mhurhangee/patent-ind-claim-en huggingface dataset:
A method of making a customized root canal obturation core , the method comprising: generating a three-dimensional image of a root canal having a coronal portion (28; 62), a middle portion , and an apical portion (32; 60), wherein the apical portion includes a physiologic apex of the root canal; generating a three-dimensional model of the root canal and of the root canal obturation core from the three-dimensional image; superimposing the three-dimensional model of the root canal obturation core within the three-dimensional model of the root canal to allow assessment of how the three-dimensional model of the root canal obturation core fills the three-dimensional model of the root canal and to verify that the three-dimensional model of the root canal obturation core fills the entire three-dimensional model of the root canal without forming voids; and using a computer controlled manufacturing system to manufacture the root canal obturation core based on the three-dimensional model of the root canal or of the root canal obturation core, wherein the computer controlled manufacturing system comprises a computer numerically controlled machine or an additive manufacturing machine, and wherein when the contour of the core is inserted in the root canal, the apical portion including the physiologic apex of the root canal, the middle portion of the root canal, and the coronal portion of the root canal are filled with the contour of the core, such that the core fills the entire canal without forming voids. generating a three-dimensional image of a root canal having a coronal portion (28; 62), a middle portion , and an apical portion (32; 60), wherein the apical portion includes a physiologic apex of the root canal; generating a three-dimensional model of the root canal and of the root canal obturation core from the three-dimensional image; superimposing the three-dimensional model of the root canal obturation core within the three-dimensional model of the root canal to allow assessment of how the three-dimensional model of the root canal obturation core fills the three-dimensional model of the root canal and to verify that the three-dimensional model of the root canal obturation core fills the entire three-dimensional model of the root canal without forming voids; and using a computer controlled manufacturing system to manufacture the root canal obturation core based on the three-dimensional model of the root canal or of the root canal obturation core, wherein the computer controlled manufacturing system comprises a computer numerically controlled machine or an additive manufacturing machine, and wherein when the contour of the core is inserted in the root canal, the apical portion including the physiologic apex of the root canal, the middle portion of the root canal, and the coronal portion of the root canal are filled with the contour of the core, such that the core fills the entire canal without forming voids.
A compound having the formula 1: wherein R is selected from unsubstituted, branched- or straight chain, saturated C 5 -C 19 alkyl; unsubstituted, branched- or straight-chain C 5 -C 17 alkenyl; unsubstituted, branched- or straight-chain C 5 -C 17 alkadienyl and unsubstituted C 3 -C 8 cycloalkyl;; R 1 is selected from unsubstituted, straight-chain or branched C 1 -C 6 alkyl or alkenyl groups; or from unsubstituted C 3 -C 8 cycloalkyl; HETN is piperidine; X is O or NH; n is 0 or 1; and m is 1. R is selected from unsubstituted, branched- or straight chain, saturated C 5 -C 19 alkyl; unsubstituted, branched- or straight-chain C 5 -C 17 alkenyl; unsubstituted, branched- or straight-chain C 5 -C 17 alkadienyl and unsubstituted C 3 -C 8 cycloalkyl;; R 1 is selected from unsubstituted, straight-chain or branched C 1 -C 6 alkyl or alkenyl groups; or from unsubstituted C 3 -C 8 cycloalkyl; HETN is piperidine; X is O or NH; n is 0 or 1; and m is 1.
A non-invasive detection method for screening for a well-developed blastocyst, characterized in that , genome of trophectoderm cells of the blastocyst to be detected is subjected to methylation detection; the average DNA methylation level of embryos identified as having a good morphology in Gardner morphological blastocyst grading system is used as a standard; and a blastocyst to be detected is well-developed when its DNA methylation level is close or equal to the standard, wherein the embryos identified as having a good morphology in the Gardner morphological blastocyst grading system refer to blastocysts of AA, AB, BA and BB grades.
A plunger-cylinder assembly, in particular for a master cylinder of a clutch actuation system in a motor vehicle, having a plunger which is arranged axially movably in a cylinder which is configured as a housing and having a sensor system which is attached to the housing and is operatively connected to a sensor fastened to the plunger , characterised in that the sensor system is positioned directly on a leadframe assembly which is integrated into the plastic housing and the plastic housing has an outwardly open recess , in which the leadframe assembly supporting the sensor system is positioned, wherein the recess is closed with a cover , in which a plug device is integrated, which receives the bent leadframe conductors serving as plug contacts of the plug device .
