mhurhangee/patent-ind-claim-en huggingface dataset:
An introducer , comprising: an inner liner including a lumen , a proximal region , and at least one folded portion extending longitudinally along the proximal region; an expandable support member , the support member includes a spine extending along the length of the support member and a plurality of ribs extending along a length of the support member , the plurality of ribs including a first set of rib members and a second set of rib members ; and a sheath attached to at least a portion of the support member ; characterized in that the support member is designed to shift from a first position in which the first set of rib members interdigitate with the second set of rib members to an expanded position in which the first set of rib members and the second set of rib members radially separate from one another, in that the spine is attached to the sheath, and in that the plurality of ribs are free to move relative to the liner , the sheath , or both the liner and the sheath . an inner liner including a lumen , a proximal region , and at least one folded portion extending longitudinally along the proximal region; an expandable support member , the support member includes a spine extending along the length of the support member and a plurality of ribs extending along a length of the support member , the plurality of ribs including a first set of rib members and a second set of rib members ; and a sheath attached to at least a portion of the support member ; characterized in that the support member is designed to shift from a first position in which the first set of rib members interdigitate with the second set of rib members to an expanded position in which the first set of rib members and the second set of rib members radially separate from one another, in that the spine is attached to the sheath, and in that the plurality of ribs are free to move relative to the liner , the sheath , or both the liner and the sheath .
A capacity control valve (V) comprising: a valve housing provided with a discharge port through which a discharge fluid of discharge pressure (Pd) passes, a suction port through which a suction fluid of suction pressure (Ps) passes, and a control port through which a control fluid of control pressure (Ps) passes; and a valve element (51, , , 351) configured to be brought into contact with and separated from a valve seat by a driving force of a solenoid to open and close a communication between the control port and the discharge port or a communication between the control port and the suction port , wherein a sliding region (S) is formed by an inner peripheral surface of the valve housing and an outer peripheral surface of the valve element , a groove extending in a circumferential direction is formed in at least one of the inner peripheral surface of the valve housing and the outer peripheral surface of the valve element , the sliding region (S) has a structure in which a swirling current (W) is generated in the groove by a fluid flowing from a high-pressure side to a low-pressure side in a clearance (C) between the inner peripheral surface of the valve housing and the outer peripheral surface of the valve element (51, , , 351), characterized in that a radial length of the clearance (C) is within a range from 1/10 to 1/300 of an axial length of the sliding region (S), and the groove includes at least two threads of spiral grooves . a valve housing provided with a discharge port through which a discharge fluid of discharge pressure (Pd) passes, a suction port through which a suction fluid of suction pressure (Ps) passes, and a control port through which a control fluid of control pressure (Ps) passes; and a valve element (51, , , 351) configured to be brought into contact with and separated from a valve seat by a driving force of a solenoid to open and close a communication between the control port and the discharge port or a communication between the control port and the suction port , wherein a sliding region (S) is formed by an inner peripheral surface of the valve housing and an outer peripheral surface of the valve element , a groove extending in a circumferential direction is formed in at least one of the inner peripheral surface of the valve housing and the outer peripheral surface of the valve element , the sliding region (S) has a structure in which a swirling current (W) is generated in the groove by a fluid flowing from a high-pressure side to a low-pressure side in a clearance (C) between the inner peripheral surface of the valve housing and the outer peripheral surface of the valve element (51, , , 351), characterized in that a radial length of the clearance (C) is within a range from 1/10 to 1/300 of an axial length of the sliding region (S), and the groove includes at least two threads of spiral grooves .
An accommodating intraocular lens, IOL, configured to be implanted within a capsular bag of a patient's eye, the lens comprising: a flexible optic membrane configured to be placed along the optical axis of the patient's eye; a flexible skirt extending from an outer periphery of the flexible optic membrane, the flexible skirt defining an outer periphery of the accommodating IOL; a capsular contact ring configured to be positioned along the optical axis of the patient's eye anterior to the flexible optic membrane, the capsular contact ring having a diameter less than a diameter at the outer periphery of the accommodating IOL; and a plurality of strut assemblies connecting the capsular contact ring and flexible skirt; wherein the lens is adapted such that when the capsular bag transitions from an accommodative state to a disaccomadative state, the capsular bag exerts a force on the capsular contact ring, at least a portion of that force being transferred to the flexible skirt by the plurality of strut assemblies, the transferred force causing a flattening of the flexible optic membrane in a manner that reduces the optical power of the accommodating IOL. a flexible optic membrane configured to be placed along the optical axis of the patient's eye; a flexible skirt extending from an outer periphery of the flexible optic membrane, the flexible skirt defining an outer periphery of the accommodating IOL; a capsular contact ring configured to be positioned along the optical axis of the patient's eye anterior to the flexible optic membrane, the capsular contact ring having a diameter less than a diameter at the outer periphery of the accommodating IOL; and a plurality of strut assemblies connecting the capsular contact ring and flexible skirt; wherein the lens is adapted such that when the capsular bag transitions from an accommodative state to a disaccomadative state, the capsular bag exerts a force on the capsular contact ring, at least a portion of that force being transferred to the flexible skirt by the plurality of strut assemblies, the transferred force causing a flattening of the flexible optic membrane in a manner that reduces the optical power of the accommodating IOL.
