mhurhangee/patent-ind-claim-en huggingface dataset:
A gas turbine engine having an engine central longitudinal axis (A-A'), the gas turbine engine comprising: at least one of a vane support , a vane stage , a blade outer air seal support , and a blade outer air seal ; characterised in that at least one of the vane support, the vane stage, the blade outer air seal support, and the blade outer air seal is rotatable about the engine central longitudinal axis. at least one of a vane support , a vane stage , a blade outer air seal support , and a blade outer air seal ; characterised in that at least one of the vane support, the vane stage, the blade outer air seal support, and the blade outer air seal is rotatable about the engine central longitudinal axis.
A method applied to a client terminal in a three-party service system, the method comprising: encrypting, by the client terminal, sensitive data by using a key in response to receipt of the sensitive data (S410) sending, by the client terminal, the encrypted sensitive data to a provider server through a first request (S420) obtaining, by the client terminal, a unique tag corresponding to the sensitive data (S430) sending, by the client terminal, the key and the unique tag to the provider server through a second request (S431) sending, by the client terminal, three-party service data identified by the unique tag to a third party server through a third request (S433) so that the third party server generates a three-party service request that carries the unique tag and the three-party service data, and sends the three-party service request to the provider servei (S436) wherein the first request, the second request, and the third request are different requests, and wherein the first request and the second request do not pass through the third party server during transmission. encrypting, by the client terminal, sensitive data by using a key in response to receipt of the sensitive data (S410) sending, by the client terminal, the encrypted sensitive data to a provider server through a first request (S420) obtaining, by the client terminal, a unique tag corresponding to the sensitive data (S430) sending, by the client terminal, the key and the unique tag to the provider server through a second request (S431) sending, by the client terminal, three-party service data identified by the unique tag to a third party server through a third request (S433) so that the third party server generates a three-party service request that carries the unique tag and the three-party service data, and sends the three-party service request to the provider servei (S436) wherein the first request, the second request, and the third request are different requests, and wherein the first request and the second request do not pass through the third party server during transmission.
A method for preparing granules, the method comprising: - preparing a slurry containing solid API powder particles dispersed in a liquid, - feeding the slurry to a continuous granulator , - mixing the slurry with a dry base powder within the granulator in order to produce a slurry/base powder mixture, and - drying the slurry/base powder mixture produced within the granulator to obtain granules containing the solid API particles and the base powder. - preparing a slurry containing solid API powder particles dispersed in a liquid, - feeding the slurry to a continuous granulator , - mixing the slurry with a dry base powder within the granulator in order to produce a slurry/base powder mixture, and - drying the slurry/base powder mixture produced within the granulator to obtain granules containing the solid API particles and the base powder.
An aircraft propulsion assembly comprising: a bypass turbojet having a space between passages separating a core stream flow passage and a bypass stream flow passage , and a stationary inter-compressor casing positioned upstream from said space between passages; a nacelle arranged around the turbojet and including at its downstream end an inner annular wall that defines the outside of the space between passages and the inside of the bypass stream flow passage, and an outer annular wall arranged around the inner wall and that defines the outside of the bypass stream flow passage, at least a portion of the inner wall being suitable for moving between a maintenance position in which it uncovers the space between passages at least in part and a working position in which it masks the space between passages; and a thrust-reverser comprising a downstream element of the outer wall that is movable in translation between a retracted position in which it defines the outside of the bypass stream flow passage and a thrust-reversal position in which bypass stream deflector elements are deployed in a radial direction, the deployment of said bypass stream deflector elements being controlled by guide rods , each having a first end fastened via a first hinged connection to a deflector element and a second end fastened via a second hinged connection to the inter-compressor casing of the turbojet. a bypass turbojet having a space between passages separating a core stream flow passage and a bypass stream flow passage , and a stationary inter-compressor casing positioned upstream from said space between passages; a nacelle arranged around the turbojet and including at its downstream end an inner annular wall that defines the outside of the space between passages and the inside of the bypass stream flow passage, and an outer annular wall arranged around the inner wall and that defines the outside of the bypass stream flow passage, at least a portion of the inner wall being suitable for moving between a maintenance position in which it uncovers the space between passages at least in part and a working position in which it masks the space between passages; and a thrust-reverser comprising a downstream element of the outer wall that is movable in translation between a retracted position in which it defines the outside of the bypass stream flow passage and a thrust-reversal position in which bypass stream deflector elements are deployed in a radial direction, the deployment of said bypass stream deflector elements being controlled by guide rods , each having a first end fastened via a first hinged connection to a deflector element and a second end fastened via a second hinged connection to the inter-compressor casing of the turbojet.
