mhurhangee/patent-ind-claim-en huggingface dataset:
A mooring device comprising: a weight structure which sinks by gravity to be seated on a seabed; an anchor portion which is settled on the seabed to anchor a floating body; and a connecting member which includes one end portion connected to the floating body and the other end portion connected to the anchor portion , the connecting member having an extension direction that is changed by passing through a direction changing portion provided in the weight structure , characterized in that the direction changing portion comprises: a rotating portion arranged to be rotatable around a rotation shaft provided in the weight structure; a holding portion provided at one end portion of the rotating portion and configured to hold inward the connecting member , allowing the connecting member to extend; and a fixer provided at the other end portion of the rotating portion , and fixed in the seabed when the rotating portion is rotated by tension of the connecting member . a weight structure which sinks by gravity to be seated on a seabed; an anchor portion which is settled on the seabed to anchor a floating body; and a connecting member which includes one end portion connected to the floating body and the other end portion connected to the anchor portion , the connecting member having an extension direction that is changed by passing through a direction changing portion provided in the weight structure , characterized in that the direction changing portion comprises: a rotating portion arranged to be rotatable around a rotation shaft provided in the weight structure; a holding portion provided at one end portion of the rotating portion and configured to hold inward the connecting member , allowing the connecting member to extend; and a fixer provided at the other end portion of the rotating portion , and fixed in the seabed when the rotating portion is rotated by tension of the connecting member . a rotating portion arranged to be rotatable around a rotation shaft provided in the weight structure; a holding portion provided at one end portion of the rotating portion and configured to hold inward the connecting member , allowing the connecting member to extend; and a fixer provided at the other end portion of the rotating portion , and fixed in the seabed when the rotating portion is rotated by tension of the connecting member .
A gas turbine engine comprising: a planetary gear system including a sun gear , intermediate gears , and a ring gear ; a carrier attached to a fan drive shaft through a torque shaft to rotate a fan , wherein the intermediate gears are supported by the carrier ; a ring gear flexible coupling connecting the ring gear to an engine static structure ; and a sun gear flexible coupling connecting the sun gear to a drive shaft ; wherein the ring gear flexible coupling and the sun gear flexible coupling define a lateral and transverse stiffness and a stop on the engine static structure limits movement of the planetary gear system , characterized in that : the gas turbine engine includes a bypass ratio of greater than 10; and a lubricant manifold is attached to the torque shaft and rotates with the torque shaft about an axis (A) of the engine , a feeder tube is configured to provide lubricant through passages within the torque shaft to an intermediate lubricant passage , the intermediate lubricant passage configured to pass lubricant through a conduit to passages defined within the carrier . a planetary gear system including a sun gear , intermediate gears , and a ring gear ; a carrier attached to a fan drive shaft through a torque shaft to rotate a fan , wherein the intermediate gears are supported by the carrier ; a ring gear flexible coupling connecting the ring gear to an engine static structure ; and a sun gear flexible coupling connecting the sun gear to a drive shaft ; wherein the ring gear flexible coupling and the sun gear flexible coupling define a lateral and transverse stiffness and a stop on the engine static structure limits movement of the planetary gear system , characterized in that : the gas turbine engine includes a bypass ratio of greater than 10; and a lubricant manifold is attached to the torque shaft and rotates with the torque shaft about an axis (A) of the engine , a feeder tube is configured to provide lubricant through passages within the torque shaft to an intermediate lubricant passage , the intermediate lubricant passage configured to pass lubricant through a conduit to passages defined within the carrier . the gas turbine engine includes a bypass ratio of greater than 10; and a lubricant manifold is attached to the torque shaft and rotates with the torque shaft about an axis (A) of the engine , a feeder tube is configured to provide lubricant through passages within the torque shaft to an intermediate lubricant passage , the intermediate lubricant passage configured to pass lubricant through a conduit to passages defined within the carrier .
A method for removing hydrophilic body soils, from fabrics comprising the steps of: a) washing the fabrics in a first wash liquor, the first wash comprising a carboxylate builder selected from the group consisting of: aminocarboxylate builders having 1 to 3 amino groups and 2 to 6 carboxylic acid groups, wherein the carboxylate builder is selected from the group consisting of: glutamic acid N,N diacetic acid (GLDA), methylglycine diacectic acid (MGDA), and mixtures thereof; and water; b) washing the fabrics in a second wash liquor comprising detersive surfactant. a) washing the fabrics in a first wash liquor, the first wash comprising a carboxylate builder selected from the group consisting of: aminocarboxylate builders having 1 to 3 amino groups and 2 to 6 carboxylic acid groups, wherein the carboxylate builder is selected from the group consisting of: glutamic acid N,N diacetic acid (GLDA), methylglycine diacectic acid (MGDA), and mixtures thereof; and water; b) washing the fabrics in a second wash liquor comprising detersive surfactant.