Luminous device for a motor vehicle comprising a substrate on which is arranged at least one element (122, 124; 222, 224; 322, 324) of an electronic circuit comprising at least one electronic component sensitive to an electrostatic discharge, and a structure that is distinct from the substrate capable of carrying electric charge, the smallest distance between the structure and each of the elements of the circuit being equal to D1, and an electrically conductive means electrically connected to ground, the device comprising at least one element for protecting against electrostatic discharges , which is placed on the structure and electrically connected thereto, characterized in that the smallest distance between the protective element and the electrically conductive means , D2, is smaller than D1 and non-zero, without there being physical contact between the protecting element and the electrically conductive means connected to ground.
A lamp for a vehicle , comprising: at least one light emitting unit ; a sensor configured to generate data about an object located outside the vehicle ; a housing having an opening, and accommodating the at least one light emitting unit and the sensor ; and a cover lens covering the opening, characterized in that the cover lens comprises: a first lens ; and a second lens contacting at least one surface of the first lens , and having a refractive index different from a refractive index of the first lens , and, wherein the refractive index of the second lens is smaller than the refractive index of the fist lens . at least one light emitting unit ; a sensor configured to generate data about an object located outside the vehicle ; a housing having an opening, and accommodating the at least one light emitting unit and the sensor ; and a cover lens covering the opening, characterized in that the cover lens comprises: a first lens ; and a second lens contacting at least one surface of the first lens , and having a refractive index different from a refractive index of the first lens , and, wherein the refractive index of the second lens is smaller than the refractive index of the fist lens . a first lens ; and a second lens contacting at least one surface of the first lens , and having a refractive index different from a refractive index of the first lens , and, wherein the refractive index of the second lens is smaller than the refractive index of the fist lens .
A method for training a machine learning engine, comprising: obtaining an executable file, and dividing the executable file into a plurality of to-be-extracted parts based on a data directory of the executable file; extracting information entropy features of all the to-be-extracted parts, and performing data transformation on the information entropy features to obtain static features; and training a machine learning engine using the static features; wherein the dividing the executable file into a plurality of to-be-extracted parts based on a data directory of the executable file comprises: dividing the executable file into an executable file header part, an executable file section part, an executable file Overlay data part, and an executable file integral part based on the data directory of the executable file. obtaining an executable file, and dividing the executable file into a plurality of to-be-extracted parts based on a data directory of the executable file; extracting information entropy features of all the to-be-extracted parts, and performing data transformation on the information entropy features to obtain static features; and training a machine learning engine using the static features; wherein the dividing the executable file into a plurality of to-be-extracted parts based on a data directory of the executable file comprises: dividing the executable file into an executable file header part, an executable file section part, an executable file Overlay data part, and an executable file integral part based on the data directory of the executable file.
A seat for aircraft passenger comprising a fixed support portion and a movable portion that is movable with respect to said fixed support portion , said movable portion providing a back part and a sitting part , said seat being turned in a first direction so that when a passenger is sitting in said seat he is turned in said first direction, said seat being configured in such a manner that said movable portion performs a recline movement along a respective recline axis (A) between a sitting position and a recline position, and vice versa, in a plan view of said seat said recline axis (A) being an apparent axis of substantial symmetry of the seat , said seat being characterized in that it is configured so that the movable portion is apt to perform a translation movement with respect to the fixed support portion , parallel to a single and predetermined translation axis (B), wherein from a plan view of said seat , said translation axis (B) is oriented with respect to said recline axis (A) by a predetermined fixed angle (α) comprised between 2° and 18°, in particular between 2° and 12°, preferably equivalent to about 5°.
