mhurhangee/patent-ind-claim-en huggingface dataset:
A method of detecting anomalies in a deployed cloud service based on mining time-evolving graphs, the method comprising the steps, implemented in one or more processors , of: receiving tracing data for a plurality of micro-services of the deployed cloud service, wherein the tracing data defines relationships between the plurality of micro-services of the deployed cloud service at a plurality of different time intervals; computing a functional graph based on the tracing data for each of the plurality of different time intervals, wherein nodes of each functional graph include the plurality of micro-services and wherein links between the nodes represent relationships between the plurality of micro-services; comparing the functional graphs for each of the plurality of time intervals to determine an anomaly score for each of the functional graphs; and detecting a presence of one or more anomalies based on the anomaly scores; wherein the step of computing a functional graph includes computing a weight for each of the links in the functional graph based on a weight function between micro-services that depend on parameters capturing the dynamic of each interaction between the plurality of micro-services; wherein the step of comparing the functional graphs includes comparing different functional graphs from consecutive or non-consecutive time windows; wherein the anomaly score scores heavy changes in historically similar graphs heavily and small changes lightly. receiving tracing data for a plurality of micro-services of the deployed cloud service, wherein the tracing data defines relationships between the plurality of micro-services of the deployed cloud service at a plurality of different time intervals; computing a functional graph based on the tracing data for each of the plurality of different time intervals, wherein nodes of each functional graph include the plurality of micro-services and wherein links between the nodes represent relationships between the plurality of micro-services; comparing the functional graphs for each of the plurality of time intervals to determine an anomaly score for each of the functional graphs; and detecting a presence of one or more anomalies based on the anomaly scores; wherein the step of computing a functional graph includes computing a weight for each of the links in the functional graph based on a weight function between micro-services that depend on parameters capturing the dynamic of each interaction between the plurality of micro-services; wherein the step of comparing the functional graphs includes comparing different functional graphs from consecutive or non-consecutive time windows; wherein the anomaly score scores heavy changes in historically similar graphs heavily and small changes lightly.
A dual-chambered drug delivery device, comprising: a cartridge having a first chamber for storing a medicament; a second chamber in fluid communication with said first chamber ; a dose setting member for setting a medicament dose to be injected at an injection site; a drive screw movably connected to said dose setting member such that rotation of said dose setting member moves said drive screw upwardly; a bevel gear rotatably connected to said dose setting member such that downward movement of said drive screw rotates said dose setting member , which rotates said bevel gear , said bevel gear including a cam shaft ; a piston movably connected to said bevel gear via said cam shaft and disposed in said second chamber , an upward stroke of said piston drawing a discrete portion of the medicament dose into said second chamber and a downward stroke of said piston expelling the discrete portion of the medicament ; and a needle communicating with said second chamber for sequentially injecting portions of the medicament dose into the injection site, characterized by a clutch connected to said dose setting member , said clutch separating said dose setting member from said bevel gear when the medicament dose is being set and causing said dose setting member to engage said bevel gear and rotate said bevel gear when said medicament dose is being delivered, and rotation of the bevel gear causing the cam shaft to drive the piston up and down in a reciprocating manner, thereby injecting the set medicament dose through several smaller sequential discrete portions of medicament injections. a cartridge having a first chamber for storing a medicament; a second chamber in fluid communication with said first chamber ; a dose setting member for setting a medicament dose to be injected at an injection site; a drive screw movably connected to said dose setting member such that rotation of said dose setting member moves said drive screw upwardly; a bevel gear rotatably connected to said dose setting member such that downward movement of said drive screw rotates said dose setting member , which rotates said bevel gear , said bevel gear including a cam shaft ; a piston movably connected to said bevel gear via said cam shaft and disposed in said second chamber , an upward stroke of said piston drawing a discrete portion of the medicament dose into said second chamber and a downward stroke of said piston expelling the discrete portion of the medicament ; and a needle communicating with said second chamber for sequentially injecting portions of the medicament dose into the injection site, characterized by a clutch connected to said dose setting member , said clutch separating said dose setting member from said bevel gear when the medicament dose is being set and causing said dose setting member to engage said bevel gear and rotate said bevel gear when said medicament dose is being delivered, and rotation of the bevel gear causing the cam shaft to drive the piston up and down in a reciprocating manner, thereby injecting the set medicament dose through several smaller sequential discrete portions of medicament injections.
