm ; and wherein the first joint is configured to allow the first slat mounting lug to slide along the axis extending parallel to the axis of rotation of the slat support arm . a slat comprising an outer face and an inner face , a slat support arm which defines an arc having an axis of rotation, wherein the slat support arm is movable to deploy the slat (23 from a leading edge of an aircraft wing about the axis of rotation of the slat support arm ; first and second slat mounting lugs to extend from the inner face of the slat and attach the slat support arm to the slat , wherein the first slat mounting lug is coupled to one end of said slat support arm by a first joint ; and a link arm to extend between the slat support arm and the slat and pivotally mounted to the slat support arm by a second joint and to the second slat mounting lug by a third joint , wherein the second joint is spaced from the first joint along the slat support arm ; wherein a triangular truss is defined by the link arm , a section of the slat support arm between the first and second joints , and a section of the slat between the first and second slat mounting lugs , to prevent rotation of the slat about the first joint on an axis extending parallel to the axis of rotation of the slat support arm ; and wherein the first joint is configured to allow the first slat mounting lug to slide along the axis extending parallel to the axis of rotation of the slat support arm .
Device for determining a respiratory feature of a subject based on a breathing gas generated by the subject when inhaling and exhaling, comprising: - an aerosol detection unit for detecting an aerosol contained in the breathing gas; - a deposition fraction measurement unit for measuring a deposition fraction for the detected aerosol, wherein the deposition fraction indicates the fraction of aerosol deposited inside the subject over the total amount of the inhaled aerosol, wherein the deposition fraction measurement unit is configured to measure a particle concentration for a plurality of particle sizes of the detected aerosol, and wherein the deposition fraction comprises a plurality of values each corresponding to a particle size of the plurality of particle sizes; and - a respiratory feature determination unit for determining the respiratory feature by relating the measured deposition fraction to a plurality of predetermined deposition fractions each corresponding to a different airway geometry of a respiratory tract, wherein each airway geometry corresponds to a different part or section of said respiratory tract. - an aerosol detection unit for detecting an aerosol contained in the breathing gas; - a deposition fraction measurement unit for measuring a deposition fraction for the detected aerosol, wherein the deposition fraction indicates the fraction of aerosol deposited inside the subject over the total amount of the inhaled aerosol, wherein the deposition fraction measurement unit is configured to measure a particle concentration for a plurality of particle sizes of the detected aerosol, and wherein the deposition fraction comprises a plurality of values each corresponding to a particle size of the plurality of particle sizes; and - a respiratory feature determination unit for determining the respiratory feature by relating the measured deposition fraction to a plurality of predetermined deposition fractions each corresponding to a different airway geometry of a respiratory tract, wherein each airway geometry corresponds to a different part or section of said respiratory tract.
A washing machine comprising: a cabinet comprising side frames that form exterior sides of the washing machine ; a tub for storing washing water disposed in the cabinet; and a rotating tub that is rotatably disposed in the tub for accommodating laundry, wherein each side frame comprises beads for reinforcing rigidity, characterized in that the beads protrude further towards an outside of the side frame as they get closer to a centre of the side frame , wherein the centre of the side frame is defined by an intersection point Q between a first imaginary centre line M that crosses upper and lower portions of the side frame , and a second imaginary centre line N that crosses the front and rear of the side frame and is perpendicular to the first centre line M. a cabinet comprising side frames that form exterior sides of the washing machine ; a tub for storing washing water disposed in the cabinet; and a rotating tub that is rotatably disposed in the tub for accommodating laundry, wherein each side frame comprises beads for reinforcing rigidity, characterized in that the beads protrude further towards an outside of the side frame as they get closer to a centre of the side frame , wherein the centre of the side frame is defined by an intersection point Q between a first imaginary centre line M that crosses upper and lower portions of the side frame , and a second imaginary centre line N that crosses the front and rear of the side frame and is perpendicular to the first centre line M.