An apparatus for forming a thermoplastic article having long fiber reinforcement, wherein the apparatus comprises (a) at least one mold body having at least one first mold section configured for defining a first mold cavity and acts as a reservoir for heating and rendering flowable the feed stock in the form of long fiber reinforced thermoplastic composite, the at least one first mold section having an inlet and an outlet and at least one second mold section including two or more fitting surfaces which come together using one or more second mold section pieces to define a second mold cavity , the second mold section having an inlet , wherein the outlet of the first mold section is in communication with the inlet of the second mold section via at least one flow port , and the second mold cavity has a configuration for forming the article; (b) a piston configured so as to be able to enter the first mold cavity ; and characterized by (c) at least one press capable of heating and cooling the mold body and the mold sections and the heated press upon opening is able to receive the mold body so that the press can apply heat and pressure to a thermoplastic composite material in the first mold cavity by pressing on the piston when the piston is inserted into the first mold cavity . (a) at least one mold body having at least one first mold section configured for defining a first mold cavity and acts as a reservoir for heating and rendering flowable the feed stock in the form of long fiber reinforced thermoplastic composite, the at least one first mold section having an inlet and an outlet and at least one second mold section including two or more fitting surfaces which come together using one or more second mold section pieces to define a second mold cavity , the second mold section having an inlet , wherein the outlet of the first mold section is in communication with the inlet of the second mold section via at least one flow port , and the second mold cavity has a configuration for forming the article; at least one first mold section configured for defining a first mold cavity and acts as a reservoir for heating and rendering flowable the feed stock in the form of long fiber reinforced thermoplastic composite, the at least one first mold section having an inlet and an outlet and at least one second mold section including two or more fitting surfaces which come together using one or more second mold section pieces to define a second mold cavity , the second mold section having an inlet , wherein the outlet of the first mold section is in communication with the inlet of the second mold section via at least one flow port , and the second mold cavity has a configuration for forming the article; (b) a piston configured so as to be able to enter the first mold cavity ; and characterized by (c) at least one press capable of heating and cooling the mold body and the mold sections and the heated press upon opening is able to receive the mold body so that the press can apply heat and pressure to a thermoplastic composite material in the first mold cavity by pressing on the piston when the piston is inserted into the first mold cavity .
A method of making terephthalic acid comprising reductive coupling of two molecules of propiolic acid or propiolic acid derivatives followed by reaction with ethylene and dehydrogenation, wherein said reductive coupling comprises a catalyst, and wherein said catalyst comprises a metal.
A video image processing pipeline controller configured to control an available bandwidth at which processing functions of a video image processing pipeline is allowed to communicate, over one or more memory access channels , with a system memory , wherein the video image processing pipeline controller is configured to reduce the available bandwidth while securing that the current frame rate does not drop below a target frame rate, at which the video image processing pipeline produces a video stream, thereby inducing a shift in an active time and/or prolonging the active time, within a frame time, of the processing functions such that a peak power consumption of the video image processing pipeline is reduced, wherein the video image processing pipeline controller is configured to reduce the available bandwidth while securing that the current frame rate does not drop below a target frame rate by decreasing the available bandwidth in steps until a current frame rate drops below the target frame rate, and, in response to the current frame rate drops below the target frame rate, increasing the available bandwidth to a bandwidth at which the current frame rate does not drop below the target frame rate. wherein the video image processing pipeline controller is configured to reduce the available bandwidth while securing that the current frame rate does not drop below a target frame rate, at which the video image processing pipeline produces a video stream, thereby inducing a shift in an active time and/or prolonging the active time, within a frame time, of the processing functions such that a peak power consumption of the video image processing pipeline is reduced, wherein the video image processing pipeline controller is configured to reduce the available bandwidth while securing that the current frame rate does not drop below a target frame rate by decreasing the available bandwidth in steps until a current frame rate drops below the target frame rate, and, in response to the current frame rate drops below the target frame rate, increasing the available bandwidth to a bandwidth at which the current frame rate does not drop below the target frame rate.