A yarn tension control device comprising: a motor that generates a driving force; a cam configured to be rotatable by the driving force of the motor ; a pair of yarn guides capable to guide a yarn (A) to a predetermined position; a spring that generates a biasing force; and an arm that is freely-rocked and supported along a virtual plane passing between the pair of yarn guides , the arm being biased by the spring , wherein the arm includes an insertion section through which the yarn (A) guided by the pair of yarn guides can be inserted, characterized in that the arm further includes an action section on which the cam can act, the arm being biased by the spring in a direction of applying a tension to the yarn (A), and the arm can be rocked in a direction away from the pair of yarn guides at a position where the biasing force of the spring and the tension of the yarn (A) are balanced by an action of the cam on the action section to increase the tension applied to the yarn (A). a motor that generates a driving force; a cam configured to be rotatable by the driving force of the motor ; a pair of yarn guides capable to guide a yarn (A) to a predetermined position; a spring that generates a biasing force; and an arm that is freely-rocked and supported along a virtual plane passing between the pair of yarn guides , the arm being biased by the spring , wherein the arm includes an insertion section through which the yarn (A) guided by the pair of yarn guides can be inserted, characterized in that the arm further includes an action section on which the cam can act, the arm being biased by the spring in a direction of applying a tension to the yarn (A), and the arm can be rocked in a direction away from the pair of yarn guides at a position where the biasing force of the spring and the tension of the yarn (A) are balanced by an action of the cam on the action section to increase the tension applied to the yarn (A).
A system for tracking movement of an eye , the system comprising: an array of photoelements; a grating configured to collect light reflected from the eye , the grating having a point spread function that focuses light from a point-source to a pattern spatially distributed across non-adjacent ones of the photoelements; and a processor coupled to the array of photoelements configured to compute a location of the point source from features of the pattern. an array of photoelements; a grating configured to collect light reflected from the eye , the grating having a point spread function that focuses light from a point-source to a pattern spatially distributed across non-adjacent ones of the photoelements; and a processor coupled to the array of photoelements configured to compute a location of the point source from features of the pattern.
A method for reporting user equipment assistance information, characterized by comprising: if a configuration in a user equipment, UE, for forbidding sending UE assistance information is not started or is closed and content of the UE assistance information is changed, sending , by the UE, the UE assistance information to a base station; determining, by the UE, a duration after the UE assistance information is sent to the base station reaches a preset duration, wherein the preset duration is 0, starting the configuration for forbidding sending the UE assistance information; and determining, by the UE, a duration in which the configuration for forbidding sending the UE assistance information is started reaches a preset threshold, closing, by the UE, the started configuration for forbidding sending the UE assistance information wherein the UE assistance information is one or more pieces of the following information: a power saving preference of the UE; a performance preference of the UE. if a configuration in a user equipment, UE, for forbidding sending UE assistance information is not started or is closed and content of the UE assistance information is changed, sending , by the UE, the UE assistance information to a base station; determining, by the UE, a duration after the UE assistance information is sent to the base station reaches a preset duration, wherein the preset duration is 0, starting the configuration for forbidding sending the UE assistance information; and determining, by the UE, a duration in which the configuration for forbidding sending the UE assistance information is started reaches a preset threshold, closing, by the UE, the started configuration for forbidding sending the UE assistance information wherein the UE assistance information is one or more pieces of the following information: a power saving preference of the UE; a performance preference of the UE. a power saving preference of the UE; a performance preference of the UE.
An annuloplasty device comprising first and second support rings having a coiled configuration in which the first and second support rings are arranged as a coil around a central axis , wherein the first and second support rings are configured to be arranged on opposite sides of native heart valve leaflets of a heart valve, the first and second support rings have respective free ends , a line attached at a proximal connection at a proximal tip of a first end of one of the free ends, wherein the proximal connection comprises a lumen sized to receive a distal tip of the line, wherein the first end is configured to be compressed to clamp the distal tip of the line inside the lumen. first and second support rings having a coiled configuration in which the first and second support rings are arranged as a coil around a central axis , wherein the first and second support rings are configured to be arranged on opposite sides of native heart valve leaflets of a heart valve, the first and second support rings have respective free ends , a line attached at a proximal connection at a proximal tip of a first end of one of the free ends, wherein the proximal connection comprises a lumen sized to receive a distal tip of the line, wherein the first end is configured to be compressed to clamp the distal tip of the line inside the lumen.