A concrete ceiling, comprising at least one module which comprises a row of a plurality of displacement bodies being adjacently arranged in a horizontal longitudinal direction (L), which are held captively in a grid structure made of at least two individual grids running in the longitudinal direction (L), wherein each of the grids comprises at least a first and a second longitudinal bar (11, 12 or 21, 22), arranged at a distance in parallel to one another and running in the longitudinal direction (L), and a plurality of transverse bars being arranged at a distance from one another, which are respectively connected with the longitudinal bars (11, 12 or 21, 22), wherein at least one of the displacement bodies for each grid comprises respectively at least one first retaining device (311 or 321) and at least one second retaining device (412 or 422) on its outer side, said retaining devices being formed and arranged in relation to one another in such a way that both respective grids are at least interlockingly and captively secured between the first and second retaining device by accommodating the first longitudinal bar (11 or 21) in the first retaining device (311 or 321) and accommodating the second longitudinal bar (12 or 22) in the second retaining device (412 or 422), and thereby holding together all displacement bodies characterized in that the grid surfaces of the grids are oriented in a transverse or inclined manner in relation to the horizontal, whereby each grid comprises a plurality of transverse bars being oriented in a transverse or inclined manner in relation to the horizontal, which are respectively connected to the longitudinal bars (11, 12 or 21, 22).
A deployment system configured for controlled release of an apparatus relative to a small satellite, comprising: an electrical power source ; an energy release device in communication with the power source, and including a resistive element configured to generate heat via the electrical power source; a fusible line configured to be affixed to a structural component of the satellite, wherein the fusible line is configured to be also affixed to at least one deployable apparatus secured to the satellite; wherein the fusible line is configured for contact with the energy release device, and is meltable by the heat of the resistive element, for deployment of the apparatus, wherein the energy release device is a burn bar , characterised in that the burn bar comprises: the resistive element, wherein the resistive element is a reusable resistive element having a substrate body securable to the satellite; an insulative material deposited on an outer surface of the substrate body; a layer of electroconductive material deposited over an external portion of the insulative material; wherein the fusible line comprises a monofilament or multi-strand line secured directly against the electroconductive material, wherein the electroconductive material is configured to be electrically heated to the melting point of the monofilament or the multi-strand line to cause release of the apparatus secured to the monofilament or the multi-strand line. an electrical power source ; an energy release device in communication with the power source, and including a resistive element configured to generate heat via the electrical power source; a fusible line configured to be affixed to a structural component of the satellite, wherein the fusible line is configured to be also affixed to at least one deployable apparatus secured to the satellite; wherein the fusible line is configured for contact with the energy release device, and is meltable by the heat of the resistive element, for deployment of the apparatus, wherein the energy release device is a burn bar , the resistive element, wherein the resistive element is a reusable resistive element having a substrate body securable to the satellite; an insulative material deposited on an outer surface of the substrate body; a layer of electroconductive material deposited over an external portion of the insulative material; wherein the fusible line comprises a monofilament or multi-strand line secured directly against the electroconductive material, wherein the electroconductive material is configured to be electrically heated to the melting point of the monofilament or the multi-strand line to cause release of the apparatus secured to the monofilament or the multi-strand line.
An antifouling structure, comprising: a base; a surface layer that is formed on a surface of the base and comprises a microporous structure with micropores; and a fluorine-containing liquid retained in the micropores of the microporous structure, wherein elemental fluorine is present in a surface of the microporous structure, wherein an average diameter of surface openings of the micropores in the microporous structure ranges from 10 nm to 500 nm, and wherein a thickness of the surface layer ranges from 100 to 1000 nm. a base; a surface layer that is formed on a surface of the base and comprises a microporous structure with micropores; and a fluorine-containing liquid retained in the micropores of the microporous structure, wherein elemental fluorine is present in a surface of the microporous structure, wherein an average diameter of surface openings of the micropores in the microporous structure ranges from 10 nm to 500 nm, and wherein a thickness of the surface layer ranges from 100 to 1000 nm.
An obstetrical instrument, in particular of the forceps type, for extracting by pulling a foetus during childbirth including two branches , each branch being equipped, at one end, with a gripping handle and, at the other end, with cephalic blades characterised in that the instrument comprises one measurement module per blade and means for connection between the measurement module and the blade , said measurement module including: - first pressure measurement means , capable of measuring the pressure exerted by said blade on the foetus, - second means for measuring the positioning of the obstetrical instrument in space, - power supply means , - means for transmitting the measurements to a processing unit. - first pressure measurement means , capable of measuring the pressure exerted by said blade on the foetus, - second means for measuring the positioning of the obstetrical instrument in space, - power supply means , - means for transmitting the measurements to a processing unit.