An asphalt composition comprising a crosslinked product prepared by ionically crosslinking a polymer derived from styrene, butadiene, and 0.5%-10% by weight of a carboxylic acid monomer using an ionic crosslinking agent and asphalt.
A method, in a multipath TCP session, comprising: for every N multipath TCP packets to be transmitted as part of the session, generating an error correction packet using payload data and control information of the N multipath TCP packets; transmitting the generated error correction packet along with the N multipath TCP packets; modifying an error correction overhead ratio , representing the ratio of error correction packets to N, according to an average payload packet loss rate; generating an average payload packet loss rate over a predetermined time interval using measures of the total transmitted payload packets and the total retransmitted payload packets over the interval; and comparing the average payload packet loss rate to a predetermined threshold value, wherein the error correction overhead ratio is modified to reduce the ratio when the average payload packet loss rate is greater than the threshold value or to increase the ratio when the average payload packet loss rate is less than the threshold value. for every N multipath TCP packets to be transmitted as part of the session, generating an error correction packet using payload data and control information of the N multipath TCP packets; transmitting the generated error correction packet along with the N multipath TCP packets; modifying an error correction overhead ratio , representing the ratio of error correction packets to N, according to an average payload packet loss rate; generating an average payload packet loss rate over a predetermined time interval using measures of the total transmitted payload packets and the total retransmitted payload packets over the interval; and comparing the average payload packet loss rate to a predetermined threshold value, wherein the error correction overhead ratio is modified to reduce the ratio when the average payload packet loss rate is greater than the threshold value or to increase the ratio when the average payload packet loss rate is less than the threshold value.
A method of wireless communication by a user equipment, UE, comprising: generating uplink control information, UCI, the UCI including a group acknowledgement/negative acknowledgement, GACK, a Rank Indicator, RI, and a channel state information, CSI, wherein the GACK includes a group of acknowledgements/negative acknowledgements for data transmission received by the UE in a plurality of downlink subframes from a base station, BS; sending the UCI to the BS in a listen before talk, LBT, subframe, wherein the generating the UCI comprises coding and multiplexing at least two of the GACK, the RI, and the CSI separately when the UCI is sent in a physical uplink shared channel, PUSCH, or an enhanced PUSCH, ePUSCH; and wherein the generating the UCI comprises coding at least two of the GACK, the RI, and the CSI jointly when the UCI is sent in a physical uplink control channel, PUCCH, or an enhanced PUCCH, ePUCCH. generating uplink control information, UCI, the UCI including a group acknowledgement/negative acknowledgement, GACK, a Rank Indicator, RI, and a channel state information, CSI, wherein the GACK includes a group of acknowledgements/negative acknowledgements for data transmission received by the UE in a plurality of downlink subframes from a base station, BS; sending the UCI to the BS in a listen before talk, LBT, subframe, wherein the generating the UCI comprises coding and multiplexing at least two of the GACK, the RI, and the CSI separately when the UCI is sent in a physical uplink shared channel, PUSCH, or an enhanced PUSCH, ePUSCH; and wherein the generating the UCI comprises coding at least two of the GACK, the RI, and the CSI jointly when the UCI is sent in a physical uplink control channel, PUCCH, or an enhanced PUCCH, ePUCCH.
Clasp for wristbands, comprising a device for adjusting the useful length of the wristband (2-8), said device for adjusting the useful length comprising a movable part and a support device (20-23), the movable part being arranged so to be displaceable relative to said support device (20-23) during a length adjustment, one of said movable part and said support device (20-23) comprising a stop structure and the other comprising an indexing member , said stop structure being intended to be positioned in a notch of the indexing member , in order to determine a discrete and stable value of the length of the wristband, characterized in that said stop structure comprises a tooth having an asymmetrical profile, said tooth comprising a first and a second bearing surface and in that , seen in profile, said bearing surfaces each follow a straight line, each of the straight lines forming an angle (α, ß) with respect to a plane which is normal to the displacement direction of the movable part, each of the angles (α, ß) being non-zero, the angles (α, ß) not being identical, and in that said movable part , said tooth and said notch are arranged in such a way that, when a determined pulling force is exerted by a user, said force acting in a direction in the longitudinal direction on said movable part or on a wristband strand connected to said movable part , said force is transmitted to said tooth so as to disengage said tooth from said notch and generate a displacement of the movable part in the longitudinal direction, resulting in the lengthening of said useful length of the wristband.