A method for displaying a virtual environment during an in-flight simulation, the method comprising the procedures of: selecting a simulation environment for a training simulation of an airborne platform ; operating the airborne platform in a flight within a real environment; determining the position and orientation with respect to the selected simulation environment of a see-through display viewable by an operator of the airborne platform ; displaying at least one simulation image overlaid conformally onto an external scene viewed via the see-through display , in accordance with the determined position and orientation, the simulation image comprising a view from a virtual altitude of simulation environmental terrain in the selected simulation environment, while the airborne platform is in flight at a real altitude above real environmental terrain in the real environment, the virtual altitude above the simulation environmental terrain being a lower altitude than the real altitude above the real environmental terrain ; and displaying the simulation image such that the simulation environment is adaptive to operator manipulations of the airborne platform , while subjecting the airborne platform to physical constraints reflecting flight limitations in the training simulation involving limitations on which flight maneuvers can be performed and in what manner. selecting a simulation environment for a training simulation of an airborne platform ; operating the airborne platform in a flight within a real environment; determining the position and orientation with respect to the selected simulation environment of a see-through display viewable by an operator of the airborne platform ; displaying at least one simulation image overlaid conformally onto an external scene viewed via the see-through display , in accordance with the determined position and orientation, the simulation image comprising a view from a virtual altitude of simulation environmental terrain in the selected simulation environment, while the airborne platform is in flight at a real altitude above real environmental terrain in the real environment, the virtual altitude above the simulation environmental terrain being a lower altitude than the real altitude above the real environmental terrain ; and displaying the simulation image such that the simulation environment is adaptive to operator manipulations of the airborne platform , while subjecting the airborne platform to physical constraints reflecting flight limitations in the training simulation involving limitations on which flight maneuvers can be performed and in what manner.
Stator stage of a compressor of an aircraft turbine engine comprising: - an annular inner ferrule comprising at least one segment constituted of a composite material; - an annular outer ferrule surrounding said inner ferrule ; - a plurality of stator blades extending radially from said inner ferrule to said outer ferrule, each comprising a pressure face to deviate an airflow; - at least one auxiliary blade disposed at a smaller distance from a first of said stator blades than other stator blades , comprising a pressure face of a smaller area than an area of the pressure face of said first stator blade ; characterised in that said at least one auxiliary blade : - comprises a root at least partially buried in said composite material; and - extends radially, from said root , parallel to and totally between said first stator blade and a second of said stator blades . - an annular inner ferrule comprising at least one segment constituted of a composite material; - an annular outer ferrule surrounding said inner ferrule ; - a plurality of stator blades extending radially from said inner ferrule to said outer ferrule, each comprising a pressure face to deviate an airflow; - at least one auxiliary blade disposed at a smaller distance from a first of said stator blades than other stator blades , comprising a pressure face of a smaller area than an area of the pressure face of said first stator blade ; characterised in that said at least one auxiliary blade : - comprises a root at least partially buried in said composite material; and - extends radially, from said root , parallel to and totally between said first stator blade and a second of said stator blades . - comprises a root at least partially buried in said composite material; and - extends radially, from said root , parallel to and totally between said first stator blade and a second of said stator blades .
Measuring device for measuring play parameters for a racket sport, such as tennis, squash or badminton, comprising a body containing at least one play data sensor , the body having grooves which are adapted to receive strings of a stringing of a racket (R), characterised in that the body also has reliefs which are compatible with the removable fixing of the measuring device in a cavity of an end of the handle of a racket (R'), in such a manner that the measuring device can be removably fixed either to the stringing of a racket (R) or in the handle of a racket (R').