A rubber composition for studless winter tires, comprising a rubber component, bionanofibers, and a silica, the bionanofibers having an average fiber diameter of 0.1 μm or less, the rubber component having a combined amount of natural rubber and polybutadiene rubber of 30% to 100% by mass based on 100% by mass of the rubber component, the rubber composition comprising the bionanofibers in an amount of 1 to 10 parts by mass relative to 100 parts by mass of the rubber component and wherein the silica is in an amount of 10 parts by mass or more relative to 100 parts by mass of the rubber component.
A tubular gripping apparatus , comprising: a housing having a bore; a plurality of gripping members movable between a gripping position and a release position; and a shield having a tubular inner body movable relative to an outer body , wherein the tubular inner body is movable between a retracted position, in which the tubular inner body is positioned above the plurality of gripping members , and an extended position, in which the inner body is at least partially positioned interiorly of the plurality of gripping members . a housing having a bore; a plurality of gripping members movable between a gripping position and a release position; and a shield having a tubular inner body movable relative to an outer body , wherein the tubular inner body is movable between a retracted position, in which the tubular inner body is positioned above the plurality of gripping members , and an extended position, in which the inner body is at least partially positioned interiorly of the plurality of gripping members .
Closure cap for a bore (B), which may be inserted into the bore (B) with a gripping device , wherein the closure cap comprises an inner diameter (DI), wherein the closure cap is pot-shaped and comprises a base wall and a side wall moulded thereon, wherein the side wall is formed circumferential and conical, characterised in that the side wall has at least one circumferential depression in the form of a groove or slot on its inner side, wherein the circumferential depression serves for the engagement of engagement elements of the gripping device .
Method of controlling an induction generator connected to a utility grid , the method comprising: receiving an actual grid frequency (f); and controlling rotor windings of the generator by a rotor control signal (25a,b,c) having a rotor winding reference frequency (Ω_ref) being set in dependence of the actual grid frequency (f), wherein the rotor winding reference frequency (Ω_ref) is set such that a slip (s) adheres to a predefined value and substantially does not change with changing actual grid frequency (f) at least in a predefined frequency range of the actual grid frequency, wherein the slip s is given by: s = Ω f − ns f / ns f , wherein: f is the actual grid frequency, Q is the actual speed of generator at the actual grid frequency f, ns(f) is a synchronous speed at the actual grid frequency f, wherein ns in rpm is given by ns = 60 * f / p, wherein p is the number of pole pairs of the generator rotor and f is given in Hz, characterized in, that the rotor winding reference frequency (Ω_ref) is set as follows: Ω_ref f = Ω f 0 ∗ 1 + f − f 0 / f 0 , wherein f0 is the nominal grid frequency, Q(f) is the rotor winding reference frequency at the actual grid frequency, Ω(f0) is the rotor winding reference frequency at the nominal grid frequency, Ω f 0 = f 0 ∗ s . receiving an actual grid frequency (f); and controlling rotor windings of the generator by a rotor control signal (25a,b,c) having a rotor winding reference frequency (Ω_ref) being set in dependence of the actual grid frequency (f), wherein the rotor winding reference frequency (Ω_ref) is set such that a slip (s) adheres to a predefined value and substantially does not change with changing actual grid frequency (f) at least in a predefined frequency range of the actual grid frequency, f is the actual grid frequency, Q is the actual speed of generator at the actual grid frequency f, ns(f) is a synchronous speed at the actual grid frequency f, wherein ns in rpm is given by ns = 60 * f / p, wherein p is the number of pole pairs of the generator rotor and f is given in Hz, characterized in, that the rotor winding reference frequency (Ω_ref) is set as follows: Ω_ref f = Ω f 0 ∗ 1 + f − f 0 / f 0 , wherein f0 is the nominal grid frequency, Q(f) is the rotor winding reference frequency at the actual grid frequency, Ω(f0) is the rotor winding reference frequency at the nominal grid frequency, Ω f 0 = f 0 ∗ s .