A method for manufacturing a shell mould with several layers including at least one contact layer , from a model of wax or other similar material of a part to be manufactured, the method comprising a step of dipping the model into a contact slip forming the contact layer and comprising a binder and a powder, characterized in that the powder comprises a mullite-zirconia composite.
Solenoid valve having an actuator body , in which a magnet coil is arranged which interacts with a magnet core , and which interacts with an armature that can be moved relative to the magnet core between two end positions and is acted upon by the spring force of an armature spring in a movement direction pointing away from the magnet core , and wherein the magnet core and the armature have stopping surfaces which are interrupted by a recess that receives the armature spring , wherein the magnet core has a rounded configuration which reduces a stress on the edges in the region of the stopping surfaces , characterized in that the rounded configuration of the magnet core is a toroidal configuration in the region of at least its stopping surface .
Drug delivery device comprising a dose setting member for setting user variable doses of a medicament and a display for indicating the dose set by the dose setting member , wherein the display comprises a number wheel , which is rotationally coupled to the dose setting member and is provided with a series of markings on its outer circumference, characterised in that the drug delivery device further comprises at least one prism deviating the image of the markings of the number wheel , preferably by 90°, wherein the number wheel is rotatable about an axis and wherein the at least one prism is arranged such that the image of the markings of the number wheel is deviated in a direction parallel to said axis.
A braided article of footwear comprising: a sole ; a unitary braided upper formed from a first yarn and coupled to the sole and having a toe portion , a heel portion , a midfoot portion extending between the toe portion and the heel portion , and a throat portion ; and at least one braided lace formed from a second yarn different from the first yarn , the braided lace integrated with the braided upper , at a lace integration portion of the braided upper , characterized in that the second yarn is a high-performance yarn .
An artwork substrate including a substantially rectangular receiving portion adapted to receive an art medium, and a frame forming element extending from each side of the receiving portion, wherein each frame forming element includes an outer side panel foldably connected to a respective side of the receiving portion , a rear panel foldably connected to the outer side panel, an inner side panel foldably connected to the rear panel and a front panel foldably connected to the inner side panel; wherein the substrate is formed from a single sheet of substrate material, the substrate has a planar configuration and a folded configuration, and when in the folded configuration the outer side panels extend substantially perpendicularly to the receiving portion , the rear panels are arranged parallel to and spaced from the receiving portion , the inner side panels extend from the rear panels towards the receiving portion such that each inner side panel is opposite and substantially parallel to the respective outer side panel, and the front panels are arranged parallel to and adjacent to the receiving panel , whereby each frame forming element forms a rectangular section frame member on one side of the receiving portion; wherein each frame forming element includes one part of a two-part locking mechanism at each end thereof; and wherein when the frame forming elements are in the folded configuration, adjacent ends of the frame forming elements are secured together by the locking mechanism, characterised in that the substrate material is formed from a laminate comprising a layer of a wood pulp material and a layer of a polymeric material; and each end of the frame forming elements includes a locking tab , wherein each tab is located within a respective channel defined by the adjacent frame forming element when the substrate is secured in its folded configuration.
A surgical device comprising: a handle assembly; an elongated portion configured to extend distally from the handle assembly and including an outer wall; an end effector configured to operatively engage a distal portion of the elongated portion; and a plurality of ventilation holes extending through the outer wall of the elongated portion and configured to allow fluid to travel therethrough from an interior portion of the elongated portion to ambient air, and characterized in that the plurality of ventilation holes is configured to minimize the amount of fluid entering into the elongated portion therethrough, wherein each of the plurality of ventilation holes is sized small enough such that fluid does not easily enter the surgical device while simultaneously being large enough such that moisture can exit the surgical device. a handle assembly; an elongated portion configured to extend distally from the handle assembly and including an outer wall; an end effector configured to operatively engage a distal portion of the elongated portion; and a plurality of ventilation holes extending through the outer wall of the elongated portion and configured to allow fluid to travel therethrough from an interior portion of the elongated portion to ambient air, and characterized in that the plurality of ventilation holes is configured to minimize the amount of fluid entering into the elongated portion therethrough, wherein each of the plurality of ventilation holes is sized small enough such that fluid does not easily enter the surgical device while simultaneously being large enough such that moisture can exit the surgical device.