Method for presenting a vehicle environment of a vehicle , comprising the steps of: - capturing at least one actual camera image using at least one camera arranged on the vehicle, wherein the actual camera image presents the vehicle environment, - spatially placing the at least one actual camera image in a virtual space by way of a projection surface, characterized by the steps of: - providing a preselected image region of the actual camera image in which image artefacts occur in a plurality of resolutions, wherein the preselected image region is an extract of the actual camera image , - producing a virtual camera image , which presents the placed actual camera image , from the view of a virtual camera at a position in the virtual space , wherein that resolution of the provided resolutions which reduces an optical presence of the image artefacts is used for the preselected image region of the actual camera image; wherein the image artefacts occur upon movement of the virtual camera and consist of a consistent change of the colour and brightness values in the virtual camera image. - capturing at least one actual camera image using at least one camera arranged on the vehicle, wherein the actual camera image presents the vehicle environment, - spatially placing the at least one actual camera image in a virtual space by way of a projection surface, characterized by the steps of: - providing a preselected image region of the actual camera image in which image artefacts occur in a plurality of resolutions, wherein the preselected image region is an extract of the actual camera image , - producing a virtual camera image , which presents the placed actual camera image , from the view of a virtual camera at a position in the virtual space , wherein that resolution of the provided resolutions which reduces an optical presence of the image artefacts is used for the preselected image region of the actual camera image;
An optical coupler , comprising: a waveguide structure comprising: a first waveguide layer having a proximal end and a distal end , the first waveguide layer including: a first waveguide that extends from the proximal end along a first portion of the first waveguide layer , wherein the first waveguide widens along a second portion of the first waveguide layer toward the distal end of the first waveguide layer ; and one or more additional waveguides that extend from the proximal end along the first portion of the first waveguide layer , wherein each of the one or more additional waveguides narrow along the second portion of the first waveguide layer to separate distal tips at the distal end of the first waveguide layer ; and wherein the waveguide structure is configured to match an integrated photonics mode to a fiber mode supported by an optical fiber at the proximal end , wherein the waveguide structure is configured to transition the mode to only the first waveguide toward the distal end ; characterized in that the one or more additional waveguides diverge from the first waveguide along the second portion of the first waveguide layer toward the distal end of the first waveguide layer . a waveguide structure comprising: a first waveguide layer having a proximal end and a distal end , the first waveguide layer including: a first waveguide that extends from the proximal end along a first portion of the first waveguide layer , wherein the first waveguide widens along a second portion of the first waveguide layer toward the distal end of the first waveguide layer ; and one or more additional waveguides that extend from the proximal end along the first portion of the first waveguide layer , wherein each of the one or more additional waveguides narrow along the second portion of the first waveguide layer to separate distal tips at the distal end of the first waveguide layer ; and a first waveguide that extends from the proximal end along a first portion of the first waveguide layer , wherein the first waveguide widens along a second portion of the first waveguide layer toward the distal end of the first waveguide layer ; and one or more additional waveguides that extend from the proximal end along the first portion of the first waveguide layer , wherein each of the one or more additional waveguides narrow along the second portion of the first waveguide layer to separate distal tips at the distal end of the first waveguide layer ; and wherein the waveguide structure is configured to match an integrated photonics mode to a fiber mode supported by an optical fiber at the proximal end , wherein the waveguide structure is configured to transition the mode to only the first waveguide toward the distal end ; characterized in that the one or more additional waveguides diverge from the first waveguide along the second portion of the first waveguide layer toward the distal end of the first waveguide layer .
A method for isolating a phenylene ether oligomer composition, the method comprising, feeding a solution comprising a solvent and a phenylene ether oligomer into a thin film evaporator comprising a cylindrical heating chamber and a rotor comprising one or more rotor blades, wherein an edge of the one or more rotor blades and an interior surface of the cylindrical heating chamber are separated by a distance of 0.5 to 3.5 millimeters; forming a film comprising the phenylene ether oligomer and the solvent on the interior surface of the cylindrical heating chamber; and heating the cylindrical heating chamber to devolatilize the solvent from the film to provide a phenylene ether oligomer composition having an intrinsic viscosity of 0.03 to 0.13 deciliter per gram measured by Ubbelohde viscometer at 25°C in chloroform and a zero shear melt viscosity of greater than 10,000 centipoise at 200°C, comprising: a phenylene ether oligomer having an external amine content of less than 1.5 weight percent; and a residual solvent in an amount of 0 to 10,000 parts per million by weight (ppm), based on the weight of the phenylene ether oligomer composition, wherein the parameters are measured according to the respective method as indicated in the description. a phenylene ether oligomer having an external amine content of less than 1.5 weight percent; and a residual solvent in an amount of 0 to 10,000 parts per million by weight (ppm), based on the weight of the phenylene ether oligomer composition, wherein the parameters are measured according to the respective method as indicated in the description.
A plurality of myeloid-derived suppressor cells (MDSCs) deficient in apoptosis-associated speck-like protein containing a CARD (ASC) (ASC-deficient MDSCs) for use in a method of treating a subject having or at risk of having graft-versus-host disease (GvHD), the method comprising: administering to the subject a plurality of ASC-deficient MDSCs.