A mounting arrangement for mounting an air-bag module to a vehicle support structure, the mounting arrangement comprising: an air-bag module which incorporates: a base element ; a central support member which is of plastic and which is carried by the base element ; and at least one side wall , the side wall being of metal and being carried by the base element ; and a plurality of spaced apart elongate attachment elements which each incorporate: a first end portion which is formed integrally with the central support member ; and a second end portion which is coupled to the first end portion by an intermediate portion so that the second end portion is positioned remotely from the support element, the second end portion comprising a retainer formation which is of plastic and which is configured to be engaged by a retainer element such that, in use, the attachment element couples the air-bag module to the vehicle support structure and the retainer element retains the air-bag module in a position adjacent to the vehicle support structure. an air-bag module which incorporates: a base element ; a central support member which is of plastic and which is carried by the base element ; and at least one side wall , the side wall being of metal and being carried by the base element ; and a base element ; a central support member which is of plastic and which is carried by the base element ; and at least one side wall , the side wall being of metal and being carried by the base element ; and a plurality of spaced apart elongate attachment elements which each incorporate: a first end portion which is formed integrally with the central support member ; and a second end portion which is coupled to the first end portion by an intermediate portion so that the second end portion is positioned remotely from the support element, the second end portion comprising a retainer formation which is of plastic and which is configured to be engaged by a retainer element such that, in use, the attachment element couples the air-bag module to the vehicle support structure and the retainer element retains the air-bag module in a position adjacent to the vehicle support structure. a first end portion which is formed integrally with the central support member ; and a second end portion which is coupled to the first end portion by an intermediate portion so that the second end portion is positioned remotely from the support element, the second end portion comprising a retainer formation which is of plastic and which is configured to be engaged by a retainer element such that, in use, the attachment element couples the air-bag module to the vehicle support structure and the retainer element retains the air-bag module in a position adjacent to the vehicle support structure.
A catheter assembly comprising: an elongate member having a proximal end and a distal end; the distal end having at least one drainage opening ; a fluid containing member ; and a container containing the elongate member and the fluid containing member; wherein the fluid containing member comprises a material which swells when exposed to a fluid and which absorbs and retains said fluid in a wall between an inner diameter and an outer diameter, and wherein the outer diameter of the fluid containing member is fluid impermeable so as not to wet the container when contacting the same, and wherein the fluid containing member is non-removably coupled to the container. an elongate member having a proximal end and a distal end; the distal end having at least one drainage opening ; a fluid containing member ; and a container containing the elongate member and the fluid containing member; wherein the fluid containing member comprises a material which swells when exposed to a fluid and which absorbs and retains said fluid in a wall between an inner diameter and an outer diameter, and wherein the outer diameter of the fluid containing member is fluid impermeable so as not to wet the container when contacting the same, and wherein the fluid containing member is non-removably coupled to the container.
A ship steering control device comprising: angle difference calculation means for calculating an angle difference (δ) between a course of a ship and a target direction; rotation speed measurement means for measuring a rotation speed of a propeller of the ship; target load calculation means of calculating a target load (Fp) serving as a target load to be applied to a rudder based on the angle difference (δ) calculated by the angle difference calculation means and the rotation speed measured by the rotation speed measurement means ; load measurement means for measuring a load on the rudder; a ship steering machine for turning the rudder; and ship steering control means for controlling a rudder angle by the ship steering machine to match the load on the rudder measured by the load measurement means to the target load (Fp) calculated by the target load calculation means . angle difference calculation means for calculating an angle difference (δ) between a course of a ship and a target direction; rotation speed measurement means for measuring a rotation speed of a propeller of the ship; target load calculation means of calculating a target load (Fp) serving as a target load to be applied to a rudder based on the angle difference (δ) calculated by the angle difference calculation means and the rotation speed measured by the rotation speed measurement means ; load measurement means for measuring a load on the rudder; a ship steering machine for turning the rudder; and ship steering control means for controlling a rudder angle by the ship steering machine to match the load on the rudder measured by the load measurement means to the target load (Fp) calculated by the target load calculation means .