A speckle measurement apparatus, comprising: an imager configured to capture scattered light images returned from an object to be measured when the object to be measured is irradiated with coherent light as speckle images; a controller configured to determine a measurement area that is a same site of the object to be measured in a plurality of the speckle images captured continuously in time series by the imager by incorporating a displacement amount of a relative positional relationship between the object to be measured and the imager ; divide a coordinate space of a speckle image captured by the imager into a plurality of divided areas (D1-D16) each having a predetermined size; determine the divided area having least area-specific noise components as the measurement area; characterised in that the controller is further configured to retrieve an area with a highest coincidence with the speckle image of the measurement area from a speckle image at next time; and regard the retrieved area as the measurement area at the next time. an imager configured to capture scattered light images returned from an object to be measured when the object to be measured is irradiated with coherent light as speckle images; a controller configured to determine a measurement area that is a same site of the object to be measured in a plurality of the speckle images captured continuously in time series by the imager by incorporating a displacement amount of a relative positional relationship between the object to be measured and the imager ; divide a coordinate space of a speckle image captured by the imager into a plurality of divided areas (D1-D16) each having a predetermined size; determine the divided area having least area-specific noise components as the measurement area; characterised in that the controller is further configured to retrieve an area with a highest coincidence with the speckle image of the measurement area from a speckle image at next time; and regard the retrieved area as the measurement area at the next time. determine a measurement area that is a same site of the object to be measured in a plurality of the speckle images captured continuously in time series by the imager by incorporating a displacement amount of a relative positional relationship between the object to be measured and the imager ; divide a coordinate space of a speckle image captured by the imager into a plurality of divided areas (D1-D16) each having a predetermined size; determine the divided area having least area-specific noise components as the measurement area; characterised in that the controller is further configured to retrieve an area with a highest coincidence with the speckle image of the measurement area from a speckle image at next time; and regard the retrieved area as the measurement area at the next time.
Method for producing a plurality of semiconductor lasers comprising the following steps: a) providing a carrier wafer containing a semiconductor material or a ceramic material, b) producing a composite by applying a plurality of optically pumpable semiconductor laser chips in a wafer composite to a top side of the carrier wafer , c) singulating the composite to form a plurality of semiconductor lasers by means of laser cutting or wafer sawing, wherein - each semiconductor laser comprises a mounting block and at least one semiconductor laser chip , - the mounting block is formed from a part of the original carrier wafer, - each mounting block has a mounting area which runs substantially perpendicular to a top surface of the mounting block , on which the semiconductor laser chip is arranged; and - the mounting area is produced during singulation of the composite, wherein - the mounting area is intended for mounting on a module carrier. a) providing a carrier wafer containing a semiconductor material or a ceramic material, b) producing a composite by applying a plurality of optically pumpable semiconductor laser chips in a wafer composite to a top side of the carrier wafer , c) singulating the composite to form a plurality of semiconductor lasers by means of laser cutting or wafer sawing, wherein - each semiconductor laser comprises a mounting block and at least one semiconductor laser chip , - the mounting block is formed from a part of the original carrier wafer, - each mounting block has a mounting area which runs substantially perpendicular to a top surface of the mounting block , on which the semiconductor laser chip is arranged; and - the mounting area is produced during singulation of the composite, wherein - the mounting area is intended for mounting on a module carrier. - the mounting block is formed from a part of the original carrier wafer, - each mounting block has a mounting area which runs substantially perpendicular to a top surface of the mounting block , on which the semiconductor laser chip is arranged; and - the mounting area is produced during singulation of the composite, wherein - the mounting area is intended for mounting on a module carrier.
An intraocular lens implant for the correction of vision comprising: a single flexible optical lens , and one or two haptics of flexible plastic material attached to the single flexible optical lens , wherein the one or two haptics comprise at least one integral shape memory bar having a shape memory alloy segment with a transition temperature between 50 degrees Celsius and 500 degrees Celsius, characterized in that the integral shape memory bar is provided with at least one crinkled portion that coincides with an expansion zone of the haptic , both deformable when the shape memory alloy segment reaches its transition temperature. a single flexible optical lens , and one or two haptics of flexible plastic material attached to the single flexible optical lens , wherein the one or two haptics comprise at least one integral shape memory bar having a shape memory alloy segment with a transition temperature between 50 degrees Celsius and 500 degrees Celsius, characterized in that the integral shape memory bar is provided with at least one crinkled portion that coincides with an expansion zone of the haptic , both deformable when the shape memory alloy segment reaches its transition temperature.