A fixture for transferring a plurality of turbine blades , each having a dovetail, into a rotor wheel of a turbomachine , the rotor wheel including a plurality of circumferentially spaced dovetail slots , the fixture comprising: a first body having an arcuate radially inward surface and a radially outward surface including a plurality of dovetail slots therein shaped to engage the dovetails of the plurality of turbine blades , wherein the arcuate radially inward surface of the first body is shaped to contact a rotor of the turbomachine and shaped to contact a platform , the platform being axially coupled to and/or mounted on an axial sidewall of the rotor wheel ; and a first alignment aperture extending axially through the first body relative to a centerline axis of the turbomachine , and positioned for alignment with a portion of the rotor wheel such that the plurality of dovetail slots of the first body are substantially axially aligned with the plurality of dovetail slots of the rotor wheel for at least partial transfer of the turbine blade thereto from the fixture , wherein the dovetails of the plurality of turbine blades are slidably removable from the plurality of dovetail slots of the first body for guided insertion into the plurality of dovetail slots of the rotor wheel , characterized in that said at least first alignment aperture is positioned circumferentially between dovetail slots of the fixture, and is designed and arranged in a way that it allows a user to align said dovetail slots of said fixture with said dovetail slots of said rotor wheel by receiving or at least partially engaging an alignment pin into said first alignment aperture. a first body having an arcuate radially inward surface and a radially outward surface including a plurality of dovetail slots therein shaped to engage the dovetails of the plurality of turbine blades , wherein the arcuate radially inward surface of the first body is shaped to contact a rotor of the turbomachine and shaped to contact a platform , the platform being axially coupled to and/or mounted on an axial sidewall of the rotor wheel ; and a first alignment aperture extending axially through the first body relative to a centerline axis of the turbomachine , and positioned for alignment with a portion of the rotor wheel such that the plurality of dovetail slots of the first body are substantially axially aligned with the plurality of dovetail slots of the rotor wheel for at least partial transfer of the turbine blade thereto from the fixture , wherein the dovetails of the plurality of turbine blades are slidably removable from the plurality of dovetail slots of the first body for guided insertion into the plurality of dovetail slots of the rotor wheel , characterized in that said at least first alignment aperture is positioned circumferentially between dovetail slots of the fixture, and is designed and arranged in a way that it allows a user to align said dovetail slots of said fixture with said dovetail slots of said rotor wheel by receiving or at least partially engaging an alignment pin into said first alignment aperture.
A handle comprising a first tube , on which a grip is arranged, and a second tube that is axially spaced apart from the first tube , and furthermore comprising an elastic body of an elastomer as a first material with a first flexural rigidity and at least one reinforcing element of a second material with a second flexural rigidity, wherein the first flexural rigidity is smaller than the second flexural rigidity, wherein the reinforcing element is entirely or partially accommodated in the elastic body , wherein the elastic body has two opposite fastening ends , by means of which it is respectively fastened on a tube , wherein the elastic body has between both fastening ends a flexurally active axial length under the influence of a force acting upon a fastening end in an arbitrary radial direction, wherein the flexurally active axial length is a part of or the entire axial length, which is located between the tubes and defines the axial distance of both tubes from one another, and wherein the flexural rigidity is the degree of the radial excursion, which occurs when an approximately radially directed force is exerted upon one of its fastening ends in relation to the opposite fastening end , upon which no force is exerted, characterized in that the flexural rigidity of the unit consisting of the elastic body and the reinforcing element can be adjusted by varying the flexurally active axial length either - by varying the fastening depth of the fastening ends in the tubes such that the axial distance between both tubes is reduced or - by means of a sleeve that can be reversibly locked and moved from one fastening end to the other fastening end . - by varying the fastening depth of the fastening ends in the tubes such that the axial distance between both tubes is reduced or - by means of a sleeve that can be reversibly locked and moved from one fastening end to the other fastening end .