A method, comprising: removing a worn portion from a component of a rotary isobaric pressure exchanger (IPX, 30) configured to exchange pressures between a first fluid and a second fluid, wherein the component comprises at least one of a rotor or an end cover including a removable end portion that is detachably connected to the rotor or the end cover , the removable end portion having the worn portion , and wherein the worn portion comprises at least one surface on the rotor or the end cover , the at least one surface being a surface of an interface region between the rotor and the end cover ; and repairing the component after the worn portion is removed from the component by coupling a replacement portion to the component , wherein the replacement portion has a similar structure to the removable end portion before the removable end portion being worn. removing a worn portion from a component of a rotary isobaric pressure exchanger (IPX, 30) configured to exchange pressures between a first fluid and a second fluid, wherein the component comprises at least one of a rotor or an end cover including a removable end portion that is detachably connected to the rotor or the end cover , the removable end portion having the worn portion , and wherein the worn portion comprises at least one surface on the rotor or the end cover , the at least one surface being a surface of an interface region between the rotor and the end cover ; and repairing the component after the worn portion is removed from the component by coupling a replacement portion to the component , wherein the replacement portion has a similar structure to the removable end portion before the removable end portion being worn.
A method comprising: receiving , at a user plane function, UPF, for use in a mobile network, from a first user equipment, UE, a first message which indicates a domain name server, DNS, request for obtaining an address of a server associated with a multi-access edge computing, MEC, application; sending , from the UPF to an address resolution server, a second message which indicates a corresponding DNS request, the corresponding DNS request including a client subnet of the first UE; receiving , at the UPF from the address resolution server as a DNS response, a third message which includes a client subnet location-dependent server address associated with the MEC application; sending , from the UPF to the first UE as a DNS response, a message which includes the received client subnet location-dependent server address; sending , from the UPF to a control plane, CP, entity for session management, the server address or location data determined from the server address; and selecting , by the CP entity and using the server address or location data, UPF instances for UE sessions based on the location of the MEC application. receiving , at a user plane function, UPF, for use in a mobile network, from a first user equipment, UE, a first message which indicates a domain name server, DNS, request for obtaining an address of a server associated with a multi-access edge computing, MEC, application; sending , from the UPF to an address resolution server, a second message which indicates a corresponding DNS request, the corresponding DNS request including a client subnet of the first UE; receiving , at the UPF from the address resolution server as a DNS response, a third message which includes a client subnet location-dependent server address associated with the MEC application; sending , from the UPF to the first UE as a DNS response, a message which includes the received client subnet location-dependent server address; sending , from the UPF to a control plane, CP, entity for session management, the server address or location data determined from the server address; and selecting , by the CP entity and using the server address or location data, UPF instances for UE sessions based on the location of the MEC application.
Connecting device (13; 113) for producing a cable-bound supply of an electrical consuming device , which is movable in at least one direction of travel (F) with respect to a feed device (12; 112), with electrical energy and/or data, wherein the feed device (12; 112) has at least one terminal (14, 14'; 114, 114', 114") to connect to a corresponding connecting element (6; 106) of a cable carried by the consuming device , wherein the connecting device (13; 113) has a manipulator (18; 118) to connect the connecting element (6; 106) to the terminal (14, 14'; 114, 114', 114"), characterised in that the connecting device (13; 113) is arranged on the feed device (12; 112).
An automatic takeoff system comprising: at least one air data measuring sensor; at least one inertial sensor; and at least one processor coupled to the air data measuring sensor and the inertial sensor, the at least one processor accessing takeoff speeds VR and V2 to provide both longitudinal and lateral-directional control surface control to provide automatic takeoff of an aircraft; characterised in that the at least one processor is configured to command the aircraft to a bank angle in which an optimal take-off performance is achieved, and limiting the bank angle to avoid the wing tips hitting the ground. at least one air data measuring sensor; at least one inertial sensor; and at least one processor coupled to the air data measuring sensor and the inertial sensor, the at least one processor accessing takeoff speeds VR and V2 to provide both longitudinal and lateral-directional control surface control to provide automatic takeoff of an aircraft; characterised in that the at least one processor is configured to command the aircraft to a bank angle in which an optimal take-off performance is achieved, and limiting the bank angle to avoid the wing tips hitting the ground.