An electrical insulation system with low environmental impact for medium- or high-voltage electrical switchgear, comprising: a) a gaseous medium formed by a mixture of: i. one or more non-flammable hydrofluoroolefins with at least 4 carbon atoms; and ii. one or more carrier gases selected from N 2 , O 2 , dry air, helium, CO 2 or mixtures thereof; b) a drying agent wherein the drying agent is a molecular sieve with a pore size of 3 to 6 Å and a polar surface wherein the hydrofluoroolefins with at least 4 carbon atoms are cis-1,1,1,4,4,4-hexafluoro-2-butene (HFO-1336mzzZ), trans-1,1,1,4,4,4-hexafluoro-2-butene (HFO-1336mzzE) or a combination of both. a) a gaseous medium formed by a mixture of: i. one or more non-flammable hydrofluoroolefins with at least 4 carbon atoms; and ii. one or more carrier gases selected from N 2 , O 2 , dry air, helium, CO 2 or mixtures thereof; i. one or more non-flammable hydrofluoroolefins with at least 4 carbon atoms; and ii. one or more carrier gases selected from N 2 , O 2 , dry air, helium, CO 2 or mixtures thereof; b) a drying agent wherein the drying agent is a molecular sieve with a pore size of 3 to 6 Å and a polar surface
A chain type cutting apparatus for continuous cutting of a rope of a center-filled consumable product into individual pieces comprising: a first continuous elongate rotary chain defining a plurality of first open die cavity portions; and a second continuous elongate rotary chain defining a plurality of second open die cavity portions; said first and second die cavity portions being mutually engageable to form a closed die cavity about said rope of product, thereby forming said pieces, said product remaining within said closed die cavity for a dwell time; wherein the number of said first and second die cavity portions being in simultaneous engagement being at least 10; and wherein said first and second chains are rotatable at a speed of from 30 m/min to 200 m/min; wherein each of said first and second chains has a major diameter length and said chain defines a length of closed die cavities, and wherein the ratio of the closed die cavity length to the major diameter length is from 0.3-0.6 to 1. a first continuous elongate rotary chain defining a plurality of first open die cavity portions; and a second continuous elongate rotary chain defining a plurality of second open die cavity portions; said first and second die cavity portions being mutually engageable to form a closed die cavity about said rope of product, thereby forming said pieces, said product remaining within said closed die cavity for a dwell time; wherein the number of said first and second die cavity portions being in simultaneous engagement being at least 10; and wherein said first and second chains are rotatable at a speed of from 30 m/min to 200 m/min; wherein each of said first and second chains has a major diameter length and said chain defines a length of closed die cavities, and wherein the ratio of the closed die cavity length to the major diameter length is from 0.3-0.6 to 1.
An amino acid dehydrogenase mutant having the sequence SEQ ID NO: 1 with a mutation, wherein the mutation is one of the following mutation sites: lysine at the 64th site is mutated into aspartic acid; cysteine at the 133rd site is mutated into threonine; phenylalanine at the 137th site is mutated into alanine; phenylalanine at the 148th site is mutated into valine; proline at the 191st site is mutated into glutamic acid; arginine at the 183rd site is mutated into cysteine and tyrosine at the 207th site is mutated into arginine; arginine at the 183rd site is mutated into cysteine, histidine at the 229th site is mutated into serine and phenylalanine at the 148th site is mutated into alanine; arginine at the 183rd site is mutated into cysteine, histidine at the 229th site is mutated into serine and tyrosine at the 207th site is mutated into arginine; arginine at the 183rd site is mutated into cysteine, histidine at the 229th site is mutated into serine and phenylalanine at the 148th site is mutated into valine; arginine at the 183rd site is mutated into cysteine, histidine at the 229th site is mutated into serine and tyrosine at the 207th site is mutated into glutamic acid; arginine at the 183rd site is mutated into valine, histidine at the 229th site is mutated into serine and phenylalanine at the 148th site is mutated into alanine; threonine at the 173rd site is mutated into histidine, histidine at the 229th site is mutated into serine and phenylalanine at the 148th site is mutated into alanine.
Electronic watch including a display device comprising a time dial , a first hand and a second hand which pivot coaxially, independently driven by two drive members, and in a first display mode, one hand indicates the hour, and the other indicates the minutes of the current time in reference to the respective position of said hands on the time dial , characterized in that the watch further includes a control member able to activate a second display mode, in which the first and second hands are positioned in reference to the time dial in order to respectively indicate the tens and units of the date.