A method for securing an execution of an algorithm of a cryptographic process comprising several operations Oj with n,j integers and j in [0..n-1], to be executed each once for a complete execution of said algorithm and which may be executed independently, said method being performed by a processor of a cryptographic device comprising further a random number generator, and characterized in that , for one execution of said algorithm, repeating the following steps, until each of said several operations has been executed at least once : - drawing (S1) at random an operation to be executed among all several operations comprised in the algorithm by generating a random index (idx) in [0.. n-1] using said random number generator, - executing said drawn operation (S2) whose index is equal to said generated index (idx). - drawing (S1) at random an operation to be executed among all several operations comprised in the algorithm by generating a random index (idx) in [0.. n-1] using said random number generator, - executing said drawn operation (S2) whose index is equal to said generated index (idx).
A force sensor comprising: a base unit ; a displacement unit configured to be displaced with respect to said base unit by receiving an external force; a first displacement sensor pair (4A and 10A, 4B and 10B) including two sets of sensors that detect a relative displacement between said base unit and said displacement unit in a first direction (X); and a second displacement sensor pair (4C and 10C, 4D and 10D) including two sets of sensors that detect a relative displacement between said base unit and said displacement unit in a second direction (Y) intersecting the first direction, wherein the first direction and the second direction lie in an XY plane of the force sensor, and among four quadrants of the XY plane divided by two straight lines along each of the first direction and the second direction, the straight lines passing through a midpoint of the two sets of sensors composing said first displacement sensor pair (4A and 10A, 4B and 10B), the two sets of sensors composing said second displacement sensor pair (4C and 10C, 4D and 10D) are respectively disposed in two quadrants in which the two sets of sensors composing said first displacement sensor pair (4A and 10A, 4B and 10B) are respectively disposed, characterized in that the two sets of sensors composing said first displacement sensor pair and the two sets of sensors composing said second displacement sensor pair are separated by a predetermined distance in each of the first direction and the second direction. a base unit ; a displacement unit configured to be displaced with respect to said base unit by receiving an external force; a first displacement sensor pair (4A and 10A, 4B and 10B) including two sets of sensors that detect a relative displacement between said base unit and said displacement unit in a first direction (X); and a second displacement sensor pair (4C and 10C, 4D and 10D) including two sets of sensors that detect a relative displacement between said base unit and said displacement unit in a second direction (Y) intersecting the first direction, wherein the first direction and the second direction lie in an XY plane of the force sensor, and among four quadrants of the XY plane divided by two straight lines along each of the first direction and the second direction, the straight lines passing through a midpoint of the two sets of sensors composing said first displacement sensor pair (4A and 10A, 4B and 10B), the two sets of sensors composing said second displacement sensor pair (4C and 10C, 4D and 10D) are respectively disposed in two quadrants in which the two sets of sensors composing said first displacement sensor pair (4A and 10A, 4B and 10B) are respectively disposed, characterized in that the two sets of sensors composing said first displacement sensor pair and the two sets of sensors composing said second displacement sensor pair are separated by a predetermined distance in each of the first direction and the second direction.
Granular material comprising an inorganic solid support on which at least one biosurfactant selected from the group comprising sophorolipids and rhamnolipids, especially sophorolipid, is present, characterized in that the support comprises at least one solid material selected from the group comprising carbonates, sesquicarbonates, percarbonates, perborates, sulphates, silicates, aluminosilicates, zeolites, precipitated silicas and fumed silicas.
A receptacle , in particular a storage box, having a base body and a removable cover element , the cover element adapted to cover an open top side of the base body , - the base body comprising a bottom wall, a front wall , a rear wall and two side walls arranged oppositely to each other, - the cover element comprising at least a first wall serving as a top wall of the receptacle when the cover element covers the base body and a second wall arranged orthogonally to the first wall , the second wall at least partially overlapping one of the front wall , the rear wall or the side walls when the cover element covers the base body , so that a first edge of the second wall arranged distantly from the first wall faces the outer surface of the respective wall of the base body , characterized in that the second wall of the cover element comprises a zone at least in the area of the first edge which is composed of a flexible material, the zone in particular being a soft lip which is fixed to a portion of the second wall composed of a rigid material, with a sealing element is arranged in the overlapping area of the second wall of the cover element and the respective wall of the base body , wherein the sealing element is a protrusion or superelevation of a conic slope of the zone and, when the cover element closes the receptacle, the protrusion or superelevation touches the outer surface of the respective wall of the base body. - the base body comprising a bottom wall, a front wall , a rear wall and two side walls arranged oppositely to each other, - the cover element comprising at least a first wall serving as a top wall of the receptacle when the cover element covers the base body and a second wall arranged orthogonally to the first wall , the second wall at least partially overlapping one of the front wall , the rear wall or the side walls when the cover element covers the base body , so that a first edge of the second wall arranged distantly from the first wall faces the outer surface of the respective wall of the base body ,