A combination comprising a luggage item ; a wireless charger for portable electronic devices , wherein said wireless charger is structurally integrated in said luggage item , wherein the wireless charger is in the form of a module secured to and extending through a wall of the luggage item, said module comprising; a frame secured to said luggage item wall; a charger panel having a charger surface and rotatably mounted in said frame to be rotatable between a closed position and an open position; wherein in said closed position said charger surface is recessed within said frame, and in said open position said charger surface projects from the luggage unit wall and is exposed to receive and support an electronic device having a battery to be charged. a frame secured to said luggage item wall; a charger panel having a charger surface and rotatably mounted in said frame to be rotatable between a closed position and an open position; wherein in said closed position said charger surface is recessed within said frame, and in said open position said charger surface projects from the luggage unit wall and is exposed to receive and support an electronic device having a battery to be charged.
A method comprising: - decoding a first depth value of a first point of a point cloud and a second depth value of a second point of the point cloud, said first point and said second point being orthogonally projected on a projection plane along a same projection line, - responsive to an information indicating that a position along said projection line is occupied, reconstructing a third point of the point cloud from said position along the projection line, - characterised by : said information is one bit obtained from a codeword comprising concatenated bits representative of occupation of positions laying in-between said first depth value and said second depth value along the projection line. - decoding a first depth value of a first point of a point cloud and a second depth value of a second point of the point cloud, said first point and said second point being orthogonally projected on a projection plane along a same projection line, - responsive to an information indicating that a position along said projection line is occupied, reconstructing a third point of the point cloud from said position along the projection line, - characterised by : said information is one bit obtained from a codeword comprising concatenated bits representative of occupation of positions laying in-between said first depth value and said second depth value along the projection line.
A refrigerator comprising: a cabinet installed to pass through or inserted into a door or a wall, defining a storage compartment for storing goods therein; a housing coupled to or formed integrally with a lower part of the cabinet ; an outdoor side door configured to open or close a front side of the storage compartment and exposed to an outside of a space, the door or the wall being a boundary of the space; an indoor side door to open or close a rear side of the storage compartment and exposed to an inside the space; a cold air supply device, at least a part of which is disposed in the housing , configured to make air in the storage compartment cold; and a controller configured to control operations of the cold air supply device, characterized in that : the cabinet has a drain hole at a bottom of the storage compartment ; the refrigerator further comprises: a drain port extending from a bottom surface of the cabinet and communicating with the drain hole ; and an actuator provided to selectively open or close an opening formed in the drain port ; and the controller is further configured to control operations of the actuator for preventing a lack of oxygen in a storage compartment from occurring if a companion animal is trapped in the storage compartment . a cabinet installed to pass through or inserted into a door or a wall, defining a storage compartment for storing goods therein; a housing coupled to or formed integrally with a lower part of the cabinet ; an outdoor side door configured to open or close a front side of the storage compartment and exposed to an outside of a space, the door or the wall being a boundary of the space; an indoor side door to open or close a rear side of the storage compartment and exposed to an inside the space; a cold air supply device, at least a part of which is disposed in the housing , configured to make air in the storage compartment cold; and a controller configured to control operations of the cold air supply device, characterized in that : the cabinet has a drain hole at a bottom of the storage compartment ; the refrigerator further comprises: a drain port extending from a bottom surface of the cabinet and communicating with the drain hole ; and an actuator provided to selectively open or close an opening formed in the drain port ; and the controller is further configured to control operations of the actuator the cabinet has a drain hole at a bottom of the storage compartment ; the refrigerator further comprises: a drain port extending from a bottom surface of the cabinet and communicating with the drain hole ; and an actuator provided to selectively open or close an opening formed in the drain port ; and the controller is further configured to control operations of the actuator a drain port extending from a bottom surface of the cabinet and communicating with the drain hole ; and an actuator provided to selectively open or close an opening formed in the drain port ; and the controller is further configured to control operations of the actuator